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	<title>Heat Transfer - Articles</title>
	<link>http://www.cheresources.com/content/articles/heat-transfer/</link>
	<pubDate>Wed, 15 Apr 2026 09:12:39 +0000</pubDate>
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		<title>Steam Tracing with MS Excel</title>
		<link>http://www.cheresources.com/content/articles/heat-transfer/steam-tracing-excel</link>
		<description><![CDATA[<p>Heat tracing is used to prevent heat loss from process fluids being transported in process fluid pipes, when there is risk of damage to piping, or interference with operation such as fouling or blockage, caused by the congealing, increase in viscosity, or separation of components, in the fluid below certain temperatures, or when there is risk of formation of corrosive substances or water due to condensation in corrosive services.  This prevention of heat loss is accomplished by employing electrical tracing, or steam tracing, and insulating both the process fluid pipe and the tracer together, using appropriate insulation lagging, in an attempt to minimise heat loss from the pipe and tracer to their surroundings.</p>{parse block="google_articles"}

<p>The existing software that was used to design steam tracing had to be evaluated in terms of its accuracy and reliability, as problems associated with steam tracing designed with the existing software have occurred in the past.  A software simulation had to be designed that could compare theoretical inputs and outputs with that of an existing simulation used to design steam tracing, as well as compare it to existing installed steam tracing, in order to determine where improvements in the software could be made.</p>

<p>The new software had to use the outputs from the existing software as inputs and its outputs had to correspond to the inputs of the existing software. Other important evaluations were also included in the new software.</p>

<p class="h1header">Theory</p>
<p>The term â€œHeat Tracingâ€ is inclusive for two methods used in the conservation of temperature. The first method is known as electrical heat tracing, and the second is known as steam tracing.  Electrical heat tracing may be described as an insulated electrical heating cable, which is spiralled around the process fluid pipe, after which the pipe and tracing is insulated with the appropriate type and thickness of insulation lagging material.  While this method of heat tracing may be installed with relative ease compared to steam tracing, it is more expensive, and poses several risks.  The most important of these, being the risk of electric spark, which may cause electric shock or ignite flammable substances resulting in explosions or fire.   If electrical heat tracing is not carefully controlled, there is also the possibility that the cable could overheat and damage the pipe or insulation.  This also renders the tracing cable unusable and the cable needs to be replaced.</p>

<table class="datatable_inset" border="0" align="left"><tbody><tr><td>In order to follow the theory, <a href="http://www.cheresources.com/invision/files/file/10-nomenclature-for-steam-tracing-with-ms-excel/" Target="New Window"><u>download</u></a> the Nomenclature from the Downloads section.<br />








<br />









<b>Download the spreadsheet developed with the method presented here in our <a href="http://www.cheresources.com/invision/files/file/85-steam-tracing-calculator/" Target="New Window"><u>Downloads Section</u></a></b></td></tr></tbody></table><br />

















<br />

















<p>Steam tracing is described by attaching a smaller pipe containing saturated steam, also known as the â€œtracerâ€, parallel to the process fluid pipe. The two pipes are then also insulated together with the specified insulation and jacketed if necessary.  Steam tracing is more labor intensive to install than electrical heat tracing, but there are very few risks associated with it.  The temperature of the tracer also cannot exceed the maximum saturation temperature of the steam, as it operates at specific steam pressures.</p>

<p>Steam tracing may be done in one of two ways.  Bare steam tracing is the most popular choice as it is fairly easily installed and maintained and it is ideally suited to lower temperature requirements.  It is simply composed of a half inch or three quarters of an inch pipe attached to the process fluid pipe by straps and both pipes are then insulated together.   The other available option is to make use of cemented steam tracing, during which heat conductive cement is placed around the steam tracer running parallel to the process fluid pipe, (shown in figure 1b), in an attempt to increase the contact area available for heat transfer, between the tracer and the process fluid pipe.</p>

<p>It is necessary to foster a better understanding of the heat loss distribution through an insulated pipe containing steam tracing, before continuing the discussion. For this purpose, detailed diagrams depicting the cross-sections of the two types of tracing methods are given below, in Figures 1a and b:</p>

<table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/steam_tracing1.gif" alt="steam-tracing-1"/></td></tr><tr><td>Figures 1a and 1b: Bare versus Cemented Tracer</td></tr></tbody></table>
Because the area around the process fluid pipe and tracer cannot be accurately described simply by assuming perfect cylindrical geometry, provision had to be made for a realistic impression of the true geometry. Detailed derivations of formulas are included in <a href="http://www.cheresources.com/invision/files/file/9-appendix-for-steam-tracing-with-ms-excel/" Target="New Window">Appendix 1</a>.

Heat transfer across a surface occurs according to the following equation: (Coulson & Richardson, 1999:634-688)
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing2.gif" alt="steam-tracing-2"/></td><td class="equationnumber" align="right">Eq. (1)</td></tr></tbody></table>
The following equations were derived in determining the different areas across which heat transfer occurs:
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing3.gif" alt="steam-tracing-3"/></td><td class="equationnumber" align="right">Eq. (2)</td></tr></tbody></table>
For bare tracing, the following formulas were derived:
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing4.gif" alt="steam-tracing-4"/></td><td class="equationnumber" align="right">Eq. (3)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing5.gif" alt="steam-tracing-5"/></td><td class="equationnumber" align="right">Eq. (4)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing6.gif" alt="steam-tracing-6"/></td><td class="equationnumber" align="right">Eq. (5)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing7.gif" alt="steam-tracing-7"/></td><td class="equationnumber" align="right">Eq. (6)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing8.gif" alt="steam-tracing-8"/></td><td class="equationnumber" align="right">Eq. (7)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing9.gif" alt="steam-tracing-9"/></td><td class="equationnumber" align="right">Eq. (8)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing10.gif" alt="steam-tracing-10"/></td><td class="equationnumber" align="right">Eq. (9)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing11.gif" alt="steam-tracing-11"/></td><td class="equationnumber" align="right">Eq. (10)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing12.gif" alt="steam-tracing-12"/></td><td class="equationnumber" align="right">Eq. (11)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing13.gif" alt="steam-tracing-13"/></td><td class="equationnumber" align="right">Eq. (12)</td></tr></tbody></table>
The following equation was used to determine the hottest surface temperature for bare tracing: (Le Roux, D.F. (1997) â€œThermal Insulation and Heat Tracingâ€, Guideline presented by D.F. le Roux, Secunda):
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing14.gif" alt="steam-tracing-14"/></td><td class="equationnumber" align="right">Eq. (13)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing15.gif" alt="steam-tracing-15"/></td><td class="equationnumber" align="right">Eq. (14)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing16.gif" alt="steam-tracing-16"/></td><td class="equationnumber" align="right">Eq. (15)</td></tr></tbody></table>
For cemented tracing, the following formulas were derived:
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing17.gif" alt="steam-tracing-17"/></td><td class="equationnumber" align="right">Eq. (16)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing18.gif" alt="steam-tracing-18"/></td><td class="equationnumber" align="right">Eq. (17)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing19.gif" alt="steam-tracing-19"/></td><td class="equationnumber" align="right">Eq. (18)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing20.gif" alt="steam-tracing-20"/></td><td class="equationnumber" align="right">Eq. (19)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing22.gif" alt="steam-tracing-22"/></td><td class="equationnumber" align="right">Eq. (20)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing23.gif" alt="steam-tracing-23"/></td><td class="equationnumber" align="right">Eq. (21)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing24.gif" alt="steam-tracing-24"/></td><td class="equationnumber" align="right">Eq. (22)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing25.gif" alt="steam-tracing-25"/></td><td class="equationnumber" align="right">Eq. (23)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing26.gif" alt="steam-tracing-26"/></td><td class="equationnumber" align="right">Eq. (24)</td></tr></tbody></table>
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing27.gif" alt="steam-tracing-27"/></td><td class="equationnumber" align="right">Eq. (25)</td></tr></tbody></table>
The following equation was used to determine the hottest surface temperature for cemented tracing:
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing28.gif" alt="steam-tracing-28"/></td><td class="equationnumber" align="right">Eq. (26)</td></tr></tbody></table>
where:
<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="../../../../invision/uploads/images/articles/steam_tracing29.gif" alt="steam-tracing-29"/></td><td class="equationnumber" align="right">Eq. (27)</td></tr></tbody></table>
<p class="h1header">Experimental</p>
The cross sections of the bare traced and cemented traced pipes are given in Figures 3a and 3b, respectively.  These figures illustrate how the geometric approach was used in describing the heat loss through the system, taking into account that spherical geometry was not assumed.
<table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/steam_tracing30.gif" alt="steam-tracing-30"/></td></tr><tr><td>Figure 3a: Bare Tracer</td></tr></tbody></table>
<table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/steam_tracing31.gif" alt="steam-tracing-31"/></td></tr><tr><td>Figure 3b: Cemented Tracer</td></tr></tbody></table>

The independent variables for the design were as follows, and were all specified variables in the software simulation:

<table class="datatable" border="0" width="38%" height="245" align="center"><caption>Independent Variables</caption>
  <tr>
    <td width="39%" height="18">Time, s</td>
    <td width="61%" height="18"></td>
  </tr>
  <tr>
    <td width="39%" height="15">Pipe length</td>
    <td width="61%" height="15">(0 to maximum length for steam trap), m</td>
  </tr>
  <tr>
    <td width="39%" height="19">Steam pressure</td>
    <td width="61%" height="19">(240 to 1700 kPa)</td>
  </tr>
  <tr>
    <td width="39%" height="19">Nominal process fluid pipe size</td>
    <td width="61%" height="19">(0.50 to 48 inches)</td>
  </tr>
  <tr>
    <td width="39%" height="19">Number of available tracers</td>
    <td width="61%" height="19">(0 to 5)</td>
  </tr>
  <tr>
    <td width="39%" height="19">Nominal pipe size of tracer pipe</td>
    <td width="61%" height="19">(0.50 to 0.75 inches)</td>
  </tr>
  <tr>
    <td width="39%" height="19">Insulation thickness</td>
    <td width="61%" height="19">(0 to process fluid pipe diameter), m</td>
  </tr>
  <tr>
    <td width="39%" height="19">Emissivity of insulation lagging</td>
    <td width="61%" height="19">(0 to 1)</td>
  </tr>
  <tr>
    <td width="39%" height="19">Ambient temperature</td>
    <td width="61%" height="19">(-10 to 50 Â°C)</td>
  </tr>
  <tr>
    <td width="39%" height="19">Wind velocity</td>
    <td width="61%" height="19">(0 to 72 km/h)</td>
  </tr>
</table>

<table class="datatable" border="0" width="38%" align="center"><caption>Dependent Variables</caption>

 <tr>
    <td width="39%">Annulus temperature</td>
    <td width="61%">(Process fluid temperature to Steam Temperature)</td>
  </tr>
  <tr>
    <td width="39%">Saturated steam temperature</td>
    <td width="61%">(126.1 to 204.3 ÂºC)</td>
  </tr>
  <tr>
    <td width="39%">Steam consumption</td>
    <td width="61%">(0 to 50 kg/h)</td>
  </tr>
  <tr>
    <td width="39%">Process fluid temperature</td>
    <td width="61%">(0 to 600 ÂºC)</td>
  </tr>
  <tr>
    <td width="39%">Pipe outer radius</td>
    <td width="61%">(10.668 to 609.62 mm)</td>
  </tr>
  <tr>
    <td width="39%">Pipe wall thickness</td>
    <td width="61%">(1.3974 to 15.6869 mm)</td>
  </tr>
  <tr>
    <td width="39%">Pipe inner radius</td>
    <td width="61%">(6.401 to 1219.2 mm)</td>
  </tr>
  <tr>
    <td width="39%">Pipe wall thermal conductivity</td>
    <td width="61%">(16 to 401 W/mK)</td>
  </tr>
  <tr>
    <td width="39%">Steam tracer outside radius</td>
    <td width="61%">(6.35 to 9.53 mm)</td>
  </tr>
  <tr>
    <td width="39%">Maximum tracer length</td>
    <td width="61%">(30 to 60 m)</td>
  </tr>
  <tr>
    <td width="39%">Thermal conductivity of insulation</td>
    <td width="61%">(0.01241 to 0.1120 W/mK)</td>
  </tr>
  <tr>
    <td width="39%">Average insulation temperature</td>
    <td width="61%">(Ambient temp. to Steam temp.)</td>
  </tr>
  <tr>
    <td width="39%">Surface temperature</td>
    <td width="61%">(N/A), K</td>
  </tr>
  <tr>
    <td width="39%">Surface film coefficient</td>
    <td width="61%">(N/A), W/m2K</td>
  </tr>
</table>
<p>The main deliverable was to obtain the minimum temperature at which the process fluid had to enter the pipeline, but other information such as the wall temperature and steam consumption were also important.</p>

<p>The interface designed for the simulation is shown in Fig. 3c and was written in Microsoft Excel:</p>
<table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/steam_tracing33.gif" alt="steam-tracing-33"/></td></tr><tr><td>Figure 3c: Interface</td></tr></tbody></table>
<p>The detailed design and calculations can be found in Appendix 1. The design was done following an unconventional approach, in an attempt to make as few assumptions as possible.</p>

<p>Most of the equations were fundamentally derived, but some equations were employed from other sources. (See References)</p>

<p>All the necessary equations were developed and simplified to eliminate ambiguity. The equations were then solved simultaneously and by making use of iterations.</p>

<p>The inputs to the simulation were highlighted in yellow, on the left side of the page, and the outputs were highlighted blue, on the right hand side, to eliminate ambiguity in deciding which were inputs and which were outputs.</p>

<p>The inputs section mostly made use of drop-down menus to facilitate data input, and mostly made use of referencing techniques to look up the necessary values used in the calculations. For example, the user was only required to choose the NPS of the process fluid pipe, and the schedule number, and the program automatically looked up the outer diameter, inside diameter and wall thicknesses from a table containing accurate standard values for pipe sizes.</p>

<p>Also, the user was only required to specify the insulation material type, steam pressure, and ambient temperature, which the program used to calculate an average insulation temperature, and interpolate between different k-values, to obtain the specific thermal conductivity at that specific temperature, since thermal conductivity is temperature dependent. The program also used the lagging emissivity, together with the ambient temperature, surface temperature and wind velocity, to calculate an exact value for the surface film coefficient on the outside, which needed to be very accurate.</p>

<p>The program was also able to calculate a maximum surface temperature, to ensure safety protection for personnel, as the surface temperature, by standard, is not allowed to exceed 60 ÂºC. Temperatures higher than this would result in injury caused by touching the outside surface.</p>

<p>The steam consumption was also calculated by determining the heat loss from the system for a certain length of pipe. The steam is invariably subject to heat loss, and thus condensation, when sufficient heat has been lost. This corresponds to the maximum length of a tracer. Fresh, saturated steam then needs to be re-introduced into the system, to ensure efficient operation, and a steam trap needs to be installed at the end of the maximum length, to collect all the condensate which has formed. The condensate may be recycled to create new steam.</p>

<p>The simulation made use of macros, in the sense that the program automatically performs the calculations necessary to converge the answers to a final answer, by simply requiring the user to press a shortcut key.</p>

<p class="h1header">Results and Discussion</p>
<p>Due to the nature of the project, definite answers are not possible to obtain, but rather different simulations could be run and each time the answers could be evaluated. As an example, one specific run could be described in terms of its equations as follows:</p>

<p>Consider the Bare Tracer.</p>

<p>Firstly, the inputs field has to be completed (see Table 1):</p>
<table class="datatable" border="0" align="left"><caption>Table 1: Input Fields</caption><tbody><tr><td><img src="../../../../invision/uploads/images/articles/steam_tracing34.gif" alt="steam-tracing-34"/></td></tr></tbody></table>

<p>After this has been done, the outputs section may be calculated:</p>

<p>Some of the outputs are values found in making use of references from other tables. These are shown first in Table 2.</p>
<table class="datatable" border="0" align="left"><caption>Table 2: Output Fields</caption><tbody><tr><td><img src="../../../../invision/uploads/images/articles/steam_tracing35.gif" alt="steam-tracing-35"/></td></tr></tbody></table>

<p>This information can now be used together with the inputs section to calculate the remaining outputs.</p>

<p>Firstly, the Average Insulation Temperature is calculated from Eq. (9):</p>
<img src="../../../../invision/uploads/images/articles/steam_tracing36.gif" alt="steam-tracing-36"/><br />

it is found that   Tins=36.67 ÂºC

<p>It should be noted that the Process fluid Temperature is not known yet, so this is not a final answer.</p>

<p>Secondly, the Annulus Temperature may be calculated from Eq. (8):</p>
<img src="../../../../invision/uploads/images/articles/steam_tracing37.gif" alt="steam-tracing-37"/><br />

T<sub>ann</sub>=76.4 ÂºC

<p>Since Tp is not known yet, and Tins has not yet been assigned a definite value, this value is also not fixed yet.</p>

<p>Now, the Average Surface Temperature needs to be calculated.  This value may be approximated by assuming that about 80% of the average surface temperature is due to the process fluid temperature and the remaining 20% is made up of the surface temperature on the tracer side.  The Average Surface Temperature may then be calculated as follows.</p>

<p>From Eq.(13) and (14):</p>
<img src="../../../../invision/uploads/images/articles/steam_tracing38.gif" alt="steam-tracing-38"/>
<table border="0" width="100%">
  <tr>
    <td width="41%"><img src="../../../../invision/uploads/images/articles/steam_tracing39.gif" alt="steam-tracing-39"/></td>
    <td width="59%">for the tracer side</td>
  </tr>
</table>
<p>and</p>
<table border="0" width="100%">
  <tr>
    <td width="41%"><img src="../../../../invision/uploads/images/articles/steam_tracing40.gif" alt="steam-tracing-40"/></td>
    <td width="59%">for the process fluid pipe side</td>
  </tr>
</table>
<p>Therefore</p>
<img src="../../../../invision/uploads/images/articles/steam_tracing41.gif" alt="steam-tracing-41"/><br />

The surface temperature is now calculated by making use of iterations to obtain the final value of<br />
<br />


T<sub>surf-Avg</sub> = 14.991 ÂºC<br />
<br />


<p>This causes the value of q to change until it stabilizes to its final answer.</p>

<p>Technically speaking, one has to calculate the area ratios that the process fluid pipe, annulus length and tracer each contribute, calculate each areaâ€™s surface temperature, and obtain the average value for the surface temperature accordingly, but due to the limited capacity of Microsoft Excel, this method was tried and it failed, because Excel could not perform all the iterations necessary to do the calculations.  The above calculation has shown to give satisfactory results for most situations.</p>

<p>As a next step, the surface coefficient needs to be calculated using Eq.(15):</p>
<img src="../../../../invision/uploads/images/articles/steam_tracing42.gif" alt="steam-tracing-42"/><br />

<p>The value for the surface coefficient then becomes:</p>
h<sub>0</sub>=10.1<br />
<br />

<p>k<sub>1</sub> is calculated using Eq.(10):</p>
<img src="../../../../invision/uploads/images/articles/steam_tracing43.gif" alt="steam-tracing-43"/><br />

but according to Eq.(5),<br />

 <img src="../../../../invision/uploads/images/articles/steam_tracing44.gif" alt="steam-tracing-44"/><br />

and<br />

<img src="../../../../invision/uploads/images/articles/steam_tracing45.gif" alt="steam-tracing-45"/><br />

therefore, k<sub>1</sub>=18.21340591<br />

k<sub>2</sub> may then be calculated using Eq.(11):<br />

<img src="../../../../invision/uploads/images/articles/steam_tracing46.gif" alt="steam-tracing-46"/><br />

and therefore amounts to k<sub>2</sub>= 0.489641399<br />
<br />

Finally the Process Fluid Temperature can be calculated using Eq.(12):<br />

<img src="../../../../invision/uploads/images/articles/steam_tracing47.gif" alt="steam-tracing-47"/><br />

<p>Excel is then programmed to perform iterations automatically, since a circular reference is created, but it causes all of the values to converge consequently, and the final answers are obtained, and with the final values of T<sub>ins</sub> known, the correct thermal conductivity values can be obtained and used in the equations:</p>

k<sub>ins</sub> = 0.02712 W/m K<br />

k<sub>w</sub> = 53.3 W/m K<br />
<br />

<p class="h1header">References</p>
Le Roux, D.F. (1997) â€œThermal Insulation and Heat Tracingâ€, Guideline presented by line manager D.F. le Roux, Secunda.<br />
<br />


Foo, K.W. (1994) â€œSizing tracers quickly (Part 1)â€. Hydrocarbon Processing, p93-97. January. â€œSizing tracers quickly (Part 2)â€. Hydrocarbon Processing, p93-97. February.<br />
<br />


Fisch, E. (1984) â€œWinterising process plantsâ€. Chemical Engineering, p128-143, 20 August.<br />
<br />


Kenny, T.M. (1992) â€Steam tracing: do it rightâ€. Chemical Engineering Progress, p40-44, August.<br />
<br />


Coulson, J.M and Richardson, J.F. (1999) Chemical Engineering, R.K. Sinnot, London.<br />
<br />


Le Roux, D.F. (2005) Theoretical discussion and problem description, Sasol Limited, Secunda.<br />
<br />


Van der Spuy, E. (2005) Theoretical advice, and steam traps, Spirax Sarco, Secunda.<br />
<br />


Smit, J. (2005) Practical information, Sasol Limited, Secunda.<br />
<br />


Technical committee of specification SP 50-4, (2004) Specification SP 50-4 Revision 2 for Steam and Hot Water Tracing, Sasol Limited, Secunda.<br />
<br />]]></description>
		<pubDate>Fri, 25 May 2012 18:05:21 +0000</pubDate>
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	</item>
	<item>
		<title>U in Heat Exchangers</title>
		<link>http://www.cheresources.com/content/articles/heat-transfer/u-in-heat-exchangers</link>
		<description><![CDATA[<p>The surface area A of heat exchangers required for a given service is determined from<br />





<br />





<a class='resized_img' rel='lightbox[8cbc6d101e4ed0b36c06bd962fd7c305]' id='ipb-attach-url-5122-0-23580000-1776244359' href="http://www.cheresources.com/invision/uploads/monthly_05_2012/ccs-1-0-34356200-1336667641.gif" title="uexchangers1.gif - Size: 1.01KB, Downloads: 276"><img src="http://www.cheresources.com/invision/uploads/monthly_05_2012/ccs-1-0-34356200-1336667641.gif" id='ipb-attach-img-5122-0-23580000-1776244359' style='width:73;height:46' class='attach' width="73" height="46" alt="Attached Image: uexchangers1.gif" /></a>
<br />





<br />





where<br />


{parse block="google_articles"}


<br />





QÂ Â Â Â = rate of heat transfer<br />





UÂ Â Â Â = mean overall heat transfer coefficient<br />





&#916;T<sub>m</sub>Â Â  = mean temperature difference<br />





<br />





For a given heat transfer service with known mass flow rates and inlet and outlet temperatures the determination of Q is straightforward and &#916;T<sub>m</sub> can be easily calculated if a flow arrangement is selected (e.g. logarithmic mean temperature difference for pure countercurrent or cocurrent flow). This is different for the overall heat transfer coefficient U. The determination of U is often tedious and needs data not yet available in preliminary stages of the design. The following is a table with values for different applications and heat exchanger types. More values can be found in the sources given below.<br />





<br />





The ranges given in the table are an indication for the order of magnitude. Lower values are for unfavorable conditions such as lower flow velocities, higher viscosities, and additional fouling resistances. Higher values are for more favorable conditions. Coefficients of actual equipment may be smaller or larger than the values listed. Note that the values should not be used as a replacement of rigorous methods for the final design of heat exchangers, although they may serve as a useful check on the results obtained by these methods.</p>
<br />





 <table class="datatable" border="0" align="center">
      <caption>Typical Overall Heat Transfer Coefficients in Heat Exchangers</caption>
      <tr>
        <td ALIGN="CENTER" WIDTH="60"><b>Type</b></td>
        <td ALIGN="CENTER" WIDTH="200"><b>Application and Conditions</b></td>
        <td ALIGN="CENTER" WIDTH="80"><b><i>U</i></b> <br />





        <font SIZE="-1">W/(m<sup>2</sup> K)<sup>1)</sup></font></td>
        <td ALIGN="CENTER" WIDTH="80"><b><i>U</i></b> <br />





        <font SIZE="-1">Btu/(ft<sup>2</sup> Â°F h)<sup>1)</sup></font></td>
      </tr>
      <tr>
        <td>Â </td>
        <td>Â </td>
        <td>Â </td>
        <td>Â </td>
      </tr>
      <tr>
        <td><b>Tubular, heating or cooling</b> </td>
        <td>Gases at atmospheric pressure inside and outside tubes </td>
        <td ALIGN="CENTER">5 - 35 </td>
        <td ALIGN="CENTER">1 - 6 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>Gases at high pressure inside and outside tubes </td>
        <td ALIGN="CENTER">150 - 500 </td>
        <td ALIGN="CENTER">25 - 90 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>Liquid outside (inside) and gas at atmospheric pressure inside (outside) tubes </td>
        <td ALIGN="CENTER">15 - 70 </td>
        <td ALIGN="CENTER">3 - 15 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>Gas at high pressure inside and liquid outside tubes </td>
        <td ALIGN="CENTER">200 - 400 </td>
        <td ALIGN="CENTER">35 - 70 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>Liquids inside and outside tubes </td>
        <td ALIGN="CENTER">150 - 1200 </td>
        <td ALIGN="CENTER">25 - 200 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>Steam outside and liquid inside tubes </td>
        <td ALIGN="CENTER">300 - 1200 </td>
        <td ALIGN="CENTER">50 - 200 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>Â </td>
        <td>Â </td>
        <td>Â </td>
      </tr>
      <tr>
        <td><b>Tubular, condensation</b> </td>
        <td>Steam outside and cooling water inside tubes </td>
        <td ALIGN="CENTER">1500 - 4000 </td>
        <td ALIGN="CENTER">250 - 700 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>Organic vapors or ammonia outside and cooling water inside tubes </td>
        <td ALIGN="CENTER">300 - 1200 </td>
        <td ALIGN="CENTER">50 - 200 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>Â </td>
        <td>Â </td>
        <td>Â </td>
      </tr>
      <tr>
        <td><b>Tubular, evaporation</b> </td>
        <td>steam outside and high-viscous liquid inside tubes, natural circulation </td>
        <td ALIGN="CENTER">300 - 900 </td>
        <td ALIGN="CENTER">50 - 150 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>steam outside and low-viscous liquid inside tubes, natural circulation </td>
        <td ALIGN="CENTER">600 - 1700 </td>
        <td ALIGN="CENTER">100 - 300 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>steam outside and liquid inside tubes, forced circulation </td>
        <td ALIGN="CENTER">900 - 3000 </td>
        <td ALIGN="CENTER">150 - 500 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>Â </td>
        <td>Â </td>
        <td>Â </td>
      </tr>
      <tr>
        <td><b>Air-cooled heat exchangers<sup>2) </sup></b></td>
        <td>Cooling of water </td>
        <td ALIGN="CENTER">600 - 750 </td>
        <td ALIGN="CENTER">100 - 130 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>Cooling of liquid light hydrocarbons </td>
        <td ALIGN="CENTER">400 - 550 </td>
        <td ALIGN="CENTER">70 - 95 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>Cooling of tar </td>
        <td ALIGN="CENTER">30 - 60 </td>
        <td ALIGN="CENTER">5 - 10 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>Cooling of air or flue gas </td>
        <td ALIGN="CENTER">60 - 180 </td>
        <td ALIGN="CENTER">10 - 30 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>Cooling of hydrocarbon gas </td>
        <td ALIGN="CENTER">200 - 450 </td>
        <td ALIGN="CENTER">35 - 80 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>Condensation of low pressure steam </td>
        <td ALIGN="CENTER">700 - 850 </td>
        <td ALIGN="CENTER">125 - 150 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>Condensation of organic vapors </td>
        <td ALIGN="CENTER">350 - 500 </td>
        <td ALIGN="CENTER">65 - 90 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>Â </td>
        <td>Â </td>
        <td>Â </td>
      </tr>
      <tr>
        <td><b>Plate heat exchanger</b> </td>
        <td>liquid to liquid </td>
        <td ALIGN="CENTER">1000 - 4000 </td>
        <td ALIGN="CENTER">150 - 700 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>Â </td>
        <td>Â </td>
        <td>Â </td>
      </tr>
      <tr>
        <td><b>Spiral heat exchanger</b> </td>
        <td>liquid to liquid </td>
        <td ALIGN="CENTER">700 - 2500 </td>
        <td ALIGN="CENTER">125 - 500 </td>
      </tr>
      <tr>
        <td>Â </td>
        <td>condensing vapor to liquid </td>
        <td ALIGN="CENTER">900 - 3500 </td>
        <td ALIGN="CENTER">150 - 700 </td>
      </tr>
    </table>

Notes:
1) 1 Btu/(ft2 Â°F h) = 5.6785 W/(m2 K)
2) Coefficients are based on outside bare tube surface

<p class="h1header">Sources</p>

SchlÃ¼nder, E. U. (Ed.): VDI Heat Atlas, Woodhead Publishing, Limited, 1993, Chapter Cc.<br />



Perry, R. H., Green, D. W. (Eds.): Perry's Chemical Engineers' Handbook, 7th edition, McGraw-Hill, 1997 , Section 11.<br />



Kern, D. Q.: Process Heat Transfer, McGraw-Hill, 1950.<br />



Ludwig, E. E.: Applied Process Design for Chemical and Petrochemical Plants, Vol. 3, 3rd edition, Gulf Publishing Company, 1998.<br />



