heatttttt raporrrrrr.doc
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INTRODUCTION:
Heat exchangers are devices that provide the flow of thermal energy between two or more
fluid streams at different temperatures. The fluids are separated by a solid wall so that they
never mix, or directly contacted. They have generally no external heat and work interactions.
Typical applications are heating or cooling of a fluid stream and evaporation or condensation
of a single or multicomponant fluid streams. Other applications are sterilization, pateurization,
distillation, cyristallization or controlling a process fluid. They are widely used in
refrigeration, air conditioning,space heating, electricity generationand chemical processing.
Heat Exchanger Classification :
The classification of heat exchangers is based on the basic operation, construction, heat
transfer, and flow arrangements, due to the large number of configurations of heat
exchangers. This classification as outlined by Kakac and iu !"##$% willbe discussed&
'ecuperators and regenerators
Transfer processes& direct contact or indirect contact
(eometry of construction& tubes, plates, and extended surfaces
Heat transfer mechanisms& single phase or two phase flow )low *rrangement& parallel flow, counter flow, or cross flow
+n this proect, + studied on the shell and tube heat exchangers.The shell and tube heat
exchanger is a class of heat exchanger designs. *s its name implies this type of heat
exchanger consists of a shell !a large tube% with a series of small tubes inside it. Two fluids
with different initial temperatures flow through the exchanger. One through the tubes and the
other through the shell. Heat is transferred from one fluid to the other.This is a great way forconservation of energy.
-hell and tube heat exchangers are employed when a process reuires large uantities of
fluid to be heated or cooled. /ue to their compact design, these heat exchangers contain a
large amount of heat transfer area and also provide a high degree of heat transfer efficiency.
They are commonly used as oil coolers, power condensers, preheaters and steam generators in
both fossil fuel and nuclear0based energy production applications, and also used in the air
conditioning and refrigeration industry.
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http://en.wikipedia.org/wiki/Refrigerationhttp://en.wikipedia.org/wiki/Air_conditioninghttp://en.wikipedia.org/wiki/Space_heatinghttp://en.wikipedia.org/wiki/Electricity_generationhttp://en.wikipedia.org/wiki/Refrigerationhttp://en.wikipedia.org/wiki/Air_conditioninghttp://en.wikipedia.org/wiki/Space_heatinghttp://en.wikipedia.org/wiki/Electricity_generation -
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There can be many variations on the shell and tube design. 1ost are either one, two or four
pass designs. This refers to the number of times the fluid in the tubes passes through the fluid
in the shell. +n a single pass heat exchanger, the fluid goes in one end and out the other. Two
and four pass designs are common because the fluid can enter and exit on the same side. This
makes construction much simpler.
*ccording to flow types of fluid through,they can be classified into two maor sections. +n
parallel0flow heat exchangers, the two fluids enter the exchanger at one end, and flow through
in the same direction and leave together at the other end while in counter0flow heat
exchangers the fluids enter the exchanger from opposite ends. The counter current design is
most efficient since they allow the highest log mean temperature difference between the hot
and cold streams. 1any companies however do not use them because they can break easily in
addition to being more expensive to build. Often multiple heat exchangers can be used to
simulate the counter current flow of a single large exchanger.
)igure.".shell and tube exchanger
2
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2. PARAMETER AND CA!CU!ATION
*ssumptions&
3egligible heat transfer from surroundings
3o heat generation within the system
4onstant properties
3o stored energy
3egligible kinetic and potential enery changes
3o phase change
Ta"le #. $i%en Para&eters
567 8thylene glycol 9ater1ass flow rate mh, mc !kg:s% 6,7;< calculated
Temperature in Ti, ti !K% 6=6,"; 2#$,";
Temperature out To, to !K% 6"6,"; 6"$,";
-pecific Heat, 4ph, 4pc !:kg K% 2#62 >"$7
/ynamic ?iscosity @ !3 s:m2% 7,777;=< 7,777#7=
Thermal 4onductivity k !9:m K% 7,>$< 7,>
4o!B:3 m% 7,7777777>>
-f 7,";
Kf !":year% 7,2
9u !kg:h% "26>=,7
Hy !hour:year% =777
Ta"le ). Design Para&eters
+nside diameter of the tube, +/ !m% 7,722
Outside diameter of the tube O/ !m% 7,72>
+nside shell diameter !+/shell % !m% 7,%G3t F7,726#>$6.7 2
ID
nLGfP ttt
= F 6,##6#>>6=6 Ca
The pressure drop of return losses, MCr&
22;." tr VnP =
?tFmc:!pG*c%F 7,2 m:s
22;." tr VnP = F "$7,,
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2.. Calc(lation of hell i*e Heat Transfer Coefficient+ ho:
*fter calculating tube side values, shell side calculations must be done. )irst step of this
calculation is euivalent diameter.
