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)
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].
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.
Net work input (part a).
$$w_{net,in}=w_{c,a}-w_{t,a}=117.61-73.84=\boxed{43.78\ \text{kJ/kg}}.$$
Refrigeration effect (part b). Cold air warms from $T_4$ back to $T_1$ at
constant pressure (100 kPa) in the refrigerated space:
$$q_L=h(T_1)-h(T_4)=\boxed{33.60\ \text{kJ/kg}}.$$
Coefficient of performance (part c).
$$\text{COP}=\frac{q_L}{w_{net,in}}=\frac{33.60}{43.78}=\boxed{0.7674}.$$
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.