Branan, C. R.: Process Engineer's Pocket Handbook, Vol. 1, Gulf Publishing Company, 1976.]]></description>
		<pubDate>Thu, 10 May 2012 15:09:50 +0000</pubDate>
		<guid isPermaLink="false">151d21647527d1079781ba6ae6571ffd</guid>
	</item>
	<item>
		<title>Correlations for Convective Heat Transfer</title>
		<link>http://www.cheresources.com/content/articles/heat-transfer/correlations-for-convective-heat-transfer</link>
		<description><![CDATA[<p>In many cases it's convenient to have simple equations for estimation of heat transfer coefficients. Below is a collection of recommended correlations for single-phase convective flow in different geometries as well as a few equations for heat transfer processes with change of phase. Note that all equations are for mean Nusselt numbers and mean heat transfer coefficients.</p><p>Â </p> <span class="h1header">Section 1: Forced Convection Flow Inside a Circular Tube</span><p>{parse block="google_articles"}Â </p><p>All properties at fluid bulk mean temperature (arithmetic mean of inlet and outlet temperature).</p><p>Nusselt numbers Nu<sub>0</sub> from sections 1-1 to 1-3 have to be corrected for temperature-dependent fluid properties according to section 1-4.</p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_1.gif" alt="convection_eq_1" width="101" height="49" /></p></td><td class="equationnumber" style="text-align: right;">Eq. (1)</td></tr></tbody></table><p>Â </p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_2.gif" alt="convection_eq_2" width="103" height="46" /></p></td><td class="equationnumber" style="text-align: right;">Eq. (2)</td></tr></tbody></table><p>Â </p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_3.gif" alt="convection_eq_3" width="98" height="46" /></p></td><td class="equationnumber" style="text-align: right;">Eq. (3)</td></tr></tbody></table><p>Â </p><p class="h2header">1-1 Thermally Developing, Hydrodynamically Developed Laminar Flow (Re<2300)</p><p>Constant wall temperature:</p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_4.gif" alt="convection_eq_4" width="270" height="89" /></p></td><td>(Hausen)</td><td class="equationnumber" style="text-align: right;">Eq. (4)</td></tr></tbody></table><p>Â </p><p>Constant wall heat flux:</p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_5.gif" alt="convection_eq_5" width="363" height="74" /></p></td><td>(Shah)</td><td class="equationnumber" style="text-align: right;">Eq. (5)</td></tr></tbody></table><p>Â </p><p class="h2header">1-2 Simultaneously Developing Laminar Flow (Re<2300)</p><p>Constant wall temperature:</p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_6.gif" alt="convection_eq_6" width="251" height="87" /></p></td><td>(Stephan)</td><td class="equationnumber" style="text-align: right;">Eq. (6)</td></tr></tbody></table><p>Â </p><p>Constant wall heat flux:</p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_7.gif" alt="convection_eq_7" width="246" height="89" /></p></td><td class="equationnumber" style="text-align: right;">Eq. (7)</td></tr></tbody></table><p>which is valid over the range 0.7 < Pr < 7 or if Re Pr <em>D</em>/<em>L</em> < 33 also for Pr > 7.</p><p class="h2header">1-3 Fully Developed Turbulent and Transition Flow (Re>2300)</p><p>Constant wall heat flux:</p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_8.gif" alt="convection_eq_8" width="300" height="96" /></p></td><td>(Petukhov, Gnielinski)</td><td class="equationnumber" style="text-align: right;">Eq. (8)</td></tr><tr><td valign="middle" scope="row"><p style="text-align: left;">where: <img src="../../../../invision/uploads/images/articles/convection_1.gif" alt="convection_1" width="174" height="51" /></p></td><td></td><td></td></tr></tbody></table><p>Constant wall temperature:</p><p>For fluids with Pr > 0.7 correlation for constant wall heat flux can be used with negligible error.</p><p class="h2header">1-4 Effects of Property Variation with Temperature</p><p>Liquids, laminar and turbulent flow:</p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_9.gif" alt="convection_eq_9" width="133" height="59" /></p></td><td class="equationnumber" style="text-align: right;">Eq. (9)</td></tr></tbody></table><p>Subscript w: at wall temperature, without subscript: at mean fluid temperature.</p><p>Gases, laminar flow:</p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;">Nu = Nu<sub>0</sub></p></td><td class="equationnumber" style="text-align: right;">Eq. (10)</td></tr></tbody></table><p>Gases, turbulent flow:</p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_11.gif" alt="convection_eq_11" width="136" height="59" /></p></td><td class="equationnumber" style="text-align: right;">Eq. (11)</td></tr></tbody></table><p>Temperatures in Kelvin.</p><hr class="system-pagebreak" title="Forced Convection Inside Annular Ducts" /><p class="h1header">Section 2: Forced Convection Flow Inside Concentric Annular Ducts, Turbulent (Re > 2300)</p><table style="text-align: center;" border="0"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_2.gif" alt="convection_2" width="197" height="257" /></td><td><p><em>D<sub>h</sub></em> = <em>D<sub>o</sub></em> - <em>D<sub>i</sub></em></p><p><img src="../../../../invision/uploads/images/articles/convection_3.gif" alt="convection_3" width="103" height="48" /></p><p><img src="../../../../invision/uploads/images/articles/convection_4.gif" alt="convection_4" width="84" height="46" /></p><p>All properties at fluid bulk mean temperature (arithmetic mean of inlet and outlet temperature).</p><p>Â </p></td></tr></tbody></table><p>Heat transfer at the inner wall, outer wall insulated:</p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_12.gif" alt="convection_eq_12" width="156" height="59" /></p></td><td>(Petukhov and Roizen)</td><td class="equationnumber" style="text-align: right;">Eq. (12)</td></tr></tbody></table><p>Heat transfer at the outer wall, inner wall insulated:</p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_13.gif" alt="convection_eq_13" width="174" height="59" /></p></td><td>(Petukhov and Roizen)</td><td class="equationnumber" style="text-align: right;">Eq. (13)</td></tr></tbody></table><p>Heat transfer at both walls, same wall temperatures:</p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_14.gif" alt="convection_eq_14" width="304" height="112" /></p></td><td>(Stephan)</td><td class="equationnumber" style="text-align: right;">Eq. (14)</td></tr></tbody></table><p></p><hr class="system-pagebreak" title="Forced Convection Inside Non-Circular Ducts" /><p class="h1header">Section 3: Forced Convection Flow Inside Non-Circular Ducts, Turbulent (Re > 2300)</p><p>Equations for circular tube with hydraulic diameter:</p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_15.gif" alt="convection_eq_15" width="216" height="50" /></p></td><td class="equationnumber" style="text-align: right;">Eq. (15)</td></tr></tbody></table><p>Â </p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_16.gif" alt="convection_eq_16" width="103" height="48" /></p></td><td class="equationnumber" style="text-align: right;">Eq. (16)</td></tr></tbody></table><p>Â </p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_17.gif" alt="convection_eq_17" width="79" height="46" /></p></td><td class="equationnumber" style="text-align: right;">Eq. (17)</td></tr></tbody></table><p></p><p class="h1header">Section 4: Forced Convection Flow Across Single Circular Cylinders and Tube Bundles</p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_18.gif" alt="convection_eq_18" width="57" height="46" /></p></td><td class="equationnumber" style="text-align: right;">Eq. (18)</td></tr></tbody></table><p>Â </p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_19.gif" alt="convection_eq_19" width="88" height="50" /></p></td><td class="equationnumber" style="text-align: right;">Eq. (19)</td></tr></tbody></table><p>Â </p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_20.gif" alt="convection_eq_20" width="64" height="42" /></p></td><td class="equationnumber" style="text-align: right;">Eq. (20)</td></tr></tbody></table><p><em>D</em> = cylinder diameter, <em>u<sub>m</sub></em> = free-stream velocity, all properties at fluid bulk mean temperature. Correction for temperature dependent fluid properties see section 4-4.</p><p class="h2header">4-1 Smooth Circular Cylinder</p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_21.gif" alt="convection_eq_21" width="222" height="35" /></p></td><td class="equationnumber" style="text-align: right;">Eq. (21)</td></tr><tr><td><p style="text-align: left;">where: <img src="../../../../invision/uploads/images/articles/convection_5.gif" alt="convection_5" width="202" height="32" /></p></td><td></td></tr></tbody></table><p>Â </p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><p style="text-align: left;"><img src="../../../../invision/uploads/images/articles/convection_eq_22.gif" alt="convection_eq_22" width="251" height="56" /></p></td><td class="equationnumber" style="text-align: right;">Eq. (22)</td></tr></tbody></table><p>Valid over the ranges 10 < Re<em><sub>l</sub></em> < 10<sup>7</sup> and 0.6 < Pr < 1000.</p><p class="h2header">4-2 Tube Bundle</p><p>Transverse pitch ratio <img style="vertical-align: middle;" src="../../../../invision/uploads/images/articles/convection_6.gif" alt="convection_6" width="54" height="50" /></p><p>Longitudinal pitch ratio <img style="vertical-align: middle;" src="../../../../invision/uploads/images/articles/convection_7.gif" alt="convection_7" width="48" height="43" /></p><p>Void ratio <img style="vertical-align: middle;" src="../../../../invision/uploads/images/articles/convection_8.gif" alt="convection_8" width="92" height="43" />for <em>b</em> <span style="text-decoration: underline;">></span> 1</p><p><img style="vertical-align: middle;" src="../../../../invision/uploads/images/articles/convection_9.gif" alt="convection_9" width="80" height="43" />for <em>b</em> < 1</p><p>Nu<sub>0,bundle</sub> = <em>f</em><sub>A</sub>Nu<sub>l,0</sub> (Gnielinski)</p><p>Nu<sub>l,0</sub> according to section 4-1 with <img style="vertical-align: middle;" src="../../../../invision/uploads/images/articles/convection_10.gif" alt="convection_10" width="102" height="51" />instead of Re<sub>l</sub>.</p><p>Arrangement factor <em>f</em><sub>A</sub> depends on tube bundle arrangement.</p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_11.gif" alt="convection_11" width="227" height="302" /></td><td><p style="text-align: left;">In line arrangement: <img style="vertical-align: middle;" src="../../../../invision/uploads/images/articles/convection_eq_23.gif" alt="convection_eq_23" width="187" height="51" /></p></td><td><p class="equationnumber" style="text-align: right;">Eq. (23)</p></td></tr></tbody></table><p>Â </p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><img style="float: left;" src="../../../../invision/uploads/images/articles/convection_12.gif" alt="convection_12" width="308" height="298" /></td><td><p style="text-align: left;">Staggered arrangement: <img style="vertical-align: middle;" src="../../../../invision/uploads/images/articles/convection_eq_24.gif" alt="convection_eq_24" width="77" height="43" /></p></td><td><p class="equationnumber" style="text-align: right;">Eq. (24)</p></td></tr></tbody></table><p>Â </p><p class="h2header">4-3 Finned Tube Bundle</p><table border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_13.gif" alt="convection_13" width="303" height="291" /></td><td><p><img src="../../../../invision/uploads/images/articles/convection_14.gif" alt="convection_14" width="248" height="87" /></p><p><img src="../../../../invision/uploads/images/articles/convection_15.gif" alt="convection_15" width="167" height="61" /></p></td></tr></tbody></table><p>In-line tube bundle arrangement:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_eq_25.gif" alt="convection_eq_25" width="301" height="57" /></td><td class="equationnumber" align="right">Eq. (25)</td></tr></tbody></table><p>Staggered tube bundle arrangement:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_eq_26.gif" alt="convection_eq_26" width="308" height="58" /></td><td class="equationnumber" align="right">Eq. (26)</td></tr></tbody></table><p>Â </p><p class="h2header">4-4 Effects of Property Variation with Temperature</p><p>Liquids:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_eq_27.gif" alt="convection_eq_27" width="158" height="65" /></td><td class="equationnumber" align="right">Eq. (27)</td></tr></tbody></table><p>Â </p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_eq_28.gif" alt="convection_eq_28" width="196" height="61" /></td><td class="equationnumber" align="right">Eq. (28)</td></tr></tbody></table><p>Subscript w: at wall temperature, without subscript: at mean fluid temperature.</p><p>Gases:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_eq_29.gif" alt="convection_eq_29" width="146" height="59" /></td><td class="equationnumber" align="right">Eq. (29)</td></tr></tbody></table><p>Â </p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_eq_30.gif" alt="convection_eq_30" width="198" height="59" /></td><td class="equationnumber" align="right">Eq. (30)</td></tr></tbody></table><p>Temperatures in Kelvin.</p><p class="h1header">Section 5: Forced Convection Flow over a Flat Plate</p><table border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_16.gif" alt="convection_16" width="301" height="137" /></td><td><img src="../../../../invision/uploads/images/articles/convection_17.gif" alt="convection_17" width="97" height="123" /></td></tr></tbody></table><p>All properties at mean film temperature <img style="vertical-align: middle;" src="../../../../invision/uploads/images/articles/convection_18.gif" alt="convection_18" width="89" height="43" />.</p><p>Laminar boundary layer, constant wall temperature:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_eq_31.gif" alt="convection_eq_31" width="183" height="30" /></td><td>(Pohlhausen)</td><td class="equationnumber" align="right">Eq. (31)</td></tr></tbody></table><p>valid for Re<sub>L</sub> < 2Â·10<sup>5</sup>, 0.6 < Pr < 10</p><p>Turbulent boundary layer along the whole plate, constant wall temperature:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_eq_32.gif" alt="convection_eq_32" width="256" height="56" /></td><td>(Petukhov)</td><td class="equationnumber" align="right">Eq. (32)</td></tr></tbody></table><p>Boundary layer with laminar-turbulent transition:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_eq_33.gif" alt="convection_eq_33" width="185" height="36" /></td><td>(Gnielinski)</td><td class="equationnumber" align="right">Eq. (33)</td></tr></tbody></table><p></p><hr class="system-pagebreak" title="Natural Convection" /><p class="h1header">Section 6: Natural Convection</p><p>All properties at <img style="vertical-align: middle;" src="../../../../invision/uploads/images/articles/convection_19.gif" alt="convection_19" width="125" height="51" />.</p><table border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_20.gif" alt="convection_20" width="199" height="140" /></td><td><em>L</em> = characteristic length (see below)</td></tr></tbody></table><p>Â </p><table class="datatable" border="0" align="center"><caption>Table 1: Characteric Length</caption> <tbody><tr><td></td><td>Nu<sub>0</sub></td><td>"Length" L</td></tr><tr><td>Vertical Wall</td><td>0.67</td><td>H</td></tr><tr><td>Horizontal Cylinder</td><td>0.36</td><td>D</td></tr><tr><td>Sphere</td><td>2.00</td><td>D</td></tr></tbody></table><p>For ideal gases: <img style="vertical-align: middle;" src="../../../../invision/uploads/images/articles/convection_21.gif" alt="convection_21" width="62" height="51" />(temperature in K)</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_eq_34.gif" alt="convection_eq_34" width="266" height="97" /></td><td>(Churchill, Thelen)</td><td class="equationnumber" align="right">Eq. (34)</td></tr></tbody></table><p>valid for 10<sup>-4</sup> <span style="text-decoration: underline;"><</span> Gr Pr <span style="text-decoration: underline;"><</span> 4Â·10<sup>14</sup>, 0.022 <span style="text-decoration: underline;"><</span> Pr <span style="text-decoration: underline;"><</span> 7640, and constant wall temperature.</p><p class="h1header">Section 7: Film Condensation</p><p>All properties without subscript are for condensate at the mean temperature <img style="vertical-align: middle;" src="../../../../invision/uploads/images/articles/convection_22.gif" alt="convection_22" width="112" height="46" />.</p><p>Exception: ?<sub>D</sub> = vapor density at saturation temperature <em>T</em><sub>s</sub></p><p class="h2header">7-1 Laminar Film Condensation</p><p>Vertical wall or tube:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_eq_35.gif" alt="convection_eq_35" width="290" height="59" /></td><td>(Nusselt)</td><td class="equationnumber" align="right">Eq. (35)</td></tr></tbody></table><p><em>T</em><sub>w</sub> = mean wall temperature</p><p>Horizontal cylinder:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_eq_36.gif" alt="convection_eq_36" width="296" height="59" /></td><td>(Nusselt)</td><td class="equationnumber" align="right">Eq. (36)</td></tr></tbody></table><p><em>T</em><sub>w</sub> = const.</p><p class="h2header">7-2 Turbulent Film Condensation</p><p>For vertical wall:</p><p>Re = C A<sup>m</sup></p><p><img src="../../../../invision/uploads/images/articles/convection_23.gif" alt="convection_23" width="334" height="58" /></p><p>Re<sub>crit</sub> = 350</p><p>For turbulent film: C = 3.8 x 10<sup>-3</sup> and m = 3/2 (Grigull).</p><p class="h1header">Section 8: Nucleate Pool Boiling</p><p><img src="../../../../invision/uploads/images/articles/convection_24.gif" alt="convection_24" width="97" height="24" /></p><p><em>T</em><sub>w</sub> = temperature of heating surface</p><p><em>T</em><sub>s</sub> = saturation temperature</p><p>Heat transfer at ambient pressure:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_eq_37.gif" alt="convection_eq_37" width="518" height="66" /></td><td>(Stephan and Preuber)</td><td class="equationnumber" align="right">Eq. (37)</td></tr></tbody></table><p>' saturated liquid</p><p>'' saturated vapor</p><p>Bubble departure diameter <img style="vertical-align: middle;" src="../../../../invision/uploads/images/articles/convection_25.gif" alt="convection_25" width="186" height="55" /></p><p>Angle ?<sub>0</sub> = ?/4 rad for water = 0.0175 rad for low-boiling liquids  = 0.611 rad for other liquids</p><p>For water in the range of 0.5 bar < <em>p</em> < 20 bar and 10<sup>4</sup> W/m<sup>2</sup> <<img style="vertical-align: middle;" src="../../../../invision/uploads/images/articles/convection_26.gif" alt="convection_26" width="15" height="25" />< 10<sup>6</sup> W/m<sup>2 </sup>the following equation may be applied:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/convection_eq_38.gif" alt="convection_eq_38" width="277" height="54" /></td><td>(Fritz)</td><td class="equationnumber" align="right">Eq. (38)</td></tr></tbody></table> <p class="h1header">List of Symbols</p><p>Â </p><table border="0" align="center"><tbody><tr><td>c<sub>p</sub></td><td>specific heat capacity at constant pressure</td></tr><tr><td>D, d</td><td>diamter</td></tr><tr><td>g</td><td>gravitational acceleration</td></tr><tr><td>h</td><td>meanÂ heat transfer coefficient</td></tr><tr><td>&#916;h</td><td>enthalpy of evaporation</td></tr><tr><td>H</td><td>height</td></tr><tr><td>k</td><td>thermal conductivity</td></tr><tr><td>L</td><td>length</td></tr><tr><td><img src="../../../../invision/uploads/images/articles/convection_26.gif" alt="convection_26" width="15" height="25" /></td><td>heat flux</td></tr><tr><td>T</td><td>temperature</td></tr><tr><td>u</td><td>flow velocity</td></tr><tr><td>&#945;</td><td>thermal diffusivity</td></tr><tr><td>&#946;</td><td>coefficient of thermal expansion</td></tr><tr><td>&#956;</td><td>dynamic viscosity</td></tr><tr><td>&#965;</td><td>kinematic viscosity</td></tr><tr><td>&#961;</td><td>density</td></tr><tr><td>&#963;</td><td>surface tension</td></tr></tbody></table><p>Â </p><p class="h2header">Subscripts</p><p>Â </p><table border="0" align="center"><tbody><tr><td>h</td><td>hydraulic</td></tr><tr><td>i</td><td>inside</td></tr><tr><td>m</td><td>mean</td></tr><tr><td>o</td><td>outside</td></tr><tr><td>s</td><td>saturation</td></tr><tr><td>w</td><td>wall</td></tr></tbody></table><p>Â </p><p class="h2header">Dimensionless Numbers</p><p>Â </p><table border="0" align="center"><tbody><tr><td>Gr</td><td>Grashof number</td></tr><tr><td>Nu</td><td>mean Nusselt number</td></tr><tr><td>Pr</td><td>Prandtl number</td></tr><tr><td>Re</td><td>Reynolds number</td></tr></tbody></table>   <p class="h1header">References</p><ol><li>Churchill, S.W.: Free convection around immersed bodies. Chapter 2.5.7 of <em>Heat Exchanger Design Handbook</em>, Hemisphere (1983). </li><li>Fritz, W.: In <em>VDI-WÃ¤rmeatlas</em>, DÃ¼sseldorf (1963), Hb2. </li><li>Gnielinski, V.: Neue Gleichungen fÃ¼r den WÃ¤rme- und den StoffÃ¼bergang in turbulent durchstrÃ¶mten Rohren und KanÃ¤len. <em>Forschung im Ingenieurwesen</em> <strong>41</strong>, 8-16 (1975). </li><li>Gnielinski, V.: Berechnung mittlerer WÃ¤rme- und StoffÃ¼bergangskoeffizienten an laminar und turbulent Ã¼berstrÃ¶mten EinzelkÃ¶rpern mit Hilfe einer einheitlichen Gleichung. <em>Forschung im Ingenieurwesen</em> <strong>41</strong>, 145-153 (1975). </li><li>Grigull, U.: WÃ¤rmeÃ¼bergang bei der Kondensation mit turbulenter Wasserhaut. <em>Forschung im Ingenieurwesen</em> <strong>13</strong>, 49-57 (1942). </li><li>Hausen, H.: Neue Gleichungen fÃ¼r die WÃ¤rmeÃ¼bertragung bei freier und erzwungener StrÃ¶mung. <em>Allg. WÃ¤rmetechnik</em> <strong>9</strong>, 75-79 (1959). </li><li>Nusselt, W.: Die OberflÃ¤chenkondensation des Wasserdampfes. <em>VDI Z.</em> <strong>60</strong>, 541-546 and 569-575 (1916). </li><li>Petukhov, B.S.: Heat transfer and friction in turbulent pipe flow with variable physical properties. <em>Adv. Heat Transfer</em> <strong>6</strong>, 503-565 (1970). </li><li>Petukhov, B.S. and L.I. Roizen: <em>High Temperature</em> <strong>2</strong>, 65-68 (1964). </li><li>Pohlhausen, E.: Der WÃ¤rmeaustausch zwischen festen KÃ¶rpern und FlÃ¼ssigkeiten mit kleiner Reibung und kleiner WÃ¤rmeleitung. <em>Z. Angew. Math. Mech.</em> <strong>1</strong>, 115-121 (1921). </li><li>Shah, R.K.: Thermal entry length solutions for the circular tube and parallel plates. <em>Proc. 3<sup>rd</sup> Natnl. Heat Mass Transfer Conference, Indian Inst. Technol Bombay,</em> Vol. I, Paper HMT-11-75 (1975). </li><li>Stephan, K.: WÃ¤rmeÃ¼bergang und Druckabfall bei nicht ausgebildeter LaminarstrÃ¶mung in Rohren und ebenen Spalten. <em>Chem.-Ing.-Tech.</em> <strong>31</strong>, 773-778 (1959). </li><li>Stephan, K.: <em>Chem.-Ing.-Tech.</em> <strong>34</strong>, 207-212 (1962). </li><li>Stephan, K. and P. PreuÃŸer: WÃ¤rmeÃ¼bergang und maximale WÃ¤rmestromdichte beim BehÃ¤ltersieden binÃ¤rer und ternÃ¤rer FlÃ¼ssigkeitsgemische. <em>Chem.-Ing.-Tech.</em> <strong>51</strong>, 37 (1979). </li><li><em>VDI-WÃ¤rmeatlas</em>, 7<sup>th</sup> edition, DÃ¼sseldorf 1994. </li></ol>]]></description>
		<pubDate>Mon, 08 Nov 2010 18:50:19 +0000</pubDate>
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		<title>Cooling Towers: Design and Operation Considerat...</title>
		<link>http://www.cheresources.com/content/articles/heat-transfer/cooling-towers-design-and-operation-considerations</link>
		<description><![CDATA[Cooling towers are a very important part of many chemical plants. They represent a relatively inexpensive and dependable means of removing low grade heat from cooling water.<br />The make-up water source is used to replenish water lost to evaporation. Hot water from heat exchangers is sent to the cooling tower. The water exits the cooling tower and is sent back to the exchangers or to other units for further cooling.{parse block="google_articles"}<br /><p class="h1header">Types of Cooling Towers</p>										<br /><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Cooling Tower Layout" href="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ctowers1.gif" target="_blank"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/thumb_ctowers1.gif" alt="cooling_tower_layout" /></a></td></tr><tr><td>Figure 1: Closed Loop Cooling Tower System</td></tr></tbody></table>		<br />Cooling towers fall into two main sub-divisions: natural draft and mechanical draft. Natural draft designs use very large concrete chimneys to introduce air through the media. Due to the tremendous size of these towers (500 ft high and 400 ft in diameter at the base) they are generally used for water flowrates above 200,000 gal/min. Usually these types of towers are only used by utility power stations in the United States. Mechanical draft cooling towers are much more widely used. These towers utilize large fans to force air through circulated water. The water falls downward over fill surfaces which help increase the contact time between the water and the air. This helps maximize heat transfer between the two.<br /><p class="h1header">Mechanical Draft Towers</p><br />Mechanical draft towers offer control of cooling rates in their fan diameter and speed of operation. These towers often contain several areas (each with their own fan) called cells.<br /><div style="width:660px;"><br /><div style="width:330px; float:left"><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Mechanical Draft Counterflow" href="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ctower2.gif" target="_blank"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/thumb_ctower2.gif" alt="mechanical_draft_counterflow" width="97" height="150" /></a></td></tr><tr><td>Figure 2: Mechanical Draft Counterflow Tower</td></tr></tbody></table></div><div style="width:330px; float:left;"><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Mechanical Draft Crossflow" href="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ctower3.gif" target="_blank"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/thumb_ctower3.gif" alt="mechanical_draft_crossflow" width="97" height="150" /></a></td></tr><tr><td>Figure 3: Mechanical Draft Crossflow Tower</td></tr></tbody></table></div></div>					<br /><br /><br /><p><p class="h1header">Cooling Tower Theory</p></p>Heat is transferred from water drops to the surrounding air by the transfer of sensible and latent heat.