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04-BS-10 · December 2018

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)

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. 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.

Find. (a) $\dot m_{LT}$, $\dot m_{HT}$ [kg/min]; (b) $\dot W_c$ [kW]; (c) COP; (d) $\dot S_{gen,comp}$ [kW/K].

Entropy s (kJ/kg·K)T (°C)Q3 — Two-evaporator R-134a system (T–s)3471256
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.

  1. 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): $$\dot Q_{LT}=3\times3.517=10.55\ \text{kW},\qquad \dot Q_{HT}=2\times3.517=7.033\ \text{kW}.$$
  2. LT-evaporator branch (3→5→6), $P_{LT}=P_{sat}(-18\ ^\circ\text{C})=144.60$ kPa. Throttle is isenthalpic, $h_5=h_3=255.50$; saturated-vapor exit $h_6=387.79$ kJ/kg: $$\dot m_{LT}=\frac{\dot Q_{LT}}{h_6-h_5}=\frac{10.55}{387.79-255.50}\times60=\boxed{4.785\ \text{kg/min}}.$$
  3. HT-evaporator branch (3→4→7), $P_{HT}=320$ kPa. $h_4=h_3=255.50$; saturated-vapor exit at 320 kPa, $h_7=400.04$ kJ/kg: $$\dot m_{HT}=\frac{\dot Q_{HT}}{h_7-h_4}=\frac{7.033}{400.04-255.50}\times60=\boxed{2.919\ \text{kg/min}}.$$
  4. 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.
  5. Compressor, actual (part b). Isentropic exit at 1 MPa: $h_{2s}=433.94$ kJ/kg; actual: $$w_{c,a}=\frac{h_{2s}-h_1}{\eta_c}=\frac{433.94-392.43}{0.90}=46.12\ \text{kJ/kg},\qquad h_2=h_1+w_{c,a}=438.55\ \text{kJ/kg}$$ $$\dot W_c=\dot m_1\,w_{c,a}=\frac{7.704}{60}\times46.12=\boxed{5.922\ \text{kW}}.$$
  6. 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: $$\dot S_{gen}=\dot m_1(s_2-s_1)=\frac{7.704}{60}(1.7716-1.7576)=\boxed{0.00180\ \text{kW/K}}.$$
QuantityResult
(a) $\dot m_{LT}$, $\dot m_{HT}$4.785, 2.919 kg/min
(b) $\dot W_c$5.922 kW
(c) COP2.969
(d) $\dot S_{gen}$0.00180 kW/K