23-Chem-A1 Process Balances and Chemical Thermodynamics · December 2017
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
National Exams — December 2017 — 16-Chem-A1 Process Balances and Chemical Thermodynamics. Three-hour, open-book exam; any non-communicating calculator permitted. Format: two parts — Part A (Q1–Q3) Process Balances, Part B (Q4–Q6) Chemical Thermodynamics; the candidate answers two questions from each part (four constitute a complete paper, equal value). All six questions are solved below for completeness. Property data not printed on the paper (molar volumes at STP, gas constant, Rankine conversion) are stated explicitly in each Given block as open-book look-ups.
Reference texts: Felder, Rousseau & Bullard, Elementary Principles of Chemical Processes (4th ed., Wiley) — recycle balances, humidity and adiabatic-flame (energy) balances; Himmelblau & Riggs, Basic Principles and Calculations in Chemical Engineering (8th ed.) — multi-unit separation balances; Smith, Van Ness, Abbott & Swihart, Introduction to Chemical Engineering Thermodynamics (8th ed., McGraw-Hill) — cubic equations of state, residual properties, reaction/phase equilibrium and gas-cycle work; supporting property data from Perry’s Chemical Engineers’ Handbook (9th ed.).
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-gas air. States: (1) compressor inlet $T_1=75\,{}^{\circ}\text{F}=534.67$ R at 1 atm; (2) compressor outlet; (3) after cooling $T_3=100\,{}^{\circ}\text{F}=559.67$ R at high $P$; (4) turbine outlet $T_4=55\,{}^{\circ}\text{F}=514.67$ R at 1 atm, into the house. Turbine work drives the compressor; net external work is the shortfall.
Find. COP $=\dfrac{\text{cooling delivered}}{\text{net work in}}$ for (a) reversible and (b) 70%-efficient compressor and turbine.
Approach. Compressor and turbine share the same pressure ratio, so for isentropic operation the temperature ratio $r=(P_2/P_1)^{(\gamma-1)/\gamma}=T_3/T_4$; the cooling effect is $C_p(T_1-T_4)$ and the net work is $W_{\text{comp}}-W_{\text{turb}}$. $C_p$ and $\gamma$ cancel in the COP.
The dramatic collapse from 11.4 to 0.37 is the key lesson: because the reversible cycle’s net work is a small difference of two large, nearly equal work terms, modest component inefficiencies inflate the net work enormously — air-cycle cooling is only attractive when the machinery is very efficient.
| Case | Net work | COP |
|---|---|---|
| (a) Reversible | 1.75 $C_p$ | 11.4 |
| (b) 70% efficient | 54.1 $C_p$ | 0.370 |