<br /><table class="imagecaption" border="0" align="center"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ctower4.gif" alt="evaporative_cooling" /></td></tr><tr><td>Figure 4: Water Drop with Interfacial Film</td></tr></tbody></table><br />			<br />This movement of heat can be modeled with a relation known as the Merkel Equation:<br /><table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ctower5.gif"</td><td class="equationnumber" align="right">Eq. (1)</td></tr></tbody></table><br />where:<br />KaV/L = tower characteristic<br />K = mass transfer coefficient (lb water/h ft<sup class='bbc'>2</sup>)<br />a= contact area/tower volume<br />V = active cooling volume/plan area<br />L = water rate (lb/h ft<sup class='bbc'>2</sup>)<br />T<sub class='bbc'>1</sub> = hot water temperature (<sup class='bbc'>Â°</sup>F or <sup class='bbc'>Â°</sup>C)<br />T<sub class='bbc'>2</sub> = cold water temperature (Â°F or <sup class='bbc'>Â°</sup>C)<br />T = bulk water temperature (<sup class='bbc'>Â°</sup>F or <sup class='bbc'>Â°</sup>C)<br />h<sub class='bbc'>w</sub> = enthalpy of air-water vapor mixture at bulk water temperature (J/kg dry air or Btu/lb dry air)<br />h<sub class='bbc'>a</sub> = enthalpy of air-water vapor mixture at wet bulb temperature (J/kg dry air or Btu/lb dry air)<br />Thermodynamics also dictate that the heat removed from the water must be equal to the heat absorbed by the surrounding air:					<table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ctower6.gif"</td><td class="equationnumber" align="right">Eq. (2)</td></tr></tbody></table>		<br /><table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ctower7.gif"</td><td class="equationnumber" align="right">Eq. (3)</td></tr></tbody></table>		<br />where:<br />L/G = liquid to gas mass flow ratio (lb/lb or kg/kg)<br />T<sub class='bbc'>1</sub> = hot water temperature (<sup class='bbc'>0</sup>F or <sup class='bbc'>0</sup>C)<br />T<sub class='bbc'>2</sub> = cold water temperature (<sup class='bbc'>0</sup>F or <sup class='bbc'>0</sup>C)<br />h<sub class='bbc'>2</sub> = enthalpy of air-water vapor mixture at exhaust wet-bulb temperature (same units as above)<br />h<sub class='bbc'>1</sub> = enthalpy of air-water vapor mixture at inlet wet-bulb temperature (same units as above)<br /><p class='bbc_left'>The tower characteristic value can be calculated by solving Equation 1 with the Chebyshev numberical method:</p><table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ctower9.gif"</td><td class="equationnumber" align="right">Eq. (4)</td></tr></tbody></table>		<br />where:<br />&#916;h<sub class='bbc'>1</sub> = value of h<sub class='bbc'>w</sub>-h<sub class='bbc'>a</sub> at T<sub class='bbc'>2</sub>+0.1(T<sub class='bbc'>1</sub>-T<sub class='bbc'>2</sub>)<br />&#916;h<sub class='bbc'>2</sub> = value of h<sub class='bbc'>w</sub>-h<sub class='bbc'>a</sub> at T<sub class='bbc'>2</sub>+0.4(T<sub class='bbc'>1</sub>-T<sub class='bbc'>2</sub>)<br />&#916;h<sub class='bbc'>3</sub> = value of h<sub class='bbc'>w</sub>-h<sub class='bbc'>a</sub> at T<sub class='bbc'>1</sub>-0.4(T<sub class='bbc'>1</sub>-T<sub class='bbc'>2</sub>)<br />&#916;h<sub class='bbc'>4</sub> = value of h<sub class='bbc'>w</sub>-h<sub class='bbc'>a</sub> at T<sub class='bbc'>1</sub>-0.1(T<sub class='bbc'>1</sub>-T<sub class='bbc'>2</sub>)<br />Figure 5 below shows a graphical representation of how heat is tranferred between the warm water and cooler surrounding air:<br /><table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ctower10.gif" alt="enthalpy-diagram"/></a></td></tr><tr><td>Figure 5: Graphical Representation of the Tower Characteristic</td></tr></tbody></table><br />			<br />The following represents a key to Figure 5:<br />C' = Entering air enthalpy at wet-bulb temperature, T<sub class='bbc'>wb</sub><br />BC = Initial enthalpy driving force<br />CD = Air operating line with slope L/G<br />DEF = Projecting the exiting air point onto the water operating line and then onto the temperature axis shows the outlet air web-bulb temperature<br /><table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ctower11.gif" alt="temperature-correction"/></a></td></tr><tr><td>Figure 6: Adjusted Hot Water Temperature</td></tr></tbody></table><br />As shown by Equation 1, by finding the area between ABCD in Figure 5, one can find the tower characteristic. An increase in heat load would have the following effects on the diagram in Figure 5:<ul class='bbcol decimal'><li>Increase in the length of line CD, and a CD line shift to the right</li><li>Increases in hot and cold water temperatures</li><li>Increases in range and approach areas</li></ul>The increased heat load causes the hot water temperature to increase considerably faster than does the cold water temperature. Although the area ABCD should remain constant, it actually decreases about 2% for every 10 <sup class='bbc'>Â°</sup>F increase in hot water temperature above 100 <sup class='bbc'>Â°</sup>F. To account for this decrease, an "adjusted hot water temperature" is usd in cooling tower design.  Figure 6 shows adjusted hot water temperatures.<br />The area ABCD is expected to change with a change in L/G, this is very key in the design of cooling towers.<br /><br /><p class="h1header">Preliminary Cooling Tower Design</p><br /><br />Although KaV/L can be calculated, designers typically use charts found in the "Cooling Tower Institute Blue Book" to estimate KaV/L for given design conditions.{parse block="google_articles"}  It is important to recall three key points in cooling tower design:<ul class='bbcol decimal'><li>A change in wet bulb temperature (due to atmospheric conditions) <span class='bbc_underline'>will not</span> change the tower characteristic (KaV/L)</li><li>A change in the cooling range <span class='bbc_underline'>will not</span> change KaV/L</li><li>Only a change in the L/G ratio <span class='bbc_underline'>will</span> change KaV/L</li></ul><table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ctower12.gif" alt="characteristic-curves"/></a></td></tr><tr><td>Figure 7: A Typical Set of Tower Characteristic Curves</td></tr></tbody></table>														<br />The straight line shown in Figure 7 is a plot of L/G vs KaV/L at a constant airflow.  The slope of this line is dependent on the tower packing, but can often be assumed to be -0.60.  Figure 7 represents a typical graph supplied by a manufacturer to the purchasing company.  From this graph, the plant engineer can see that the proposed tower will be capable of cooling the water to a temperature that is 10 <sup class='bbc'>Â°</sup>F above the wet-bulb temperature.  This is another key point in cooling tower design.<br />Cooling towers are designed according to the highest geographic wet bulb temperatures.  This temperature will dictate the minimum performance available by the tower.  As the wet bulb temperature decreases, so will the available cooling water temperature.  For example, in the cooling tower represented by Figure 7, if the wet bulb temperature dropped to 75 <sup class='bbc'>Â°</sup>F, the cooling water would still be exiting 10 <sup class='bbc'>Â°</sup>F above this temperature (85 <sup class='bbc'>Â°</sup>F) due to the tower design.<br />Below is the summary of steps in the cooling tower design process in industry.  More detail on these steps will be given later.<ul class='bbcol decimal'><li>Plant engineer defines the cooling water flowrate, and the inlet and outlet water temperatures for the tower.</li><li>Manufacturer designs the tower to be able to meet this criteria on a "worst case scenario" (ie. during the hottest months).  The tower characteristic curves and the estimate is given to the plant engineer.</li><li>Plant engineer reviews bids and makes a selection</li></ul><br /><p class="h1header">Other Design Considerations</p><br />Once a tower characteristic has been established between the plant engineer and the manufacturer, the manufacturer must design a tower that matches this value.  The required tower size will be a function of:<ul class='bbcol decimal'><li>Cooling range</li><li>Approach to wet bulb temperature</li><li>Mass flowrate of water</li><li>Web bulb temperature</li><li>Air velocity through tower or individual tower cell</li><li>Tower height</li></ul>In short, nomographs such as the one shown on page 12-15 of "Perry's Chemical Engineers' Handbook 6th Ed" utilize the cold water temperature, wet bulb temperature, and hot water temperature to find the water concentration in gal/min ft<sup class='bbc'>2</sup>.   The <em class='bbc'>tower area</em> can then be calculated by dividing the water circulated by the water concentration.  General rules are usually used to determine <em class='bbc'>tower height</em> depending on the necessary time of contact:		<br /><table class="datatable" border="0" align="center"><caption>Table 1: Tower Height as a Function of Approach to Wet Bulb Temperature</caption><tr><td width="33%"><p align="center">Approach to Wet Bulb (<sup>0</sup>F)</td><td width="33%"><p align="center">Cooling Range (<sup>0</sup>F)</td><td width="34%"><p align="center">Tower Height (ft)</td></tr><tr><td width="33%" align="center">15-20</td><td width="33%" align="center">25-35</td><td width="34%" align="center">15-20</td></tr><tr><td width="33%" align="center">10-15</td><td width="33%" align="center">25-35</td><td width="34%" align="center">25-30</td></tr><tr><td width="33%" align="center">5-10</td><td width="33%" align="center">25-35</td><td width="34%" align="center">35-40</td></tr></table>		<br />Other design characteristics to consider are fan horsepower, pump horsepower, make-up water source, fogging abatement, and drift eliminators.<br /><br /><p class="h1header">Operation Considerations</p><br /><p class="h2header">Water Makeup</p><br />Water losses include evaporation, drift (water entrained in discharge vapor), and blowdown (water released to discard solids).  Drift losses are estimated to be between 0.1 and 0.2% of water supply.<br /><br /><table class="equationtable" border="0" align="center"><tbody><tr><td valign="top">Evaporation Loss = 0.00085 * water flowrate(T<sub class='bbc'>1</sub>-T<sub class='bbc'>2</sub>)</td><td class="equationnumber" align="right">Eq. (5)</td></tr></tbody></table><br /><table class="equationtable" border="0" align="center"><tbody><tr><td valign="top">Blowdown Loss = Evaporation Loss/(cycles-1)</td><td class="equationnumber" align="right">Eq. (6)</td></tr></tbody></table>where cycles is the ratio of solids in the circulating water to the solids in the make-up water<br /><br /><table class="equationtable" border="0" align="center"><tbody><tr><td valign="top">Total Losses = Drift Losses + Evaporation Losses + Blowdown Losses</td><td class="equationnumber" align="right">Eq. (7)</td></tr></tbody></table><br /><p class="h2header">Cold Weather Operation</p><br />Even during cold weather months, the plant engineer should maintain the design water flowrate and heat load in each cell of the cooling tower.   If less water is needed due to temperature changes (ie. the water is colder), one or more cells should be turned off to maintain the design flow in the other cells.   The water in the base of the tower should be maintained between 60 and 70 <sup class='bbc'>0</sup>F by adjusting air volume if necessary.  Usual practice is to run the fans at half speed or turn them off during colder months to maintain this temperature range.<br /><br /><p class="h1header">References</p><ul class='bbcol decimal'><li>The Standard Handbook of Plant Engineering, 2nd Edition, Rosaler, Robert C., McGraw-Hill, New York, 1995</li><li>Perry's Chemical Engineers' Handbook, 6th Edition, Green, Don W. et al, McGraw-Hill, New York, 1984</li></ul>]]></description>
		<pubDate>Mon, 08 Nov 2010 18:50:19 +0000</pubDate>
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		<title>Design Considerations for Shell and Tube Heat E...</title>
		<link>http://www.cheresources.com/content/articles/heat-transfer/design-considerations-for-shell-and-tube-heat-exchangers</link>
		<description><![CDATA[When preparing to design a heat exchanger, do you ever wonder where to start?  You've done it before, but you hate that feeling of getting half way through the design and realizing that you forgot to consider one important element.<br />The thought process involved is just as important as the calculations involved.  Let's try to map out a heat exchanger design strategy.  We'll do so with a series of questions followed by information to help you answer the questions.<br /><p class="h1header">Asking the Right Questions</p><br /><p class="h2header">Is there a phase change involved?</p><br />The thought process involved is just as important as the calculations involved.  Let's try to map out a heat exchanger design strategy.  We'll do so with a series of questions followed by information to help you answer the questions.{parse block="google_articles"}<br /><p class="h2header">How many zones are there in my system?</p><br />"Zones" can best be defined as regimes of phase changes where the overall heat transfer coefficient (Uo) will vary.  Using T-Q (Temperature-Heat) diagrams are the best way to pinpoint zones.  The system is defined as co-current or countercurrent and the diagram is constructed.  The diagram on the left illustrates the use of T-Q diagrams. These diagrams should accompany your basic (input-output) diagram of the heat exchanger.   Chemical #1 enters the shell at 200 <sup class='bbc'>Â°</sup>C as a superheated vapor. In Zone 1, it releases heat to the tubeside chemical (Chemical #2).  Zone 1 ends just a Chemical #1 begins to condense.  The tubeside (Chemical #2) enters as a liquid or gas and does not change phase throughout the exchanger.  Chemical #1 leaves Zone 1 and enters Zone 2 at its boiling temperature, Tb1.  T* marks the temperature of Chemical #2 when Chemical #1 begins to condense.  In Zone 2, Chemical #1 condenses to completion while Chemical #2 continues to increase in temperature.  The temperature of Chemical #2 when Chemical #1 is fully condensed is denoted at T**.  Finally, in Zone 3, both chemicals are liquids.  Chemical #1 is simply liberating heat to Chemical #2 as it becomes a subcooled liquid and exits the shell at 100 <sup class='bbc'>Â°</sup>C.<br /><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Heat Transfer Zones" href="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/designex.gif" target="_blank"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/thumb_designex.gif" alt="heat exchanger zones" /></a></td></tr><tr><td>Figure 1: Zones Analysis</td></tr></tbody></table>				<br />Defining zones is one of the most important aspects of heat exchanger design.  It is also important to remember that if your process simulator does not support zoned analysis (such as Chemcad III), you should model each zone with a separate heat exchanger.  Thus, the previous illustration would require 3 heat exchangers in the simulation.  BUT, do <span class='bbc_underline'>not</span> draw 3 exchangers on your PFD (Process Flow Diagram).  This is all happening in one exchanger.<br /><p class="h2header">What are the flowrates and operating pressures involved in my system?</p><br />This information is critical in establishing the mass and energy balance around the exchanger.  Operating pressures are particularly important for gases as their physical properties vary greatly with pressure.<br /><p class="h2header">What are the physical properties of the streams involved?</p><br />If you're using a process simulator, obtaining the physical properties of your streams should be just a click of the mouse away.  However, if performing the calculation by hand, you may have to do some estimating as the streams may not be of pure substances.  Also, you should get the physical properties for each zone separately to ensure accuracy, but in some cases it is acceptable to use an average value.  This would be true of Chemical #2 in the tubes since it is not changing phase or undergoing a truly significant temperature change (over 100 <sup class='bbc'>Â°</sup>C).  Physical properties that you will want to collect for each phase of each stream will include:  heat capacity, viscosity, thermal conductivity, density, and latent heat (for phase changes).  These are in addition to the boiling points of the streams at their respective pressures.<br /><p class="h2header">What are the allowable pressure drops and velocities in the exchanger?</p><br />Pressure drops are very important in exchanger design (especially for gases).  As the pressure drops, so does viscosity and the fluids ability to transfer heat.  Therefore, the pressure drop and velocities must be limited.  The velocity is directly proportional to the heat transfer coefficient which is motivation to keep it high, while erosion and material limits are motivation to keep the velocity low.  Typical liquid velocities are 1-3 m/s (3-10 ft/s).  Typical gas velocities are 15-30 m/s (50-100 ft/s).  Typical pressure drops are 30-60 kPa (5-8 psi) on the tubeside and 20-30 kPa (3-5 psi) on the shellside.<br /><p class="h2header">What is the heat duty of the system?</p><br />This can be answered by a simple energy balance from one of the streams.<br /><p class="h2header">What is the estimated area of the exchanger?</p><br />Unfortunately, this is where the real fun begins in heat exchanger design!  You'll need to find estimates for the heat transfer coefficients for your system.  These can be found in most textbooks dedicated to the subject or in "Perry's Chemical Engineers' Handbook".  Once you've estimated the overall heat transfer coefficient, use the equation Q=Uo x A x LMTD ("LMTD" is short for Log Mean Temperature Difference) to get your preliminary area estimate.  Remember to use the above equation to get an area for <em class='bbc'>each zone</em>, then add them together.<br /><p class="h2header">What geometric configuration is right for my exchanger?</p><br />Now that you have an area estimate, it's time to find a geometry that meets your needs.  Once you've selected a shell diameter, tubesheet layout, baffle and tube spacing, etc., it's time to check your velocity and pressure drop requirements to see if they're being met.  Experienced designers will usually combine these steps and actually obtain a tube size that meets the velocity and pressure drop requirements and then proceed.  Some guidelines may be as follows:  3/4 in. and 1.0 in. diameter tubes are the most popular and smaller sizes should only be used for exchangers needing less than 30 m<sup class='bbc'>2</sup> of area.  If your pressure drop requirements are low, avoid using four or more tube passes as this will drastically increase your pressure drop.  Once you have a geometry selected that meets all of your needs, it's on to the next step.<br /><p class="h2header">Now that I have a geometry in mind, what is the actual overall heat transfer coefficient?</p><br />This is where you'll spend much of your time in designing a heat exchanger.  Although many textbooks show Nu=0.027(N<sub class='bbc'>RE</sub>)<sup class='bbc'>0.8</sup>(N<sub class='bbc'>PR</sub>)<sup class='bbc'>0.33</sup> as the "fundamental equation for turbulent flow heat transfer", what they sometimes fail to tell you is that the exponents can vary widely for different situations.   For example, condensation in the shell has different exponents than condensation in the tubes.  Use this fundamental equation if you must, but you should consult a good resource for accurate equations.  I highly recommend the following:  "Handbook of Chemical Engineering Calculations", 2nd Ed., by Nicholas P. Chopey from McGraw-Hill publishers (ISBN 0070110212).  Also, don't forget to include the transfer coefficient across the tube wall and the fouling coefficient.  These can be very significant!<br /><p class="h2header">What is the actual area of the exchanger using the 'actual' heat transfer coefficient?</p><br />If you recall, you used estimated heat transfer coefficients to get an initial area.  Now it's time to recalculate the area.<br /><br /><p class="h1header">Enter the Calculation Loop</p><br />Now you're on your way, pick a new geometry corresponding to your new ("actual") area, check the velocity and pressure drop, calculate the overall heat transfer coefficient again.  How does it compare with the previously calculated value?  If it is <span class='bbc_underline'>not</span> within 5-10%, recalculate the process over and over (using your new value for Uo) until it does!  Sounds like alot of work.  Add in the fact that some of the individual heat transfer coefficients require iterative solutions and it's not hard to see why people usually use a complex spreadsheet or a program to do this.  You can save some time by using estimates that you've undoubtedly seen, however you must realize that each time you estimate, you're losing accuracy.<br />Remember two main items:<ul class='bbcol decimal'><li>ZONED ANALYSIS</li><li>ACCURACY OF INITIAL OVERALL HEAT TRANSFER COEFFICIENT</li></ul>The zoned analysis is the key to starting the process correctly.  The accuracy of the initial overall heat transfer coefficient will in part determine how many time you will be going through the calculation.  Other factors to consider when designing heat exchangers can include materials of construction, ease of maintenance, cost of the heat exchanger, and overall heat integration in the process.]]></description>
		<pubDate>Mon, 08 Nov 2010 18:50:19 +0000</pubDate>
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		<title>Falling Film Evaporators in the Food Industry</title>
		<link>http://www.cheresources.com/content/articles/heat-transfer/falling-film-evaporators-in-the-food-industry</link>
		<description><![CDATA[<p>That orange juice that you had this morning sure tasted good didn't it?Â  Did you ever wonder how they get it concentrated into that little can?Â  Chances are the manufacturers used a falling film evaporator.Â </p><p> Falling film evaporators are especially popular in the food industry where many substances are heat sensitive.Â  {parse block="google_articles"}A thin film of the product to be concentrated trickles down inside the wall of the heat exchanging tubes. Â  Steam condenses on the outside of the tubes supplying the required energy to the inside of the tubes.Â  As the water from the process stream evaporates (inside the tubes) from the solids dissolved, the product become more and more concentrated.Â  The evaporators are designed such that a given flow of material can be concentrated to needed solids concentration by the time the stream exits the evaporator.Â  The two-phase product stream is usually run through a vapor-liquid separator after exiting the evaporator.Â  This separator allows the vapors to be drawn off the top and the concentrated liquid to exit the bottom (most falling film evaporators are run under vacuum conditions on the process side).</p><p class="h1header">Understanding the Heat Transfer</p><p>The simple heat transfer balance for falling film evaporators is:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/evap_eq_1.gif" alt="evap_eq_1" width="147" height="32" /></td><td class="equationnumber" align="right">Eq. (1)</td></tr></tbody></table><p>where:</p><table class="imagecaption" border="0" align="right"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Typical Falling Film Evaporator Configuration" href="../../../../invision/uploads/images/articles/evap1.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_evap1.gif" alt="falming-film-evaporator" width="229" height="250" /></a></td></tr><tr><td>Figure 1: Typical Falling Film <br />Evaporator Configuration</td></tr></tbody></table><p>Q = heat duty<br />U = overall heat transfer coefficient<br />A = heat transfer area<br />T<sub>S</sub> = temperature of condensing steam<br />T<sub>1</sub> = boiling point of process liquid</p><p>The overall heat transfer coefficient consist of the steam side condensing coefficient (usually about 5700 W/m<sup>2</sup> K), a metal wall with small resistance (depending on steam pressure, wall thickness), scale resistance on the process side, and a liquid film coefficient on the process side which will be extremely dependent on the viscosity of the process liquid over the concentration range.<br />Â Â Â </p><p>The steam side coefficient can be estimated as above or it can be calculated by the following equation for laminar flow:</p><p>Â </p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/evap_eq_2.gif" alt="evap_eq_2" width="324" height="74" /></td><td class="equationnumber" align="right">Eq. (2)</td></tr></tbody></table><p>Â and</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/evap_eq_3.gif" alt="evap_eq_3" width="320" height="67" /></td><td class="equationnumber" align="right">Eq. (3)</td></tr></tbody></table><p>for turbulent flow.Â  For the equations above,</p><p>&rho;<sub>L</sub> = liquid density (kg/m<sup>3</sup>)<br />&rho;<sub>V</sub> = vapor density (kg/m<sup>3</sup>)Â <br />g = 9.8066 m/s<sup>2</sup><br />L = vertical height of tubes (M)<br />&mu;<sub>L</sub> = liquid viscosity (Pa s)<br />&mu;<sub>V</sub> = vapor viscosity (Pa s)<br />k<sub>L</sub> = liquid thermal conductivity (W/m K)<br />&#916;T = T<sub>sat</sub>-T<sub>wall</sub> (K)<br />&#955; = latent heat (J/kg)</p><p>All physical properties should be evaluated at the film temperature, T<sub>f</sub> = (T<sub>sat</sub> - T<sub>wall</sub>)/2 except for the latent heat which is evaluated at the saturation temperature.Â  The resistance due to scale formation cannot be predicted and will probably have to be estimated or compensated for by added a fouling coefficient or by added 5-10% to the calculated heat transfer area (sometimesÂ industry data is available for similar fluids to help estimate this value).Â Â </p><p>For the process fluid, the heat transfer coefficient can be calculated with the following exp<b></b>ression:Â </p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/evap_eq_4.gif" alt="evap_eq_4" width="509" height="67" /></td><td class="equationnumber" align="right">Eq. (4)</td></tr></tbody></table><p>where:</p><p>b = 128 (SI units) or 39 (Imperial units)<br />N<sub>Pr</sub> = Prandtl number = <img style="vertical-align: middle;" src="../../../../invision/uploads/images/articles/evap2.gif" alt="evap2" width="50" height="59" /><br />D = tube diameter<br />N<sub>Re</sub> = Reynolds number = <img style="vertical-align: middle;" src="../../../../invision/uploads/images/articles/evap3.gif" alt="evap3" width="145" height="59" /><br />&rho; = density (subscript "L" for liquids, "V" for vapor)<br />&mu; = viscosity (subscript "L" for liquids, "V" for vapor)</p><p>Calculating pressure drops in falling film evaporators has been investigated since the late 1940's.Â  A universal equation is really not agreed upon.Â  Typically, a constant dependent on the percentage of vapor exiting the evaporator is used in a pressure drop relationship.Â  If your process fluid shares physical properties close to water, you may be able to accurately predict the pressure drop by using graphs and relations found in <em>Perry's Chemical Engineers' Handbook</em>.Â Â </p><p class="h1header">Food Industry</p><p>Evaporating fruit and vegetable juices presents a special challenge for chemical engineers.Â  Juices are heat sensitive and their viscosities increase significantly as they are concentrated.Â  Small solids in the juices tend to cling to the heat transfer surface thus causing spoilage and burning.{parse block="google_articles"}</p><p>Juice evaporations are usually performed in a vacuum to reduce boiling temperatures (due to heat sensitivity).Â  High flow circulation rates help avoid build-ups on the tube walls.</p><p>For some juices (e.g. orange), it is unavoidalbe that the flavor changes as concentration increases.Â  Some of the volatile, flavor-containing components are lost during evaporation.Â  In this case, some of the raw juice is mixed with the concentrate to replace the lost flavors.</p><p>Considering that the components of juices have close boiling points, a standard, single evaporator is seldom sufficient.Â  Either a multi-effect evaporation system must be used (lower capital cost, higher energy costs) or a vapor recompression evaporator (higher capital cost, lower energy costs) is employed.Â  In a multi-effect system, the pressure is incrementally lowered in each stage, thus pushing the boiling point lower gradually.Â  This permits more control over the vapor products to be discarded from the system (mainly water) and the vapors to be condensed back into the system (volatile juice components).</p><p>The vapor recompression evaporator was designed for maximum efficiency. Â  These units generally operate at low optimum temperature differences of 5-10 Â°C. Â  This requires a larger heat transfer area than multi-effect evaporators, thus the larger capital costs.Â  However, the energy savings, generally make vapor recompression the evaporator of choice in the food industry.</p><table class="imagecaption" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/evap4.gif" alt="evap4" width="585" height="339" /></td></tr><tr><td>Figure 2: Typical Vapor Recompression Evaporator Arrangement</td></tr></tbody></table><p></p>
<p class="h1header">References:</p>