8uivalent diameter, /e, for a suare pitch&
OD
ODPD Te
.
%>:!> 22
= F 7,726=>$6 m
4learance between the tubes, 4&
4FCt0O/F 7,77
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MT"F Ti0to
MT2F To0ti
TiF 6=6,"; K ToF 6"6,"; K tiF 2#$,"; K toF 6"$,"; K
NTlmF 67,=$"76 m K:9
!oGO/%F 62,
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3umber of passes 2
3umber of tubes 2";"
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+n this study number of tubes is main design parameter. *ccording to )igure.2 hi decreases
when number of tubes increases. hi depends on 'eynolds number and 'eynolds and it
changes with different tube numbers. Therefore, changing number of tubes affects the hi value
inversely proportional.
ho vs Nt
0
500
1000
1500
2000
2500
60 61 62 63 64 65 66
Nt
ho ho (W/m 2K)
)igure.6.ho versus 3t graph
This graph shows that ho value is constant with increasing number of tubes because the
parameters that affect the ho value does not depend on tube number.
Uo vs Nt
1352
1354
1356
1358
1360
1362
1364
1366
1368
1370
1372
60 61 62 63 64 65 66
Nt
Uo Uo
)igure.>.o versus 3t graph
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)igure > indicates the relation between o and 3t. o decreases while 3t increases
according to this plot. o is directly related on hi and ho values. Decause of the fact that hi
decreases and ho remains constant with increasing 3t, an increase in o value is observed.
P vs Nt
170
175
180
185
190
195
200
60 61 62 63 64 65 66
Nt
P P (Pa)
)igure.;. MC versus 3t graph
Total pressure drop euals to summation of pressure drop of return losses and tube side
pressure drop. Cressure drop of return losses is related with the velocity of tube side and tube
side pressure drop depends on tube side 'eynold number and length. /uring the optimization
tube side velocity remains constant whereas 'eynold number and length decrease with
increasing tube number. *s a result, total pressure drop inversely proportional with tube
number as it is seen in )igure ;.
""
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Ao(m 2)
18,5
18,55
18,6
18,65
18,7
18,75
60 61 62 63 64 65 66
Nt
Ao Ao(m 2)
)igure.>7,>7
B:year when the the tube number is
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of cost, 8o and *o are the most significant parameters. /uring optimization *o value arises
as in )igure < and 8o decreases as in the calculations. p to the optimum 3t value, decreasing
in the 8o is much more effective than increasing in the *o.However, after this optimum point,
opposite situation is valid. Therefore, cost is decrasing upto optimum tube number value and
after this value an increase is observed for cost.
,.CONC!UION
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)or this heat exchanger design, carbon steel is selected due to its low cost and higher
thermal conductivity. 8xcept from carbon steel, the other materials can be used for the desired
stainless properties. +n addition, " shell 2 tube pass heat exchanger type and suare pitch are
assumed.
+n calculations, the tube number range between
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http&::www.the0engineering0page.com
http&::www.cheresources.com:designexzz.html
http&::en.wikipedia.org:wiki:-hellandtubeheatexchanger
).C. +ncropera, /.C. /ewitt, T.. Dergman, *.-. avine, )undamentals of Heat and
1ass Transfer.
4. 4aputo, C. 1. Celagagge, C. -alini, Heat exchanger design based on economic
optimisation, *pplied Thermal 8ngineering. 277=
";
http://www.the-engineering-page.com/http://www.cheresources.com/designexzz.htmlhttp://en.wikipedia.org/wiki/Shell_and_tube_heat_exchangerhttp://www.the-engineering-page.com/http://www.cheresources.com/designexzz.htmlhttp://en.wikipedia.org/wiki/Shell_and_tube_heat_exchanger