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22-Agric-A3 Heat Engineering · May 2018

Question 1 of 4: R-134a Ideal Vapor-Compression Refrigeration Cycle

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

Notes on this paper

National Exams — May 2018 — 04-Agric-A3 Heat Engineering. Three-hour, open-book exam; any non-communicating calculator permitted. Four questions constitute a complete paper, each of equal value, and all four questions require calculation — the first four problems as printed are worked below in full.

Reference texts: M.J. Moran, H.N. Shapiro, D.D. Boettner & M.B. Bailey, Fundamentals of Engineering Thermodynamics, 8th ed. (ideal vapor-compression refrigeration cycle, R-134a property tables); Y.A. Çengel & A.J. Ghajar, Heat and Mass Transfer: Fundamentals and Applications, 5th ed. (convection coefficients, forced-convection boundary layers); F.P. Incropera & D.P. DeWitt, Fundamentals of Heat and Mass Transfer, 7th ed. (Blasius boundary-layer solution, Table 6.1); J.P. Holman, Heat Transfer, 10th ed. (radiation view factors for coaxial disks and enclosures).

Problem 1: R-134a Ideal Vapor-Compression Refrigeration Cycle (25 points)

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. Ideal vapor-compression cycle (compressor, condenser, expansion valve, evaporator); refrigerant R-134a; saturated vapor enters the compressor at T₁ = 0°C; saturated liquid leaves the condenser at T₃ = 26°C; isentropic compression 1→2s; isenthalpic throttling 3→4; mass flow rate 0.08 kg/s.

StateConditionT
1 (compressor inlet)saturated vapor0°C
2s (compressor exit)superheated, isentropic from 1—
3 (condenser exit)saturated liquid26°C
4 (evaporator inlet)throttled from 3, h₄=h₃0°C

Find. (a) The compressor power ḏc in kW; (b) the coefficient of performance, COP.

Approach. Fix states 1 and 3 from the saturation properties at the two reservoir temperatures, get state 2s by following the isentrope from state 1 up to the condenser pressure, get state 4 by throttling (constant h) from state 3 down to the evaporator pressure, then apply the steady-flow energy balance to the compressor and evaporator.

Enthalpy h (kJ/kg)ln P12s34P-h diagram - R-134a vapor-compression cycle
P–h diagram of the ideal cycle: 1→2s isentropic compression, 2s→3 condensation at constant P, 3→4 isenthalpic throttling, 4→1 evaporation at constant P.
Check: the source supplies only a saturation-property table for R-134a (Table A-10, reproduced on the exam's last page); state 2s is superheated, so no table entry in the source covers it directly. State 2s is fixed here from the R-134a Helmholtz-energy equation of state — the same real-gas surface an open-book candidate would read off a superheated R-134a table (e.g. Moran/Shapiro Table A-12 or Çengel Table A-13). This agrees with the source's own saturation values (Table A-10) to within about 0.7% at both 0°C and 26°C, so the same reference state is used consistently for all four cycle points and cancels out of every energy difference used below.
  1. State 1 — saturated vapor entering the compressor. At T₁ = 0°C, the saturation pressure is p₁ = 2.93 bar, and $$h_1 = 398.60\ \text{kJ/kg}, \qquad s_1 = 1.7271\ \text{kJ/kg}\cdot\text{K}$$
  2. State 3 — saturated liquid leaving the condenser. At T₃ = 26°C, the saturation pressure is p₃ = 6.85 bar, and $$h_3 = 235.97\ \text{kJ/kg}$$
  3. State 2s — isentropic compression to the condenser pressure. Following the s₁ = 1.7271 kJ/kg·K isentrope up to p₃ = 6.85 bar lands in the superheated region, only $T_{2s}-T_{sat}(p_3) \approx 3.3^{\circ}\text{C}$ above the condensing temperature (R-134a's saturated-vapor line is nearly vertical over this modest pressure ratio, so little superheat is generated), giving $$h_{2s} = 416.21\ \text{kJ/kg}$$
  4. State 4 — throttling to the evaporator pressure. The expansion valve is adiabatic with no work, so $h_4 = h_3 = 235.97$ kJ/kg (constant-enthalpy line down to p₁ = 2.93 bar, ending in the two-phase region).
  5. Compressor power. A steady-flow energy balance on the adiabatic compressor gives $$\dot{W}_c = \dot{m}\left(h_{2s}-h_1\right) = 0.08\ \frac{\text{kg}}{\text{s}}\times(416.21-398.60)\ \frac{\text{kJ}}{\text{kg}} = \boxed{1.41\ \text{kW}}$$
  6. Coefficient of performance. The refrigerating effect is $\dot{Q}_{in}=\dot{m}(h_1-h_4)=0.08\times(398.60-235.97)=13.01\ \text{kW}$, so $$\text{COP} = \frac{\dot{Q}_{in}}{\dot{W}_c} = \frac{13.01}{1.41} = \boxed{9.24}$$ For reference, the Carnot COP between the same two reservoirs is $T_C/(T_H-T_C)=273.15/26=10.51$, so the ideal cycle here reaches about 88% of the Carnot limit — plausible given the small superheat and the modest 26°C temperature lift.
QuantityResult
Compressor power, ḏc1.41 kW
Coefficient of performance, COP9.24
(reference) Carnot COP, same reservoirs10.51
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