THERMODYNAMICS (LL)-W/ACCESS >CUSTOM<
THERMODYNAMICS (LL)-W/ACCESS >CUSTOM<
9th Edition
ISBN: 9781266657610
Author: CENGEL
Publisher: MCG CUSTOM
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Chapter 11.10, Problem 79P

A gas refrigeration system using air as the working fluid has a pressure ratio of 5. Air enters the compressor at 0°C. The high-pressure air is cooled to 35°C by rejecting heat to the surroundings. The refrigerant leaves the turbine at −80°C and then it absorbs heat from the refrigerated space before entering the regenerator. The mass flow rate of air is 0.4 kg/s. Assuming isentropic efficiencies of 80 percent for the compressor and 85 percent for the turbine and using constant specific heats at room temperature, determine (a) the effectiveness of the regenerator, (b) the rate of heat removal from the refrigerated space, and (c) the COP of the cycle. Also, determine (d) the refrigeration load and the COP if this system operated on the simple gas refrigeration cycle. Use the same compressor inlet temperature as given, the same turbine inlet temperature as calculated, and the same compressor and turbine efficiencies.

Chapter 11.10, Problem 79P, A gas refrigeration system using air as the working fluid has a pressure ratio of 5. Air enters the

FIGURE P11–79

(a)

Expert Solution
Check Mark
To determine

The effectiveness of the regenerator.

Answer to Problem 79P

The effectiveness of the regenerator is 0.434.

Explanation of Solution

Show the T-s diagram as in Figure (1).

THERMODYNAMICS (LL)-W/ACCESS >CUSTOM<, Chapter 11.10, Problem 79P , additional homework tip  1

Express the temperature at state 2s.

T2s=T1[P2P1](k1)/k (I)

Here, temperature at state 1 is T1, pressure at state 1 and 2 is P1andP2 respectively, and heat capacity ratio is k.

Express the temperature at state 2 from the isentropic relations.

ηC=h2sh1h2h1=T2sT1T2T1 (II)

Here, isentropic efficiency is ηC, enthalpy at state 2s, 1 and 2 is h2s,h1andh2 respectively, temperature at state 2s, 1 and 2 is T2s,T1andT2 respectively.

Express temperature at state 5s.

T5s=T4[P5P4](k1)/k                                                                                   (III)

Here, temperature at state 4 is T5, pressure at state 5 and 4 is P5andP4 respectively.

Express temperature at state 4.

ηT=h4h5h4h5s=T4T5T4T5s (IV)

Here, thermal efficiency is ηT, enthalpy at state 4, 5 and 5s is h4,h5andh5s respectively, temperature at state 4, 5 and 5s is T4,T5andT5s.

Express the temperature at state 6 using an energy balance.

m˙cp(T3T4)=m˙cp(T1T6)T3T4=T1T6T6=T1T3+T4 (V)

Here, mass flow rate is m˙, specific heat at constant pressure is cp, temperature at state 1,3,4 and 6 is T1,T3,T4andT6 respectively.

Express the effectiveness of the regenerator.

εregen=h3h4h3h6=T3T4T3T6                                                                                      (VI)

Here, enthalpy at state 3, 4 and 6 is h3,h4andh6 respectively.

Conclusion:

Perform unit conversion of temperature at state 1, 3, and 5 from °CtoK.

T1=0°C=(0+273.2)K=273.2K

T3=35°C=(35+273.2)K=308.2K

T5=80°C=(80+273.2)K=193.2K

Refer Table A-2, “ideal gas specific heats of various common gas”, and write the properties of air.

cp=1.005kJ/kgKk=1.4

Substitute 273.2K for T1, 5 for P2/P1 and 1.4 for k in Equation (I).

T2s=(273.2K)(5)(1.41)/1.4=432.4K

Substitute 0.80 for ηC, 432.4K for T2s and 273.2K for T1 in Equation (II).

0.80=432.4K273.2KT2273.2KT2=472.5K

Substitute 15 for P5/P4 and 1.4 for k in Equation (III).

T5s=T4[15](1.41)/1.4 (VII)

Substitute 0.85 for ηT and 193.2K for T5 in Equation (IV).

0.85=T4193.2K5T4T5s (VIII)

Solve Equations (VII) and (VIII) simultaneously by online calculator to get,

T4=281.3KT5s=177.60K

Substitute 273.2K for T1, 308.2K for T3 and 281.3K for T4 in Equation (V).

T6=273.2K308.2K+281.3K=246.3K

Substitute 308.2K for T3, 281.3K for T4, and 246.3K for T6 in Equation (VI).

εregen=308.2K281.3K308.2K246.3K=0.434

Hence, the effectiveness of the regenerator is 0.434.

(b)

Expert Solution
Check Mark
To determine

The rate of heat removal from the refrigerated space.

Answer to Problem 79P

The rate of heat removal from the refrigerated space is 21.4kW.

Explanation of Solution

Express the rate of heat removal from the refrigerated space.

Q˙L=m˙cp(T6T5) (IX)

Conclusion:

Substitute 0.4kg/s for m˙, 1.005kJ/kgK for cp, 246.3K for T6 and 193.2K for T5 in Equation (IX).

Q˙L=(0.4kg/s)(1.005kJ/kgK)(246.3K193.2K)=21.4kJ/s[kWkJ/s]=21.4kW

Hence, the rate of heat removal from the refrigerated space is 21.4kW.

