Question 3 of 9: Two-Stage R-134a Compression Refrigeration with Flash Chamber
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Examinations — 04-BS-10, Thermodynamics. Three hours. Closed-book exam with one
8.5×11 in. double-sided sheet of notes allowed and an approved Casio or Sharp calculator;
property tables and charts are supplied and interpolation is not necessary — the closest tabular
value may be used. Part A: two of three 20-mark questions; Part B: four of six 15-mark questions.
Every question is answered in full.
Reference texts. Cengel & Boles, Thermodynamics: An Engineering
Approach, 8th ed. (Vapor Power Cycles Ch. 10; Gas Power Cycles Ch. 9; Refrigeration Cycles
Ch. 11; Gas Mixtures Ch. 13; Psychrometrics Ch. 14; Exergy Ch. 8).
Check — paper format. The paper is headed "National Examination – May 2019 / 04-BS-10, Thermodynamics, 3 Hours Duration": four question pages followed by a 22-page appendix of property tables and a psychrometric chart. All nine questions are answered in full (Part A questions 1–3 at 20 marks each, Part B questions 4–9 at 15 marks each; the paper asks for two of Part A and four of Part B). Two wording notes from the printed page: Question 2's final sub-part is printed "(d) the second law efficiency" after an earlier "(d)", i.e. the paper repeats the letter, and Question 3(d) is printed "in kJ/K" for a quantity that is a rate of exergy destruction in kJ/s.
Question 3: Two-Stage R-134a Compression Refrigeration with Flash Chamber (Part A – 20 marks)
[Part (d) is printed "in kJ/K"; the quantity asked for is a rate of exergy
destruction and is reported below in kJ/s.]
Given. $P_{low}=0.14$ MPa (evaporator), $P_{flash}=0.5$ MPa,
$P_{high}=1.0$ MPa (condenser). $\eta_c=0.90$ for both compressors. Mass flow through the condenser
(and high-pressure compressor) $\dot m_{cond}=0.25$ kg/s — part (a) then asks for the
DIFFERENT, smaller flow rate through the evaporator/low-pressure compressor, found from the
flash-chamber mass+energy balance. $T_0=300$ K. The printed apparatus diagram shows a single flash
chamber with TWO inlets (the throttled condensate, state 6, and the low-pressure compressor
discharge, state 2) and two outlets (saturated vapour, state 3, to compressor 2 and saturated liquid,
state 7, to the second throttle), so the chamber is an equilibrium separator.
State
Description
P (MPa)
T (°C)
h (kJ/kg)
s (kJ/kg·K)
1
Evaporator exit, sat. vapor
0.14
−18.76
387.32
1.7402
2
Low-P compressor exit (actual)
0.5
24.97
416.37
1.7500
3
Flash chamber vapor exit
0.5
15.73
407.47
1.7197
4
High-P compressor exit (actual)
1.0
43.15
423.40
1.7247
5
Condenser exit, sat. liquid
1.0
39.39
255.50
—
6
Throttled into flash chamber
0.5
15.73
255.50
—
7
Flash chamber liquid exit
0.5
15.73
221.50
—
8
Throttled into evaporator
0.14
−18.76
221.50
—
Find. (a) $\dot m_{evap}$; (b) $\dot Q_L$; (c) COP; (d) $\dot X_{dest}$ in both
compressors.
Fig. Q3 — P–h state points, two-stage flash-chamber cycle. Low-pressure
loop $8\to1\to2$, high-pressure loop $3\to4\to5\to6$, flash chamber mixes $2$ and $6$ into vapor
$3$ / liquid $7$.
Fig. Q3b — the same eight state points on the T–s diagram the question asks for, with the R-134a saturation dome. $8\to1$ evaporator, $1\to2$ low-pressure compressor, $3\to4$ high-pressure compressor, $4\to5$ condenser, $5\to6$ and $7\to8$ throttles; the flash chamber separates the mixed stream at 0.5 MPa into saturated vapour $3$ and saturated liquid $7$.
Approach
Fix the eight states (R-134a), then close the flash chamber with a combined
mass-and-energy balance to solve for the unknown low-pressure (evaporator) flow rate, since only the
high-pressure (condenser) flow rate is given.
Flash-chamber balance — evaporator mass flow rate, part (a). Steady-flow
mass and energy balance on the flash chamber ($\dot m_{evap}$ through state 2 in,
$\dot m_{cond}$ through state 6 in; $\dot m_{evap}$ leaves as liquid state 7, $\dot m_{cond}$ leaves
as vapor state 3):
$$\dot m_{evap}\,h_2+\dot m_{cond}\,h_6=\dot m_{evap}\,h_7+\dot m_{cond}\,h_3$$
$$\dot m_{evap}=\dot m_{cond}\,\frac{h_3-h_6}{h_2-h_7}=0.25\times\frac{407.47-255.50}{416.37-221.50}
=0.25\times0.7799=\boxed{0.1950\ \text{kg/s}}.$$
Refrigeration capacity, part (b). All the evaporator flow passes through
$8\to1$, with $h_8=h_7$ (isenthalpic throttle):
$$\dot Q_L=\dot m_{evap}(h_1-h_8)=0.1950\times(387.32-221.50)=\boxed{32.33\ \text{kJ/s}}.$$
Total compressor work and COP, part (c).
$$\dot W_{c1}=\dot m_{evap}(h_2-h_1)=0.1950\times29.05=5.664\ \text{kW};\quad
\dot W_{c2}=\dot m_{cond}(h_4-h_3)=0.25\times15.92=3.981\ \text{kW}.$$
$$\dot W_{total}=5.664+3.981=9.645\ \text{kW}\quad\Rightarrow\quad
COP=\frac{\dot Q_L}{\dot W_{total}}=\frac{32.33}{9.645}=\boxed{3.352}.$$
Exergy destruction in both compressors, part (d). Each compressor is adiabatic,
so $\dot X_{dest}=\dot m\,T_0\,\Delta s$ across it:
$$\dot X_{c1}=\dot m_{evap}\,T_0(s_2-s_1)=0.1950\times300\times(1.7500-1.7402)=\boxed{0.573\ \text{kJ/s}}$$
$$\dot X_{c2}=\dot m_{cond}\,T_0(s_4-s_3)=0.25\times300\times(1.7247-1.7197)=\boxed{0.378\ \text{kJ/s}}$$