Geankoplis, Christie J., Transport Processes and Unit Operations, 3rd Ed., Prentice Hall, 1993, ISBN 0139304398, pages 263-267<br /><br />

Perry, Robert H., et al, Perry's Chemical Engineers' Handbook, 6th Ed., McGraw-Hill, 1984, ISBN 0070494797, pages 10-34 through 10-38<br /><br />

**Special thanks to Rossana Milie from the Department of Chemical Engineering, University of Pisa, Italy for supplying the idea for this article.]]></description>
		<pubDate>Mon, 08 Nov 2010 18:50:19 +0000</pubDate>
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		<title>Basics of Industrial Heat Transfer</title>
		<link>http://www.cheresources.com/content/articles/heat-transfer/basics-of-industrial-heat-transfer</link>
		<description><![CDATA[Heat transfer is one of the most important industrial processes. Throughout any industrial facility, heat must be added, removed, or moved from one process stream to another. Understanding the basics of the heart of this operation is key to any engineers' mastery of the subject.  <br /><br />There are three basic types of heat transfer: conduction, convection, and radiation. The two most common forms encountered in the chemical processing industry are conduction and convection. This course will focus on these key types of heat transfer.<br /><br />In theory, the heat given up by the hot fluid is never exactly equal to the heat gained by the cold fluid due to environmental heat losses. In practice, however, they are generally assumed to be equal to simplify the calculations involved. Any environmental losses are generally minimized with insulation of equipment and piping.  <br /><br />Any overall energy balance starts with the following equations:<br /><table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Eqn1.gif" width="225" height="30"></td><td class="equationnumber" align="right">Eq. (1)</td></tr><br /><tr><td valign="top"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Eqn2.gif" width="218" height="30"></td><td class="equationnumber" align="right">Eq. (2)</td></tr><br /></tbody></table><br /><br />Where:{parse block="google_articles"}<br />Q = heat transferred in thermal unit per time (Btu/h or kW)<br />M = mass flow rate<br />T = temperature<br />Cp = heat capacity or specific heat of fluid<br />Subscript "H" = hot fluid<br />Subscript "C" = cold fluid<br />When examining industrial systems, it is common practice to use a graphical form of these equations know as "T-Q diagrams" to enhance understanding and to make sure that the Second Law of Thermodynamics is not disobeyed. In other words, heat can only move from a higher to a lower temperature fluid. Here is how the generic diagram is constructed:<br /><table class="imagecaption" border="0" align="center"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Image1.gif"></td><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Image2.gif"></td></tr><tr><td>Figure 1: Correct Example of a T-Q Diagram</td><td>Figure 2: Incorrect Example of a T-Q Diagram</td></tr></tbody></table>												<br />It's easy to see how viewing a particular heat transfer problem in this way is extremely valuable.<br />Now that's we've seen how heat moves from a hot fluid to a cold fluid, let's examine the third basic equation that is used to govern the equipment used for transferring heat.<br />The "Heat Exchanger Equation" takes the form:<br /><table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Eqn3.gif"</td><td class="equationnumber" align="right">Eq. (3)</td></tr></tbody></table><br />Where:<br />Q = heat transferred in thermal unit per time (Btu/h)<br />f = temperature correction factor<br />U = overall heat transfer coefficient (Btu/h ft<sup class='bbc'>2</sup> Â°F)<br />A = heat transfer area (ft<sup class='bbc'>2</sup>)<br />LMTD = log mean temperature difference<br />These three (3) equations are the basis for virtually all heat exchanger design.<br /><br /><p class="h1header">Examining the "Heat Exchanger Equation"</p><br />If we take a closer look at the heat exchanger equation, it's worth noting some assumptions that are made in its derivation. First, the overall heat transfer coefficient and the specific heat (also called heat capacity) of the fluids are assumed to remain constant through the heat exchanger.<br />If we look at the change in the heat capacity of water, for example, over a reasonable temperature range, here is what we find:{parse block="google_articles"}<br />Specific heat of water at 100 Â°F and atmospheric pressure = 0.9979 Btu / lb Â°F<br />Specific heat of water at 210 Â°F and atmospheric pressure = 1.0066 Btu / lb Â°F<br />So, we can see that this is a fairly reasonable assumption for water and it remains reasonable for most industrial fluids. The specific heat of a substance is defined as the amount of heat required to raise the temperature of one pound of the substance by a single degree Fahrenheit (other units can apply as well).<br />The overall heat transfer coefficient is a calculated variable based on the physical properties of the fluids involved in the heat transfer (hot and cold) as well as the geometry and type of heat exchanger to be used. We'll examine this closer a little later.<br />The log mean temperature difference or LMTD is used to describe the average temperature difference throughout the exchanger. The difference between the temperatures of the fluids provides the "driving force" for the heat transfer to occur. The larger the temperature difference, the smaller the required heat exchanger and vice versa.<br />You'll notice from our T-Q diagram used to explain the equations:<br /><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Eqn1.gif"><br /><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Eqn2.gif"><br />that it appears that the temperature difference between the fluids remains almost constant throughout the heat exchanger. This is rarely the case. Let's look at a more practical example. Let's assume that a process stream containing water at 200 Â°F is to be cooled to 150 Â°F using cooling tower water available at 85 Â°F. It is common practice in industry to return cooling tower no higher than 120 Â°F. In other words, the cooling tower water flow must be such that its outlet temperature from the heat exchanger is less than 120 Â°F. The reason for this is that cooling tower water often contains treatment chemicals that can plate out onto heat transfer surfaces and cause severe fouling or degradation of the heat transfer rate at elevated temperatures.<br />Here is what the T-Q diagram may look like for our example case:<br /><table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Image3.gif"></td></tr><tr><td>Figure 3: T-Q Diagram for the Example Problem</td></tr></tbody></table>	<br />You can see that the temperature difference between the two streams will vary widely. This is why the log mean temperature difference is used.Here is how the log mean temperature difference works:<br /><table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Image4.gif"></td></tr><tr><td>Figure 4: Graphical Representation of the Log Mean Temperature Difference</td></tr></tbody></table>																<br /><p class='bbc_left'>So, for a heat exchanger as described above, we calculate the LMTD as follows:</p><table class="imagecaption" border="0" align="center"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Image5.gif"></td></tr><tr><td>Figure 5: Exchange Heat Exchanger Duty</td></tr></tbody></table><br /><br /><table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Eqn4.gif"></td><td class="equationnumber" align="right">Eq. (4)</td></tr></tbody></table><br /><br /><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Eqn5.gif"><br /><p class='bbc_left'>There can be special cases where the LMTD equation shown above is not applicable.   Consider the case below:</p><table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Image6.gif"></td></tr><tr><td>Figure 6: Special Case for Calculating LMTD</td></tr></tbody></table>	<br /><br /><p class='bbc_left'>If you tried apply the LMTD equation to this special case, you'd find that the result would be zero.  In this case the LMTD is the same as the temperature difference on each "end" of the heat exchanger, or 100 Â°F.</p><br /><p class="h2header">A Brief Word on Flow Direction</p><br />Notice that up to this point, the two fluids considered in a heat exchanger have been moving in opposite directions to one another.  This is known as counter-current flow.  This is the predominantly preferred flow direction because it results in higher temperature difference driving forces within the heat exchanger, thus minimizing the heat transfer area required.<br /><br />The other flow configuration, where the fluids flow in the same direction, is called co-current flow.  Co-current flow, while it is rarely used, does have the advantage of lowering the heat exchanger wall temperature on the hot side fluid.  This can be useful for temperature sensitive fluids or as a means of minimizing deposits that are temperature sensitive.<br /><br /><p class="h2header">The Temperature Correction Factor, f</p><br />The temperature correction factor, f, is used to correct the log mean temperature difference for heat exchangers than lack truly counter-current flow.  Many different heat transfer technologies lack truly counter-current flow patterns as a result of their inherent mechanical design.  Generally, the value for f should be between 0.75 of 0.97.  There are cases when this value can be taken as one, but only if the flow in the exchanger is purely counter-current.  There are countless charts available to look up the temperature correction factor for a given configuration.<br /><p class="h2header">The Overall Heat Transfer Coefficient</p><br />The overall heat transfer coefficient describes the rate of heat transfer in the heat exchanger.  Generically, it is described by the following equation:<br /><table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Eqn6.gif"></td><td class="equationnumber" align="right">Eq. (5)</td></tr></tbody></table>						<br />Where:<br />U = overall heat transfer coefficient (Btu / h ft<sup class='bbc'>2</sup> Â°F)<br />h<sub class='bbc'>H</sub> = hot side heat transfer coefficient<br />h<sub class='bbc'>C</sub> = cold side heat transfer coefficient<br />Delta x = exchanger wall thickness<br />k = exchanger wall material thermal conductivity<br />R<sub class='bbc'>f</sub> = fouling coefficient (h ft<sup class='bbc'>2</sup> Â°F / Btu)<br />The equation for the overall heat transfer coefficient is often reduced to the following:						<br /><table class="equationtable" border="0" align="center"><tbody><tr><td valign="top"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Eqn7.gif"></td><td class="equationnumber" align="right">Eq. (6)</td></tr></tbody></table>																										<br />Because the term Delta x / k seldom has any significant impact on the overall U-value.<br />The overall heat transfer coefficient can either be calculated, looked up in reference materials for a given duty, estimated from past plant experience, or supplied by a heat exchanger vendor.<br /><br /><br /><p class="h1header">Brief Overview of Heat Exchanger Types</p><br />In the chemical processing industry, there are numerous types of heat exchanger devices.  The types of exchangers can be classified by the duty that they perform, surface compactness, construction features, flow arrangements, and others.  In general, a heat exchanger can fall into one of these processing categories:<br /><span class='bbc_underline'>No Phase Change</span><br /><ul><li>Liquid to Liquid heat transfer</li>{parse block="google_articles"}<br /><li>Liquid to Gas heat transfer</li><br /><li>Gas to Gas heat transfer</li></ul><br /><br /><span class='bbc_underline'>Phase Change</span><br /><ul><li>Condensing a vapor with a liquid or gas service fluid</li><br /><li>Vaporizing a liquid with a liquid, gas, or condensing fluid</li></ul><br /><br /><span class='bbc_underline'>Heat exchangers can also be broken down into the following two types of mechanical geometries:</span><br /><ul><li>Shell and Tube Heat Exchangers</li><br /><li>Compact and Extended Surface Heat Exchangers</li></ul><br /><br />Approximately 70-80% of the heat exchanger market is dominated by the shell and tube type heat exchanger.  It is largely favored due to its long performance history, relative simplicity, and its wide temperature and pressure design ranges.  We will explore this technology in further detail later.<br />The second category mentioned, compact and extended surface heat exchangers, play a smaller role in the chemical processing industry.  Some of the available technologies that fit into this category are the plate and frame heat exchanger, finned tube heat exchangers, spiral heat exchangers, fin-fan heat exchangers, and many others.<br /><br /><p class="h1header">Compact Heat Exchanger Technologies</p><br />The plate exchanger, shown below, consists of corrugated plates assembled into a frame.  The hot fluid flows in one direction in alternating channels while the cold fluid flows in true countercurrent flow in the opposite alternating channels.  The fluids are directed into their proper channels either by a rubber gasket or a weld depending on the type of exchanger chosen.<br /><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Components of a Plate Heat Exchanger" href="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Image7.gif" target="_blank"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/thumb_ht_basics_Image7.gif" alt="plate-heat-exchanger" /></a></td></tr><tr><td>Figure 7: Components of a Plate Heat Exchanger</td></tr></tbody></table><br />	<br />Traditionally, plate and frame exchangers have been used almost exclusively for liquid to liquid heat transfer.  Today, many variations of the plate technology have proven useful in applications where a phase change occurs as well.  This includes condensing duties as well as vaporization duties.  Plate heat exchangers are best known for having overall heat transfer coefficients (U-values) in excess of 3-5 times the U-value in a shell and tube designed for the same service.<br />Plate exchangers can be especially attractive when more expensive materials of construction are required.  The significantly higher U-value results in far less area for a given application, thus a lower purchased and installed cost due to its relatively small size.  The higher U-values are gained by inducing extremely high wall shear on the plate surface.  The best way to think of a plate heat exchanger is that it is essentially a static mixer that happens to transfer heat very well.  The plate exchanger, by virtue of its high wall shear stress also minimizes fouling very well.<br /><br />Typical plate thicknesses range from 0.40 mm to 0.60 mm and passage channel openings can range from 1.5 mm up to 11.0 mm depending on the application and required design pressure (the larger the opening, the lower the design pressure available).  These small passages also restrict the size of solids that can be successfully passed through the exchanger.<br /><br />Perhaps the biggest advantage of the plate and frame heat exchanger, and a situation where it is most often used, is when the heat transfer application calls for the cold side fluid to exit the exchanger at a temperature significantly higher than the hot side fluid exit temperature.  This situation is best explained with another set of T-Q diagrams:<br /><table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Image8.gif"/></td></tr><tr><td>Figure 8: Heat Transfer Duty with No Temperature Cross</td></tr></tbody></table><br /><br />Duty 1 shown above is easily accomplished in a single and tube heat exchanger.<br /><table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Image9.gif"/></td></tr><tr><td>Figure 9: Heat Transfer Duty with a Temperature Cross</td></tr></tbody></table><br /><br />Duty 2 shows a severe "temperature cross" or the cold side fluid exiting higher than the hot side fluid.  This would require several shell and tube exchangers in series due to the lack of purely counter-current flow.  On the other hand, this duty is easily accomplished in a single plate and frame heat exchanger.<br /><table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Image10.gif"/></td></tr><tr><td>Figure 10: Finned Tubes</td></tr></tbody></table><br />	<br />Finned tube heat exchangers are commonly used to transfer heat between a gas and liquid.  The tubes used in these units are equipped with fins that extend outward from the tubes as shown in Figure 10.<br /><br />The fins on the tubes allow for a much larger surface area to be packed into a small volume.  This is especially important when transferring heat to or from a gas as gasses have extremely low heat transfer coefficients (meaning that large amounts of area are required).<br />Fin-fan heat exchangers are designed to use air to cool process fluids.   Think of them as a giant radiator.  The process fluid is passed through the coils and a fan helps pull air over the outside surface to promote cooling.  These units again must provide a very large surface area to make up for the poor heat transfer of the air.<br /><table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Image11.gif"/></td></tr><tr><td>Figure 11: Fin-Fan Heat Exchanger</td></tr></tbody></table><br /><br /><p class="h1header">Shell and Tube Heat Exchanger Technologies</p><br />Shell and tube heat exchangers are known as the work-horse of the chemical process industry when it comes to transferring heat.  These devices are available in a wide range of configurations as defined by the Tubular Exchanger Manufacturers Association (TEMA, <a class='bbc_url' href='http://www.tema.org/'>www.tema.org</a>).  In essence, a shell and tube exchanger is a pressure vessel with many tubes inside of it.  One process fluids flows through the tubes of the exchanger while the other flows outside of the tubes within the shell.  The tube side and shell side fluids are separated by a tube sheet.<br /><br />The shell and tube type is usually indicated as a three (3) letter code from the TEMA specifications as shown in Figure 13.<br />The shell side of a shell and tube exchanger usually contains baffles as shown above to direct the shell side flow around the tubes to enhance heat transfer.  As you can see, shell and tube exchangers can be configured for liquid-liquid, gas-liquid, condensing, or vaporizing heat transfer.<br /><table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Image12.gif"></td></tr><tr><td>Figure 12: Example of a Shell and Tube Heat Exchanger</td></tr></tbody></table>												<br />The tubes can be a different material than shell and the shell can either be cladded or of solid construction.  It's impossible to go over all of the mechanical details of the shell and tube here, but this should provide you with a general overview of the construction.  There are numerous other sources of information freely available on these types of units.<br /><br />The tubes and shell can be designed for a variety of design temperatures and pressures.  The thermal design of shell and tube heat exchangers is often performed by vendors.  The process engineer generally completes a TEMA specification sheet and submits it to vendors for bids.  If you're interested in more details on the thermal design aspects of shell and tube heat exchangers, you can visit Wolverine Engineering's website at:<br /><a class='bbc_url' href='http://www.wlv.com/products/databook/databook.pdf'>http://www.wlv.com/p...ok/databook.pdf</a><br />This online design manual is extremely well done and is a valuable, freely available resource.<br /><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="TEMA Datasheet" href="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/ht_basics_Image13.gif" target="_blank"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/thumbnails/thumb_ht_basics_Image13.gif" alt="TEMA-Datasheet"></a></td></tr><tr><td>Figure 13: TEMA Datasheet</td></tr></tbody></table><br />here are well documented sources of estimated overall heat transfer coefficients and fouling factors that can be specified.  Fouling factors are historic safety factors that allow for the oversizing of a shell and tube in anticipation of eventual surface build-up that will form a resistance to heat transfer.  Remember, the overall heat transfer coefficient of a new heat exchanger will slowly degrade over time until it "levels off" to what is known as the "service U-value".  This is the actual rate of a heat transfer that the unit will achieve on a nominal basis.  The combination of a well selected U-value and a fouling factor should ensure a good shell and tube design.   Typical U-values for various services and fouling factors can be found on the internet or in various text references.<br /><br />Understanding the basics of industrial heat transfer will help you better understand opportunities for cost savings in your plant.  With energy prices showing no sign of declining, a good basis in heat transfer will help you calculate just how much you can save by installing a new heat exchanger in your plant.  With the use a T-Q diagram and a basic understanding of the equipment available to you, making the right choice in heat transfer equipment can yield results for years to come.]]></description>
		<pubDate>Mon, 08 Nov 2010 18:50:19 +0000</pubDate>
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		<title>Heat Exchanger Effectiveness</title>
		<link>http://www.cheresources.com/content/articles/heat-transfer/heat-exchanger-effectiveness</link>
		<description><![CDATA[<p>Calculating heat exchanger effectiveness allows engineers to predict how a given heat exchanger will perform a new job. Essentially, it helps engineers predict the stream outlet temperatures without a trial-and-error solution that would otherwise be necessary. Heat exchanger effectiveness is defined as the ratio of the actual amount of heat transferred to the maximum possible amount of heat that could be transferred with an infinite area.</p> <p>Two common methods are used to calculate the effectiveness, equations and graphical. The equations are shown below:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/ht_effectiveness_eq_1.gif" alt="ht_effectiveness_eq_1" width="534" height="92" /></td><td class="equationnumber" align="right">Eq. (1)</td></tr></tbody></table><br /><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/ht_effectiveness_eq_2.gif" alt="ht_effectiveness_eq_2" width="446" height="99" /></td><td class="equationnumber" align="right">Eq. (2)</td></tr></tbody></table><p><br />where:{parse block="google_articles"}Â <br />U = Overall heat transfer coefficient<br />A = Heat transfer area<br />C<sub>min</sub> = Lower of the two fluid's heat capacities<br />C<sub>max</sub> = Higher of the two fluid's heat capacities</p><p align="left">Oten times, another variable is defined called the NTU (number of transfer units):<br />NTU = UA/Cmin</p><p align="left">When NTU is placed into the effectiveness equations and they are plotted, you can construct the plots shown below which are more often used than the equations:</p><table class="imagecaption" border="0" align="center"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Heat Exchanger Effectiveness for Countercurrent Flow" href="../../../../invision/uploads/images/articles/ht_effectiveness_1.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_ht_effectiveness_1.gif" alt="ht_effectiveness_1" width="250" height="171" /></a></td><td><a class='resized_img' rel='lightbox[2]' title="Heat Exchanger Effectiveness for Cocurrent Flow" href="../../../../invision/uploads/images/articles/ht_effectiveness_2.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_ht_effectiveness_2.gif" alt="ht_effectiveness_2" width="250" height="171" /></a></td></tr><tr><td>Figure 1: Heat Exchanger Effectiveness <br />for Countercurrent Flow</td><td>Figure 2: Heat Exchanger Effectiveness <br />for Cocurrent Flow</td></tr></tbody></table>Then, by calculating the Cmin/Cmax and the NTU, the effectiveness can be read from these charts. Once the effectiveness has been found, the heat load is calculated by:<p align="left">Q = Effectiveness x Cmin x (Hot Temperature in - Cold Temperature in)<br /><br />and the outlet temperatures can be calculated by:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/ht_effectiveness_eq_3.gif" alt="ht_effectiveness_eq_3" width="262" height="60" /></td><td class="equationnumber" align="right">Eq. (3)</td></tr></tbody></table><br /><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/ht_effectiveness_eq_4.gif" alt="ht_effectiveness_eq_4" width="280" height="57" /></td><td class="equationnumber" align="right">Eq. (4)</td></tr></tbody></table>]]></description>
		<pubDate>Mon, 08 Nov 2010 18:50:19 +0000</pubDate>
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		<title>Making Decisions with Insulation</title>
		<link>http://www.cheresources.com/content/articles/heat-transfer/making-decisions-with-insulation</link>
		<description><![CDATA[<p><span style="font-size: small;">Many people overlook the importance of insulation in the chemical industry. Some estimates have predicted that insulation in U.S. industry alone saves approximately 200 million barrels of oil every year. </span></p><p><br />
While placing insulation onto a pipe is fairly easy, resolving issues such as what type of insulation to use and how much is not so easy. Insulation is available in nearly any material imaginable. The most important characteristics of any insulation material include a low thermal conductivity, low tendency toward absorbing water, and of course the material should be inexpensive. In the chemical industry, {parse block="google_articles"}the most common insulators are various types of calcium silicate or fiberglass. Calcium silicate is generally more appropriate for temperatures above 225 <sup>Â°</sup>C (437 <sup>Â°</sup>F), while fiberglass is generally used at temperatures below 225 <sup>Â°</sup>C.</p><table class="imagecaption" style="text-align: center;" border="0"><tbody><tr><td class="imagecaption"><a class='resized_img' rel='lightbox[2]' title="Thermal Conductivity of Calcium Silicate Insulation" href="../../../../invision/uploads/images/articles/insthcond1.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_insthcond1.gif" alt="insthcond1" width="200" height="136" /></a></td><td> </td><td class="imagecaption"><a class='resized_img' rel='lightbox[2]' title="Thermal Conductivity of Fiberglass Insulation" href="../../../../invision/uploads/images/articles/insthcond2.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_insthcond2.gif" alt="insthcond2" width="200" height="136" /></a></td></tr><tr><td>Figure 1: Thermal Conductivity of<br />
Calcium Silicate Insulation</td><td> </td><td>Figure 2: Thermal Conductivity of<br />
Fiberglass Insulation</td></tr></tbody></table><p class="h1header">A Brief Look at Theory</p><p><span style="font-size: small;"><img style="margin: 3px; float: left;" src="../../../../invision/uploads/images/articles/ins1.gif" alt="ins1" width="235" height="171" />The most basic model for insulation on a pipe is shown below. R1 and R2 show the inside and outside radius of the pipe respectively. R3 shows the radius of the insulation. Typically when dealing with insulations, engineers must be concerned with linear heat loss or heat loss per unit length.</span></p><p><span style="font-size: small;">Generally, the heat transfer coefficient of ambient air is 40 W/m<sup>2</sup> K. This coefficient can of course increase with wind velocity if the pipe is outside. A good estimate for an outdoor air coefficient in warm climates with wind speeds under 15 mph is around 50 W/m<sup>2</sup> K.</span></p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><span style="font-size: small;"><img src="../../../../invision/uploads/images/articles/inseq1.gif" alt="inseq1" width="328" height="58" /></span></td><td class="equationnumber" style="text-align: right;">Eq. (1)</td></tr></tbody></table><p><br />
The total heat loss per unit length is calculated by:</p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><img style="float: left;" src="../../../../invision/uploads/images/articles/inseq2.gif" alt="inseq2" width="179" height="62" /></td><td class="equationnumber" style="text-align: right;">Eq. (2)</td></tr></tbody></table><br />
<br />
<table class="imagecaption" style="text-align: left;" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Heat Loss vs. Insulation Thickness" href="../../../../invision/uploads/images/articles/ins2.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_ins2.gif" alt="ins2" width="200" height="136" /></a></td></tr><tr><td>Figure 3: Heat Loss vs. Insulation<br />
Thickness</td></tr></tbody></table><p>Since heat loss through insulation is a conductive heat transfer, there are instances when adding insulation actually <span style="text-decoration: underline;">increases</span> heat loss. The thickness at which insulation begins to <span style="text-decoration: underline;">decrease</span> heat loss is described as the critical thickness. Since the critical thickness is almost always a few millimeters, it is seldom (if ever) an issue for piping. Critical thickness is a concern however in insulating wires. Figure 3 shows the heat loss vs. insulation thickness for a typical insulation. It's easy to see why wire insulation is kept to a minimum as adding insulation would increase the heat transfer.</p><p class="h2header">Thinking About Insulation from All Sides</p><p>Three major factors play an important role in determining insulation type and thickness. Here, we'll focus on resolving the thickness issue since many manufacturing facilities have a "standard" type of insulation that they use. The three key factors to examine are:</p><ol><li>Economics</li><li>Safety</li><li>Process Conditions</li></ol><p>Each situation must be studied to determine how to meet each one of these criteria. First, we'll examine each aspect individually, then we'll see how to consider all three for an example.</p><p class="h1header">Economics</p>{parse block="google_articles"}Economic thickness of insulation is a well documented calculation procedure. The calculations typically take in the entire scope of the installation including plant depreciation to wind speed. Data charts for calculating the economic thickness of insulation are widely available. Below are links to economic thickness tables that have been adapted from Perry's Chemical Engineers' Handbook:<p style="text-align: left;"><span style="font-size: small;"><a class='resized_img' rel='lightbox[2]' href="../../../../invision/uploads/images/articles/indamer.gif" alt="indamer" width="561" height="1183">Table 1: Economic Indoor Insulation Thickness (American Units)</a></span></p><p style="text-align: left;"><a class='resized_img' rel='lightbox[2]' href="../../../../invision/uploads/images/articles/indmetric.gif" alt="indmetric" width="538" height="1183">Table 2: Economic Indoor Insulation Thickness (Metric Units)</a></p><p style="text-align: left;"><a class='resized_img' rel='lightbox[2]' href="../../../../invision/uploads/images/articles/outdamer.gif" alt="outdamer" width="565" height="1433">Table 3: Economic Outdoor Insulation Thickness (American Units)</a></p><p style="text-align: left;"><a class='resized_img' rel='lightbox[2]' href="../../../../invision/uploads/images/articles/outdmetric.gif" alt="outdmetric" width="565" height="1433">Table 4: Economic Outdoor Insulation Thickness (Metric Units)</a></p><p class="h2header" style="text-align: left;">Example of Economic Thickness Calculation</p><p style="text-align: left;">Using the tables above, assuming a 6.0 in pipe at 500 <sup>Â°</sup>F in an indoor setting with an energy cost of $5.00/million Btu, what is the economic thickness?<br />
<span style="text-decoration: underline;">Answer</span>: Finding the corresponding block to 6.0 in pipe and $5.00/million Btu energy costs, we see temperatures of 250 <sup>Â°</sup>F, 600 <sup>Â°</sup>F, 650 <sup>Â°</sup>F, and 850 <sup>Â°</sup>F. Since our temperature does not meet 600 <sup>Â°</sup>F, we use the thickness before it. In this case, 250 <sup>Â°</sup>F or 1 1/2 inches of insulation. At 600 <sup>Â°</sup>F, we would increase to 2.0 inches of insulation.<br />
Economic thickness charts from other sources will work in much the same way as this example.</p><p class="h1header" style="text-align: left;">Safety</p><p style="text-align: left;">{parse block="google_articles"}Pipes that are readily accessible by workers are subject to safety constraints. The recommended safe "touch" temperature range is from 130 <sup>Â°</sup>F to 150 <sup>Â°</sup>F (54.4 <sup>Â°</sup>C to 65.5 <sup>Â°</sup>C). Insulation calculations should aim to keep the outside temperature of the insulation around 140 <sup>Â°</sup>F (60 <sup>Â°</sup>C). An additional tool employed to help meet this goal is aluminum covering wrapped around the outside of the insulation. Aluminum's thermal conductivity of 209 W/m K does not offer much resistance to heat transfer, but it does act as another resistance while also holding the insulation in place. Typical thickness of aluminum used for this purpose ranges from 0.2 mm to 0.4 mm. The addition of aluminum adds another resistance term to <a class='resized_img' rel='lightbox[2]' href="../../../../invision/uploads/images/articles/inseq1.gif">Equation 1</a> when calculating the total heat loss:</p><table class="equationtable" style="text-align: center;" border="0"><tbody><tr><td><img style="float: left;" src="../../../../invision/uploads/images/articles/inseq3.gif" alt="inseq3" width="478" height="149" /></td><td class="equationnumber" style="text-align: right;">Eq. (3)</td></tr></tbody></table><p style="text-align: left;">However, when considering safety, engineers need a quick way to calculate the surface temperature that will come into contact with the workers. This can be done with equations or the use of charts. We start by looking at another diagram:</p><p style="text-align: left;"><img style="text-align: center;" src="../../../../invision/uploads/images/articles/ins3.gif" alt="ins3" width="542" height="263" /></p><p style="text-align: justify;">At steady state, the heat transfer rate will be the same for each layer:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/inseq4.gif" alt="inseq4" width="510" height="263" /></td><td class="equationnumber" align="right">Eq. (4)</td></tr></tbody></table><p align="left">Rearranging Equation 4 by solving the three exp<b></b>ressions for the temperature difference yields:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/inseq5.gif" alt="inseq5" width="347" height="65" /></td><td class="equationnumber" align="right">Eq. (5)</td></tr></tbody></table><p align="left">Each term in the denominator of Equation 5 is referred to as the "resistance" of each layer. We will define this as Rs and rewrite the equation as:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/inseq6.gif" alt="inseq6" width="173" height="43" /></td><td class="equationnumber" align="right">Eq. (6)</td></tr></tbody></table><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Equivalent Thickness Chart for Calcium Silicate Insulation" href="../../../../invision/uploads/images/articles/insfig4.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_insfig4.gif" alt="insfig4" width="200" height="136" /></a></td></tr><tr><td>Figure 4: Equivalent Thickness<br />
Chart for Calcium Silicate Insulation</td></tr></tbody></table><p align="left">Since the heat loss is constant for each layer, use Equation 4 to calculate Q from the bare pipe, then solve Equation 6 for T4 (surface temperature). Use the economic thickness of your insulation as a basis for your calculation, after all, if the most affordable layer of insulation is safe, that's the one you'd want to use. If the economic thickness results in too high a surface temperature, repeat the calculation by increasing the insulation thickness by 1/2 inch each time until a safe touch temperature is reached.</p><p align="left"><br />
As you can see, using heat balance equations is certainly a valid means of estimating surface temperatures, but it may not always be the fastest. Charts are available that utilize a characteristic called "equivalent thickness" to simplify the heat balance equations. This correlation also uses the surface resistance of the outer covering of the pipe. Figure 4 shows the equivalent thickness chart for calcium silicate insulation. Table 5 shows surface resistances for three popular covering materials for insulation.</p><table class="datatable" border="0" align="center"><caption>Table 5: Values for Surface Resistances<br />
h ft<sup>2</sup> Â°F/Btu (m<sup>2</sup> Â°C/W)</caption><tbody><tr><td><img src="../../../../invision/uploads/images/articles/instable5.gif" alt="instable5" width="438" height="195" /></td></tr></tbody></table><p align="left">With the help of Figure 4 and Table 5 (or similar data for another material you may be dealing with), the relation:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/inseq7.gif" alt="inseq7" width="280" height="40" /></td><td class="equationnumber" align="right">Eq. (7)</td></tr></tbody></table><p align="left">can be used to easily determine how much insulation will be needed to achieve a specific surface temperature. Let's look at an example to illustrate the various uses of this equation.</p><p class="h2header" align="left">Example of Outer Surface Temperature Determination</p><p align="left">Your supervisor asks you to install insulation on a new pipe in the plant. Recently, two workers suffered severe burns while incidentally touching the new piping so safety is of primary concern. He instructs you to be sure that this incident does not repeat itself. The pipe contains a heat transfer fluid at 850 <sup>Â°</sup>F (454 <sup>Â°</sup>C). The ambient temperature is usually near 85 <sup>Â°</sup>F (29.4 <sup>Â°</sup>C). After checking the supplies that you have available, you notice that you have calcium silicate insulation and aluminum available for covering. You would like to insulate the 16 inch pipe for a surface temperature of 130 <sup>Â°</sup>F.</p><p align="left"><img src="../../../../invision/uploads/images/articles/inseq7.gif" alt="inseq7" width="280" height="40" /></p><p align="left">Tsurface - Tambient = 130 <sup>Â°</sup>F - 85 <sup>Â°</sup>F = 45 <sup>Â°</sup>F, from Table 5 we estimate a Rs value for aluminum at 0.865 h ft<sup>2</sup> <sup>Â°</sup>F/Btu.<br />
