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17-Phys-B6 Applied Thermodynamics and Heat Transfer · December 2017

Question 3 of 8: Ammonia vs. R134a — Comparative Vapour-Compression Refrigeration Cycle

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

Notes on this paper

Paper format. 98-Phys-B6 Applied Thermodynamics and Heat Transfer, National Examination December 2017 — a three-hour open-book examination; candidates are expected to bring both a thermodynamics text and a heat-transfer text to make use of the property tables. A complete examination is five questions — either three from Part A (Thermodynamics, Q1–Q4) and two from Part B (Heat Transfer, Q5–Q8), or two from Part A and three from Part B — every question carrying equal value; all eight are solved below as a complete study set. Candidates are invited to state any assumptions where a question is open to interpretation; this licence is used explicitly in Question 4 (the exam's own printed text is ambiguous about whether the piston displacement is 1.00 m³, read here as the intended value) and Question 6 (the external air stream is treated as an effectively infinite, constant-temperature reservoir since no air mass flow rate or duct is specified).

Reference texts. Y. A. Çengel and M. A. Boles, Thermodynamics: An Engineering Approach, 8th ed. (two-phase closed systems, flash chambers, steam turbines, vapour-compression refrigeration, reciprocating compressors); F. P. Incropera and D. P. DeWitt, Fundamentals of Heat and Mass Transfer, 7th ed. (composite cylindrical conduction, internal and external forced convection correlations, natural convection from a vertical plate, heat-exchanger LMTD analysis). Saturation and superheat property values below were computed (Bell et al., IAPWS-95 / REFPROP-quality equations of state for water, ammonia and R134a) and cross-checked against the printed appendix tables on pages 5–8 of the source exam, which they matched to 3–4 significant figures throughout.

Question 3: Ammonia vs. R134a — Comparative Vapour-Compression Refrigeration Cycle

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. An ideal vapour-compression cycle skeleton (saturated liquid into the expansion valve, dry saturated vapour into the compressor) run at identical condenser/evaporator temperatures and identical cooling duty for two candidate refrigerants; the compressor floor efficiency of 90% applies equally to both, so it scales both fluids' actual work by the same factor and cannot change which fluid needs less power — it is evaluated anyway for a defensible absolute number.

Given data
QuantitySymbolValue
Condenser (saturation) temperature$T_{cond}$$34\,{}^{\circ}\text{C}$
Evaporator (saturation) temperature$T_{evap}$$-16\,{}^{\circ}\text{C}$
Compressor isentropic efficiency$\eta_c$90%
Refrigeration effect$\dot Q_L$3.5 kJ/s

Find. Which refrigerant, ammonia or R134a, gives the lower compressor power for the stated cycle and duty.

Enthalpy h (kJ/kg)ln P12s234p-h diagram — ammonia vapour-compression cycle
$p$–$h$ diagram (ammonia cycle shown): 1 (sat. vapour, evaporator exit) → 2s/2 (isentropic / actual compression) → 3 (sat. liquid, condenser exit) → 4 (throttling, $h_4=h_3$) back to state 1.

Approach. For each fluid: state 1 is saturated vapour at $T_{evap}$; state 3 is saturated liquid at $T_{cond}$, and $h_4=h_3$ across the (isenthalpic) expansion valve. Compress isentropically from state 1 to the condenser pressure to get $h_{2s}$, then apply the compressor efficiency to get the actual work; the mass flow rate follows from the refrigeration effect $\dot Q_L=\dot m(h_1-h_4)$, and the compressor power is $\dot m$ times the actual specific work.

  1. Ammonia state points. $P_{evap}=226.25\text{ kPa}$, $P_{cond}=1311.66\text{ kPa}$ (matches the source's own saturation table to better than 0.1%). $h_1=1588.38\text{ kJ/kg}$, $s_1=6.3258\text{ kJ/kg}\cdot\text{K}$, $h_3=h_4=506.67\text{ kJ/kg}$. Isentropic compression to $P_{cond}$ gives $h_{2s}=1846.94\text{ kJ/kg}$, so $$w_{s,NH_3}=h_{2s}-h_1=258.56\text{ kJ/kg}, \qquad w_{a,NH_3}=\frac{w_{s,NH_3}}{\eta_c}=287.29\text{ kJ/kg}$$ The refrigeration effect per unit mass is $h_1-h_4=1081.71\text{ kJ/kg}$ (the printed appendix table gives $h_g(-16\,{}^{\circ}\text{C})-h_f(34\,{}^{\circ}\text{C})=1424.4-342.3=1082.1\text{ kJ/kg}$, within 0.04% — a good cross-check), so $$\dot m_{NH_3}=\frac{\dot Q_L}{h_1-h_4}=\frac{3.5}{1081.71}=0.003236\text{ kg/s}$$ $$\boxed{\dot W_{c,NH_3}=\dot m_{NH_3}\,w_{a,NH_3}=0.003236\times287.29=0.930\text{ kW}}$$
  2. R134a state points. $P_{evap}=157.28\text{ kPa}$, $P_{cond}=862.63\text{ kPa}$. $h_1=389.02\text{ kJ/kg}$, $s_1=1.7379\text{ kJ/kg}\cdot\text{K}$, $h_3=h_4=247.54\text{ kJ/kg}$. Isentropic compression gives $h_{2s}=424.42\text{ kJ/kg}$, so $$w_{s,R134a}=35.40\text{ kJ/kg}, \qquad w_{a,R134a}=\frac{35.40}{0.90}=39.34\text{ kJ/kg}$$ Refrigeration effect per unit mass $h_1-h_4=141.48\text{ kJ/kg}$ (table cross-check: $237.74-97.31=140.43\text{ kJ/kg}$, within 0.7%), so $$\dot m_{R134a}=\frac{3.5}{141.48}=0.02474\text{ kg/s}$$ $$\boxed{\dot W_{c,R134a}=0.02474\times39.34=0.973\text{ kW}}$$
  3. Comparison. Ammonia's much larger latent heat of vaporisation lets it move the same refrigeration duty with roughly $1/8$ the mass flow rate of R134a, more than offsetting its larger specific compression work: $$\boxed{\dot W_{c,NH_3}=0.930\text{ kW} \lt \dot W_{c,R134a}=0.973\text{ kW}}$$ Ammonia requires the lower compressor power (equivalently, $COP_{NH_3}=\dot Q_L/\dot W_{c,NH_3}=3.77$ versus $COP_{R134a}=3.60$).
Question 3 — results
QuantityAmmoniaR134a
Refrigeration effect, $h_1-h_4$1081.71 kJ/kg141.48 kJ/kg
Mass flow rate $\dot m$0.003236 kg/s0.02474 kg/s
Actual compressor work $w_a$287.29 kJ/kg39.34 kJ/kg
Compressor power $\dot W_c$0.930 kW0.973 kW
COP3.773.60