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04-BS-10 · May 2016

Question 7 of 9: Adiabatic Steam Turbine, Efficiency from a Measured Work Output

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

Notes on this paper

National Exam 04-BS-10, Thermodynamics — May 2016. 3 hours, Closed-Book Exam (approved calculator and one double-sided 8.5x11-inch aid sheet permitted; property tables and charts supplied in an appendix, interpolation not required). Part A: answer 2 of Questions 1-3 (20 marks each). Part B: answer 4 of Questions 4-9 (15 marks each), for a 100-mark paper. Only the first two Part-A and first four Part-B questions as they appear in the answer book are marked. All nine questions (Part A complete, Part B complete) are solved below for completeness.

Reference texts: Cengel & Boles, Thermodynamics: An Engineering Approach, 8th ed.; Moran, Shapiro, Boettner & Bailey, Fundamentals of Engineering Thermodynamics, 8th ed. All state properties (water/steam, R-134a, air, N₂, CO₂, moist air) were computed from high-accuracy equations of state in place of printed property-table interpolation; every boxed numeric result.

Question 7: Adiabatic Steam Turbine, Efficiency from a Measured Work Output (15 marks)

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. Inlet: $P_1=1.0$ MPa, $T_1=320\ ^\circ$C. Exit pressure $P_2=20$ kPa. Insulated (adiabatic) turbine, $\dot m=10$ kg/s. Actual work developed $w_{actual}=630$ kJ/kg.

Find. (a) $\eta_t$; (b) $T_2$; (c) $x_2$; (d) reversible or not?

Approach

Fix the inlet state, then find the isentropic exit enthalpy at 20 kPa from the inlet entropy to get the isentropic (maximum possible) work. The isentropic efficiency is the ratio of the actual measured work to that isentropic work. The actual exit enthalpy follows directly from the actual work by an energy balance, which fixes the actual exit state (and its entropy, for the reversibility check).

  1. Inlet state. At 1.0 MPa, 320°C: $h_1=3094.36$ kJ/kg, $s_1=7.1979$ kJ/kg·K.
  2. Isentropic exit and efficiency (part a). At 20 kPa with $s_{2s}=s_1=7.1979$ kJ/kg·K, the exit is wet: $h_{2s}=2372.59$ kJ/kg, giving isentropic work $w_s=h_1-h_{2s}=3094.36-2372.59=721.78$ kJ/kg. $$\eta_t=\frac{w_{actual}}{w_s}=\frac{630}{721.78}=\boxed{0.8728\ (87.3\%)}.$$
  3. Actual exit state (parts b, c). Energy balance on the adiabatic turbine: $$h_2=h_1-w_{actual}=3094.36-630=2464.36\ \text{kJ/kg}.$$ At 20 kPa, $h_f=251.42$ kJ/kg and $h_g=2608.94$ kJ/kg, so $h_2$ lies between them — a two-phase mixture, with $T_2=T_{sat}(20\ \text{kPa})=\boxed{60.06\ ^\circ\text{C}}$ and $$x_2=\frac{h_2-h_f}{h_g-h_f}=\frac{2464.36-251.42}{2608.94-251.42}=\boxed{0.9387}.$$
  4. Reversibility check (part d). Entropy at the actual exit state: $s_2=s_f+x_2 s_{fg}=7.4733$ kJ/kg·K. Since $s_2=7.4733>s_1=7.1979$ kJ/kg·K, entropy increased across this adiabatic turbine, so $$\boxed{\text{the process is irreversible}}$$ (consistent with $\eta_t=87.3\%<100\%$ — a truly reversible adiabatic turbine would be isentropic, $s_2=s_1$, and would achieve $\eta_t=100\%$).
QuantityResult
(a) $\eta_t$0.8728 (87.3%)
(b) $T_2$60.06°C
(c) $x_2$0.9387
(d)Irreversible ($s_2>s_1$)