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ME 200 L18:ME 200 L18: Conservation Laws: Heat ExchangersHW 7 Posted Due in One Week:
Kim See’s Office ME Gatewood Wing Room 2172
https://engineering.purdue.edu/ME200/ThermoMentor© Program Launched
Spring 2014 MWF 1030-1120 AMI. Sircar for
J. P. Gore (No Office Hours Today) [email protected]
Gatewood Wing 3166, 765 494 0061Office Hours: MWF 1130-1230
TAs: Robert Kapaku [email protected] Dong Han [email protected]
2
Common Steady-flow Energy DevicesCommon Steady-flow Energy Devices
NozzlesNozzles
CompressorsCompressorsHeat Exchangers and MixersHeat Exchangers and Mixers
ThrottlesThrottles
2
Water, Steam, Gas TurbinesWater, Steam, Gas Turbines
PumpPump
DiffusersDiffusers
3
Rotating Machinery
A turbine is a steady-flow device used to produce mechanical work (W) by reducing the internal &/or kinetic &/or potential energy of the working fluid.
•For gas turbines, the fluid drives rotating blades while the υ increases from inlet to exit as the working fluid expands (or the p drops).
3
4
Steam Turbine Example
4
6 Kg/s of steam at an inlet velocity of 75 m/s enter a turbine stage at 3 MPa and 400 oC and exit at a velocity of 125 m/s at a pressure of 2 Mpa at 360 oC. Find: (a) the power developed by this steam turbine stage, (b) the percentage change in the steam density across the turbine and (c) the percentage change in the flow area. The heat loss through the casing is 33 kW.
kWcvQ 33
cvWskgm /61
skgm /61
2 21 2
1 2
2 2 2 1 12
2 2 1
2 2
2 1 1 1 2 2
2 2
75 12533 6 3230.9 3159.3
2000 2000
( ) 33 6 (71.6 5) 366.6
( ) ( ) / ( ) / (0.094 0.141) / 0
Turbine Turbine
e
Turbine
Turbine
V VQ W m h h
V A V AVm m m
v v v
W
a W kW
b v v v
2 2 2 1 1 1 2 1
2 1
.141 33%
( ) / / 125 / 0.141 75 / 0.094
/ (75 /125)*(0.141/ 0.094) 0.9
c A V v AV v A A
A A
Air Compressors
September 17th, 2010 ME 200 5
A pump is a steady-flow device that consumes shaft work from rotating blades that compress the fluid.•Compressors are used for gas systems, pumps for liquids so operating assumptions are similar.
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Example
At steady state, a well-insulated compressor takes in air at 60 ºF, 14.2 psi, with a volumetric flow rate of 1200 ft3/min, and compresses it to 500 ºF, 120 psi. Kinetic and potential energy changes from inlet to exit can be neglected. Determine the compressor power, in hp, and the volumetric flow rate at the exit, in ft3/min.
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7
Example
Find– Wcv = ? in hp– A2V2 = ? in ft3/min
System (air flowing through compressor)
Assumptions•The control volume is at steady state; the flow is steady•Q, Δke, and Δpe are negligible. •The air is an ideal gas.
Basic Equations
e
ee
eei
ii
iicvcv
cv gzV
hmgzV
hmWQdt
dE
22
22
RTP airP1 = 14.2 psiT1 = 60 ºFA1V1 = 1200 ft3/min
P2 = 120 psiT2 = 500 ºF
compressor1 2
7
e
eii
cv mmdt
dm
8
Example
Solution
e
ee
eei
ii
iicvcv
cv gzV
hmgzV
hmWQdt
dE
22
22
P
RT
AV
m
8
e
eii
cv mmdt
dm mmm 21
21 hhmWcv
1
111RT
PVAm
9
Example
9
3 2
2
14.2 1200 min 60min 1441540 1 152028.9
f
m
psi ft inm
ft lb h ftRlb R
hlbm m5310
From Table A-22E
mlbBtuh 1241 mlbBtuh 2312
21 hhmWcv
15310 124 231
2540
m
cvm
lb Btu hpW
h lb Btu h 223cvW hp
10
Example
10
222 mVA
2
2 2 2
15405310 960
1 128.9120 144 60min
m
m
lb lbf ftR
ft hh lb RAV
psi in
min262 322 ftVA
2
222 P
RTmVA
Heat Exchangers
►Direct contact: A mixing chamber in which hot and cold streams are mixed directly.
►Tube-within-a-tube counterflow: A gas or liquid stream is separated from another gas or liquid by a wall through which energy is conducted. Heat transfer occurs from the hot stream to the cold stream as the streams flow in opposite directions.
► if there is no stirring shaft or moving boundary.
► ΔKE = (Vi2/2-Ve
2/2) negligible unless specified.
► ΔPE = negligible unless specified.
► If Heat transfer with surroundings is negligible.
►Control Volume includes both hot and cold flows. The “heat exchange,” between them is internal!
e
ee
eei
ii
ii gzhmgzhmWQ )2
()2
(022 VV
cvcv
Heat Exchanger Modeling
ee
eiii hmhm 0
)( iiee gzmgzm
0cvW
0cvQ
Example Problem: Heat Exchanger
Given: Air and Refrigerant R-22 pass through separate streams through an insulated heat exchanger. Inlet and exit states of each are defined.
Find: (a) Mass flow rates, (b) Energy transfer from air to the refrigerant.
R-22
Air
3
4
1
2
Assumptions: Flow work only, insulated casing, steady state, steady flow, no leaks.
34
2122
242213220
hh
hhmm
hmhmhmhm
AirR
AirRAirR
Data: Av1= 40m3/min,1=27 C=300K, P1= 1.1 barsT2=15 C= 288 K, P2= 1barP4= 7 bars, T4=15 C, P3=7 bars, x3=0.16
min/11.51)300)(/287.0(
min)/340)(1.1(
1
11
1
1
kgKKkgkJ
mbars
RT
AVP
v
AVmAir
R22 properties: Table A-9, A-8. P=7 bars, Tsat=10.91 C. Therefore, 4 is superheated and h4=256.86 kJ/kg. Table A-8 h3=hf3+x3hfg3= 58.04+(.16)(195.6) =89.34 kJ/kg.
Example Problem: Heat Exchanger
Given: Air and Refrigerant R-22 pass through separate streams through an insulated heat exchanger. Inlet and exit states of each are defined.
Find: (a) Mass flow rates, (b) Energy transfer from air to the refrigerant.
R-22
Air
3
4
1
2Assumptions: Flow work only, insulated casing, steady state, steady flow, no leaks.
min/673.334.8986.256
15.28819.30011.51
34
2122
kghh
hhmm AirR
Data: Av1= 40m3/min,1=27 C=300K, P1= 1.1 barsT2=15 C= 288 K, P2= 1barP4= 7 bars, T4=15 C, P3=7 bars, x3=0.16
min/3.61519.30015.28811.51)(
min/3.615)34.8986.256(673.3)(
12
342222
kJhhmQ
kJhhmQ
AirAir
RR
15
SummarySummary
• Control volume energy and mass conservation equations that we learned are applicable to many practical energy devices and equipment.
• Important learning comes from application of appropriate assumptions, considering the appropriate working substances and their and their propertiesproperties in the proper range of operation to estimate different energy quantities.
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