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17-Phys-B6 Applied Thermodynamics and Heat Transfer · May 2016

Question 4 of 8: Real Freon-12 Vapour-Compression Cycle from Test Data

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 May 2016 — 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 and charts. 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. Where the exam's own "state your assumptions" licence applies (Part A cold-air-standard properties in Question 3; the rectangular-case geometry read from the printed illustration in Question 7), the assumption is flagged explicitly in a check callout rather than hedged inside the answer.

Reference texts. Y. A. Çengel and M. A. Boles, Thermodynamics: An Engineering Approach, 8th ed. (ideal-gas processes, vapour power cycles, gas-turbine/Brayton cycles, vapour-compression refrigeration); F. P. Incropera and D. P. DeWitt, Fundamentals of Heat and Mass Transfer, 7th ed. (conduction with convective boundaries, internal/external convection correlations, natural convection, radiation exchange, cross-flow heat-exchanger effectiveness–NTU analysis).

Question 4: Real Freon-12 Vapour-Compression Cycle from Test Data

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. This is REAL test data, not an idealized four-state cycle: the compressor inlet is superheated above the evaporator-outlet state (suction-line pick-up), the condenser inlet is desuperheated below the compressor-outlet state (discharge-line loss), and the expansion-valve inlet is subcooled further below the condenser-outlet state (liquid-line heat gain). Compression is NOT adiabatic — 3.35 kJ/kg is rejected from the refrigerant while it is being compressed.

Given data (R-12, all states along the loop)
StationPressureTemperature
Compressor inlet150 kPa$0\,{}^{\circ}\text{C}$
Compressor outlet700 kPa$70\,{}^{\circ}\text{C}$
Condenser inlet700 kPa$60\,{}^{\circ}\text{C}$
Condenser outlet700 kPa$15\,{}^{\circ}\text{C}$
Expansion-valve inlet700 kPa$20\,{}^{\circ}\text{C}$
Evaporator outlet150 kPa$-10\,{}^{\circ}\text{C}$
Entropy s (kJ/kg·K)Temperature Tsaturation domecomp,incomp,outcond,incond,outvalve,inevap,out
Fig. 4 — T-s diagram of the actual (non-idealized) R-12 cycle: suction superheat, discharge desuperheat and liquid subcooling are all visible as departures from the idealized four-corner cycle.

Find. The cycle COP and the "thermal efficiency of the compression process" (read as the compressor's isentropic efficiency, since compression here is explicitly non-adiabatic and a comparison against the ideal adiabatic work is the only quantity this phrase can sensibly mean).

Approach. Evaluate R-12 enthalpy at each printed state directly; the refrigeration effect follows from the isenthalpic throttle (valve-inlet enthalpy = evaporator-inlet enthalpy); the actual compressor work follows from a steady-flow energy balance that includes the stated heat loss; the isentropic work uses the compressor-inlet entropy carried to the condenser pressure.

  1. Key enthalpies (R-12). $$h_{\text{comp,in}}(0\,{}^{\circ}\text{C},150\text{ kPa})=355.50\text{ kJ/kg},\quad s_{\text{comp,in}}=1.6159\text{ kJ/kg}\cdot\text{K}$$ $$h_{\text{comp,out}}(70\,{}^{\circ}\text{C},700\text{ kPa})=393.81\text{ kJ/kg}$$ $$h_{\text{valve,in}}(20\,{}^{\circ}\text{C},700\text{ kPa})=219.16\text{ kJ/kg},\qquad h_{\text{evap,out}}(-10\,{}^{\circ}\text{C},150\text{ kPa})=349.55\text{ kJ/kg}$$
  2. Refrigeration effect. The expansion valve is isenthalpic, so $h_{\text{evap,in}}=h_{\text{valve,in}}$: $$q_{\text{evap}}=h_{\text{evap,out}}-h_{\text{valve,in}}=349.55-219.16=\boxed{130.4\text{ kJ/kg}}$$
  3. Actual compressor work. Steady-flow energy balance with heat REJECTED during compression, $q_{\text{out}}=3.35$ kJ/kg: $$w_{\text{actual}}=(h_{\text{comp,out}}-h_{\text{comp,in}})+q_{\text{out}}=(393.81-355.50)+3.35=\boxed{41.66\text{ kJ/kg}}$$
  4. Coefficient of performance. $$\text{COP}=\frac{q_{\text{evap}}}{w_{\text{actual}}}=\frac{130.4}{41.66}=\boxed{3.13}$$
  5. Isentropic compressor work (for the compression-efficiency comparison). Carrying $s_{\text{comp,in}}=1.6159\text{ kJ/kg}\cdot\text{K}$ to 700 kPa isentropically gives $T_{\text{out},s}=57.7\,{}^{\circ}\text{C}$ and $h_{\text{out},s}=385.30$ kJ/kg, so $$w_{\text{isentropic}}=h_{\text{out},s}-h_{\text{comp,in}}=385.30-355.50=29.80\text{ kJ/kg}$$
  6. "Thermal efficiency" of the compression process. $$\eta_{\text{compression}}=\frac{w_{\text{isentropic}}}{w_{\text{actual}}}=\frac{29.80}{41.66}=\boxed{71.5\%}$$
Question 4 — results
QuantityValue
Refrigeration effect, $q_{\text{evap}}$130.4 kJ/kg
Actual compressor work, $w_{\text{actual}}$41.66 kJ/kg
Coefficient of performance, COP3.13
Isentropic compressor work, $w_{\text{isentropic}}$29.80 kJ/kg
Compression-process efficiency, $\eta_{\text{compression}}$71.5%