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More Thermodynamic Cycles
P M V Subbarao
Professor
Mechanical Engineering Department
The Engineering Systems for High end Extra-
somatic Needs…
Brayton Cycle for Power Generation
1-2 Adiabatic compression (in a compressor)
2-3 Constant pressure heat addition
3-4 IAdiabaticexpansion (in a turbine)
4-1 Constant pressure heat rejection
Thermodynamic Analysis of Adiabatic Compression
Comp
W
h
m
h
m 

 


 2
2
1
1












 
 2
1
2
2
1
1 vdp
m
h
m
h
m 

For an infinitesimal compression:
   
vdp
m
dh
h
m
h
m 

 





vdp
m
dh
m 
 

vdp
dT
cp 
Model for infinitesimal Adiabatic Process by a
perfect Gas
















p
dp
T
dT

 1
C
p
T ln
ln
1
ln 




C
p
T ln
ln
ln
1













C
p
T
ln
ln 1














C
p
T



 1
C
Tp 



1
Finite Compression of Perfect gas
C
Tp 



1
C
pv 

2
1
1
1
2
1
1
p
p
p
C
m
h
m
h
m

















 
















 
 2
1
2
1 vdp
m
h
m
h
m 













 
 2
1
1
2
1

p
dp
C
m
h
m
h
m 

 
2
1
1
1
2
1
1
p
p
comp p
C
m
h
h
m
W















 




Constant Pressure Heat Addition (combustion)
Adiabatic Expansion
 
4
3
1
1
4
3
1
p
p
turb p
C
m
h
h
m
W















 




)
( 1
2
1
2 T
T
c
h
h
w p
comp 



1 –2 : Specific work input :
2 – 3 : Specific heat input :
3 – 4 : Specific work output :
4 – 1 : Specific heat rejection :
)
( 2
3
2
3 T
T
c
h
h
q p
in 



)
( 4
3
4
3 T
T
c
h
h
w p
tur 



)
( 1
4
1
4 T
T
c
h
h
q p
out 



Adiabatic Processes:

 1
1
2
1
2










p
p
T
T 
 1
4
3
4
3










p
p
T
T
Cycle Analysis
   
1
2
4
3 h
h
h
h
w
w
w comp
tur
net 




















 











)
1
(
1
)
(
)
(
1
3
1
1
3
3





T
T
c
T
T
T
T
c
w
p
p
net
)
( 1
3
1
3

















 T
T
T
T
c
w p
net


 
)
(
)
( 1
2
4
3 T
T
T
T
c
w p
net 



)
( 1
3
2
3 T
T
c
h
h
q p
in 




 
)
(
1
3
1
3
1
3
T
T
c
T
T
T
T
c
q
w
p
p
in
net
th
























in
net
th
q
w


 
1
1
3
1
3
T
T
c
T
T
c
p
p












1
1



1
1 1

 


p
r
0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0 10 20 30
th

p
r
Pressure Ratio Vs Efficiency
Reciprocating IC Engine : A Heat Engine
Qin
Qout
Wout
Greatness of Heat Engines
• Balance Sheet for A Heat Engine:
– All heat inputs consume resources : Total Input Heat :
Qin (Cost incurred).
– All heat outputs are just mere a loss.
– Net work Out put is positive and this is the final
benefit : Wnet (Benefit Achieved)
– Performance : Benefit to cost ratio (in energy units).

 
  1
1 i
i
i
i W
Q



 


 


out
i
i
in
i
i
out
i
i
in
i
i W
W
Q
Q 1
1
1
1
Otto’s Engine for Propulsion
Modification of Brayton Cycle for Air Craft
Propulsion : Invented by Frank Whittle
Large Aircrafts : Boeing 747
Physical Properties of Standard
Atmosphere
Altitude
(meters)
Temperature
(K)
Pressure
(kPa)
0 288.15 101.3
1,000 281.65 89.87
2,000 275.15 79.49
3,000 268.65 70.10
4,000 262.15 61.64
5,000 255.65 54.02
6,000 249.15 47.18
7,000 242.65 41.06
8,000 236.15 35.59
9,000 229.65 30.74
10,000 223.15 26.43
12,000 216.65 19.33
15,000 216.65 12.04
Air Craft Engine Bleed for Refrigeration System
Air Standard Refrigeration Cycle for Aircraft
Cooling
Air Craft Engine Refrigeration System
Air to Cabin
•The gas power cycle can be used as refrigeration cycles by
simply reversing them.
•Of these, the reversed Brayton cycle, which is also known as
the gas refrigeration cycle, is used to cool aircraft.
• Further Modification this cycle is used to obtain very low
(cryogenic) temperatures.
•The work output of the turbine can be used to reduce the
work input requirements to the compressor.
•Thus, the performance index of a gas refrigeration cycle is
defined as
COP
q
w
q
w w
R
L
net in
L
comp in turb out
 

