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04-BS-10 · December 2015

Question 3 of 9: Gas Refrigeration Cycle (Reverse Brayton)

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

National Exam 04-BS-10, Thermodynamics — December 2015. 3 hours, Closed-Book Exam (approved calculator and one double-sided 8.5x11-inch aid sheet permitted; property tables and charts supplied in an appendix). Part A: answer 2 of Questions 1-3 (20 marks each). Part B: answer 4 of Questions 4-9 (15 marks each), for a 100-mark paper. Only the first two Part-A and first four Part-B questions as they appear in the answer book are marked. All nine questions (Part A complete, Part B complete) are solved below for completeness.

Reference texts: Cengel & Boles, Thermodynamics: An Engineering Approach, 8th ed.; Moran, Shapiro, Boettner & Bailey, Fundamentals of Engineering Thermodynamics, 8th ed. All state properties (water/steam, air, N₂, CO₂, moist air) were computed from high-accuracy equations of state in place of printed property-table interpolation; every boxed numeric result.

Question 3: Gas Refrigeration Cycle (Reverse Brayton) (20 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given. Compressor inlet (state 1): $P_1=100$ kPa, $T_1=270$ K. Pressure ratio $=3$ ($P_2=300$ kPa). Turbine inlet (state 3): $T_3=310$ K at 300 kPa, expanding to 100 kPa. $\eta_c=0.85$, $\eta_t=0.88$. Variable specific heats.

Find. (a) $w_{net,in}$ [kJ/kg]; (b) $q_L$ [kJ/kg]; (c) COP; (d) $s_{gen}$ in compressor and turbine [kJ/kg·K].

Entropy s (kJ/kg·K)T (°C)Q3 — Gas refrigeration cycle, air (T–s, variable-cp, no dome)1234
Fig. Q3 — T–s state points for the gas (reverse-Brayton) refrigeration cycle (1→2 actual compressor, 2→3 constant-P heat rejection, 3→4 actual turbine/expander, 4→1 constant-P heat absorption — refrigeration effect). No saturation dome for an ideal-gas working fluid.

Approach

This is the reverse (refrigeration) counterpart of the Brayton cycle: the compressor raises pressure from the cold space, an ambient-temperature heat exchanger rejects heat at constant pressure down to the given turbine-inlet temperature, an expander (turbine) drops the pressure and temperature further than a throttle would, and the resulting cold air absorbs the refrigeration load before returning to the compressor inlet. Solve the compressor and turbine independently with the same variable-cp root-finding method as the power-cycle version, then combine for net work, cooling load, and COP.

  1. Compressor (1→2), 100→300 kPa. Isentropic exit $T_{2s}=369.22$ K gives $w_{c,s}=99.97$ kJ/kg. Actual: $$w_{c,a}=\frac{99.97}{0.85}=\boxed{117.61\ \text{kJ/kg}},\qquad T_2=386.66\ \text{K}\ (113.51\ ^\circ\text{C}).$$
  2. Turbine/expander (3→4), 300→100 kPa. Isentropic exit $T_{4s}=226.58$ K gives $w_{t,s}=83.91$ kJ/kg. Actual: $$w_{t,a}=0.88\times83.91=\boxed{73.84\ \text{kJ/kg}},\qquad T_4=236.59\ \text{K}\ (-36.56\ ^\circ\text{C}).$$
  3. Net work input (part a). $$w_{net,in}=w_{c,a}-w_{t,a}=117.61-73.84=\boxed{43.78\ \text{kJ/kg}}.$$
  4. Refrigeration effect (part b). Cold air warms from $T_4$ back to $T_1$ at constant pressure (100 kPa) in the refrigerated space: $$q_L=h(T_1)-h(T_4)=\boxed{33.60\ \text{kJ/kg}}.$$
  5. Coefficient of performance (part c). $$\text{COP}=\frac{q_L}{w_{net,in}}=\frac{33.60}{43.78}=\boxed{0.7674}.$$
  6. Entropy generation, compressor and turbine (part d). Both are adiabatic, so $s_{gen}$ equals the actual entropy rise across each: $$s_{gen,c}=s(T_2,P_2)-s(T_1,P_1)=\boxed{0.04669\ \text{kJ/kg}\cdot\text{K}}$$ $$s_{gen,t}=s(T_4,P_1)-s(T_3,P_2)=\boxed{0.04349\ \text{kJ/kg}\cdot\text{K}}$$ Both positive, consistent with irreversible (non-isentropic) adiabatic devices.
QuantityResult
(a) $w_{net,in}$43.78 kJ/kg
(b) $q_L$33.60 kJ/kg
(c) COP0.7674
(d) $s_{gen,c}$0.04669 kJ/kg·K
(d) $s_{gen,t}$0.04349 kJ/kg·K