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Modern Engineering Thermodynamics

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14.18 Second Law Analysis of Refrigeration Cycles 581<br />

Note that the designer computes pressure losses of 75.0 kPa in the condenser and 27.0 kPa in the evaporator. The refrigerant<br />

mass flow rate is 0.500 kg/s, the local environmental temperature is T 0 = 25.0°C, and the isentropic efficiency of the<br />

compressor is 70.0%. Determine<br />

a. The irreversibility rate of each component in the system and the total irreversibility rate of the system.<br />

b. The system COP and ε (the first and second law efficiencies).<br />

c. Select the component with the highest irreversibility rate and suggest ways to improve it.<br />

Solution<br />

Using Figure 14.36 as the illustration for this example, the properties at the four stations can be found in Tables C.7e, C.7f,<br />

and C.8d as<br />

Station 1 Station 2s Station 3 Station 4h<br />

Compressor inlet Compressor outlet Condenser outlet Expansion valve outlet<br />

x 1 = 1:00 p 2s = 800: kPa x 3 = 0:0 h 4h = h 3<br />

T 1 = −20:0°C s 2s = s 1 p 3 = 725 kPa p 4h = 160 kPa<br />

= 0:9332 kJ/kg.K h 3 = 87:46 kJ/kg h 4h = 87:46 kJ/kg<br />

h 1 = 235:31 kJ/kg h 2s = 271:10 kJ/kg s 3 = 0:3257 kJ/kg.K x 4h = 0:280<br />

s 1 = 0:9332 kJ/kg.K T 2s = 39:8°C T 3 = 27:9°C s 4h = 0:3449 kJ/kg.K<br />

p 1 = 132:99 kPa<br />

T 4h = −15:6°C<br />

Conditions at stations 2s, 3, and 4h are determined by interpolation in Table C.7f or with a computer program containing the<br />

appropriate properties. Also, note that the condenser outlet temperature T 3 is about 3°C above the environmental temperature<br />

of T 0 = 25°C, which is an appropriate temperature drop across the wall of the condenser. A temperature drop of this magnitude<br />

also occurs in the evaporator, so the temperature of the refrigerated space is about −12.6°C instead of −15.6°C.<br />

We can now determine the actual conditions at the outlet of the compressor from the two properties h 2 = (h 2s − h 1 )/(η s ) comp +<br />

h 1 = 288.03 kJ/kg and p 2 = p 2s = 800 kPa. Interpolation in Table C.7f in Thermodynamic Tables to accompany <strong>Modern</strong> <strong>Engineering</strong><br />

<strong>Thermodynamics</strong> (or through the use of an appropriate computer program) gives the following additional properties at this state:<br />

s 2 = 0:9814 kJ=kg . KandT 2 = 54:97°C<br />

The condenser and evaporator heat transfer rates and the compressor work rate are<br />

Now we can calculate the desired quantities.<br />

_Q condenser = _m ref ðh 3 − h 2 Þ = ð0:5kg/sÞð87:46 − 288:03 kJ/kgÞ = −100:3 kJ/s<br />

_Q evaporator = _m ref ðh 1 − h 4h Þ = ð0:5kg/sÞð235:31 − 87:46 kJ/kgÞ = 73:9 kJ/s<br />

_Q compressor = _m ref ðh 2 − h 1 Þ = ð0:5kg/sÞð288:03 − 235:31 kJ/kgÞ = 26:36 kJ/s<br />

a. The irreversibility rate of the compressor is given by<br />

_I adiabatic<br />

= _m ref T 0 ðs 2 − s 1 Þ<br />

compressor<br />

<br />

= 0:500 kJ<br />

<br />

<br />

ð25:0 + 273:15 KÞ 0:9814 − 0:9317 kJ<br />

<br />

s<br />

kg.K<br />

= 7:41 kJ = 7:41 kW<br />

s<br />

<br />

Q<br />

_I condenser = T 0 _m ref ðs 3 − s 2 Þ − _ <br />

condenser<br />

T 0<br />

_I expansion<br />

valve<br />

<br />

= ð25:0 + 273:15 KÞ 0:500 kg <br />

0:3257 − 0:9814 kJ<br />

<br />

s<br />

kg.K<br />

= 2:55 kJ = 2:55 kW<br />

s<br />

= _m ref T 0 ðs 4h − s 3 Þ<br />

−<br />

<br />

−100:3 kJ/s<br />

25:0 + 273:15 K<br />

<br />

= 0:500 kg <br />

<br />

ð25:0 + 273:15 KÞ 0:3449 − 0:3257 kJ<br />

<br />

s<br />

kg.K<br />

= 2:86 kJ<br />

s = 2:86 kW (Continued )

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