, , ,
Gas Refrigeration Systems
More Cycles for Exotic Needs of Urban World …….
An Urban world that was present till the end of first
decade of the 20th century.
• Only fresh foods that could be grown locally were available,
and they had to be purchased and used on a daily basis.
• Meat was bought during the daily trip to the butcher's; the
milkman made his rounds every morning.
• If you could afford weekly deliveries of ice blocks—harvested
in the winter from frozen northern lakes—you could keep
some perishable foods around for 2 or 3 days in an icebox.
• New York was a virtual ghost town in the summer months.
• Homes were built with natural cooling in mind.
• Ceilings were high, porches were deep and shaded, and
windows were placed to take every possible advantage of
cross-ventilation
Urban Life after the end of first decade of the 21st
century.
• Frozen foods of all kinds were available just about
anywhere in the world all year round.
• The milkman was all but gone and forgotten, and the
butcher now did his work behind a counter at the
supermarket.
• Indeed, many families concentrated the entire week's food
shopping into one trip to the market, stocking the
refrigerator with perishables that would last a week or
more.
• New York is a busy town even in the summer months.
• Buildings are totally isolated from fresh air.
Creation of Artificial Temperature/Quality
Why not use the reversed Rankine cycle for Refrigeration ?
• Very costly to expand the liquid using a turbine with very low
or negligible power output!?!
• May become negative under friction.
• Cheaper to have irreversible expansion through an expansion
valve.
Thermodynamics of Ideal VCR Cycle
• Ideal Vapor-Compression Refrigeration Cycle
• Process Description
• 1-2 Adiabatic compression
• 2-3 Constant pressure heat rejection in the condenser
• 3-4 Throttling in an expansion valve
• 4-1 Constant pressure heat addition in the evaporator
Performance Index
The performance of refrigerators and heat pumps is expressed in
terms of coefficient of performance (COP), defined as
COP
Q
W
COP
Q
W
R
L
net in
HP
H
net in
  
  
Desired output
Required input
Cooling effect
Work input
Desired output
Required input
Heating effect
Work input
,
,
Under the same operating conditions, the COPs are related by
COP COP
HP R
 1
Samsung Split A/c Model No : AQ24UUA
Cooling Capacity : 7.03kW
Power Consumption (Cooling) : 2,600Watts
Refrigerant Type R22
The refrigerant leaves the evaporator at 7.2o
C
Condenser pressure : 2.71 MPa.
Heat Pump Systems