(c)

Expert Solution
Check Mark
To determine

The COP of the gas refrigeration cycle.

Answer to Problem 79P

The COP of the gas refrigeration cycle is 0.478.

Explanation of Solution

Express the net work input of the compressor.

W˙C,in=m˙cp(T2T1) (X)

Express the net work output of the turbine.

W˙T,out=m˙cp(T4T5) (XI)

Express the coefficient of performance of the gas refrigeration cycle.

COP=Q˙LW˙C,inW˙T,out (XII)

Conclusion:

Substitute 0.4kg/s for m˙, 1.005kJ/kgK for cp, 472.5K for T2 and 273.2K for T1 in Equation (X).

W˙C,in=(0.4kg/s)(1.005kJ/kgK)(472.5K273.2K)=80.13kJ/s[kWkJ/s]=80.13kW

Substitute 0.4kg/s for m˙, 1.005kJ/kgK for cp, 281.3K for T4 and 193.2K for T5 in Equation (XI).

W˙T,out=(0.4kg/s)(1.005kJ/kgK)(281.3K193.2K)=35.43kJ/s[kWkJ/s]=35.43kW

Substitute 21.36kW for Q˙L, 80.13kW for W˙C,in and 35.43kW for W˙T,out in Equation (XII).

COP=21.36kW80.13kW35.43kW=0.478

Hence, the COP of the gas refrigeration cycle is 0.478.

(d)

Expert Solution
Check Mark
To determine

The refrigeration load and the COP of the system.

Answer to Problem 79P

The refrigeration load is 24.74kW and the COP of the system is 0.599.

Explanation of Solution

Show the T-s diagram as in Figure (2).

THERMODYNAMICS (LL)-W/ACCESS >CUSTOM<, Chapter 11.10, Problem 79P , additional homework tip  2

Express temperature at state 4s.

T4s=T3[P4P3](k1)/k (XIII)

Here, temperature at state 3 is T3, pressure at state 3 and 4 is P3andP4 respectively.

Express temperature at state 4.

ηT=T3T4T3T4s (XIV)

Express the refrigeration load.

Q˙L=m˙cp(T1T4) (XV)

Express the net work input.

W˙net,in=m˙cp(T2T1)m˙cp(T3T4) (XVI)

Express the coefficient of performance of the system.

COP=Q˙LW˙net,in (XVII)

Conclusion:

Substitute 308.2K for T3, 15 for P4/P3 and 1.4 for k in Equation (XIII).

T4s=(308.2K)[15](1.41)/1.4=194.6K

Substitute 0.85 for ηT308.2K for T3 and 194.6K for T4s in Equation (XIV).

0.85=308.2KT4308.2K194.6KT4=211.6K

Substitute 0.4kg/s for m˙, 1.005kJ/kgK for cp, 211.6K for T4 and 273.2K for T1 in Equation (XV).

Q˙L=(0.4kg/s)(1.005kJ/kgK)(273.2K211.6K)=24.74kJ/s[kWkJ/s]=24.74kW

Hence, the refrigeration load is 24.74kW.

Substitute 0.4kg/s for m˙, 1.005kJ/kgK for cp, 472.5K for T2, 273.2K for T1, 308.2K for T3 and 211.6K for T4 in Equation (XVI).

W˙net,in=[(0.4kg/s)(1.005kJ/kgK)(472.5K273.2K)(0.4kg/s)(1.005kJ/kgK)(308.2K211.6K)]=41.32[kWkJ/s]=41.32kW

Substitute 24.74kW for Q˙L and 41.32kW for W˙net,in in Equation (XVII).

COP=24.74kW41.32kW=0.599

Hence, the coefficient of performance of the system is 0.599.

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A gas refrigeration system utilizing air as the working fluid possesses a pressure ratio of 3. The air is directed into the compressor at 5°C. The high- pressure air is then cooled down to 40°C by rejecting heat to the ambient environment. The refrigerant exits the turbine at -85°C and subsequently absorbs heat from the cooling area prior to its entry into the regenerator. The mass flow rate of air is 0.45 kg/s. Given that the isentropic efficiencies are 82 percent for the compressor and 87 percent for the turbine, and using constant specific heats at ambient temperature, find:  ) The refrigeration load and the COP if this system functioned based on thesimple gas refrigeration cycle.Ensure that the same compressor inlet temperature is maintained as given, andthe turbine inlet temperature is kept constant as calculated, along withidentical compressor and turbine efficiencies.
A gas refrigeration system utilizing air as the working fluid possesses a pressure ratio of 3. The air is directed into the compressor at 5°C. The high- pressure air is then cooled down to 40°C by rejecting heat to the ambient environment. The refrigerant exits the turbine at -85°C and subsequently absorbs heat from the cooling area prior to its entry into the regenerator. The mass flow rate of air is 0.45 kg/s. Given that the isentropic efficiencies are 82 percent for the compressor and 87 percent for the turbine, and using constant specific heats at ambient temperature, find: (a) The effectiveness of the regenerator. (b) The rate at which heat is extracted from the cooling area. (c) The Coefficient of Performance (COP) of the cycle.

Chapter 11 Solutions

THERMODYNAMICS (LL)-W/ACCESS >CUSTOM<

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