Taverage = (850 <sup>Â°</sup>F + 85 <sup>Â°</sup>F)/2 = 467.5 <sup>Â°</sup>F (242 <sup>Â°</sup>C), from <span style="font-size: small;"><a class='resized_img' rel='lightbox[2]' href="../../../../invision/uploads/images/articles/insthcond1.gif">Figure 1</a> we estimate a thermal conductivity of 0.0365 Btu/h ft <sup>Â°</sup>F (0.06317 W/m <sup>Â°</sup>C) for calcium silicate insulation.</span></p><p align="left"><span style="font-size: small;"><img src="../../../../invision/uploads/images/articles/inseq7a.gif" alt="inseq7a" width="491" height="42" /></span></p>Equivalent Thickness = 6.1 in (155 mm)<p align="left">From <a class='resized_img' rel='lightbox[2]' href="../../../../invision/uploads/images/articles/insfig4.gif">Figure 4</a> above, an equivalent thickness of 6 in corresponds to an actual thickness of <span style="text-decoration: underline;">nearly 5.0 in of insulation</span>.</p><p class="h1header" align="left">Process Conditions</p><p align="left">The temperature of a fluid inside an insulated pipe is an important process variable that must be considered in many situations. Consider the length of pipe connecting two pieces of process equipment shown below:</p><p align="left"><img src="../../../../invision/uploads/images/articles/ins4.gif" alt="ins4" width="506" height="167" /></p><p align="left">In order to predict T2 for a given insulation thickness, we first make the following assumptions:</p><ol><li><div>Constant fluid heat capacity over the fluid temperature range</div></li><li><div>Constant ambient temperature</div></li><li><div>Constant thermal conductivity for fluid, pipe, and insulation</div></li><li><div>Constant overall heat transfer coefficient</div></li><li><div>Turbulent flow inside pipe</div></li><li><div>15 mph wind for outdoor calculations</div></li></ol><p align="left"><img src="../../../../invision/uploads/images/articles/inseq8b.gif" alt="inseq8b" width="144" height="22" /></p><p align="left">where</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/inseq8a.gif" alt="inseq8a" width="319" height="342" /></td><td class="equationnumber" align="right">Eq. (8)</td></tr></tbody></table><p>and another heat balance equation yields:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/inseq9.gif" alt="inseq9" width="171" height="65" /></td><td class="equationnumber" align="right">Eq. (9)</td></tr></tbody></table><p>Setting Equation 8 equal to Equation 9 and solving for T2 yields:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/inseq10.gif" alt="inseq10" width="253" height="47" /></td><td class="equationnumber" align="right">Eq. (10)</td></tr></tbody></table><p><span class="download">Equation 10 provides another useful tool for analyzing insulation and its impact on a process. Equation 10 has been incorporated into the <a href="../../../../invision/files/file/13-insulated-and-bare-pipe-temperature-prediction/">"Insulated Pipe Temperature Prediction Spreadsheet"</a> available in the Download Section.</span></p><p>One example may be the importance of designing insulation thickness to prevent condensation on cold lines. Usually, when we hear the word "insulation" we instantly think of hot lines. However, there are times when insulation is used to prevent heat from <span style="text-decoration: underline;">entering</span> a line. In this situation, the dew point temperature of the ambient air must be considered. Table 6 and Table 7 show dewpoint temperatures as a function of relative humidity and dry bulb temperatures.</p><table class="imagecaption" border="0" align="center"><tbody><tr><td>Table 6: Dew Point<br />
Temperatures of Air<br />
(Fahrenheit)</td><td> </td><td>Table 7: Dew Point<br />
Temperatures of Air<br />
(Celsius)</td></tr><tr><td><a class='resized_img' rel='lightbox[2]' title="Dew Point Temperatures of Air (Â°F)" href="../../../../invision/uploads/images/articles/instable6.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_instable6.gif" alt="instable6" width="200" height="142" /></a></td><td> </td><td><a class='resized_img' rel='lightbox[2]' title="Dew Point Temperatures of Air (Â°C)" href="../../../../invision/uploads/images/articles/instable7.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_instable7.gif" alt="instable7" width="200" height="139" /></a></td></tr></tbody></table><p align="left"><span style="font-size: small;">It is crucial that sufficient insulation is added so that the outer temperature of the insulation remains <span style="text-decoration: underline;">above</span> the dewpoint temperature. At the dewpoint temperature, moisture in the air will condense onto the insulation and essentially ruin it.</span></p><p align="left"><span class="h2header">Special Case</span></p><p align="left"><span style="font-size: small;">For the case of a bare pipe running outside, the chart below can be used to adjust the external heat transfer coefficient from 50 W/m2 K (8.8 Btu/h ft2 Â°F) to account for temperature difference and wind velocity:</span></p><table class="imagecaption" border="0" align="center"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Bare pipe external heat transfer coefficient adjustment" href="../../../../invision/uploads/images/articles/ins6.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_ins6.gif" alt="ins6" width="200" height="110" /></a></td></tr><tr><td>Figure 6: Bare Pipe External Heat<br />
Transfer Coefficient Adjustment</td></tr></tbody></table><p class="h1header"> <hr class="system-pagebreak" title="Practical Example and Summary" />Practical Example</p><p><img src="../../../../invision/uploads/images/articles/ins5.gif" alt="ins5" width="490" height="305" /></p><p>{parse block="google_articles"}In the figure above, a typical reactor feed preheater (interchanger) is shown. The heat exchanger resides on the first level of the structure while the reactor is on the second level. During construction, stream 2 was not insulated because it runs from the exchanger directly to the ceiling away from workers so it posed no safety risk. The reaction is endothermic, so heat is supplied by a Dowtherm jacket surrounding the vessel. The equivalent length of the pipe containing stream 2 is 100 meters. A recent rise is fuel oil costs (which is used to heat the Dowtherm) has prompted the company to search for ways to conserve energy. With the data provided below, you recognize an opportunity for energy savings. Any increase in the reactor feed temperature will reduce the reactor duty and save money. What is the current reactor entrance temperature compared with the entrance temperature after applying the economic insulation thickness to the pipe?</p><p align="left"><em>Data:<br />
</em>Calcium silicate insulation<br />
Temperature of stream 2 exiting the heat exchanger is 400 <sup>Â°</sup>C (752 <sup>Â°</sup>F)<br />
Ambient temperature is 23.8 <sup>Â°</sup>C (75 <sup>Â°</sup>F)<br />
Mass flow = 350,000 kg/h (771,470 lbs/h)<br />
R<sub>inside pipe</sub> = R1 = 101.6 mm (4.0 in)<br />
R<sub>outside pipe</sub> = R2 = 108.0 mm (4.25 in)<br />
Thermal conductivity of pipe = k<sub>pipe</sub> = 30 W/m K (56.2 Btu/h ft <sup>Â°</sup>F)<br />
Ambient air heat transfer coefficient = ho = 50 W/m<sup>2</sup> K (8.8 Btu/h ft<sup>2</sup> <sup>Â°</sup>F)<br />
Fluid heat capacity = Cp<sub>fluid</sub> = 2.57 kJ/kg K (2.0 Btu/lb <sup>Â°</sup>F)<br />
Fluid thermal conductivity = k<sub>fluid</sub> = 0.60 W/m K (1.12 Btu/h ft <sup>Â°</sup>F)<br />
Fluid viscosity = u<sub>fluid</sub> = 5.2 cP<br />
Energy costs = $4.74/million kJ ($5.00/million Btu)<br />
Equivalent length of pipe = 100 meters (328 feet)</p><p align="left"><em>Calculations:<br /><br />
First, we'll assume little or no wind affects the pipe heat loss and we'll estimate the heat loss from the bare pipe:<br />
<img src="../../../../invision/uploads/images/articles/ins8.gif" alt="ins8" /><br />
Now, we'll estimate the radiant heat losses:<br />
<img src="../../../../invision/uploads/images/articles/ins9.gif" alt="ins9" /><br />
where:
&#963; = Stefan-Boltzmann constant = 5.678 x 10<sup>-8</sup> W/m<sup>2</sup> K<br />
A = circumference of pipe to the outer diameter, m<br />
&#949; = emissivity of pipe material, taken at 673 K, assume 0.75<br />
T = absolute temperatures, K<br /><br />
Now, we'll estimate the losses due to convection:<br />
<img src="../../../../invision/uploads/images/articles/ins10.gif" alt="ins10" /><br />
and we'll add these together to arrive at the total heat loss for the bare pipe:<br />
<img src="../../../../invision/uploads/images/articles/ins11.gif" alt="ins11" /><br />
We can now calculate the temperature entering the reactor from the heat exchanger for the bare pipe scenario:<br />
<img src="../../../../invision/uploads/images/articles/ins12.gif" alt="ins12" /><br /><br />
Now, we perform a similar analysis for the insulated pipe:<br />
<img src="../../../../invision/uploads/images/articles/ins7.gif" alt="ins7" /><br />
<p align="left">Temperature difference with insulation is 3.56 <sup>0</sup>C. While this doesn't sound too dramatic, consider the energy savings over one year with the insulation:</p><p align="left">Q = mass flow x Cpfluid x temperature difference<br />
Q = (350,000 kg/h)(2.57 kJ/kg K)(3.56 K) = 3,202,220 kJ/h<br />
3,202,220 kJ/h x 8760 hours/year = 28,051 million kJ/year<br />
28,051 million kJ/year x $4.74/million kJ = <span style="text-decoration: underline;">$132,961 per year</span></p><p align="left"><span style="color: #0000ff; font-size: small;">By insulating the pipe, energy costs have decreased by nearly $133,000 per year</span></p><p class="h1header">Summary</p><p align="left"><span style="font-size: small;">There are many factors to consider when thinking about insulation.  Insulation save money for certain, but it can also be effective as a safety and process control device.  Insulation can be used to regulate process temperatures, protect workers from serious injury, and save thousands of dollars in energy costs.  One should never overlook it's usefulness.  It's also bad practice to consider only one of the important factors discussed in this article.  The key is to consider all factors that will be affected by installing insulation on a pipe or any other piece of equipment.  </span></p>]]></description>
		<pubDate>Mon, 08 Nov 2010 18:50:19 +0000</pubDate>
		<guid isPermaLink="false">2b38c2df6a49b97f706ec9148ce48d86</guid>
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	<item>
		<title>Jacketed Vessel Design</title>
		<link>http://www.cheresources.com/content/articles/heat-transfer/jacketed-vessel-design</link>
		<description><![CDATA[<p>Jacketing a process vessel provided excellent heat transfer in terms of efficiency, control and product quality. All liquids can be used as well as steam and other high temperature vapor circulation. The temperature and velocity of the heat transfer media can be accurately controlled.</p><p> </p><p>The various types of jackets used in process industry are :{parse block="google_articles"}</p><ol><li>Spirally baffled jackets/ conventional jackets</li><li>Dimple jackets</li><li>Partial-pipe coil /limpet jacket</li><li>Panel type/ plate type coil jackets</li></ol><p>Commonly used heat transfer medias include water, steam (various pressures), hot oil (such as Therminol&trade;), and Dowtherm&trade; vapor.</p><p><span class="h1header">Matching Jacket Types to Heat Transfer Media</span></p><p align="left"><strong>Water</strong>: Depending on the process temperature, stress corrosion cracking can sometimes be a concern due to the chlorides usually found in water. In some cases, dimple jackets may requires the use of high-nickel alloys which are very expensive. The half-pipe coil can use 1/4'' thick carbon steel for the jacketing but their economy versus conventional jackets must to be considered. With services involving large volumes of water (used to maintain a high temperature difference) the conventional jacket usually offers the best solution.</p><p align="left"><strong>Steam</strong>:<strong> </strong>Both dimple and half coil jackets are well suited use with high pressure steam. The dimple jackets are generally limited to 300 psig design pressure while half-coil jackets can be used up to a design pressure of 750 psig. For half-pipe coil jacket, the higher heat flux rate may require multiple sections of jackets to avoid having condensate covering too much of the heat transfer area. For low pressure steam services convention jackets are a much more economical choice.</p><p align="left"><strong>Hot Oils and Heat Transfer Fluids</strong>: Although pressures are usually low when using oils or heat transfer fluids, the temperatures are usually high. The result is low allowable stress values for the inner-vessel material. Therefore both half-pipe jackets and dimple jackets can provide good solutions. Conventional jackets require a greater shell thickness along with expansion joints to eliminate stresses induced by the difference in thermal expansion when the jacket is not manufacturered from the same material as that of shell.</p><p align="left"><strong>Dowtherm&trade; Vapors</strong>:The ability to vary the distance between the outer and innver vessel walls makes conventional jackets ideally suited to handle Dowtherm&trade; vapors. Also since Dowtherm vapor has a low enthalpy (1/10 that of steam) a large jacket space is needed for given heat flux. The jacket must be designed in accordance with ASME Code specifications. The maximum allowable space is limited by section UA-104 Paragraph c and s.</p><p class="h1header" align="left">Conventional Jackets</p><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Conventional Jacket" href="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/jacketed_vessel_design1.gif" target="_blank"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/thumb_jacketed_vessel_design1.gif" alt="jacketed_vessel_design1" width="97" height="150" /></a></td></tr><tr><td>Figure 1: Conventional<br />
Jacket</td></tr></tbody></table><p align="left">"Conventional jackets" can be divided into two (2) main categories: baffled and non-baffled. Baffled jackets often utilize what is known as a spirally wound baffle. The baffle consist of a metal strip wound around the inner vessel wall from the jacket utility inlet to the utility outlet. The baffle directs the flow in a spiral path with a fluid velocity of 1-4 ft/s. The fabrication methods does allow for small internal leakage or bypass around the baffle. Generally, bypass flows can exceed 1/3 to 1/2 of the total circulating flow.{parse block="google_articles"}</p><p align="left">Conventional baffled jackets are usually applied with small vessels using high temperatures where the internal pressure in more than twice the jacket pressure.</p><p>Spirally baffled jackets are limited to a pressure of 100 psig because vessel wall thickness becomes large and the heat transfer is greatly reduced. In the case of an alloy reactor, a very costly vessel can result. For high temperature applications, the thermal expansion differential must be considered when choosing materials for the vessel and jacket. Design and construction details are given in Division 1 of the ASME Code, Section VIII, Appendix IX, "Jacketed Vessel".</p><p class="h2header">Heat Transfer Coefficients: Conventional Jackets without Baffles</p><table class="equationtable" border="0" align="center"><tbody><tr><td valign="top">(h<sub>j</sub> D<sub>e</sub> / k) = 1.02 (N<sub>Re</sub>) <sup>0.45</sup> (N<sub>Pr</sub>) <sup>0.33</sup> (D<sub>e</sub>/ L) <sup>0.4</sup> (D<sub>jo</sub>/ D<sub>ji</sub>) <sup>0.8</sup> (N<sub>Gr</sub>) <sup>0.05</sup></td><td class="equationnumber" align="right">Eq. (1)</td></tr></tbody></table><table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/jacketed_vessel_design2.gif" alt="jacketed_vessel_design2" width="198" height="194" /></td></tr><tr><td>Figure 2: Schematic of Conventional<br />
Jacket</td></tr></tbody></table><p>Where:<br />
h<sub>j</sub> = Local heat transfer coefficient on the jacket side<br />
D<sub>e</sub> = Equivalent hydraulic diameter<br />
N<sub>Re</sub> = Reynolds Number<br />
N<sub>Pr</sub> = Prandtl Number<br />
L = Length of jacket passage<br />
D<sub>jo</sub> = Outer diameter of jacket<br />
D<sub>ji</sub> = Inner diameter of jacket<br />
N<sub>Gr</sub> = Graetz number</p>The Reynolds Number is defined as:<p>N<sub>Re</sub> = DV&rho;/&mu;<br />
Where D is the equivalent diameter, V is the fluid velocity, &rho; is the fluid density, &mu; and is the fluid viscosity.</p><p>The Prandtl Number is defined as:</p><p>N<sub>Pr</sub> = C<sub>p</sub> &mu; / k<br />
Where Cp is the specific heat, &mu; is the viscosity, and k is the thermal conducitivity of the fluid.</p><p>The Graetz Number is defined as:</p><p>N<sub>Gr</sub> = (m C<sub>p</sub>) / (k L)<br />
Where m is the mass flow rate, C<sub>p</sub> is the specific heat, k is the thermal conducitivity, and L is the jacket passage length.</p><p>The equivalent diameter is defined as follows:</p><p>D<sub>e</sub> = D<sub>jo</sub>-D<sub>ji</sub> for laminar flow<br />
D<sub>e</sub> = ((D<sub>jo</sub>)2 - (D<sub>ji</sub>)2)/D<sub>ji</sub> for turbulent flow</p><p><span class="h2header">Conventional Jackets with Baffles</span></p><p>For conventional jackets with baffles, the following can be used to calculate the heat transfer coefficient:</p><table class="equationtable" border="0" align="center"><tbody><tr><td valign="top">h<sub>j</sub> D<sub>e</sub>/k= 0.027(N<sub>Re</sub>)<sup>0.8</sup> (N<sub>Pr</sub>)<sup>0.33</sup> (&micro;/&micro;<sub>w</sub>)<sup>0.14</sup> (1+3.5 (D<sub>e</sub>/D<sub>c</sub>) ) ( For N<sub>Re</sub> > 10,000)</td><td class="equationnumber" align="right">Eq. (2)</td></tr></tbody></table><table class="equationtable" border="0" align="center"><tbody><tr><td valign="top">h<sub>j</sub> D<sub>e</sub>/k = 1.86 [ (N<sub>Re</sub>) (N<sub>Pr</sub>) (D<sub>c</sub>/D<sub>e</sub>) ] <sup>0.33</sup> (&micro;/&micro;<sub>w</sub>)<sup>0.14</sup> ( For N<sub>Re</sub> < 2100 )</td><td class="equationnumber" align="right">Eq. (3)</td></tr></tbody></table><table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/jacketed_vessel_design3.gif" alt="jacketed_vessel_design3" width="244" height="372" /></td></tr><tr><td><p>Figure 3: Schematic of Conventional Jacket<br />
with Baffle</p></td></tr></tbody></table><p>Two new variables are introduced. Dc is defined as the centerline diameter of the jacket passage. It is calculated as D<sub>ji</sub> + ((D<sub>jo</sub>-D<sub>ji</sub>)/2). The viscosity at the jacket wall is now defined as &micro;<sub>w</sub>. When calculating the heat transfer cofficients, an effective mass flow rate should be taken as 0.60 x feed mass flow rate to account for the substantial bypassing that will be expected. D<sub>e</sub> is defined at 4 x jacket spacing. The flow cross sectional area is defined as the baffle pitch x jacket spacing.</p><table class="equationtable" style="width: 54%;" border="0" align="right"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/jacketed_vessel_design14.gif" alt="jacketed_vessel_design14" width="310" height="210" /></td><td class="equationnumber" align="right"><p>Eq. (4)</p><p> </p><p>Eq. (5)</p><p> </p><p> </p><p>Eq. (6)</p></td></tr></tbody></table><p> </p><p> </p><p> </p><p> </p><p> </p><p> </p><p> </p><p> </p><p class="h1header"> </p><p class="h1header"> </p><p class="h1header"></p><p class="h1header">Half Pipe Coil Jackets</p><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Half Pipe Coil Jacket" href="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/jacketed_vessel_design4.gif" target="_blank"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/thumb_jacketed_vessel_design4.gif" alt="jacketed_vessel_design4" width="114" height="150" /></a></td></tr><tr><td>Figure 4: Half Pipe<br />
Coil Jacket</td></tr></tbody></table><p>Half pipe coils provide high velocity and turbulence. The velocity can be closely controlled to achieve a good film coefficient. The good heat transfer rates, combined with the structural rigidity of the design, make half-pipe coils a good choice for a wide range of applications. A good design velocity for liquid utilities is 2.5 to 5 ft/s. {parse block="google_articles"}The maximumspacing between coils should be limited to 3/4". Half-pipe coils are ideally suited for high temperature applications where the utility fluid is a liquid.</p><p>There are no limitations of the number of inlet and outlet nozzles, so the jacket can be divided in multipass zones for maximum flexibility. The rigidity of the half-pipe coil design can also minimize the thickness of the inner vessel wall which can be especially attractive when utilizing alloys.</p><p>Half-pipe coil jackets are not covered in Section VIII, Division I of the ASME code. Generally, they are limited to 600 psig design pressure and a design temperature up to 720 &deg;F. A carbon steel half-pipe jacket can be applied to a stainless steel vessel up to 300 &deg;F. Over 300 &deg;F, the jacket should be stainless steel as well.</p><p class="h2header">Heat Transfer Coefficients: Half-Pipe Coil Jackets</p><p>Half-pipe coil jackets are generally manufactured with either 180&deg; or 120&deg; central angles (D<sub>ci</sub>):</p><table class="imagecaption" border="0" align="center"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/jacketed_vessel_design13.gif" alt="jacketed_vessel_design13" width="326" height="78" /></td></tr><tr><td>Figure 5: Depiction of Center Angles</td></tr></tbody></table><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Half-Pipe Coil to Tank Details" href="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/jacketed_vessel_design5.gif" target="_blank"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/thumb_jacketed_vessel_design5.gif" alt="jacketed_vessel_design5" width="150" height="62" /></a></td></tr><tr><td>Figure 6: Half-Pipe Coil<br />
to Tank Details</td></tr></tbody></table><p>For a 180&deg; central angle:<br />
<br />
Equivalent Heat Transfer Diameter, De = &Pi; / (4 D<sub>ci</sub>)</p><p>Cross Section Area of Flow, Ax = &Pi; / (8 (D<sub>ci</sub><sup>2</sup>))</p><p>For a 120&deg; central angle:<br />
<br />
Equivalent Heat Transfer Diameter, De = 0.708 D<sub>ci</sub></p><p>Cross Section Area of Flow, Ax = 0.154 (D<sub>ci</sub><sup>2</sup>)</p><p>Using the same nomenclature as previous, the heat transfer coefficients are calculated as follows:</p><table class="equationtable" border="0" align="center"><tbody><tr><td valign="top">h<sub>j</sub> D<sub>e</sub>/ k= 0.027(N<sub>Re</sub>)<sup>0.8 </sup>(N<sub>Pr</sub>)<sup>0.33</sup> (&micro;/&micro;<sub>W</sub>)<sup>0.14</sup> (1+3.5 (D<sub>c</sub>/D<sub>e</sub>) ) (For N<sub>Re</sub>>10,000)</td><td class="equationnumber" align="right">Eq. (7)</td></tr></tbody></table><table class="equationtable" border="0" align="center"><tbody><tr><td valign="top">h<sub>j</sub> D<sub>e</sub>/ k = 1.86 [ (N<sub>Re</sub>) (N<sub>Pr</sub>) (D<sub>c</sub>/D<sub>e</sub>) ] <sup>0.33</sup> (&micro;/&micro;<sub>W</sub>)<sup>0.14</sup> (For N<sub>Re</sub><2,100)</td><td class="equationnumber" align="right">Eq. (8)</td></tr></tbody></table><p><em><strong>Do not confuse D<sub>ci</sub> with D<sub>c</sub>.</strong> </em>D<sub>c</sub> is defined as D<sub>ji</sub> + ((D<sub>jo</sub>-D<sub>ji</sub>)/2).</p><p class="h2header">Hydraulic Radius: Half-Pipe Coil Jackets</p><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Hydraulic Radius Dimensions" href="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/jacketed_vessel_design6.gif" target="_blank"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/thumb_jacketed_vessel_design6.gif" alt="jacketed_vessel_design6" width="128" height="150" /></a></td></tr><tr><td>Figure 7: Hydraulic Radius<br />
Dimensions</td></tr></tbody></table><p>Referring to Figure7:</p><table class="equationtable" style="width: 75%;" border="0" align="center"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/jacketed_vessel_design15.gif" alt="jacketed_vessel_design15" width="336" height="92" /></td><td class="equationnumber" align="right" valign="middle"><br />
<br />
Eq. (9)</td></tr></tbody></table><p> </p><p> </p><p> </p><p class="h1header"> <span class="h1header">Dimple Jackets or Plate Coils</span></p><p>The design of dimple jackets permits construction from light gauge metals without sacrificing the strength required to withstand the specified pressure. This results in considerable cost saving as compared to convention jackets. Design calculation begin with an assumed flow velocity between 2 and 5 ft/s. As a rule of thumb the jacket pressure will be governing when internal pressure of vessel is less than 1.67 times the jacket pressure. {parse block="google_articles"}At such conditions, dimple jackets are typically more economical than other choices. However in small vessels (less than 10 gallons) it is not practical to apply dimple jackets.</p><p>The design of dimple jackets is governed by the National Board of Boiler and Pressure Vessel Inspectors and can be stamped in accordance with ASME Unfired Pressure Vessel Code. Dimple jackets are limited to a pressure of 300 psi by <span style="text-decoration: underline;">Section VIII</span>, <span style="text-decoration: underline;">Div.I of the ASME Code</span>. The design temperature is limited to 700 &deg;F. At high temperatures, it is mandatory that jacket be fabricated from a metal having same thermal coefficient of expansion as that used in inner vessel.</p><table class="imagecaption" border="0" align="center"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Vessel with Dimple Jacket Installed" href="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/jacketed_vessel_design7.gif" target="_blank"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/thumbnails/thumb_jacketed_vessel_design7.gif" alt="jacketed_vessel_design7" width="98" height="150" /></a></td><td> </td><td><a class='resized_img' rel='lightbox[2]' title="Dimple Jacket Details" href="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/jacketed_vessel_design8.gif" target="_blank"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/thumbnails/thumb_jacketed_vessel_design8.gif" alt="jacketed_vessel_design8" width="150" height="75" /></a></td></tr><tr><td>Figure 8: Vessel with Dimple<br />
Jacket Installed</td><td> </td><td>Figure 9: Dimple Jacket Details</td></tr></tbody></table><p class="h2header">Heat Transfer Coefficients: Dimple Jackets</p><table class="equationtable" border="0" align="center"><tbody><tr><td valign="top">h<sub>j</sub> D<sub>o</sub>/k= j (N<sub>Re</sub>) (N<sub>Pr</sub>)<sup>0.33</sup> (For 1000 < N<sub>Re</sub> < 50,000)</td><td class="equationnumber" align="right">Eq. (10)</td></tr></tbody></table><table style="width: 100%;" border="0"><tbody><tr><td colspan="2" width="100%">Where:<p>j = 0.0845 (w/x)<sup>0.368</sup> (A<sub>min</sub>/A<sub>max</sub>)<sup>-0.383</sup> N<sub>Re</sub><sup>-0.305</sup></p><p>w = center-to-center distance between dimples<br />
x = center-to-center distance between dimples parallel to flow<br />
<em>Note: (w/x) is equal to one for square spacings as is often the case<br />
</em>D<sub>o</sub> = (d<sub>1</sub> + d<sub>2</sub>)/2<br />
A<sub>min</sub> = z (w-D<sub>o</sub>)<br />
A<sub>max</sub> = zw</p></td></tr></tbody></table><p>All other variables are as previously defined. Garvin (<em>CEP Magazine, April 2001) </em>reports an average error of 9.8% with manufacturers data for the above correlation and a maximum error of 30% over 116 data points. This results in average deviations in the heat transfer coefficient of 15-20% most of which was at velocities below 2 ft/s. Good agreement with manufacturers data was found between 3 and 6 ft/s. A recommended excess area of 15% should be used in this velocity range.</p><p><span class="info">The correlation above is for integrally welded jackets (ie. jackets welded directly to the vessel). If a dimple jacket is clamped onto an existing vessel and adhered with heat transfer mastic, the overall heat transfer coefficient of the system will be very low. Mastic is used to try to minimize air pocket resistances between the vessel wall and the jacket. Historically, this arrangement results in poor heat transfer. A recommended overall heat transfer coefficient of 10-15 Btu/h ft<sup>2</sup> &deg;F should be used for such systems regardless of the utility used.</span></p><p class="h2header">Pressure Drop: Dimple Jackets</p><p>The pressure loss in a dimple jacket can be estimated from the following for water or water-like fluids:</p><p>Pressure Loss in Jacket = (Total Lenght of Flow, ft) x ((0.40 x Velocity, ft/s) - 0.35)</p><p>Pressure Loss Across Entire Jacket (including inlets and outlets) = Pressure Loss in Jacket + (0.10)(Pressure Loss in Jacket)</p><p>The above estimates should be used for velocities ranging from 1.5 to 6 ft/s.</p><p>This method is based on a graph found on page 217 of the <em>Encyclopedia of Pharmaceutical Technology</em> by James Swarbrick.</p><p>For detailed design, it is advisable to rely on manufacturer's data for pressure drop calculations.</p><p class="h1header">Heat Transfer Coefficients Inside Agitated Vessels</p><p>In order to complete the overall heat transfer coefficient calculation, an estimate must also be made inside the process vessel. The following estimate should yield reasonable results:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/jacketed_vessel_design16.gif" alt="jacketed_vessel_design16" width="355" height="63" /></td><td class="equationnumber" align="right"><br />
Eq. (11)</td></tr></tbody></table><p>Where:</p><p>A<sub>d</sub> = agitator diameter<br />
N = agitator speed, rev/s<br />
All other variables as previously defined<br />
a is defined by the table below:</p><table class="datatable" border="0" align="center"><caption>Table 1: Dimension "a" for Use with Equation 11</caption><tbody><tr><td><strong>Agitator</strong></td><td><strong>Surface</strong></td><td><strong>"a"</strong></td></tr><tr><td>Turbine</td><td>Jacket</td><td>0.62</td></tr><tr><td>Turbine</td><td>Coil</td><td>1.50</td></tr><tr><td>Paddle</td><td>Jacket</td><td>0.36</td></tr><tr><td>Paddle</td><td>Coil</td><td>0.87</td></tr><tr><td>Anchor</td><td>Jacket</td><td>0.46</td></tr><tr><td>Propeller</td><td>Jacket</td><td>0.54</td></tr><tr><td>Propeller</td><td>Coil</td><td>0.83</td></tr></tbody></table><p class="h2header">Calculating the Overall Heat Transfer Coefficient</p><p>When calculating the overall heat transfer coefficient for a system, the vessel wall resistance and any jacket fouling must be taken into account:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/jacketed_vessel_design17.gif" alt="jacketed_vessel_design17" width="343" height="70" /></td><td class="equationnumber" align="right"><br />
Eq. (12)</td></tr></tbody></table><p>Notice that the thermal conducitivity of the vessel wall and the wall thickness are included in the calculation. A typical jacket fouling factor is around 0.001 h ft<sup>2</sup> &deg;F/Btu. When calculating the overall heat transfer coefficient, use a "common sense" analysis of the final value. The tables below will give some guidance to reasonable final values:</p><table class="imagecaption" border="0" align="center"><tbody><tr><td>Table 2: Estimated Overall<br />
Heat Transfer Coefficients<br />
for Jacketed Tank Systems<br />
(Imperial Units)</td><td> </td><td>Table 3: Estimated Overall<br />
Heat Transfer Coefficients<br />
for Jacketed Tank Systems<br />
(Metric Units)</td></tr><tr><td><a class='resized_img' rel='lightbox[2]' title="Estimated Overall Heat Transfer Coefficients for Jacketed Tank Systems (Imperial Units)" href="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/jacketed_vessel_design18.gif" target="_blank"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/thumbnails/thumb_jacketed_vessel_design18.gif" alt="jacketed_vessel_design18" width="150" height="99" /></a></td><td> </td><td><a class='resized_img' rel='lightbox[2]' title="Estimated Overall Heat Transfer Coefficients for Jacketed Tank Systems (Metric Units)" href="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/jacketed_vessel_design19.gif" target="_blank"><img src="&#46;&#46;/&#46;&#46;/&#46;&#46;/&#46;&#46;/invision/uploads/images/articles/thumbnails/thumbnails/thumb_jacketed_vessel_design19.gif" alt="jacketed_vessel_design19" width="150" height="97" /></a></td></tr></tbody></table><p class="h1header">References</p><ol><li>Heat Transfer Design Methods by 'John J. McKetta'</li><li>Hand Book of chemical Engineering Calculation 3rd Edition by 'Micclas P. Chopey'.</li><li>Applied Process Design for Chemical and Petrochemical Plants by 'Ludwig' Volume 3.</li><li>Estimate Heat Transfer and Friction in Dimple Jackets, 'John Garvin', <em>CEP Magazine</em>, April 2001, p. 73</li><li>Heat Transfer in Agitated Jacketed Vessels, 'Robert Dream', <em>Chemical Engineering</em>, January 1999, p. 90</li><li>Encyclopedia of Pharmaceutical Technology, 'James Swarbrick', p. 217</li><li>Tranter Plate Coil Product Manual</li></ol>]]></description>
		<pubDate>Mon, 08 Nov 2010 18:50:19 +0000</pubDate>
		<guid isPermaLink="false">9da187a7a191431db943a9a5a6fec6f4</guid>
	</item>
	<item>
		<title>Pinch Technology: Basics for Beginners</title>
		<link>http://www.cheresources.com/content/articles/heat-transfer/pinch-technology-basics-for-beginners</link>
		<description><![CDATA[<p align="justify">While oil prices continue to climb, energy conservation remains the prime concern for many process industries. The challenge every process engineer is faced with is to seek answers to questions related to their process energy patterns.</p><p> </p><p>A few of the frequently asked questions are:</p><ol><li><div>Are the existing processes as energy efficient as they should be?</div></li><li><div>How can new projects be evaluated with respect to their energy requirements?{parse block="google_articles"}</div></li><li><div>What changes can be made to increase the energy efficiency without incurring any cost?</div></li><li><div>What investments can be made to improve energy efficiency?</div></li><li><div>What is the most appropriate utility mix for the process?</div></li><li><div>How to put energy efficiency and other targets like reducing emissions, increasing plant capacities, improve product qualities etc, into a one coherent strategic plan for the overall site?</div></li></ol><p align="justify">All of these questions and more can be answered with a full understanding of <em><strong>Pinch Technology</strong></em> and an awareness of the available tools. for applying it in a practical way. This article aims to provide the basic knowledge of the concepts in pinch technology and how they have been be applied across a wide range of process industries.</p><p class="h1header">What is Pinch Technology</p><p class="h2header">Meaning of the Term "Pinch Technology"</p><p>The term "Pinch Technology" was introduced by Linnhoff and Vredeveld to represent a new set of thermodynamically based methods that guarantee minimum energy levels in design of heat exchanger networks. Over the last two decades it has emerged as an unconventional development in process design and energy conservation. The term â€˜Pinch Analysisâ€™ is often used to represent the application of the tools and algorithms of Pinch Technology for studying industrial processes. Developments of rigorous software programs like PinchExpressTM, SuperTargetTM, Aspen PinchTM have proved to be very useful in pinch analysis of complex industrial processes with speed and efficiency.</p><p class="h2header">Basis of Pinch Analysis</p><p>Pinch technology presents a simple methodology for systematically analysing chemical processes and the surrounding utility systems with the help of the First and Second Laws of Thermodynamics. The First Law of Thermodynamics provides the energy equation for calculating the enthalpy changes (dH) in the streams passing through a heat exchanger. The Second Law determines the direction of heat flow. That is, heat energy may only flow in the direction of hot to cold. This prohibits â€˜temperature crossoversâ€™ of the hot and cold stream profiles through the exchanger unit. In a heat exchanger unit neither a hot stream can be cooled below cold stream supply temperature nor a cold stream can be heated to a temperature more than the supply temperature of hot stream. In practice the hot stream can only be cooled to a temperature defined by the â€˜temperature approachâ€™ of the heat exchanger. The temperature approach is the minimum allowable temperature difference (DTmin) in the stream temperature profiles, for the heat exchanger unit. The temperature level at which DTmin is observed in the process is referred to as "pinch point" or "pinch condition". The pinch defines the minimum driving force allowed in the exchanger unit.</p><p class="h2header">Objectives of the Pinch Analysis</p><p>Pinch Analysis is used to identify energy cost and heat exchanger network (HEN) capital cost targets for a process and recognizing the pinch point. The procedure first predicts, ahead of design, the minimum requirements of external energy, network area, and the number of units for a given process at the pinch point. Next a heat exchanger network design that satisfies these targets is synthesized. Finally the network is optimized by comparing energy cost and the capital cost of the network so that the total annual cost is minimized. Thus, the prime objective of pinch analysis is to achieve financial savings by better process heat integration (maximizing process-to-process heat recovery and reducing the external utility loads). The concept of process heat integration is illustrated in the example discussed below.</p><p class="h2header">A Simple Example of Process Integration by Pinch Analysis</p><p>Consider the following simple process [Figure 1a] where feed stream to a reactor is heated before inlet to a reactor and the product stream is to be cooled. The heating and cooling are done by use of steam (Heat Exchanger -1) and cooling water (Heat Exchanger-2), respectively. The Temperature (T) vs. Enthalpy (H) plot for the feed and product streams depicts the hot (Steam) and cold (CW) utility loads when there is no vertical overlap of the hot and cold stream profiles.</p><table class="imagecaption" border="0" align="center"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="A Simple Flow Scheme with T-H profile" href="../../../../invision/uploads/images/articles/pinchtech9.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_pinchtech9.gif" alt="pinchtech9" width="150" height="96" /></a></td><td><a class='resized_img' rel='lightbox[2]' title="Improved Flow Scheme with T-H profile" href="../../../../invision/uploads/images/articles/pinchtech10.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_pinchtech10.gif" alt="pinchtech10" width="150" height="121" /></a></td></tr><tr><td>Figure 1a: A Simple Flow Scheme<br />