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Thermodynamic cycles

  • 1. More Thermodynamic Cycles P M V Subbarao Professor Mechanical Engineering Department The Engineering Systems for High end Extra- somatic Needs…
  • 2. Brayton Cycle for Power Generation 1-2 Adiabatic compression (in a compressor) 2-3 Constant pressure heat addition 3-4 IAdiabaticexpansion (in a turbine) 4-1 Constant pressure heat rejection
  • 3. Thermodynamic Analysis of Adiabatic Compression Comp W h m h m        2 2 1 1                2 1 2 2 1 1 vdp m h m h m   For an infinitesimal compression:     vdp m dh h m h m          vdp m dh m     vdp dT cp 
  • 4. Model for infinitesimal Adiabatic Process by a perfect Gas                 p dp T dT   1 C p T ln ln 1 ln      C p T ln ln ln 1              C p T ln ln 1               C p T     1 C Tp     1
  • 5. Finite Compression of Perfect gas C Tp     1 C pv   2 1 1 1 2 1 1 p p p C m h m h m                                       2 1 2 1 vdp m h m h m                  2 1 1 2 1  p dp C m h m h m     2 1 1 1 2 1 1 p p comp p C m h h m W                     
  • 6. Constant Pressure Heat Addition (combustion)
  • 7. Adiabatic Expansion   4 3 1 1 4 3 1 p p turb p C m h h m W                     
  • 8. ) ( 1 2 1 2 T T c h h w p comp     1 –2 : Specific work input : 2 – 3 : Specific heat input : 3 – 4 : Specific work output : 4 – 1 : Specific heat rejection : ) ( 2 3 2 3 T T c h h q p in     ) ( 4 3 4 3 T T c h h w p tur     ) ( 1 4 1 4 T T c h h q p out     Adiabatic Processes:   1 1 2 1 2           p p T T   1 4 3 4 3           p p T T Cycle Analysis
  • 9.     1 2 4 3 h h h h w w w comp tur net                                   ) 1 ( 1 ) ( ) ( 1 3 1 1 3 3      T T c T T T T c w p p net ) ( 1 3 1 3                   T T T T c w p net     ) ( ) ( 1 2 4 3 T T T T c w p net    
  • 10. ) ( 1 3 2 3 T T c h h q p in        ) ( 1 3 1 3 1 3 T T c T T T T c q w p p in net th                         in net th q w     1 1 3 1 3 T T c T T c p p             1 1    1 1 1      p r
  • 11. 0 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0 10 20 30 th  p r Pressure Ratio Vs Efficiency
  • 12. Reciprocating IC Engine : A Heat Engine Qin Qout Wout
  • 13. Greatness of Heat Engines • Balance Sheet for A Heat Engine: – All heat inputs consume resources : Total Input Heat : Qin (Cost incurred). – All heat outputs are just mere a loss. – Net work Out put is positive and this is the final benefit : Wnet (Benefit Achieved) – Performance : Benefit to cost ratio (in energy units).      1 1 i i i i W Q            out i i in i i out i i in i i W W Q Q 1 1 1 1
  • 14. Otto’s Engine for Propulsion
  • 15. Modification of Brayton Cycle for Air Craft Propulsion : Invented by Frank Whittle
  • 16. Large Aircrafts : Boeing 747
  • 17. Physical Properties of Standard Atmosphere Altitude (meters) Temperature (K) Pressure (kPa) 0 288.15 101.3 1,000 281.65 89.87 2,000 275.15 79.49 3,000 268.65 70.10 4,000 262.15 61.64 5,000 255.65 54.02 6,000 249.15 47.18 7,000 242.65 41.06 8,000 236.15 35.59 9,000 229.65 30.74 10,000 223.15 26.43 12,000 216.65 19.33 15,000 216.65 12.04
  • 18. Air Craft Engine Bleed for Refrigeration System
  • 19. Air Standard Refrigeration Cycle for Aircraft Cooling
  • 20. Air Craft Engine Refrigeration System Air to Cabin
  • 21. •The gas power cycle can be used as refrigeration cycles by simply reversing them. •Of these, the reversed Brayton cycle, which is also known as the gas refrigeration cycle, is used to cool aircraft. • Further Modification this cycle is used to obtain very low (cryogenic) temperatures. •The work output of the turbine can be used to reduce the work input requirements to the compressor. •Thus, the performance index of a gas refrigeration cycle is defined as COP q w q w w R L net in L comp in turb out    , , , Gas Refrigeration Systems
  • 22. More Cycles for Exotic Needs of Urban World …….
  • 23. An Urban world that was present till the end of first decade of the 20th century. • Only fresh foods that could be grown locally were available, and they had to be purchased and used on a daily basis. • Meat was bought during the daily trip to the butcher's; the milkman made his rounds every morning. • If you could afford weekly deliveries of ice blocks—harvested in the winter from frozen northern lakes—you could keep some perishable foods around for 2 or 3 days in an icebox. • New York was a virtual ghost town in the summer months. • Homes were built with natural cooling in mind. • Ceilings were high, porches were deep and shaded, and windows were placed to take every possible advantage of cross-ventilation
  • 24. Urban Life after the end of first decade of the 21st century. • Frozen foods of all kinds were available just about anywhere in the world all year round. • The milkman was all but gone and forgotten, and the butcher now did his work behind a counter at the supermarket. • Indeed, many families concentrated the entire week's food shopping into one trip to the market, stocking the refrigerator with perishables that would last a week or more. • New York is a busy town even in the summer months. • Buildings are totally isolated from fresh air.
  • 25. Creation of Artificial Temperature/Quality
  • 26. Why not use the reversed Rankine cycle for Refrigeration ? • Very costly to expand the liquid using a turbine with very low or negligible power output!?! • May become negative under friction. • Cheaper to have irreversible expansion through an expansion valve.
  • 27. Thermodynamics of Ideal VCR Cycle • Ideal Vapor-Compression Refrigeration Cycle • Process Description • 1-2 Adiabatic compression • 2-3 Constant pressure heat rejection in the condenser • 3-4 Throttling in an expansion valve • 4-1 Constant pressure heat addition in the evaporator
  • 28. Performance Index The performance of refrigerators and heat pumps is expressed in terms of coefficient of performance (COP), defined as COP Q W COP Q W R L net in HP H net in       Desired output Required input Cooling effect Work input Desired output Required input Heating effect Work input , , Under the same operating conditions, the COPs are related by COP COP HP R  1
  • 29. Samsung Split A/c Model No : AQ24UUA Cooling Capacity : 7.03kW Power Consumption (Cooling) : 2,600Watts Refrigerant Type R22 The refrigerant leaves the evaporator at 7.2o C Condenser pressure : 2.71 MPa.