22-Mec-A1 Applied Thermodynamics and Heat Transfer · December 2019
Question 3 of 8: Reciprocating air compressor power
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format: National Examination 16-Mec-A1 Applied Thermodynamics and Heat Transfer, 3 hours, open book. Eight questions of equal value: Part A — Thermodynamics (Q1–Q4) and Part B — Heat Transfer (Q5–Q8). A complete paper is any five questions (three from one part and two from the other).
Reference texts: Çengel & Boles, Thermodynamics: An Engineering Approach (9th ed., McGraw-Hill) — ideal-gas processes and entropy generation, polytropic compression, rigid-vessel charging, the reciprocating air compressor, throttling/flash separation, the steam turbine, and vapour-compression refrigeration/heat-pump cycles; Çengel & Ghajar, Heat and Mass Transfer (6th ed.) and Incropera, DeWitt, Bergman & Lavine, Fundamentals of Heat and Mass Transfer (8th ed., Wiley) — steady radial conduction through a cylindrical wall with convection, conduction with uniform internal generation, transient (lumped) cooling by combined convection and radiation, and the effectiveness–NTU method for shell-and-tube exchangers. Steam and Freon-12 (R-12) properties are evaluated, which reproduces the IAPWS steam tables and the standard R-12 property tables to graphing accuracy; enthalpy differences (the only quantities used) are datum-independent. Air and combustion gases are treated as ideal with constant specific heats ($\gamma=1.4$, $R=0.287\ \text{kJ/kg}\cdot\text{K}$, $c_p=1.005$, $c_v=0.718\ \text{kJ/kg}\cdot\text{K}$).
Question 3 — Reciprocating air compressor power (Part A, equal value)
Find. Shaft (brake) power to drive the compressor.
Approach. The swept-volume rate from the geometry and speed, de-rated by $\eta_v$, gives the induced air rate at suction; the reversible-adiabatic (isentropic) indicated work per unit volume then follows, and dividing by the compression efficiency yields the required drive power.
Swept volume per revolution and its rate.
$$V_\text{sw}=\frac{\pi}{4}D^2L=\frac{\pi}{4}(0.075)^2(0.100)=4.418\times10^{-4}\ \text{m}^3,\quad \dot V_\text{sw}=V_\text{sw}\frac{N}{60}=5.890\times10^{-3}\ \text{m}^3/\text{s}$$
Induced (actual) air rate at suction.
$$\dot V_1=\eta_v\,\dot V_\text{sw}=0.80(5.890\times10^{-3})=\boxed{4.712\times10^{-3}\ \text{m}^3/\text{s}}$$
Reversible-adiabatic indicated power. With $r_p=P_2/P_1=4.066$,
$$\dot W_s=\frac{\gamma}{\gamma-1}P_1\dot V_1\!\left[r_p^{\frac{\gamma-1}{\gamma}}-1\right]=\frac{1.4}{0.4}(101.325)(4.712\times10^{-3})\big[4.066^{0.2857}-1\big]=0.824\ \text{kW}$$
Drive power from the compression efficiency.
$$\dot W_\text{brake}=\frac{\dot W_s}{\eta_c}=\frac{0.824}{0.90}=\boxed{0.915\ \text{kW}}$$
Check — interpretation of "thermal efficiency of the compression process".
The phrase is read as the compressor's isentropic (adiabatic) efficiency, i.e. the ideal reversible-adiabatic work is 90 % of the actual, so the required power is $\dot W_s/0.90$. The machine is taken as single-acting (one induction per revolution). If it were double-acting the induced volume — and hence the power — would roughly double (≈ 1.83 kW). The delivery pressure 412 kPa is treated as absolute. All three assumptions are standard for this stem; the efficiency and $\eta_v$ enter only as scalar multipliers, so the method is unchanged if a different convention is adopted.