with T-H profile</td><td>Figure 1b: Improved Flow Scheme <br />
with T-H profile</td></tr></tbody></table><p>An alternative, improved scheme is shown in Figure 1b where the addition of a new â€˜Heat Exchangerâ€“3â€™ recovers product heat (X) to preheat the feed. The steam and cooling water requirements also get reduced by the same amount (X). The amount of heat recovered (X) depends on the â€˜minimum approach temperatureâ€™ allowed for the new exchanger. The minimum temperature approach between the two curves on the vertical axis is DTmin and the point where this occurs is defined as the "pinch". From the T-H plot, the X amount corresponds to a DTmin value of 20 oC. Increasing the DTmin value leads to higher utility requirements and lower area requirements.</p><p class="h2header">Development of the Pinch Technology Approach</p><p>When the process involves single hot and cold streams (as in above example) it is easy to design an optimum heat recovery exchanger network intuitively by heuristic methods. In any industrial set-up the number of streams is so large that the traditional design approach has been found to be limiting in the design of a good network. With the development of pinch technology in the late 1980â€™s, not only optimal network design was made possible, but also considerable process improvements could be discovered. Both the traditional and pinch approaches are depicted in Figure 2.</p><table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/pinchtech11.gif" alt="pinchtech11" width="382" height="182" /></td></tr><tr><td>Figure 2: Graphic Representation of <br />
Traditional and Pinch Design Approaches</td></tr></tbody></table><p>First, the core of the process is designed with fixed flow rates and temperatures yielding the heat and mass balance for the process. Then the design of a heat recovery system is completed. Next, the remaining duties are satisfied by the use of the utility system. Each of these exercises is performed independently of the others.</p><p>Process integration using pinch technology offers a novel approach to generate targets for minimum energy consumption before heat recovery network design. Heat recovery and utility system constraints are then considered in the design of the core process. Interactions between the heat recovery and utility systems are also considered. The pinch design can reveal opportunities to modify the core process to improve heat integration. The pinch approach is unique because it treats all processes with multiple streams as a single, integrated system. This method helps to optimize the heat transfer equipment during the design of the equipment.{parse block="google_articles"}</p><p>Pinch originated in the petrochemical sector and is now being applied to solve a wide range of problems in mainstream chemical engineering. Wherever heating and cooling of process materials takes places there is a potential opportunity. Thus initial applications of the technology were found in projects relating to energy saving in industries as diverse as iron and steel, food and drink, textiles, paper and cardboard, cement, base chemicals, oil, and petrochemicals.</p><p>Early emphasis on energy conservation led to the misconception that conservation is the main area of application for pinch technology. The technology, when applied with imagination, can affect reactor design, separator design, and the overall process optimization in any plant. It has been applied to processing problems that go far beyond energy conservation. It has been employed to solve problems as diverse as improving effluent quality, reducing emissions, increasing product yield, debottlenecking, increasing throughput, and improving the flexibility and safety of the processes.</p><p>Since its commercial introduction, pinch technology has achieved an outstanding record of success in the design and retrofit of chemical manufacturing facilities. Documented results reported in the literature show that energy costs have been reduced by 15-40%, capacity debottlenecking achieved by 5-15% for retrofits, and capital cost reduction of 5-10% for new designs.</p><p class="h1header">Basic Concepts of Pinch Analysis</p><p>Most industrial processes involve transfer of heat either from one process stream to another process stream (interchanging) or from a utility stream to a process stream. In the present energy crisis scenario all over the world, the target in any industrial process design is to maximize the process-to-process heat recovery and to minimize the utility (energy) requirements. To meet the goal of maximum energy recovery or minimum energy requirement (MER) an appropriate heat exchanger network (HEN) is required. The design of such a network is not an easy task considering the fact that most processes involve a large number of process and utility streams. As explained in the previous section, the traditional design approach has resulted in networks with high capital and utility costs. With the advent of pinch analysis concepts, the network design has become very systematic and methodical.{parse block="google_articles"}</p><p>A summary of the key concepts, their significance, and the nomenclature used in pinch analysis is given below:</p><ul><li>Combined (Hot and Cold ) Composite Curves: Used to predict targets for: <ul><li>Minimum energy (both hot and cold utility) required,</li><li>Minimum network area required, and</li><li>Minimum number of exchanger units required.</li></ul></li><li>DTmin and Pinch Point: The DTmin value determines how closely the hot and cold composite curves can be â€˜pinchedâ€™ (or squeezed) without violating the Second Law of Thermodynamics (none of the heat exchangers can have a temperature crossover).</li><li>Grand Composite Curve: Used to select appropriate levels of utilities (maximize cheaper utilities) to meet over all energy requirements.</li><li>Energy and Capital Cost Targeting: Used to calculate total annual cost of utilities and capital cost of heat exchanger network.</li><li>Total Cost Targeting: Used to determine the optimum level of heat recovery or the optimum DTmin value, by balancing energy and capital costs. Using this method, it is possible to obtain an accurate estimate (within 10 - 15%) of overall heat recovery system costs without having to design the system. The essence of the pinch approach is the speed of economic evaluation. </li><li>Plus/Minus and Appropriate Placement Principles: The "Plus/Minus" Principle provides guidance regarding how a process can be modified in order to reduce associated utility needs and costs. The Appropriate Placement Principles provide insights for proper integration of key equipments like distillation columns, evaporators, furnaces, heat engines, heat pumps, etc. in order to reduce the utility requirements of the combined system.</li><li>Total Site Analysis: This concept enables the analysis of the energy usage for an entire plant site that consists of several processes served by a central utility system.</li></ul><p>With further research, new topics like â€˜Regional Energy Analysisâ€™, â€˜Network Pinchâ€™, â€˜Top Level Analysisâ€™, â€˜Optimisation of Combined Heat & Powerâ€™, â€˜Water Pinchâ€™, and â€˜Hydrogen Pinchâ€™ are being developed. These basic terms and concepts have become the foundation of what we now call Pinch Technology.</p><p class="h1header">Steps of the Pinch Analysis</p><p>In any Pinch Analysis problem, whether a new project or a retrofit situation, a well-defined stepwise procedure is followed (Figure 3). It should be noted that these steps are not necessarily performed on a once-through basis, independent of one another. Additional activities such as re-simulation and data modification occur as the analysis proceeds and some iteration between the various steps is always required.</p><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Steps in Pinch Analysis" href="../../../../invision/uploads/images/articles/pinchtech12.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_pinchtech12.gif" alt="pinchtech12" width="150" height="119" /></a></td></tr><tr><td>Figure 3: Steps in Pinch Analysis</td></tr></tbody></table><p class="h2header">Step 1: Identification of the Hot, Cold and Utility Streams in the Process</p><ul><li>â€˜Hot Streamsâ€™ are those that must be cooled or are available to be cooled. e.g. product cooling before storage</li><li>â€˜Cold Streamsâ€™ are those that must be heated e.g. feed preheat before a reactor.</li><li>â€˜Utility Streamsâ€™ are used to heat or cool process streams, when heat exchange between process streams is not practical or economic. A number of different hot utilities (steam, hot water, flue gas, etc.) and cold utilities (cooling water, air, refrigerant, etc.) are used in industry.</li></ul><p>The identification of streams needs to be done with care as sometimes, despite undergoing changes in temperature, the stream is not available for heat exchange. For example, when a gas stream is compressed the stream temperature rises because of the conversion of mechanical energy into heat and not by any fluid to fluid heat exchange. Hence such a stream may not be available to take part in any heat exchange. In the context of pinch analysis, this stream may or may not be considered to be a process stream.</p><p class="h2header">Step 2: Thermal Data Extraction for Process & Utility Streams</p><p>For each hot, cold and utility stream identified, the following thermal data is extracted from the process material and heat balance flow sheet:</p><ul><li>Supply temperature (TS Â°C) : the temperature at which the stream is available.</li><li>Target temperature (TT Â°C) : the temperature the stream must be taken to.</li><li>Heat capacity flow rate (CP kW/ Â°C) : the product of flow rate (m) in kg/sec and specific heat (Cp kJ/kg Â°C).<br />
CP = m x Cp</li><li>Enthalpy Change (dH) associated with a stream passing through the exchanger is given by the First Law of Thermodynamics:<br />
First Law energy equation: d H = Q Â± W<br />
In a heat exchanger, no mechanical work is being performed:<br />
W = 0 (zero)<br />
The above equation simplifies to: d H = Q, where Q represents the heat supply or demand associated with the stream. It is given by the relationship: Q= CP x (TS - TT).<br />
Enthalpy Change, dH = CP x (TS - TT)<br />
<em>** Here the specific heat values have been assumed to be temperature independent within the operating range.</em></li></ul><p>The stream data and their potential effect on the conclusions of a pinch analysis should be considered during all steps of the analysis. Any erroneous or incorrect data can lead to false conclusions. In order to avoid mistakes, the data extraction is based on certain qualified principles.</p><table class="datatable" border="0" align="center"><caption>Table 1: Typical Stream Data</caption><tbody><tr><td><strong>Stream<br />
Number</strong></td><td><strong>Stream<br />
Name</strong></td><td><strong>Supply <br />
Temp (Â°C)</strong></td><td><strong>Target<br />
Temp (Â°C)</strong></td><td><strong>Heat<br />
Cap Flow<br />
(kW/Â°C)</strong></td><td><strong>Enth.<br />
Change<br />
(kW)</strong></td></tr><tr><td>1</td><td>Feed</td><td>60</td><td>205</td><td>20</td><td>2900</td></tr><tr><td>2</td><td>Reac. Out</td><td>270</td><td>160</td><td>18</td><td>1980</td></tr><tr><td>3</td><td>Product</td><td>220</td><td>70</td><td>35</td><td>5250</td></tr><tr><td>4</td><td>Recycle</td><td>160</td><td>210</td><td>50</td><td>2500</td></tr></tbody></table><p class="h2header">Step 3: Selection of the Initial DTmin Value</p><p>The design of any heat transfer equipment must always adhere to the Second Law of Thermodynamics that prohibits any temperature crossover between the hot and the cold stream i.e. a minimum heat transfer driving force must always be allowed for a feasible heat transfer design. Thus the temperature of the hot and cold streams at any point in the exchanger must always have a minimum temperature difference (DTmin). This DTmin value represents the bottleneck in the heat recovery.</p><p>In mathematical terms, at any point in the exchanger:</p><table class="datatable_inset" border="0" align="center"><tbody><tr><td><p>Â <strong>Hot stream Temp. ( TH ) - ( TC ) Cold stream Temp. >= DTmin</strong></p></td></tr></tbody></table><p>The value of DTmin is determined by the overall heat transfer coefficients (U) and the geometry of the heat exchanger. In a network design, the type of heat exchanger to be used at the pinch will determine the practical Dtmin for the network. For example, an initial selection for the Dtmin value for shell and tubes may be 3-5 0C (at best) while compact exchangers such as plate and frame often allow for an initial selection of 2-3 0C. The heat transfer equation, which relates Q, U, A and LMTD (Log Mean Temperature Difference) is depicted in Figure 4.</p><table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/pinchtech13.gif" alt="pinchtech13" width="312" height="164" /></td></tr><tr><td>Figure 4: The Heat Transfer Equation</td></tr></tbody></table><p>For a given value of heat transfer load (Q), if smaller values of DTmin are chosen, the area requirements rise. If a higher value of DTmin is selected the heat recovery in the exchanger decreases and demand for external utilities increases. Thus, the selection of DTmin value has implications for both capital and energy costs. This concept will become clearer with the help of composite curves and total cost targeting discussed later.</p><p>Just as for a single heat exchanger, the choice of DTmin (or approach temperature) is vital in the design of a heat exchanger networks. To begin the process an initial DTmin value is chosen and pinch analysis is carried out. Typical DTmin values based on experience are available in literature for reference. A few values based on Linnoff Marchâ€™s application experience are tabulated below for shell and tube heat exchangers.</p><table class="datatable" border="0" align="center"><tbody><tr><td><strong>No</strong></td><td><strong>Industrial Sector</strong></td><td><strong>Experience DTmin<br />
Values</strong></td></tr><tr><td>1</td><td>Oil Refining</td><td>20-40 Â°C</td></tr><tr><td>2</td><td>Petrochemical</td><td>10-20 Â°C</td></tr><tr><td>3</td><td>Chemical</td><td>10-20 Â°C</td></tr><tr><td>4</td><td>Low Temp<br />
Processes</td><td>3-5 Â°C</td></tr></tbody></table><p class="h2header"><span class="h2header">Step 4: Construction of the Composite Curves and Grand Composite Curve</span></p><ul><li>COMPOSITE CURVES: Temperature - Enthalpy (T - H) plots known as â€˜Composite curvesâ€™ have been used for many years to set energy targets ahead of design. Composite curves consist of temperature (T) â€“ enthalpy (H) profiles of heat availability in the process (the hot composite curve) and heat demands in the process (the cold composite curve) together in a graphical representation.</li></ul><p>In general any stream with a constant heat capacity (CP) value is represented on a T - H diagram by a straight line running from stream supply temperature to stream target temperature. When there are a number of hot and cold streams, the construction of hot and cold composite curves simply involves the addition of the enthalpy changes of the streams in the respective temperature intervals. An example of hot composite curve construction is shown in Figure 5a and b. A complete hot or cold composite curve consists of a series of connected straight lines, each change in slope represents a change in overall hot stream heat capacity flow rate (CP).{parse block="google_articles"}</p><p>For heat exchange to occur from the hot stream to the cold stream, the hot stream cooling curve must lie above the cold stream-heating curve. Because of the â€˜kinkedâ€™ nature of the composite curves (Figure 6), they approach each other most closely at one point defined as the minimum approach temperature (DTmin). DTmin can be measured directly from the T-H profiles as being the minimum vertical difference between the hot and cold curves. This point of minimum temperature difference represents a bottleneck in heat recovery and is commonly referred to as the "Pinch". Increasing the DTmin value results in shifting the of the curves horizontally apart resulting in lower process to process heat exchange and higher utility requirements. At a particular DTmin value, the overlap shows the maximum possible scope for heat recovery within the process.Â  The hot end and cold end overshoots indicate minimum hot utility requirement (QHmin) and minimum cold utility requirement (QCmin), of the process for the chosen DTmin.</p><table class="imagecaption" border="0" align="center"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Temperature-Enthalpy Relations Used to Construct Composite Curves" href="../../../../invision/uploads/images/articles/pinchtech14.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_pinchtech14.gif" alt="pinchtech14" width="150" height="113" /></a></td><td>Â </td><td><a class='resized_img' rel='lightbox[2]' title="Combined Composite Curve" href="../../../../invision/uploads/images/articles/pinchtech15.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_pinchtech15.gif" alt="pinchtech15" width="150" height="113" /></a></td></tr><tr><td>Figure 5: Temperature-Enthalpy <br />
Relations Used to Construct<br />
Composite Curves</td><td>Â </td><td>Figure 6: Combined Composite <br />
Curves</td></tr></tbody></table><p>Thus, the energy requirement for a process is supplied via process to process heat exchange and/or exchange with several utility levels (steam levels, refrigeration levels, hot oil circuit, furnace flue gas, etc.).</p><p>Graphical constructions are not the most convenient means of determining energy needs. A numerical approach called the "Problem Table Algorithm" (PTA) was developed by Linnhoff & Flower (1978) as a means of determining the utility needs of a process and the location of the process pinch. The PTA lends itself to hand calculations of the energy targets.Â </p><p>To summarize, the composite curves provide overall energy targets but do not clearly indicate how much energy must be supplied by different utility levels. The utility mix is determined by the Grand Composite Curve.</p><ul><li>GRAND COMPOSITE CURVE (GCC): In selecting utilities to be used, determining utility temperatures, and deciding on utility requirements, the composite curves and PTA are not particularily useful. The introduction of a new tool, the Grand Composite Curve (GCC), was introduced in 1982 by Itoh, Shiroko and Umeda. The GCC (Figure 7) shows the variation of heat supply and demand within the process.Â Using this diagramÂ  the designer canÂ  find which utilities are to be used. The designer aims to maximize the use of the cheaper utility levels and minimize the use of the expensive utility levels. Low-pressure steam and cooling water are preferred instead of high-pressure steam and refrigeration, respectively.</li></ul><p>The information required for the construction of the GCC comes directly from the Problem Table Algorithm developed by Linnhoff & Flower (1978). The method involves shifting (along the temperature [Y] axis) of the hot composite curve down by Â½ DTmin and that of cold composite curve up by Â½ DTmin. The vertical axis on the shifted composite curves shows processÂ  interval temperature. In other words, the curves are shifted by subtracting part of the allowable temperature approach from the hot stream temperatures and adding the remaining part of the allowable temperature approach to the cold stream temperatures. The result is a scale based upon process temperature having an allowance for temperature approach (DTmin). The Grand Composite Curve is then constructed from the enthalpy (horizontal) differences between the shifted composite curves at different temperatures. On the GCC, the horizontal distance separating the curve from the vertical axis at the top of the temperature scale shows the overall hot utility consumption of the process.</p><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Grand Composite Curve" href="../../../../invision/uploads/images/articles/pinchtech16.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_pinchtech16.gif" alt="pinchtech16" width="150" height="100" /></a></td></tr><tr><td>Figure 7: Grand Composite<br />
Curve</td></tr></tbody></table><p>Figure 7 shows that it is not necessary to supply the hot utility at the top temperature level. The GCC indicates that we can supply the hot utility over two temperature levels TH1 (HP steam) and TH2 (LP steam).Â  Recall that, when placing utilities in the GCC, intervals, and not actual utility temperatures, should be used. The total minimum hot utility requirement remains the same: QHmin = H1 (HP steam) + H2 (LP steam). Similarly, QCmin = C1 (Refrigerant) +C2 (CW). The points TH2 and TC2 where the H2 and C2 levels touch the grand composite curve are called the "Utility Pinches." The shaded green pockets represent the process-to-process heat exchange.</p><p>In summary, the grand composite curve is one of the most basic tools used in pinch analysis for the selection of the appropriate utility levels and for targeting of a given set of multiple utility levels. The targeting involves setting appropriate loads for the various utility levels by maximizing the least expensive utility loads and minimizing the loads on the most expensive utilities.</p><p class="h2header">Step 5: Estimation of Minimum Energy Cost Targets</p><p>Once the DTmin is chosen, minimum hot and cold utility requirements can be evaluated from the composite curves. The GCC provides information regarding the utility levels selected to meet QHmin and QCmin requirements.</p><p>If the unit cost of each utility is known, the total energy cost can be calculated using the energy equation given below.</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/pinchtecheq1.gif" alt="pinchtecheq1" width="287" height="75" /></td><td class="equationnumber" align="right">Eq. (1)</td></tr></tbody></table><p>where Q<sub>U</sub> = Duty of utility, kW, C<sub>U</sub> = Unit cost of utility U, $/kW per year, and U = Total number of utilities used.</p><p class="h2header">Step 6: Estimation of Heat Exchanger Network ( HEN ) Capital Cost Targets</p><p>The capital cost of a heat exchanger network is dependent upon three factors:</p><ol><li>the number of exchangers,</li><li>the overall network area,</li><li>the distribution of area between the exchangers</li></ol><p>Pinch analysis enables targets for the overall heat transfer area and minimum number of units of a heat exchanger network (HEN) to be predicted prior to detailed design. It is assumed that the area is evenly distributed between the units. The area distribution cannot be predicted ahead of design.</p><ul><li>AREA TARGETING: The calculation of surface area for a single counter-current heat exchanger requires the knowledge of the temperatures of streams in and out (dTLM i.e. Log Mean Temperature Difference or LMTD), overall heat transfer coefficient (U-value), and total heat transferred (Q). The area is given by the relation:</li></ul><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/pinchtecheq2.gif" alt="pinchtecheq2" width="173" height="65" /></td><td class="equationnumber" align="right">Eq. (2)</td></tr></tbody></table><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="HEN AREA min Estimation from Composite Curves" href="../../../../invision/uploads/images/articles/pinchtech18.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_pinchtech18.gif" alt="pinchtech18" width="150" height="115" /></a></td></tr><tr><td>Figure 8: HEN AREA min <br />
Estimation from Composite Curves</td></tr></tbody></table><p>The composite curves can be divided into a set of adjoining enthalpy intervals such that within each interval, the hot and cold composite curves do not change slope. Here the heat exchange is assumed to be "vertical" (pure counter-current heat exchange). The hot streams in any enthalpy interval, at any point, exchanges heat with the cold streams at the temperature vertically below it. The total area of the HEN (Amin) is given by the formula in Figure 8, where i denotes the ith enthalpy and interval j denotes the jth stream and dT<sub>LM</sub> denotes LMTD in the ith interval.</p><p>The actual HEN total area required is generally within 10% of the area target as calculated above. With inclusion of temperature correction factors area targeting can be extended to non counter-current heat exchange as well</p><ul><li>NUMBER OF UNITS TARGETING: For the minimum number of heat exchanger units (N<sub>min</sub>) required for MER (minimum energy requirement or maximum energy recovery), the HEN can be evaluated prior to HEN design by using a simplified form of Eulerâ€™s graph theorem. In designing for the minimum energy requirement (MER), no heat transfer is allowed across the pinch and so a realistic target for the minimum number of units (N<sub>minMER</sub>) is the sum of the targets evaluated both above and below the pinch separately.</li></ul><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/pinchtecheq3.gif" alt="pinchtecheq3" width="479" height="44" /></td><td class="equationnumber" align="right">Eq. (3)</td></tr></tbody></table><p>Where N<sub>h</sub> = Number of hot streams, N<sub>c</sub>=Number of cold streams, N<sub>u</sub> = Number of utility streams, AP / BP : Above / Below Pinch</p><ul><li>HEN TOTAL CAPITAL COST TARGETING: The targets for the minimum surface area (Amin) and the number of units (Nmin) can be combined together with the heat exchanger cost law to determine the targets for HEN capital cost (CHEN). The capital cost is annualized using an annualization factor that takes into account interest payments on borrowed capital. The equation used for calculating the total capital cost and exchanger cost law is given below.</li></ul><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/pinchtecheq4.gif" alt="pinchtecheq4" width="606" height="41" /></td><td class="equationnumber" align="right">Eq. (4)</td></tr></tbody></table><p>where a, b, and c are constants in the heat exchanger cost law, Exchanger cost ($) = a + b(Area)<sup>c</sup></p><p>For the Exchanger Cost Equation shown above, typical values for a carbon steel shell and tube exchnager would be a = 16,000, b = 3,200, and c = 0.7. The installed cost can be considered to be 3.5 times the purchased cost given by the Exchanger Cost Equation.</p><p class="h2header">Step 7: Estimation of the Optimum DTmin Value by Energy-Capital Trade Off</p><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Energy-Capital Cost Trade Off (Optimum DTmin) " href="../../../../invision/uploads/images/articles/pinchtech20.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_pinchtech20.gif" alt="pinchtech20" width="150" height="96" /></a></td></tr><tr><td>Figure 9: Energy-Capital Cost <br />
Trade Off (Optimum DTmin)</td></tr></tbody></table><p>To arrive at an optimum DTmin value, the total annual cost (the sum of total annual energy and capital cost) is plotted at varying DTmin values (Figure 7). Three key observations can be made from Figure 9:</p><ol><li>An increase in DTmin values result in higher energy costs and lower capital costs.</li><li>A decrease in DTmin values result in lower energy costs and higher capital costs.</li><li>An optimum DTmin exists where the total annual cost of energy and capital costs is minimized.{parse block="google_articles"}</li></ol><p>Thus, by systematically varying the temperature approach we can determine the optimum heat recovery level or the DT<sub>minOPTIMUM</sub> for the process.</p><p class="h2header">Step 8: Estimation of Practical Targets for HEN Design</p><p>The heat exchanger network designed on the basis of the estimated optimum DTmin value is not always the most appropriate design. A very small DTmin value, perhaps 8 0C, can lead to a very complicated network design with a large total area due to low driving forces. The designer, in practice, selects a higher value (15 Â°C) and calculates the marginal increases in utility duties and area requirements. If the marginal cost increase is small, the higher value of DTmin is selected as the practical pinch point for the HEN design.</p><p>Recognizing the significance of the pinch temperature allows energy targets to be realized by design of appropriate heat recovery network.</p><p><em>So what is the signficance of the pinch temperature?</em></p><p>The pinch divides the process into two separate systems each of which is in enthalpy balance with the utility. The pinch point is unique for each process. Above the pinch, only the hot utility is required. Below the pinch, only the cold utility is required. Hence, for an optimum design, no heat should be transferred across the pinch. This is known as the key concept in Pinch Technology.</p><p>To summarize, Pinch Technology gives three rules that form the basis for practical network design:</p><ul><li>No external heating below the Pinch.</li><li>No external cooling above the Pinch.</li><li>No heat transfer across the Pinch.</li></ul><p>Violation of any of the above rules results in higher energy requirements than the minimum requirements theoretically possible.</p><p><span style="text-decoration: underline;">The Plus/Minus Principle</span></p><p>The overall energy needs of a process can be further reduced by introducing process changes (changes in the process heat and material balance). There are several parameters that could be changed such as reactor conversions, distillation column operating pressures and reflux ratios, feed vaporization pressures, or pump-around flow rates. The number of possible process changes is nearly infinite. By applying the pinch rules as discussed above, it is possible to identify changes in the appropriate process parameter that will have a favorable impact on energy consumption. This is called the "Plus/Minus Principle."</p><p>Applying the pinch rules to study of composite curves provide us the following guidelines:</p><ul><li>Increase (+) in hot stream duty above the pinch.</li><li>Decrease (-) in cold stream duty above the pinch.</li></ul><p>This will result in a reduced hot utility target, and any</p><ul><li>Decrease (-) in hot stream duty below the pinch.</li><li>Increase (+) in cold stream duty below the pinch</li></ul><p>will result in a reduced cold utility target.</p><p>These simple guidelines provide a definite reference for the adjustment of single heat duties such as vaporization of a recycle, pump-around condensing duty, and others. Often it is possible to change temperatures rather than the heat duties. The target should be to</p><ul><li>Shift hot streams from below the pinch to above and</li><li>Shift cold streams from above the pinch to below.</li></ul><p>The process changes that can help achieve such stream shifts essentially involve changes in following operating parameters:</p><ul><li>reactor pressure/temperatures</li><li>distillation column temperatures, reflux ratios, feed conditions, pump around conditions, intermediate condensers</li><li>evaporator pressures</li><li>storage vessel temperatures</li></ul><p>For example, if the pressure for a feed vaporizer is lowered, vaporization duty can shift from above to below the pinch. The leads to reduction in both hot and cold utilities.</p><p><span style="text-decoration: underline;">Appropriate Placement Principles</span></p><p>Apart from the changes in process parameters, proper integration of key equipment in process with respect to the pinch point should also be considered. The pinch concept of "Appropriate Placement" (integration of operations in such a way that there is reduction in the utility requirement of the combined system) is used for this purpose. Appropriate placement principles have been developed for distillation columns, evaporators, heat engines, furnaces, and heat pumps. For example, a single-effect evaporator having equal vaporization and condensation loads, should be placed such that both loads balance each other and the evaporator can be operated without any utility costs. This means that appropriate placement of the evaporator is on either side of the pinch and not across the pinch.</p><p>In addition to the above pinch rules and principles, a large number of factors must also be considered during the design of heat recovery networks. The most important are operating cost, capital cost, safety, operability, future requirements, and plant operating integrity. Operating costs are dependent on hot and cold utility requirements as well as pumping and compressor costs. The capital cost of a network is dependent on a number of factors including the number of heat exchangers, heat transfer areas, materials of construction, piping, and the cost of supporting foundations and structures.</p><p>With a little practice, the above principles enable the designer to quickly pan through 40-50 possible modifications and choose 3 or 4 that will lead to the best overall cost effects.</p><p>The essence of the pinch approach is to explore the options of modifying the core process design, heat exchangers, and utility systems with the ultimate goal of reducing the energy and/or capital cost.</p><p class="h2header">StepÂ 9: Design of the Heat Exchanger Network</p><p>The design of a new HEN is best executed using the "Pinch Design Method (PDM)". The systematic application of the PDM allows the design of a good network that achieves the energy targets within practical limits. The method incorporates two fundamentally important features: (1) it recognizes that the pinch region is the most constrained part of the problem (consequently it starts the design at the pinch and develops by moving away) and (2) it allows the designer to choose between match options.</p><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Typical Grid Diagram" href="../../../../invision/uploads/images/articles/pinchtech21.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_pinchtech21.gif" alt="pinchtech21" width="150" height="101" /></a></td></tr><tr><td>Figure 10: Typical <br />
