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17-Phys-B6 Applied Thermodynamics and Heat Transfer · December 2017

Question 2 of 8: Flash-Chamber Separation and Steam Turbine Power

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 December 2017 — 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. 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. Candidates are invited to state any assumptions where a question is open to interpretation; this licence is used explicitly in Question 4 (the exam's own printed text is ambiguous about whether the piston displacement is 1.00 m³, read here as the intended value) and Question 6 (the external air stream is treated as an effectively infinite, constant-temperature reservoir since no air mass flow rate or duct is specified).

Reference texts. Y. A. Çengel and M. A. Boles, Thermodynamics: An Engineering Approach, 8th ed. (two-phase closed systems, flash chambers, steam turbines, vapour-compression refrigeration, reciprocating compressors); F. P. Incropera and D. P. DeWitt, Fundamentals of Heat and Mass Transfer, 7th ed. (composite cylindrical conduction, internal and external forced convection correlations, natural convection from a vertical plate, heat-exchanger LMTD analysis). Saturation and superheat property values below were computed (Bell et al., IAPWS-95 / REFPROP-quality equations of state for water, ammonia and R134a) and cross-checked against the printed appendix tables on pages 5–8 of the source exam, which they matched to 3–4 significant figures throughout.

Question 2: Flash-Chamber Separation and Steam Turbine Power

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. Saturated LIQUID water at 300 kPa is throttled (adiabatically, no work) in a flash chamber to 150 kPa, where it separates by gravity into a saturated-liquid stream (drained from the bottom) and a saturated-vapour stream (drawn off the top); the vapour stream alone feeds a steam turbine of isentropic efficiency 90% that exhausts at 15 kPa.

Given data
QuantitySymbolValue
Total mass flow into flash chamber$\dot m_1$100 kg/s
Flash-chamber inlet pressure$P_1$300 kPa (sat. liquid)
Flash-chamber exit pressure$P_2$150 kPa
Turbine isentropic efficiency$\eta_t$90%
Turbine exhaust pressure$P_4$15 kPa

Find. The turbine power output $\dot W_t$, with the processes sketched on a $T$–$s$ diagram.

FlashChamberSteamTurbine1: sat. water300 kPa, 100 kg/s2: sat. liquid150 kPa, 95.76 kg/s3: sat. vapour150 kPa, 4.24 kg/sWork output4: 15 kPa
Flash chamber fed by saturated liquid at 300 kPa; the saturated-vapour stream drawn off the top alone feeds the steam turbine.

Approach. The flash chamber is an adiabatic throttle (no work, negligible ΔKE/ΔPE), so its steady-flow energy equation collapses to $h_1=h_2$; splitting that mixed enthalpy between the saturated-liquid and saturated-vapour states at 150 kPa gives the vapour quality $x_2$, and hence the mass flow rate actually entering the turbine. The turbine is then a standard isentropic-efficiency expansion from saturated vapour at 150 kPa to 15 kPa.

  1. Flash-chamber energy balance — vapour fraction. Sat. liquid at 300 kPa: $h_1=561.43\text{ kJ/kg}$. At 150 kPa: $h_f=467.13\text{ kJ/kg}$, $h_g=2693.11\text{ kJ/kg}$. Since the throttle conserves enthalpy, $h_1=h_2=x_2h_g+(1-x_2)h_f$, so $$x_2=\frac{h_1-h_f}{h_g-h_f}=\frac{561.43-467.13}{2693.11-467.13}$$ $$\boxed{x_2=0.0424}$$ The vapour stream feeding the turbine is therefore $\dot m_{vap}=x_2\dot m_1=0.0424\times100=4.236\text{ kg/s}$ (the remaining 95.76 kg/s leaves as saturated liquid and is not used further).
  2. Turbine inlet and isentropic exit state. State 3 (turbine inlet) is saturated vapour at 150 kPa: $h_3=h_g=2693.11\text{ kJ/kg}$, $s_3=s_g=7.2230\text{ kJ/kg}\cdot\text{K}$. Expanding isentropically to 15 kPa ($s_{4s}=s_3$), with $s_f=0.7549$, $s_g=7.2536\text{ kJ/kg}\cdot\text{K}$ at 15 kPa: $$\begin{aligned} x_{4s}&=\frac{s_3-s_f}{s_g-s_f}=0.8919 \\ h_{4s}&=h_f+x_{4s}h_{fg}=225.99+0.8919\times2373.14=2341.79\text{ kJ/kg} \end{aligned}$$ so the isentropic specific work is $$w_s=h_3-h_{4s}=2693.11-2341.79=351.32\text{ kJ/kg}$$
  3. Actual turbine work and power. With $\eta_t=90\%$, $$w_a=\eta_tw_s=0.90\times351.32=316.18\text{ kJ/kg}$$ $$\dot W_t=\dot m_{vap}\,w_a=4.236\times316.18$$ $$\boxed{\dot W_t=1339.5\text{ kW}\approx1.34\text{ MW}}$$ (the actual exit state is wet steam, $x_{4a}=0.907$, confirming the turbine exhausts safely inside the two-phase region rather than as superheated vapour.)
Entropy s (kJ/kg·K)Temperature Tsaturation dome1 (300 kPa, sat. liq.)2 (150 kPa, x=0.042)3 (150 kPa, sat. vap.)4s (15 kPa, x=0.892)4a (15 kPa, x=0.907)
$T$–$s$ diagram: 1 (sat. liquid, 300 kPa) → 2 (throttling to 150 kPa, $x=0.042$) · the mixture splits into the saturated-vapour branch 2→3 (150 kPa) that feeds the turbine, expanding to 4s (isentropic) / 4a (actual, $\eta_t=90\%$) at 15 kPa.
Question 2 — results
QuantityValue
Flash quality $x_2$0.0424
Vapour mass flow to turbine $\dot m_{vap}$4.236 kg/s
Isentropic specific work $w_s$351.32 kJ/kg
Actual specific work $w_a$316.18 kJ/kg
Turbine power $\dot W_t$1339.5 kW (1.34 MW)