Question 3 of 9: Two-Evaporator R-134a Refrigeration System
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Exam 04-BS-10, Thermodynamics — December 2018. 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, interpolation not required — the closest tabular value may be used). 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, R-134a, air, N₂, O₂, humid
air) were computed from high-accuracy equations of state in place of printed property-table interpolation; every boxed numeric result.
Question 3: Two-Evaporator R-134a Refrigeration System (20 marks)
Given. LT evaporator: $-18\ ^\circ$C, saturated vapor exit, $\dot Q_{LT}=3$ tons.
HT evaporator: saturated vapor exit at 320 kPa, $\dot Q_{HT}=2$ tons. $P_{cond}=1$ MPa, saturated
liquid at condenser exit. $\eta_c=0.90$. No pressure drop across either evaporator or the condenser.
Both evaporator feed lines are throttled independently from the same condenser-exit liquid; the
higher-pressure evaporator's vapor is throttled down to the low-temperature evaporator's pressure
before the two streams mix at the single compressor's suction.
Fig. Q3 — T–s on the real R-134a dome: solid path is the LT-evaporator
loop (3→5 throttle, 5→6 evaporation at $-18\ ^\circ$C, 6→1 mixing, 1→2 actual
compression, 2→3 condensing); dashed path is the HT-evaporator branch (3→4 throttle, 4→7
evaporation at 320 kPa) whose vapor (state 7) is throttled down to the LT pressure before joining
state 6 at the compressor inlet (state 1).
Approach
Fix the condenser-exit liquid state once, then run each evaporator's own throttle+evaporation leg
independently (LT at $-18\ ^\circ$C, HT at 320 kPa) to get each branch's mass flow from its stated
capacity. The HT-evaporator vapor is throttled down to the LT pressure and mixed with the LT vapor in
an energy balance to fix the single compressor-inlet state, after which the compressor is a standard
isentropic-efficiency calculation.
Condenser exit and evaporator capacities in kW. Saturated liquid at 1 MPa:
$h_3=255.50$ kJ/kg. Converting tons to kW ($1\ \text{ton}=211/60=3.517$ kW):
$$\dot Q_{LT}=3\times3.517=10.55\ \text{kW},\qquad \dot Q_{HT}=2\times3.517=7.033\ \text{kW}.$$
Mixing at the compressor inlet (state 1). State 7 is throttled down to
$P_{LT}$ (isenthalpic, $h_8=h_7=400.04$) and combines with state 6:
$$\dot m_1=\dot m_{LT}+\dot m_{HT}=4.785+2.919=7.704\ \text{kg/min}$$
$$h_1=\frac{\dot m_{LT}\,h_6+\dot m_{HT}\,h_8}{\dot m_1}
=\frac{4.785(387.79)+2.919(400.04)}{7.704}=392.43\ \text{kJ/kg}.$$
At $P_{LT}=144.60$ kPa this fixes a superheated state, $T_1=-12.35\ ^\circ$C ($5.65\ ^\circ$C of
superheat above $T_{sat}=-18\ ^\circ$C), $s_1=1.7576$ kJ/kg·K.
Compressor, actual (part b). Isentropic exit at 1 MPa:
$h_{2s}=433.94$ kJ/kg; actual:
$$w_{c,a}=\frac{h_{2s}-h_1}{\eta_c}=\frac{433.94-392.43}{0.90}=46.12\ \text{kJ/kg},\qquad
h_2=h_1+w_{c,a}=438.55\ \text{kJ/kg}$$
$$\dot W_c=\dot m_1\,w_{c,a}=\frac{7.704}{60}\times46.12=\boxed{5.922\ \text{kW}}.$$
COP (part c) and compressor entropy increase (part d).
$$\text{COP}=\frac{\dot Q_{LT}+\dot Q_{HT}}{\dot W_c}=\frac{10.55+7.033}{5.922}=\boxed{2.969}.$$
At $P=1$ MPa, $h_2=438.55$ kJ/kg fixes $s_2=1.7716$ kJ/kg·K; the compressor is adiabatic so its
entropy generation equals its entropy rise directly:
$$\dot S_{gen}=\dot m_1(s_2-s_1)=\frac{7.704}{60}(1.7716-1.7576)=\boxed{0.00180\ \text{kW/K}}.$$