Grid Diagram</td></tr></tbody></table><p>In effect, the design of network examines which "hot" streams can be matched to "cold" streams via heat recovery. This can be achieved by employing "tick off" heuristics to identify the heat loads on the pinch exchanger. Every match brings one stream to it target temperature. As the pinch divides the heat exchange system into two thermally independent regions, HENs for both above and below pinch regions are designed separately. When the heat recovery is maximized the remaining thermal needs must be supplied by hot utility.</p><p>The graphical method of representing flow streams and heat recovery matches is called a â€˜grid diagramâ€™ (Figure 10).</p><p>All the cold (blue lines) and hot (red line) streams are represented by horizontal lines. The entrance and exit temperatures are shown at either end. The vertical line in the middle represents the pinch temperature. The circles represent heat exchangers. Unconnected circles represent exchangers using utility heating and cooling.</p><p>The design of a network is based on certain guidelines like the "CP Inequality Rule", "Stream Splitting", "Driving Force Plot" and "Remaining Problem Analysis". The stepwise procedure can be understood better with the help of an example problem.</p><p>Having made all the possible matches, the two designs above and below the pinch are then brought together and usually refined to further minimize the capital cost. After the network has been designed according to the pinch rules, it can be further subjected to energy optimization. Optimizing the network involves both topological and parametric changes of the initial design in order to minimize the total cost.</p><p class="h1header">Benefits and Applications for Pinch Technology</p><p>One of the main advantages of Pinch Technology over conventional design methods is the ability to set energy and capital cost targets for an individual process or for an entire production site ahead of design. Therefore, in advance of identifying any projects, we know the scope for energy savings and investment requirements.</p><p class="h2header">General Process Improvements</p><p>In addition to energy conservation studies, Pinch Technology enables process engineers to achieve the following general process improvements:</p><p><span style="text-decoration: underline;">Update or Modify Process Flow Diagrams (PFDs){parse block="google_articles"}</span></p><p>Pinch quantifies the savings available by changing the process itself. It shows where process changes reduce the overall energy target, not just local energy consumption.</p><p><span style="text-decoration: underline;">Conduct Process Simulation Studies</span></p><p>Pinch replaces the old energy studies with information that can be easily updated using simulation. Such simulation studies can help avoid unnecessary capital costs by identifying energy savings with a smaller investment before the projects are implemented.</p><p><span style="text-decoration: underline;">Set Practical Targets</span></p><p>By taking into account practical constraints (difficult fluids, layout, safety, etc.), theoretical targets are modified so that they can be realistically achieved. Comparing practical with theoretical targets quantifies opportunities "lost" by constraints - a vital insight for long-term development.</p><p><span style="text-decoration: underline;">Debottlenecking</span></p><p>Pinch Analysis, when specifically applied to debottlenecking studies, can lead to the following benefits compared to a conventional revamp:</p><ul><li>Reduction in capital costs</li><li>Decrease in specific energy demand giving a more competitive production facility</li></ul><p>For example, debottlenecking of distillation columns by Column Targeting can be used to identify less expensive alternatives to column retraying or installation of a new column.</p><p><span style="text-decoration: underline;">Determine Opportunities for Combined Heat and Power (CHP) Generation</span></p><p>A well-designed CHP system significantly reduces power costs. Pinch shows the best type of CHP system that matches the inherent thermodynamic opportunities on the site. Unnecessary investments and operating costs can be avoided by sizing plants to supply energy that takes heat recovery into consideration. Heat recovery should be optimized by Pinch Analysis before specifying CHP systems.</p><p>Decide what to do with low-grade waste heat: Pinch shows, which waste heat streams, can be recovered and lends insight into the most effective means of recovery.</p><p class="h2header">Industrial Applications</p><p>The application of Pinch Technology has resulted in significant improvements in the energy and capital efficiency of industrial facilities worldwide. It has been successfully applied in many different industries from petroleum and base chemicals to food and paper. Both continuous and batch processes have been successfully analyzed on an individual unit and site-wide basis. Pinch technology has been extensively used to capitalize on the mistakes of the past. It identifies the existence of built-in spare heat transfer areas and presents the designer with opportunities for cheap retrofits. In case of the design of new plants, Pinch Analysis has played a very important role and minimized capital costs.</p><p><span style="text-decoration: underline;">A Case Study</span></p><p>When Pennzoil was adding a residual catalytic cracking (RCC) unit, the gas plant associated with the RCC and an alkylation unit at its Atlas Refining facility in Shreveport, energy efficiency was one of their major considerations in engineering the refinery expansion. Electric Power Research Institute (EPRI) and Pennzoil's energy provider, SWEPCO, used pinch technology to carry out an optimization study of the new units and the utility systems that serve them rather than simply incorporating standard process packages provided by licensors. The pinch study identified opportunities for saving up to 23.7% of the process heating through improved heat integration. Net savings for Pennzoil were estimated at $13.7 million over 10 years.</p><p class="h1header">Future Outlook</p><p>The development of Pinch Technology started in the late 1970s and still continues. Besides applications in energy conservation, new developments in Pinch Analysis are being made in the areas of water use minimization, waste minimization, hydrogen management, plastics manufacturing, and others. A few of key areas of research are mentioned decribed below.</p><p class="h2header">Regional Energy Analysis</p><p>By examining the net energy demands of different companies combined, the potential for sharing heat between companies can be identified. These analyses can lend insight into the amount and temperature of waste heat in an industrial area that is available for export. Depending on the temperature of this waste heat, it can be used for district heating or power generation.</p><p class="h2header">Total Site Analysis</p><p>Typically, refinery and petrochemical processes operate as parts of large sites or factories. These sites have several processes serviced by a centralized utility system. There is both consumption and recovery of process steam via the steam mains. The site imports or exports power to balance the on-site power generation. The process stream heating and cooling demands, and co-generation potential, dictate the site-wide fuel demand via the utility system.{parse block="google_articles"}</p><p>In such large sites, usually the individual production processes and the central services are controlled by different departments which operate independently. The site infrastructure usually suffers from inadequate integration. To improve integration, a simultaneous approach to consider individual process issues alongside sitewide utility planning is necessary. Similar to a single process, a Total Site Analysis using Pinch Technology can be used to calculate energy targets for the entire site. For example, how much low pressure, medium pressure, and high pressure steam should the site be using? How much steam can be raised and how much power it can generate? This also helps to identify key process changes that will lower the overall site utility consumption.</p><p class="h2header">Network Pinch</p><p>When optimizing energy consumption in an existing industrial process, a number of practical constraints must be recognized. Traditional Pinch Technology focuses on new network designs. Network Pinch addresses the additional constraints in problems associated with existing facilities. This analysis identifies the heat exchanger forming the bottleneck to increasing heat recovery. Then provides a systematic approach to remove this bottleneck. This step-by-step method provides an approach for implementing energy savings in a series of consecutive projects.</p><p class="h2header">Top Level Analysis</p><p>Gathering the required data in industrial areas is not an easy task. With a Top Level Analysis, only efficiencies and constraints of the utility system are used to determine which utility is worth saving. Data can be gathered from those processes or units that use these utilities. A pinch analysis can then be performed on this equipment.</p><p class="h2header">Optimization of Combined Heat and Power</p><p>Typically, multiple steam turbines are used in complex steam systems. CHP optimization gives a way to determine the load distribution in a network of turbines with a given total load.</p><p class="h2header">Water Pinch</p><p>In view of rising fresh water costs and more stringent discharge regulations, Pinch Analysis is helping companies to systematically minimize freshwater and wastewater volumes. Water Pinch is a systematic technique for analyzing water networks and reducing water costs for processes. It uses advanced algorithms to identify and optimize the best water reuse, regeneration, and effluent treatment opportunities. It has also helped to reduce losses of both feedstock and valuable products in effluent streams.</p><p class="h2header">Hydrogen Pinch</p><p>The Pinch Technology approach applied to hydrogen management is called Hydrogen Pinch. Hydrogen Pinch enables a designer to set targets for the minimum hydrogen plant production and/or imports without the need for any process design. Methods have also been developed for the design of hydrogen distribution networks in order to achieve the targets. Hydrogen Pinch also lends insight into the effective use of hydrogen purification units.</p><p class="h1header">Conclusions</p><p>With all of the tools that pinch analysis provides, one of the most important challenges before process engineers is to properly integrate pinch tools into the conceptual process design phase. Decisions made in this phase of planning affect the entire life cycle of a process facility. Using pinch technology tools and understanding the process does not ensure the desired results. These tools must be applied at the right point in the process design phase. Just as it would be incorrect to conduct a Pinch Analysis after completion of the process design phase, wherein critical process parameters have been fixed, it is just as incorrect to conduct a Pinch Analysis without direct interaction with the process specialists and downstream engineering disciplines. It is Pinch Technology's role to identify "what might be". However, input from other engineering disciplines ultimately determines "what can be".{parse block="google_articles"}</p><p class="h1header">References</p><ol><li>General Process Improvements Through Pinch Technology, B. Linnhoff and G.T.Polley, Univ of Manchaster, U.K and V.Sahdev, Linnhoff March Ltd., U.K., Chemical Engineering Progress, June 1988</li><li>Pinch Technology Has Come of Age, B. Linnhoff, Univ of Manchaster, U.K, Don R.Vredeveld, Union Carbide Corp., Chemical Engineering Progress, July 1984</li><li>Don't let the Pinch Pinch You, Polley G.T. & Heggs P.J.,Â Chemical Engineering Progress, December, 1999</li><li>Practical Process Integration - An Introduction to Pinch Technology, By Su Ahmad, Ph.D, Stephen G. Hall, Ph.D, Steve W. Morgan, and Stuart J. Parker, Ph.D, Aspen Technology, Inc.</li><li>B. Linnhoff and J. R. Flower, AIChEJ. 24, (4), pp 633-642, July, (1978).</li></ol>]]></description>
		<pubDate>Mon, 08 Nov 2010 18:50:19 +0000</pubDate>
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		<title>Plate Heat Exchangers: Preliminary Design</title>
		<link>http://www.cheresources.com/content/articles/heat-transfer/plate-heat-exchangers-preliminary-design</link>
		<description><![CDATA[<p>Numerous articles have been published regarding the advantages of compact heat exchangers. Briefly, their higher heat transfer coefficients, compact size, ease of service, cost effectiveness, and their unique ability to handle fouling fluids make compact exchangers a good choice for many services.</p><br />
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<p class="h1header">A Quick Look at the Basics</p><p>Plate heat exchangers consist of pressed, corrugated metal plates fitted between a thick, carbon steel frame. Each plate flow channel is sealed with a gasket, a weld, or an alternating combination of the two. It is not uncommon for plate and frame heat exchangers to have overall heat transfer coefficient that are 3-4 times those found in shell and tube heat exchangers.</p><p> </p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/plate_frame_heat_exchangers1.gif" alt="plate_frame_heat_exchangers1" width="331" height="90" /></td><td class="equationnumber" align="right">Eq. (1)</td></tr></tbody></table><br />
<p class="h1header">Specifying a Plate and Frame Heat Exchanger</p><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Parts Structure for a Plate Heat Exchanger" href="../../../../invision/uploads/images/articles/plate_frame_heat_exchangers2.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_plate_frame_heat_exchangers2.gif" alt="plate_frame_heat_exchangers2" width="150" height="94" /></a></td></tr><tr><td>Figure 1: Parts Structure for a<br />
Plate Heat Exchanger</td></tr></tbody></table><p>Engineers often fail to realize the differences between heat transfer technologies when preparing a specification. This specification is then sent to vendors of different types of heat exchangers. Consider the following example:</p><p>A process stream requires C276 material to guard against corrosion. The stream needs to be cooled with cooling water before being sent to storage. The metallurgy makes the process stream an immediate candidate for the tubeside of a shell and tube heat exchanger. The cooling water is available at 80 Â°F and must be returned at a temperature no higher than 115 Â°F. The process engineer realizes that with the water flow being placed on the shellside, larger flowrates will enhance the heat transfer coefficient. The basis for the heat exchanger quotation was specified as follows:</p><table class="datatable" border="0" align="center"><caption>Table 1: Data for Example Illustration</caption><tbody><tr><td> </td><td><strong>Tubeside</strong></td><td><strong>Shellside</strong></td></tr><tr><td>Flow Rate (GPM)</td><td>500</td><td>1800</td></tr><tr><td>Temperature In (Â°F)</td><td>280</td><td>80</td></tr><tr><td>Temperature Out (Â°F)</td><td>150</td><td>92</td></tr><tr><td>Allowable Pressure<br />
Drop (psig)</td><td>15</td><td>15</td></tr></tbody></table><p>According to the engineer's calculations, these basic parameters should provide a good shell and tube design with a minimum amount of C276 material (an expensive alloy). The completed specification sheet is forwarded to many manufacturers, including those that could easily quote plate and frame or another compact technology. A typical plate and frame unit designed to meet this specification would have about 650 ft<sup>2</sup> of area compared to about 420 ft<sup>2</sup> for a shell and tube exchanger. A plate and frame unit designed to the above specification is limited by the allowable pressure drop on the cooling water. If the cooling water flow is reduced to 655 GPM and the outlet water temperature allowed to rise to 115 Â°F, the plate and frame heat exchanger would contain about 185 ft<sup>2</sup> of area. The unit is smaller, less expensive, and uses less water. The load being transferred to the cooling tower is the same.</p><p>The theory that applied to the shell and tube heat exchanger (increasing water flow will minimize heat transfer area), works in exactly the opposite direction for compact technologies. The larger water flow actually drives the cost of the unit upward. Rather than supplying a rigid specification to all heat exchanger manufacturers, the engineer should have explained his goal in regards to the process stream. Then he could have stated the following:</p><p class="blockquote_j"><p>The process stream is to be cooled with cooling water. Up to 2000 GPM of water is available at 80 Â°F. The maximum return temperature is 115 Â°F.</p><p>This simple statement could result in vastly different configurations when compared with the designs that would result from the original specification.</p><p class="h1header">Design Charts for Plate and Frame Heat Exchangers</p><p>Often, in compact heat transfer technology, engineers find themselves at the mercy of the manufacturers of the equipment. For example, limited literature correlations are available to help in the preliminary design of plate and frame heat exchangers. We will introduce a series of charts that can be used for performing preliminary sizing of plate and frame exchangers. After introducing the charts, we will follow with examples to help clarify the use of the charts. The following should be noted regarding the use of the charts:</p><ol><li>These charts are valid for single pass units with 0.50 mm thick plates. The accuracy of the charts will not be compromised for most materials of construction.</li><li>Wetted material thermal conductivity is taken as 8.67 Btu/h ft Â°F (value for SS)</li><li>Heat transfer correlations are valid for single phase, liquid-liquid designs</li><li>The following physical properties were used for the basis:<br />
<table class="datatable" border="0" align="center"><caption>Table 2: Physical Property Data Used for Chart Construction</caption><tbody><tr><td> </td><td>Hydrocarbon-<br />
Based Fluids</td><td>Water-<br />
Based Fluids</td></tr><tr><td>Thermal Conductivity<br />
(Btu/h ft<sup>2</sup> Â°F)</td><td>0.06</td><td>0.33</td></tr><tr><td>Density (lb/ft<sup>3</sup>)</td><td>55</td><td>62</td></tr><tr><td>Heat Capacity<br />
(Btu/lb Â°F)</td><td>0.85</td><td>0.85</td></tr></tbody></table></li><li>Degree of accuracy should be within Â± 15% of the service value for the overall heat transfer coefficient, assuming a nominal 10% excess heat transfer area.</li><li>For fluids with viscosities between 100 and 500 cP, used the 100 cP line of the graphs.  For fluids in excess of 500 cP, consult with manufacturers.</li></ol><span class="download"><p><a href="../../../../invision/files/file/15-preliminary-design-charts-for-plate-heat-exchangers/">Download these design charts in MS Excel format from our File Repository.</a></p></span><table class="imagecaption" border="0" align="center"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="Heat Transfer Data for 0.25 < NTU < 2.0 for Plate and Frame Heat Exchangers, Water Based Properties" href="../../../../invision/uploads/images/articles/plate_frame_heat_exchangers3.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_plate_frame_heat_exchangers3.gif" alt="plate_frame_heat_exchangers3" width="150" height="102" /></a></td><td> </td><td><a class='resized_img' rel='lightbox[2]' title="Heat Transfer Data for 2.0 < NTU < 4.0 for Plate and Frame Heat Exchangers, Water Based Properties" href="../../../../invision/uploads/images/articles/plate_frame_heat_exchangers5.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_plate_frame_heat_exchangers5.gif" alt="plate_frame_heat_exchangers5" width="150" height="102" /></a></td><td> </td><td><a class='resized_img' rel='lightbox[2]' title="Heat Transfer Data for 4.0 < NTU < 5.0 for Plate and Frame Heat Exchangers, Water Based Properties" href="../../../../invision/uploads/images/articles/plate_frame_heat_exchangers7.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_plate_frame_heat_exchangers7.gif" alt="plate_frame_heat_exchangers7" width="150" height="102" /></a></td></tr><tr><td>Figure 2: Heat Transfer<br />
Data for 0.25 < NTU < 2.0<br />
for Plate and Frame<br />
Heat Exchangers,<br />
Water Based Properties</td><td> </td><td>Figure 3: Heat Transfer<br />
Data for 2.0 < NTU < 4.0<br />
for Plate and Frame<br />
Heat Exchangers,<br />
Water Based Properties</td><td> </td><td>Figure 4: Heat Transfer<br />
Data for 4.0 < NTU < 5.0<br />
for Plate and Frame<br />
Heat Exchangers,<br />
Water Based Properties</td></tr><tr><td> </td><td> </td><td> </td><td> </td><td> </td></tr><tr><td><a class='resized_img' rel='lightbox[2]' title="Heat Transfer Data for 0.25 < NTU < 2.0 for Plate and Frame Heat Exchangers, Hydrocarbon Based Properties" href="../../../../invision/uploads/images/articles/plate_frame_heat_exchangers4.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_plate_frame_heat_exchangers4.gif" alt="plate_frame_heat_exchangers4" width="150" height="102" /></a></td><td> </td><td><a class='resized_img' rel='lightbox[2]' title="Heat Transfer Data for 2.0 < NTU < 4.0 for Plate and Frame Heat Exchangers, Hydrocarbon Based Properties" href="../../../../invision/uploads/images/articles/plate_frame_heat_exchangers6.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_plate_frame_heat_exchangers6.gif" alt="plate_frame_heat_exchangers6" width="150" height="102" /></a></td><td> </td><td><a class='resized_img' rel='lightbox[2]' title="Heat Transfer Data for 4.0 < NTU < 5.0 for Plate and Frame Heat Exchangers, Hydrocarbon Based Properties" href="../../../../invision/uploads/images/articles/plate_frame_heat_exchangers8.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_plate_frame_heat_exchangers8.gif" alt="plate_frame_heat_exchangers8" width="150" height="102" /></a></td></tr><tr><td>Figure 5: Heat Transfer<br />
Data for 0.25 < NTU < 2.0<br />
for Plate and Frame<br />
Heat Exchangers,<br />
Hydrocarbon Based Properties</td><td> </td><td>Figure 6: Heat Transfer<br />
Data for 2.0 < NTU < 4.0<br />
for Plate and Frame<br />
Heat Exchangers,<br />
Hydrocarbon Based Properties</td><td> </td><td>Figure 7: Heat Transfer<br />
Data for 4.0 < NTU < 5.0<br />
for Plate and Frame<br />
Heat Exchangers,<br />
Hydrocarbon Based Properties</td></tr></tbody></table><p class="h2header">Example Problem</p><p>Consider the following example:</p><p><img style="float: left;" src="../../../../invision/uploads/images/articles/thumbnails/plate_frame_heat_exchangers9.gif" alt="plate_frame_heat_exchangers9" width="249" height="177" />150,000 lb/h of SAE 30 oil is being cooled from 200 Â°F to 175 Â°F by 75,000 lb/h of water.   The water enters the exchanger at 60 Â°F and leaves at 168 Â°F.  The average viscosity of the water passing through the unit is 0.33 cP and the average viscosity of the oil in the unit is 215 cP.  The maximum allowable pressure drop through the plate heat exchanger is 15 psig on the hot and cold sides.</p><p><strong>Step 1: Calculate the LMTD</strong></p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/thumbnails/plate_frame_heat_exchangers10.gif" alt="plate_frame_heat_exchangers10" width="401" height="180" /></td><td class="equationnumber" align="right">Eq. (2)</td></tr></tbody></table><p><strong>Step 2: Calculate NTU<sub>HOT</sub> and NTU<sub>COLD</sub></strong></p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/thumbnails/plate_frame_heat_exchangers11.gif" alt="plate_frame_heat_exchangers11" width="569" height="142" /></td><td class="equationnumber" align="right">Eq. (3)</td></tr></tbody></table><p><strong>Step 3: Read h<sub>Hot</sub> from 0.25 < NTU < 2.0 chart for hydrocarbons</strong></p><p>Although is there not a viscosity line for 215 cP, the line representing "100 cP" can be or viscosities up to about 400-500 cP.  The heat exchanger will be pressure drop limited and the heat transfer coefficient will not change appreciably over this viscosity range for plate and frame exchangers.  Reading from the chart, a pressure drop of 15 psig corresponds to h<sub>Hot</sub> @ 50 Btu/h ft<sup>2</sup> Â°F.</p><p><strong>Step 4: Read h<sub>Cold</sub> from 0.25 < NTU < 2.0 chart for water based liquids</strong></p><p>Again, you will note that the exact viscosity line needed for pure water (0.33 cP) in this case is not available.  However, the "1.0 cP" line on the chart will provide a very good estimate of the heat transfer coefficient that pure water will exhibit.  Reading from the chart, a pressure drop of 15 psig corresponds to h<sub>Cold</sub> @ 3000 Btu/h ft<sup>2</sup> Â°F.</p><p><strong>Step 5:  Calculate the Overall Heat Transfer Coefficient (OHTC)</strong></p><p>Assume a stainless steel plate with a thickness of 0.50 mm is being used.  316 stainless steel has a thermal conductivity of 8.67 Btu/h ft Â°F.</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/plate_frame_heat_exchangers12.gif" alt="plate_frame_heat_exchangers12" width="332" height="157" /></td><td class="equationnumber" align="right">Eq. (4)</td></tr></tbody></table><p><br />
<span class="h2header">Another Example</span></p><p><span class="h2header"> </span><img style="float: left;" src="../../../../invision/uploads/images/articles/plate_frame_heat_exchangers13.gif" alt="plate_frame_heat_exchangers13" width="313" height="219" />150,000 lb/h of water is being cooled from 200 Â°Â°F by 150,000 lb/h of NaCl brine. The brine enters the exchanger at 50 Â°F and leaves at 171 Â°F. The average viscosity of the water passing through the unit is 0.46 cP and the average viscosity of the brine in the unit is 1.10 cP. The maximum allowable pressure drop through the plate heat exchanger is 10 psig on the hot (water) side and 20 psig on the cold (brine) side.</p><p>As before, the LMTD is calculated to be 38.5 Â°F. NTU<sub>Hot</sub> and NTU<sub>Cold</sub> are calculated as 2.59 and 3.14 respectively. Reading hHot and hCold from the chart for 2.0 < NTU < 4.0 (water based), gives about 2000 Btu/h ft<sup>2</sup> Â°F and 2500 Btu/h ft<sup>2</sup> Â°F respectively. Although the material of choice may be Titanium or Palladium stabilized Titanium, we will use the properties for stainless steel for our preliminary sizing. Calculating the OHTC as before yields 918 Btu/h ft<sup>2</sup> Â°F.</p><p class="h1header">Implications for Size Reduction</p><p>We have seen that alternative technologies have significant size advantage over shell-and-tube heat exchangers. Now let's consider the implications of this. The first advantage is smaller plot plan for the process plant. The spacing between process equipment can be reduced. So, if the plant is to be housed in a building, the size of the building can be reduced. In any event, the amount of structural steel used to support the plant can be reduced and given the weight saving, the load on that structure is also reduced. The weight advantage extends to the design of the foundations used to support the plant.</p><p>Since, the spacing between individual equipment items is reduced, expenditure on piping is reduced.  Once more we stress the savings associated with size and weight reduction can only be achieved if these advantages are recognized at the earliest stages of the plant design.{parse block="google_articles"}</p><p>As we will briefly show, the use of alternative exchanger technologies can result in significant reduction in plant complexity. This not only enforces the savings associated with reduced size and weight (reduced plot space, structural cost savings, piping cost reduction etc.) but also has safety implications. The simpler the plant structure the easier it is for the process operator to understand the plant. The simpler the plant structure, the safer, easier and more straight forward the plant maintenance (the fewer the pipe branches that must be blanked etc.).</p><p>The alternative technologies result in reduced complexity by reducing the number of heat exchangers. This is achieved through:</p><ul><li>improved 'thermal contacting'</li><li>multi-streaming.</li></ul><p>Mechanical constraints play a significant role in the design of shell-and-tube heat exchangers. For instance, it is common to find that some users place restrictions on the length of the tubes used in such a unit. Such a restriction can have important implications for the design. In the case of exchangers requiring large surface areas the restriction drives the design towards large tube counts. If such tube counts then lead to low tube side velocity, the designer is tempted to increase the number of tube side passes in order to maintain a reasonable tube-side heat transfer coefficient.</p><p>Thermal expansion considerations can also lead the designer to opt for multiple tube passes for the cost of a floating head is generally lower than the cost of installing an expansion bellows in the exchanger shell.</p><p>The use of multiple tube passes has four detrimental effects. First, it leads to a reduction in the number of tubes that can be accommodated in a given size of shell (so it leads to increased shell diameter and cost). Second, for bundles having more than four tube passes, the pass partition lanes introduced into the bundle give rise to an  increase in the quantity of shell-side fluid bypassing the tube bundle and a reduction in tube-side heat transfer coefficient. Thirdly, it gives rise to wasted tube side pressure drop in the return headers. Finally, and most significantly, the use of multiple tube passes results in the thermal contacting of the streams not being pure counter-flow. This has two effects. The first is that the Effective Mean Temperature Driving Force is reduced. The second, and more serious effect, is that a 'temperature cross' can occur.</p><p>If a 'temperature cross' occurs, the designer must split the duty between a number of individual heat exchangers arranged in series.  Figures 8 and 9 below illustrate the difference between temperatures that are said to be 'crossing' and those that are not.</p><p>Many of the alternative heat exchanger technologies allow the application of pure counter-flow across all size and flow ranges. The results are better use of available temperature driving force and the use of single heat exchangers.</p><table class="imagecaption" border="0" align="center"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="No Temperature Cross" href="../../../../invision/uploads/images/articles/plate_frame_heat_exchangers14.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_plate_frame_heat_exchangers14.gif" alt="plate_frame_heat_exchangers14" width="150" height="108" /></a></td><td> </td><td><a class='resized_img' rel='lightbox[2]' title="Deep Temperature Cross" href="../../../../invision/uploads/images/articles/plate_frame_heat_exchangers15.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_plate_frame_heat_exchangers15.gif" alt="plate_frame_heat_exchangers15" width="150" height="104" /></a></td></tr><tr><td>Figure 8: No Temerature<br />
Cross</td><td> </td><td>Figure 9: Deep Temperature<br />
Cross</td></tr></tbody></table><p>Let's now consider multi-streaming. The traditional shell-and-tube heat exchanger only handles one hot and one cold stream. Some heat exchanger technologies (most notably plate-fin and printed circuit exchangers) can handle many streams. It is not uncommon to find plate-fin heat exchangers transferring heat between ten individual process.  Such units can be considered to contain a whole heat exchanger network within the body of a single exchanger. Distribution and recombination of process flows is undertaken inside the exchanger. The result is a major saving in piping cost.</p><p>Engineers often over-look the opportunities of using a plate and frame unit as a multi-stream unit. (Again, this will be a regular oversight if exchanger selection is not made until after the flow sheet has been developed).</p><p>A good example of multi-streaming is the use of a plate heat exchanger serving as a process interchanger on one side and a trim cooler on the other.   This arrangement is particularly useful for product streams that are exiting a process and must be cooled for storage.  Another popular function of multi-streaming is in lowering material costs.  Often times, once streams are cooled to a certain temperature, they pose much less of a corrosion risk.   Half of the exchanger can contain a higher alloy, while the other side can utilize stainless steel or a lower alloy.</p><p>In Figure 10 we show how a plate and frame unit has been applied to a problem involving three process streams. The heat transfer properties used for styrene are given in Table 3.  Just one unit is used and this unit has 1,335 sq.ft. of effective surface area.</p><p>In Figure 11 we show the equivalent shell-and-tube solution. In order to avoid temperature crosses we need six individual exchangers: the cooler having two shells in series (each having 1,440 sq.ft of effective surface); the heat recovery unit having four shells in series (each having 2,116 sq.ft. of surface).</p><p>So, our plate-and-frame design involves the use of 1,335 sq.ft. of surface in a single unit. The equivalent shell-and-tube design has 11,344 sq.ft. of surface distributed across four separate exchangers.</p><table class="imagecaption" border="0" align="center"><tbody><tr><td><a class='resized_img' rel='lightbox[2]' title="A multi-stream plate exchanger serving as an interchanger and a trim cooler" href="../../../../invision/uploads/images/articles/plate_frame_heat_exchangers16.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_plate_frame_heat_exchangers16.gif" alt="plate_frame_heat_exchangers16" width="150" height="43" /></a></td><td> </td><td><a class='resized_img' rel='lightbox[2]' title="Equivalent Shell and Tube Design" href="../../../../invision/uploads/images/articles/plate_frame_heat_exchangers17.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_plate_frame_heat_exchangers17.gif" alt="plate_frame_heat_exchangers17" width="150" height="111" /></a></td></tr><tr><td>Figure 10: A Multi-Stream<br />
Plate Exchanger Serving as an<br />
Interchanger and a Trim Cooler</td><td> </td><td>Figure 11: Equivalent Shell and<br />
Tube Design</td></tr></tbody></table><p> </p><table class="datatable" border="0" align="center"><caption>Table 3: Heat Transfer Properties Used for Styrene in the Multi-Stream Example</caption><tbody><tr><td> </td><td><strong>100 Â°F</strong></td><td><strong>150 Â°F</strong></td><td><strong>200 Â°F</strong></td></tr><tr><td>Density (lb/ft<sup>3</sup>)</td><td>55.5</td><td>53.9</td><td>52.3</td></tr><tr><td>Specific Heat<br />
(Btu/lb Â°F)</td><td>0.427</td><td>0.447</td><td>0.471</td></tr><tr><td>Viscosity (cP)</td><td>0.590</td><td>0.428</td><td>0.329</td></tr><tr><td>Thermal<br />
Conductivity<br />
(Btu/h ft Â°F)</td><td>0.077</td><td>0.074</td><td>0.070</td></tr><tr><td colspan="4">Data from PhysPropsÂ© by G.P. Engineering, Version 1.5.0</td></tr></tbody></table>]]></description>
		<pubDate>Mon, 08 Nov 2010 18:50:19 +0000</pubDate>
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		<title>Specifying  A Liquid-Liquid Heat Exchanger</title>
		<link>http://www.cheresources.com/content/articles/heat-transfer/specifying-a-liquid-liquid-heat-exchanger</link>
		<description><![CDATA[<p>As an engineer, specifying heat exchangers for procurement is an important step in the successful execution of any heat transfer or energy conservation project. Early recognition that there are many different heat transfer technologies available can help in receiving optimized bids for each type of equipment available to you. Through process investigation, the specifying engineer can collect the necessary data to allow the heat exchanger designer to optimize both the mechanical and thermodynamic design of the heat exchanger. Through the specification process, you can uncover critical variables such solids loading, heat transfer duty requirements, available footprint space, maintenance considerations, and others.</p><p class="h1header">Heat Transfer Resources</p><p>Although most engineers who are asked to specify a heat exchanger may have the appropriate background in heat transfer knowledge, there are cases when the engineer could benefit from a refresher on the basics of heat transfer and the equipment types involved. Here are some resources that will help you review the basics of industrial heat transfer:</p>{parse block="google_articles"}<p>Industrial Heat Transfer Basics:<br />
<a href="http://www.cheresources.com/heat_transfer_basics.shtml" target="_blank">http://www.cheresources.com/heat_transfer_basics.shtml</a></p><p>Design Considerations for Shell and Tube Exchangers<br />
<a href="http://www.cheresources.com/designexzz.shtml" target="_blank">http://www.cheresources.com/designexzz.shtml</a></p><p>Overall Heat Transfer Coefficients in Heat Exchangers<br />
<a href="http://www.cheresources.com/uexchangers.shtml" target="_blank">http://www.cheresources.com/uexchangers.shtml</a></p><p>Correlations for Convective Heat Transfer<br />
<a href="http://www.cheresources.com/convection.shtml" target="_blank">http://www.cheresources.com/convection.shtml</a></p><p>Shell and Tube Heat Exchanger Design Manual<br />
<a href="http://www.wlv.com/products/databook/databook.pdf" target="_blank">http://www.wlv.com/products/databook/databook.pdf</a></p><p class="h1header">Recognizing and Evaluating the Duty Requirements</p><p>The first step in specifying any heat exchanger is to properly evaluate and identify the necessary heat transfer duty requirements. In other words, "what do you need the exchanger to do once it's installed?"Â</p><p>A useful tool in evaluating heat transfer duty requirements is the T-Q diagram. This visual tool can help the specifying engineer easily determine what is possible in a given heat exchanger.   Let's begin with a simple example.</p><p class="blockquote_j">Due to a process change, one of the plant's main products is exiting the process unit 30 Â°F higher than before. Sending the product to the storage tank at this elevated temperature may cause safety concerns. As the plant engineer, you've been tasked with specifying a product cooler for this new requirement. The total product stream flow rate is 500,000 lb/h</p><p>Previously, the product stream was sent to storage at approximately 130 Â°F.   Now, it's exiting the processing unit at 160 Â°F. The new product cooler must be able to cool the product stream back down to 130 Â°F for safe operation.   The product stream has physical properties that are very close to those of phenol. For the initial heat balance examination, we'll check the heat capacity of phenol at the midpoint of the cooling duty which is 145 Â°F to get an average heat capacity through the exchanger. At 145 Â°F, the heat capacity of phenol is reported as 0.529 Btu/lb Â°F. Using the following equations:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/shell_tube_heat_exchanger_1_Eqn1.gif" alt="shell_tube_heat_exchanger_1_Eqn1" width="225" height="30" /></td><td class="equationnumber" align="right">Eq. (1)</td></tr></tbody></table><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/shell_tube_heat_exchanger_1_Eqn2.gif" alt="shell_tube_heat_exchanger_1_Eqn2" width="218" height="30" /></td><td class="equationnumber" align="right">Eq. (2)</td></tr></tbody></table><p>Where:</p><p>Q = heat transferred in thermal unit per time (Btu/h or kW)<br />
M = mass flow rate<br />
T = temperature<br />
Cp = heat capacity or specific heat of fluid<br />
Subscript "H"Â = hot fluid<br />
Subscript "C"Â = cold fluid</p><p>Solving Equation 1, we find that the heat transfer duty is:</p><p>Q<sub>H</sub> = (500,000 lb/h) x (0.529 Btu/lb Â°F) x (160 - 130 Â°F) = 7,935,000 Btu/h</p><p>Now, we make the following assumption:</p><ol><li>The heat capacity of the cooling tower water is 1.0 Btu/lb Â°F </li><li>Cooling tower water is available at 88 Â°F during the warmest summer month </li><li>Q<sub>H</sub> = Q<sub>C</sub> (perfect heat transfer, a typical assumption) </li><li>The tower water can undergo a 20 Â°F temperature rise in the exchanger </li></ol><p>Then, we solve Equation 2 for m<sub>C</sub>.</p><p>m<sub>C</sub> = (7,935,000 Btu/h) / (1.0 Btu/lb Â°F x 20 Â°F) = 396,750 lb/h</p><p>This is converted to gallon per minute as follows:</p><p>(396,740 lb/h) / (8.27 lb/gal) / (60 min/h) = 800 GPM (nearly a factor of 500, actually 496)</p><p>Now, we can construct our T-Q diagram for our system:</p><table class="imagecaption" border="0" align="left"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/shell_tube_heat_exchanger_1_Image1.gif" alt="shell_tube_heat_exchanger_1_Image1" width="340" height="265" /></td></tr><tr><td>Figure 1: T-Q Diagram for the<br />
First Example</td></tr></tbody></table><p>Now, we have the basis for what our heat exchanger needs to perform and we've begun to identify the utility requirements for the duty. At this time, we need to note of couple of items. Firstly, as defined, our heat exchanger may require as much as 800 GPM of cooling tower water to perform the cooling task. An investigation should be made to determine if 800 GPM of cooling tower water is actually available. If not, the duty must be re-examined. In this situation, the engineer finds that he has up to 1000 GPM of water available, so this will not be a concern.</p><p>Secondly, we note that our duty does not contain any thermodynamic violations and it does not contain a temperature cross. There are two cases are illustrated below in Figure 2:</p><p> </p><table class="imagecaption" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/shell_tube_heat_exchanger_1_Image2.gif" alt="shell_tube_heat_exchanger_1_Image2" width="244" height="287" /></td><td> </td><td><img src="../../../../invision/uploads/images/articles/shell_tube_heat_exchanger_1_Image3.gif" alt="shell_tube_heat_exchanger_1_Image3" width="343" height="297" /></td></tr><tr><td>Figure 2: T-Q Diagram<br />
Showing a Violation</td><td> </td><td>Figure 3: T-Q Diagram<br />
Showing a Temperature Cross</td></tr></tbody></table><p>Notice the T-Q diagram that shows a thermodynamic violation. The cold side is being heated to a temperature that is above the inlet temperature of the hot side. Suppose that in our example, the engineer found that there were only 100 GPM of water available. His analysis would have shown the water would have exited the exchanger far above the 160 Â°F hot side inlet temperature. In short, this is not enough water to accomplish the duty. At that point, he would have to investigate other utility options.</p><p>In the second image above, the T-Q diagram shows what is know as a temperature cross. The cold side outlet temperature is higher than the hot side outlet temperature. It's important to note whether or not your duty contains a temperature cross as it will have a significant impact on the type and number of heat exchangers that may be required to perform the duty.</p><p>As the engineer is examining a new heat transfer duty, the concept of NTU or Number of Transfer Units should be used to help guide the specification. A good rule of thumb is that a single shell and tube heat exchanger should be designed with a minimum temperature approach of 10 Â°F. The "temperature approach"Â is defined as the temperature difference between the hot side outlet temperature and the cold side outlet temperature. In our example above, the approach temperature is 130 Â°F-108Â°F = 22 Â°F. This duty can easily be accomplished in a single shell and tube heat exchanger.</p><p>Now, consider the following duty shown in "Duty 2"Â above. This unit has a deep "temperature cross"Â. This is where the concept of NTU can be helpful. For Duty 2 above (Figure 3), we calculate the NTU for the hot side and the cold side as follows:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/shell_tube_heat_exchanger_1_Eqn6.gif" alt="shell_tube_heat_exchanger_1_Eqn6" width="277" height="61" /></td><td class="equationnumber" align="right">Eq. (3)</td></tr></tbody></table><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/shell_tube_heat_exchanger_1_Eqn7.gif" alt="shell_tube_heat_exchanger_1_Eqn7" width="278" height="67" /></td><td class="equationnumber" align="right">Eq. (4)</td></tr></tbody></table><br />
<table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/shell_tube_heat_exchanger_1_Eqn8.gif" alt="shell_tube_heat_exchanger_1_Eqn8" width="396" height="91" /></td><td class="equationnumber" align="right">Eq. (5)</td></tr></tbody></table><p>LMTD = 39.15 Â°F<br />
NTU<sub>HOT</sub> = 150 / 39.15 = 3.83<br />
NTU<sub>COLD</sub> = 170 / 39.15 = 4.34</p><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]'title="Shell and Tube Heat Exchanger Flow Pattern" href="../../../../invision/uploads/images/articles/shell_tube_heat_exchanger_1_Image5.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumb_shell_tube_heat_exchanger_1_Image5.gif" alt="shell_tube_heat_exchanger_1_Image5" width="150" height="79" /></a></td></tr><tr><td>Figure 4: Shell and Tube Heat<br />
Exchanger Flow Pattern</td></tr></tbody></table><p>The NTU can be translated into the approximate number of shell and tube heat exchangers in series that will be required to perform a given duty. The engineer must realize that if it is necessary to perform Duty 2 just as it is shown, it will be an expensive proposition in terms of purchased equipment costs, installation costs, and maintenance costs over the life of the shell and tube heat exchangers.</p><p>Shell and tube heat exchanger do a relatively poor job of "temperature crossing"Â due to their lack of purely countercurrent flow as shown in Figure 4.</p><p>The shell side of the exchanger is almost always baffled so that a reasonable heat transfer coefficient can be obtained. The tube side flow in this image shows a single tube pass. While this is possible, it's not very common. The tube side velocity is the key to the tube side heat transfer coefficient and the ability to mitigate fouling. For these reasons, multiple tube passes are typically used in shell and tube exchangers.   The result of these flow patterns is a lack of countercurrent flow. In fact, the LMTD or Log Mean Temperature Difference in shell and tube heat exchangers has be corrected for these flow patterns. Typically, the calculated LMTD has to be multiplied by a factor of 0.70 to 0.90 to account for the flow patterns.</p><p>If Duty 2 is required, the engineer may want to consider a heat exchanger type with truly countercurrent flow such as a pipe-in-pipe (commonly called a hairpin exchanger) or a plate heat exchanger. These devices, with their truly countercurrent flow patterns, can perform duties with temperature crosses in a single unit rather than requiring multiple units in series.</p><p>Regardless of the heat exchanger type chosen, the engineer <strong>must</strong> be aware of this scenario during the initial specification stage for the heat exchanger.</p><p>At this point, the engineer has established the basic parameters for the heat exchanger and now other factors need to be investigated prior to the specification process.</p><p class="h1header">Exploring Other Considerations in Heat Exchanger Specification</p><p>Prior to completing the heat exchanger specification data sheet, the engineer should answer questions such as:</p><ul><li><p>Are there any phase changes expected to occur in the heat exchanger?</p></li><li><p>Are there any dissolved gases in either stream?{parse block="google_articles"}</p></li><li><p>Are there any dissolved or suspended solids in either stream?</p></li><li><p>What are the operating pressures of the streams?</p></li><li><p>How much pressure loss is available in the exchanger (for existing pumps)?</p></li><li><p>What are the fouling tendencies of the fluids involved?</p></li><li><p>Are either of the fluids non-newtonian?</p></li><li><p>Are either of the fluids corrosive? What material of constructions are required?</p></li><li><p>What types of elastomers and/or compression gaskets are compatible with the fluids?</p></li><li><p>Are either of the fluids considered lethal to plant personnel?</p></li><li><p>Is mechanical cleaning expected to be necessary for one or both fluids?</p></li><li><p>Is there a cleaning solution that may be effective for the exchanger?</p></li><li><p>How much room is required for maintenance of the new exchanger?</p></li></ul><p>Having answers to these questions can help ensure that your heat exchanger specification, and ultimately the heat exchanger that you purchase, is right for your heat transfer duty.</p><p class="h2header">Phase Change</p><p>Even in liquid-liquid heat transfer duties, it's important to recognize the potential for phase changes inside the heat exchanger. For example, if a process stream is available to 350 Â°F to plant water from 100 Â°F to 300 Â°F, it's very important to note that both the inlet and outlet pressure of the plant water stream. If the water stream is not under enough pressure, it may undergo partial vaporization.   In this case, the vapor pressure of water at 300 Â°F is about 52 psig. So, for a heat exchanger with a nominal pressure loss of 10 psig, the process water should enter the exchanger at a minimum pressure of around 70 psig.</p><p class="h2header">Dissolved Gases</p><p>While not always common, there are several instances where a mostly liquid process stream may pickup dissolved gases. It's important to recognize that dissolved gases can have a profound negative impact on liquid heat transfer as the dissolved gases serve as a significant resistance to heat transfer. If you suspect that dissolved gases may be present, the best bet is to run the process stream through a separation vessel to allow for vapor disengagement prior to transferring heat to or from the stream. Trying to design for a stream with dissolved gases is very difficult and often times uneconomical. A classic example of this can often be found in the interchangers in amine units used to treat natural gases. Through the absorption column, the amine solutions can pick up significant quantities of carbon dioxide that should be removed prior to transferring heat with the amine solution.</p><p class="h2header">Dissolved and Suspended Solids</p><p>Dissolved solids can be very common in the chemical processing industry. In fact, a general rule of thumb for cooling tower water is that it should not be heated to temperatures in excess of 120 Â°F. The reason behind this guideline is that at temperatures above 120 Â°F, some of the common water treatment chemicals used in the water can quickly plate out onto heat transfer surfaces. Usually, these are carbonate salts which follow an inverse solubility curve. This means that as temperature increases, the salts actually become less soluble in water rather than more soluble as is usually the case. Inverse soluble salts can be found in other processing stream as well and are not confined only to cooling tower water.</p><p>Suspended solids can pose obvious problems for heat exchangers. Aside from the common problem of pluggage, suspended solids can also cause erosion of the heat transfer surfaces if the velocity in the heat exchanger is too high. If suspended solids are present, it's advisable to obtain a particle size distribution and chemical analysis to determine the relative hardness of the particles. For example, hard particles that range in size from a few microns to up to 0.20 mm would have to be addressed differently than a slurry of relatively soft particles such as a powdered solid. Usually, a plant will have a well documented history of what type of exchangers work well with a solid-laden stream and often times, plants will establish velocity limitations for pipelines and other processing equipment.</p><p class="h2header">Operating Pressure</p><p>Examine the operating pressures of each stream that are to enter the heat exchanger. Many companies have policies dictating that the design pressure of a process vessel must be a certain factor above the highest operating pressure. For example, if the highest operating pressure for a heat exchanger is to 100 psi, then a reasonable design pressure may be 150 psi or 200 psi. Remember, that the higher the design pressure, the more expensive the exchanger will become as the wall becomes thicker.</p><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]'title="Operating Pressure vs. Time Chart" href="../../../../invision/uploads/images/articles/thumbnails/shell_tube_heat_exchanger_1_Image4.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumbnails/thumb_shell_tube_heat_exchanger_1_Image4.gif" alt="shell_tube_heat_exchanger_1_Image4" width="150" height="107" /></a></td></tr><tr><td>Figure 5: Operating Pressure<br />
vs. Time Chart</td></tr></tbody></table><p>Additionally, give some thought to what will happen if a leak occurs within the heat exchanger. The higher pressure fluid will leak to the lower pressure fluid. For example, consider a process stream at 50 psi and cooling tower water at 75 psi.   If a leak occurs, the cooling tower water will leak into the process stream. The engineer must evaluate the consequences of such leakage and determine which fluid should be at the higher pressure.</p><p>As with any piece of chemical process equipment, it can be subject to mechanical fatigue. Consider a heat exchanger where the two streams have operating pressures that are very close to one another.   Without extreme pressure stability (which is often difficult to maintain), a run chart of the pressure versus time may look like the chart in Figure 5.</p><p>Notice how the stream can be allowed to actually cross pressures in the heat exchanger if the two streams are close in operating pressures. This scenario, if extreme enough, can cause flexing of thinner material surfaces inside of heat exchangers and lead to premature failures.</p><p class="h2header">Available Pressure Loss</p><p>If preparing to install a heat exchanger in an existing process system, the engineer should examine any pumps in the system to determine how much pressure loss is available. Generally speaking, most heat exchangers should need between 5 and 15 psi of pressure loss to operate effectively. For known fouling fluids, a higher pressure loss (corresponding to a higher velocity) will help keep the exchanger clean for a longer period of time. Also remember that pressure loss is proportional to the fluid viscosity. Specifying a pressure loss of 5 psi for a process fluid with a viscosity of 300 cP may result in a very large heat exchanger.</p><p>If your pumping system cannot handle the necessary additional pressure loss to obtain a good heat exchanger design, then an impeller change out, a new pump, or an additional pump in series may be justified.   When utilizing a shell and tube exchanger, you can expect the pressure loss on the tube side to be higher than the shell side in most cases.</p><p class="h2header">Fouling Tendencies of the Fluid</p><p>The engineer should also be aware of the fouling tendencies of the fluids involved. Through personal experience, interviews with other plant personnel, or investigation into other heat exchangers, the engineer can usually determine how quickly a particular fluid may foul an exchanger. Many plants will have a library of shell and tube fouling factors for various process duties.</p><p>Probably one of the most common errors made in specifying a new heat exchanger is overdesign. Anticipating fouling is smart, overdesigning too far however will ensure that fouling will occur. Choose your fouling coefficient carefully. Remember, that specifying too large a fouling factor will often result in more tube or parallel channels. This will lower the velocity in the exchanger and actually promote the fouling. This is a balancing act that is well worth a little time and effort.</p><p>When considering a fouling factor, it's very important to note the type of equipment that may be used in the service. Another common mistake during heat exchanger specification is to apply fouling factor information from one type of equipment to a completely different type of equipment.</p><p>Remember that shell and tube fouling factors have been compiled over decades through experience and temperature measurement. Also, realize that typical overall heat transfer coefficients for shell and tube may range from 150 to 400 Btu/h ft<sup>2</sup> Â°F while compact heat transfer technologies can easily obtain overall heat transfer coefficients ranging from 600 to 1000 Btu/h ft<sup>2</sup> Â°F. If we examine the equation:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/thumbnails/shell_tube_heat_exchanger_1_Eqn3.gif" alt="shell_tube_heat_exchanger_1_Eqn3" width="175" height="56" /></td><td class="equationnumber" align="right">Eq. (6)</td></tr></tbody></table><p> for a shell and tube exchanger and for a compact heat exchanger, we'll see how the difference can impact designs. If the engineer were to specify a fouling factor of 0.001 h ft<sup>2</sup> Â°F/Btu independent of the type of heat exchanger used, the result would look like this:</p><p><img src="../../../../invision/uploads/images/articles/thumbnails/shell_tube_heat_exchanger_1_Eqn4.gif" alt="shell_tube_heat_exchanger_1_Eqn4" width="415" height="60" /></p><p><img src="../../../../invision/uploads/images/articles/thumbnails/shell_tube_heat_exchanger_1_Eqn5.gif" alt="shell_tube_heat_exchanger_1_Eqn5" width="436" height="61" /></p><p>So, the U-value for the shell and tube went from 136 to 120 Btu/h ft<sup>2</sup> Â°F through the fouling coefficient. The U-value for the compact exchanger went from 445 to 308 Btu/h ft<sup>2</sup> Â°F through the fouling coefficient. Therefore, the shell and tube overdesign is about 12% while the compact exchanger overdesign is over 40%.</p><p>The specifying engineer must realize where the fouling factor information is derived from and apply it properly in the future. While shell and tube exchangers have long used fouling factors, compact heat exchangers generally utilize a "heat transfer margin"Â that is typically 10-25% over the clean heat transfer coefficient. This change in language was designed to avoid confusion as shown above and to bring the overdesign between the two technologies onto even ground to avoid problems. Also realize that overdesigning in compact heat exchangers is even more detrimental to performance than in a shell and tube heat exchanger.</p><p class="h2header">Non-Newtonian Fluids</p><p>While most fluids in the chemical processing industry are Newtonian in their flow behavior, some are not. In short, a Newtonian fluid is one whose viscosity in NOT dependent on the forces acting upon it (shear stress in heat exchangers), only on the fluid's temperature. Some fluid, know as being non-Newtonian, have flow characteristics such that they can actually become more or less viscous depending on the forces acting on the fluid.   Confirming that a fluid is Newtonian during the design stage can save the engineer from procuring a heat exchanger that is vastly over or under sized later.</p><p class="h2header">Corrosion Potential and Materials of Construction</p><p>Specifying materials on construction for the heat exchanger is an extremely important part of the overall process. Again, most plants have some history regarding what metals are appropriate for their process fluids. Typically, if one fluid requires a higher metallurgy than another, then that fluid is placed on the tube side of a shell and tube exchanger to minimize costs as cladding a shell can become quite expensive.</p><p>It's important to consider temperature and pH when deciding on a material of construction for your exchanger. If you're not sure what metal you need, consult with a corrosion expert as this is one aspect of heat exchanger design that no one can afford to get wrong.</p><p>If your duty does require an expensive alloy, then a compact heat exchanger may cost significantly less considering their higher overall heat transfer coefficients.   Another point to remember is that just because a fluid is compatible with a stainless steel tube for example, it may not be compatible with a stainless steel plate that has been pre-stressed (during the pressing process).   Pre-stressing of metals can make them susceptible to pitting corrosion such as chloride attack. Consult with manufacturers of compact equipment. While they will seldom take the legal responsibility for choosing a material of construction, then can point you in the right direction and save you from making a costly mistake.</p><p class="h2header">Elastomer and Compreesion Gasket Compatibility</p><p>Depending on the type of heat transfer technology that is being considered for the application, a check of gasket compatibility may be required. Elastomer gaskets are most commonly offered in materials such as EPDM, Nitrile, PTFE, and FKMG (a generic form of Viton-G from Dupont). Elastomer gaskets can seldom be rated for temperatures in excess of 320 Â°F. Generally speaking, the engineer should seek a recommendation from the heat exchanger manufacturer as they usually have extensive databases that show the best gasket choice for a given application.</p><p>For compression gaskets, such as those used on the heads of shell and tube exchangers, there are a couple of rules of thumb to keep in mind. In addition to the need for the gasket to be compatible with the process or service fluid, the engineer may need to decide between a metallic or non-metallic compression gasket. Consider this guideline:</p><table class="datatable_inset" border="0" align="center"><tbody><tr><td><p><em>Find the value of : Operating Pressure (psig) x Operating Temperature (Â°F)</em></p><p><em>If this value exceeds 250,000, the use of a metallic gasket should be strongly considered. Additionally, non-metallic gaskets are seldom used at pressures in excess of 1200 psig and temperatures in excess of 850 Â°F.</em></p></td></tr></tbody></table><p class="h2header">Lethal Service Requirements</p><p>The ASME pressure vessel code stipulates very specific pressure vessel requirements for heat transfer service that are qualified as "lethal"Â. If the service requires an ASME "L"Â stamp, be sure to specify this to the heat exchanger manufacturer.</p><p class="h2header">Cleaning Considerations</p><p>Some process fluids can leave fouling deposits that can be especially difficult to remove. Sometimes, these deposits can be removed by chemical cleaning. Chemical cleaning of heat exchangers, in general, is popular in industries that utilize sanitary protocols (food, pharmaceutical, etc.) and chemical cleaning is widely accepted in the chemical process industry in Europe. Chemical cleaning requires additional equipment, cleaning chemical, and a method of disposing of the chemical cleaning agent. Chemical cleaning can be a good choice in the following instances:</p><ol><li>The fouling deposit can be easily dissolved and removed by a readily available cleaning agent. </li><li>The heat exchanger fouls quickly and must be cleaned fairly often (4 or more times a year) </li><li>The heat exchanger to be cleaned has a relatively small hold up volume so that chemical cleaning equipment and the volume of cleaning agents can be minimized. </li></ol><p>For heat transfer duties where chemical cleaning does not seem like the best choice, the engineer must be sure that the fouling fluid is placed on a side of the heat exchanger that is readily accessible for mechanical cleaning. Mechanical cleaning usually consists of a high pressure water spray of the affect area, although additional scraping can sometimes be necessary. Floating head shell and tube heat exchangers, gasketed plate exchangers, spiral heat exchangers, and some welded plate heat exchangers allow good access for mechanical cleaning.</p><p>A final consideration for mechanical cleaning is the space required around the heat exchanger. When choosing an installation location, be sure that the necessary maintenance space is available for proper and safe maintenance of the new equipment.</p><p class="h1header">Shell and Tube Exchangers: Where Should I Put the Fluids?</p><p>In shell and tube heat exchangers, the specifying engineer has to decide whether each fluid should be placed on the shell side or the tube side. In general, fluids that exhibit these characteristic are preferred for the tube side:</p><ol><li>High pressure fluids{parse block="google_articles"} </li><li>Corrosive fluids </li><li>Fouling fluids </li><li>Viscous fluids </li><li>Slurries or fluids with significant solid loading </li></ol><p>Placing the high pressure fluid in the tubes will minimize the cost associated with the exchanger because the cost of thicker tube walls is generally less expensive than a thick shell. Corrosive fluids that require a higher alloy are also best placed in the tubes so that the shell does not have to be cladded with or fabricated from an expensive material. It is a "must"Â to place the most fouling fluid inside the tubes. The shell sides of shell and tube heat exchangers are notoriously difficult to clean. Viscous fluids are certainly good candidates for tube side flow as well. The heat transfer coefficient in an exchanger with a viscous fluid will almost certainly be limited by the viscous fluid. The heat transfer coefficient of a viscous fluid will be higher on the tube side than the shell side.</p><p>There may be situations where the engineer would prefer both fluids be on the tube side. In such cases, the engineer will have to consider each fluid carefully. In some cases, a shell and tube heat exchanger may not be the best choice and another heat transfer technology may have to be considered.</p><p class="h1header">TEMA Designations for Liquid-Liquid Shell and Tube Exchangers</p><p>Shell and tube heat exchangers are available in a wide range of configurations as defined by the Tubular Exchanger Manufacturers Association (TEMA, <a href="http://www.tema.org/" target="_blank">www.tema.org</a>). In essence, a shell and tube exchanger is a pressure vessel with many tubes inside of it. One process fluids flows through the tubes of the exchanger while the other flows outside of the tubes within the shell. The tube side and shell side fluids are separated by a tube sheet.{parse block="google_articles"}</p><p>Each shell and tube exchanger is designated by a three (3) letter code. The letters refer to the specific type of stationary head at the front, the shell type, and rear head type. Fixed tube sheet style exchangers with TEMA designations of BEM, AEM, or NEN are fairly common for liquid-liquid heat transfer duties. While fixed head arrangements have the advantage of being inexpensive and avoiding gaskets or packing to contain the shell side fluid, they do not allow for mechanical cleaning of the shell side.</p><p>For liquid-liquid heat transfer duties where the ability to mechanically clean the shell side as well as the tube side is a requirement, a floating head design should be chosen. With a floating head design, the tube bundle can be pulled out of the shell to allow access to the shell side.   Some of the most commonly used floating head designs for liquid-liquid duties include AES and BES. Another advantage of the floating head design is the ability to accommodate larger temperature differentials between the hot side and cold side fluids.</p><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]'title="TEMA Designations for Shell and Tube Heat Exchangers" href="../../../../invision/uploads/images/articles/thumbnails/shell_tube_heat_exchanger_1_Image6.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumbnails/thumb_shell_tube_heat_exchanger_1_Image6.gif" alt="shell_tube_heat_exchanger_1_Image6" width="113" height="150" /></a></td></tr><tr><td>Figure 6: TEMA Designations<br />
for Shell and Tube<br />
Heat Exchangers</td></tr><tr><td> </td></tr><tr><td><a class='resized_img' rel='lightbox[2]'title="Photo of a U-tube Bundle" href="../../../../invision/uploads/images/articles/thumbnails/shell_tube_heat_exchanger_1_Image7.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumbnails/thumb_shell_tube_heat_exchanger_1_Image7.gif" alt="shell_tube_heat_exchanger_1_Image7" width="150" height="106" /></a></td></tr><tr><td>Figure 7: Photo of a U-tube<br />
Bundle</td></tr></tbody></table><p>All of the designations discussed so far (BEM, AEM, NEN, AES, and BES) allow for multiple tube passes which are usually required for liquid-liquid duties so that the tube side velocities can be manipulated during the design stage of the exchanger.</p><p>The final type of shell and tube exchanger commonly used for liquid-liquid duties is commonly referred to as the "U-tube"Â type. Common TEMA designations are BEU and AEU. In this arrangement the tubes are bent into a series of concentrically tighter U-shapes with the end of the tubes being attached to the tube sheet.</p><p>The U-tube bundle can be removed to access the shell side for mechanical cleaning. The U-tube design is preferred for services with temperature or pressure cycling, intermittent service, and when there is a large temperature differential between the shell side and tube side fluids.</p><p>Since the "U"Â bend of the tubes cannot be accessed for mechanical cleaning, the tube side fluid should be clean or a suitable chemical cleaning agent should be identified.</p><p> <span class="h1header">Methods of Estimating Physical Properties</span></p><p>When specifying a liquid-liquid heat exchanger, the specifying engineer must be able to provide physical properties that are as accurate as possible. For liquid-liquid duties, the following data should be provided for each fluid: density, thermal conductivity, specific heat (sometimes called heat capacity), and viscosity. Ideally, these properties should be provided for each fluid at both the inlet and outlet temperature of the exchanger.{parse block="google_articles"}</p><p>If data is limited, there are some estimating rules that be of assistance.   The physical properties that will impact the design of the exchangers the most are the viscosity and the specific heat. Recall that the specific heat of a fluid is required in order to accurately specify the exchanger. Now, we'll examine estimation methods for each of the physical properties. While actual plant data or experimentally determined data is preferred, these methods can be used when no other data is available. For our estimation methods, we'll assume that typical process fluids are made up of mixtures of components and that the data for each component is available. This is almost always the case.</p><p class="h2header">Specific Heat</p><p>For fluid mixtures where there is no known heat of mixing, a weighted average can be used:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/thumbnails/shell_tube_heat_exchanger_1_Eqn9.gif" alt="shell_tube_heat_exchanger_1_Eqn9" width="282" height="46" /></td><td class="equationnumber" align="right">Eq. (8)</td></tr></tbody></table><p>Where:</p><p>C<sub>pmix</sub> = Heat capacity of the mixture in consistent units<br />
W<sub>1</sub> = Weight fraction of component one<br />
C<sub>pL1</sub> = Heat capacity of component one in consistent units<br />
W<sub>2</sub> = Weight fraction of component two<br />
C<sub>pL2</sub> = Heat capacity of component two in consistent units </p><p>If using the above method, look up the heat capacity of the components at the average temperature through the heat exchanger. It's not uncommon to provide heat exchanger designers with a single heat capacity point for each fluid. Be aware that the heat capacity of most liquids will increase with temperature.</p><p class="h2header">Viscosity</p><p>While it's not critical to supply a physical property point at the inlet and outlet temperature for other properties, it's very beneficial to do for the viscosity of the fluids. Using only a single viscosity point will affect both the heat transfer and pressure drop calculation of any heat exchanger.</p><p>For non-polar mixtures, the following has shown to provide viscosity estimates to within +/- 5 -10%:</p><table class="equationtable" border="0" align="center"><tbody><tr><td><img src="../../../../invision/uploads/images/articles/thumbnails/shell_tube_heat_exchanger_1_Eqn10.gif" alt="shell_tube_heat_exchanger_1_Eqn10" width="316" height="46" /></td><td class="equationnumber" align="right">Eq. (9)</td></tr></tbody></table><p>Where:</p><p>Âµ<sub>mix</sub> = Viscosity of mixture in centipoise<br />
W<sub>1</sub> = Weight fraction of component one<br />
Âµ<sub>1</sub> = Viscosity of component one in centipoise<br />
W<sub>2</sub> = Weight fraction of component two<br />
Âµ<sub>2</sub> = Viscosity of component two in centipoises</p><table class="imagecaption" border="0" align="left"><tbody><tr><td><a class='resized_img' rel='lightbox[2]'title="Viscosity Correlation Chart" href="../../../../invision/uploads/images/articles/thumbnails/shell_tube_heat_exchanger_1_Image8.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumbnails/thumb_shell_tube_heat_exchanger_1_Image8.gif" alt="shell_tube_heat_exchanger_1_Image8" width="108" height="150" /></a></td></tr><tr><td>Figure 8: Viscosity<br />
Correlation Chart</td></tr></tbody></table><p>For polar fluids, electrolyte solutions, and non-newtonian fluids, it is highly advisable to either find reliable data or have an outside lab perform testing.   There is an estimation method available for polar mixtures called the "Method of Grunberg and Nissan"Â. This method is detailed in <em>Properties of Liquids and Gases</em>, Edition 4 by Reid et al. (ISBN 0070517991, see page 474).</p><p>If viscosity data is available at one temperature, the following correlation chart (Figure 8) that has been used for years to estimate the viscosity at a second temperature. This chart is used by finding the single available viscosity point on the Y-axis and move left to meet the curve. Then, on the X-axis, adjust the temperature difference up or down by the temperature change required. Next, move up to hit the curve again and read the resulting viscosity from the Y-axis.</p><p> </p><p class="h2header">Thermal Conductivity</p><p>The thermal conductivities of mixtures can be estimated via the same weighted average method shown in Equation 9 for specific heat calculations. The calculation is the same, just replace the component specific heats with the component thermal conductivities. In cases where there is a complete absence of data, keep the following ranges in mind:</p><p>Water based mixtures, thermal conductivity range is about 0.28 to 0.35 Btu/ h ft Â°F</p><p>Hydrocarbon based mixtures, thermal conductivity range is about 0.055 to 0.080 Btu/ h ft Â°F</p><p class="h2header">Density</p><p>The density of mixtures represents another case where a weighted average method is usually adequate as an estimate for heat exchanger design.</p><p class="h1header">Avoiding Specifications That Are Too Specific</p><p>One final pitfall that the specifying engineer should avoid is making the heat exchanger specification too rigid. The engineers that design the heat exchangers are the experts, give them as much freedom as possible and allow them to present you with the best option(s) that will work well for your application.</p><p>As an example, consider the following:</p><p>A process stream requires Alloy C-276 material to guard against corrosion. The stream needs to be cooled with cooling water before being sent to storage. The metallurgy makes the process stream an immediate candidate for the tube side of a shell and tube heat exchanger.  The cooling water is available at 80 <sup>0</sup>F and must be returned at a temperature no higher than 115 <sup>0</sup>F. The process engineer realizes that with the water flow being placed on the shell side, larger flow rates will enhance the heat transfer coefficient. The basis for the heat exchanger quotation was specified as follows:</p><table class="datatable" border="0" align="center"><caption>Table 1: Sample Specifications</caption><tbody><tr><td> </td><td><span style="text-decoration: underline;"><strong>Tube Side</strong></span></td><td><span style="text-decoration: underline;"><strong>Shell Side</strong></span></td></tr><tr><td>Flow Rate (GPM)</td><td>500</td><td>1800</td></tr><tr><td>Temperature In (Â°F)</td><td>280</td><td>80</td></tr><tr><td>Temperature Out (Â°F)</td><td>150</td><td>92</td></tr><tr><td>Allowable Pressure Drop (psig)</td><td>15</td><td>15</td></tr></tbody></table><p>According to the engineer's calculations, these basic parameters should provide a good shell and tube design with a minimum amount of Alloy C-276 material (an expensive alloy). The completed specification sheet is forwarded to many manufacturers, including those that could easily quote plate and frame or another compact technology. A typical plate and frame unit designed to meet this specification would have about 650 ft<sup>2</sup> of area compared to about 420 ft<sup>2</sup> for a shell and tube exchanger. A plate and frame unit designed to the above specification is limited by the allowable pressure drop on the cooling water. If the cooling water flow is reduced to 655 GPM and the outlet water temperature rose to 115 <sup>Â°</sup>F, the plate and frame heat exchanger would contain about 185 ft<sup>2</sup> of area.   The unit is smaller, less expensive, and uses less water. The load being transferred to the cooling tower is the same.</p><p>The theory that applied to the shell and tube heat exchanger (increasing water flow will minimize heat transfer area), works in exactly the opposite direction for compact technologies. The larger water flow actually drives the cost of the unit upward. Rather than supplying a rigid specification to all heat exchanger manufacturers, the engineer should have explained his goal in regards to the process stream. Then he could have stated the following:</p><blockquotes><p>The process stream is to be cooled with cooling water. Up to 2000 GPM of water is available at 80 <sup>Â°</sup>F.   The maximum return temperature is 115 <sup>Â°</sup>F.</p></blockquotes><p>This simple statement could result in vastly different configurations when compared with the designs that would result from the original specification.</p><p class="h1header">Completing the TEMA Specification Sheet</p><p>The TEMA specification sheet shown below has been color coded to help explain which information should be provided by the specifying engineer and which information should be provided by the designer/manufacturer. Green cells are to be completed by the specifying engineer, yellow cells by the designer/manufacturer, and gray cells could be completed by either party.{parse block="google_articles"}</p><p>The information on the first page of the specification is essentially a description of the problem as has been covered herein. On the second page, the specifying engineer is asked to indicate the design pressure and temperature. The test pressure is generally accepted as 1.3 times the design pressure as specified by the latest version of the ASME Pressure Vessel code. Some times, however, the specifying engineer may request a higher design pressure (perhaps 1.5 times design pressure).   The engineer is also expected to specify materials or choices of materials for the heads, shell, tube sheets, tubes, and the compression gaskets (if applicable).</p><p>The specifying engineer can also indicate any required corrosion allowances required as well as any special mechanical or non-destructive testing that may be required for an exchanger to be installed in a particular duty.</p><p>If the installation of the exchanger would be simplified by a particular nozzle arrangement or maximum overall length, this type of information can be provided in the sketch box or in the remarks section. Use the remarks section to convey any other pertinent information to the designer.</p><table class="imagecaption" border="0" align="center"><tbody><tr><td><a class='resized_img' rel='lightbox[2]'title="TEMA Specification Sheet, Page 1" href="../../../../invision/uploads/images/articles/thumbnails/shell_tube_heat_exchanger_1_Image9.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumbnails/thumb_shell_tube_heat_exchanger_1_Image9.gif" alt="shell_tube_heat_exchanger_1_Image9" width="102" height="150" /></a></td><td> </td><td><a class='resized_img' rel='lightbox[2]'title="TEMA Specification Sheet, Page 2" href="../../../../invision/uploads/images/articles/thumbnails/shell_tube_heat_exchanger_1_Image10.gif" target="_blank"><img src="../../../../invision/uploads/images/articles/thumbnails/thumbnails/thumb_shell_tube_heat_exchanger_1_Image10.gif" alt="shell_tube_heat_exchanger_1_Image10" width="99" height="150" /></a></td></tr><tr><td>Figure 9: TEMA Specification<br />
Sheet, Page 1</td><td> </td><td>Figure 10: TEMA Specifiation<br />
Sheet, Page 2</td></tr></tbody></table><p class="h1header">Conclusions</p>Specifying a liquid-liquid heat exchanger is not always as easy as it may appear. But an engineer who examines the problem carefully and prepares an accurate, yet flexible, specification will find the entire process much easier. Thinking about all aspects of the heat exchanger to be installed can also help avoid problems in the future or surprises during the installation of the equipment.]]></description>
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