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22-Mec-A6 Fluid Machinery · December 2013

Question 1 of 8: Hydro Turbines

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

Notes on this paper

National Examination 07-Mec-A6 — Fluid Machinery, December 2013. Closed book, 3 hours. Section A (Calculative) Q1–Q5, Section B (Descriptive) Q6–Q8; candidates answer four from A and two from B (six of eight, 60 marks). All eight questions are solved as a study resource.

Reference texts: Fox & McDonald, Introduction to Fluid Mechanics (turbomachinery chapter); S.L. Dixon & C.A. Hall, Fluid Mechanics and Thermodynamics of Turbomachinery; R.K. Turton, Principles of Turbomachinery; Cohen, Rogers & Saravanamuttoo, Gas Turbine Theory. Constants used (exam reference sheet): g = 9.81 m/s², ρwater = 1000 kg/m³, Patm = 100 kPa.

Question 1: Hydro Turbines (10 marks)

Part I — Hydro turbine plant (Kaplan, 4 MW)

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. From FIG. 602 the water surfaces are: reservoir normal high WL 45.54 m, normal low WL 42.97 m; tailrace full-load WL 27.30 m. Turbine-generator max power 4 MW, η = 100%, frictionless. The 18.52 m vertical dimension on the drawing sets the drawing scale, from which the steel penstock bore scales to ≈ 2.8 m.

Find. Flow rate and penstock velocity at the design (low-water) head, and the velocity at the higher (normal-high-water) head.

Head diagram — 4 MW Kaplan setting (FIG. 602)Normal high WL 45.54 mNormal low WL 42.97 mFull-load tailrace WL 27.30 mpenstock D ≈ 2.8 mKaplan turbine / generator (4 MW)H = 15.67 m
Gross head is the difference between reservoir and tailrace water surfaces; the penstock bore is scaled from the 18.52 m dimension on the drawing.

Approach. With 100% efficiency and no friction the gross head between reservoir and tailrace surfaces is the head across the machine; get Q from P = ρgQH, then V = Q/A with the scaled penstock area.

  1. Operating head at low water. Gross head between reservoir normal-low and tailrace full-load surfaces: $$H_a = 42.97-27.30 = \boxed{15.67\ \text{m}}$$
  2. Flow rate at maximum power. From $P=\rho g Q H$ with $\eta=1$: $$Q_a=\frac{P}{\rho g H_a}=\frac{4\times10^{6}}{1000\cdot 9.81\cdot 15.67}=\boxed{26.0\ \text{m}^3/\text{s}}$$
  3. Penstock diameter from the drawing. Scaling the penstock bore against the 18.52 m reference gives $D\approx 2.8\ \text{m}$, so $A=\tfrac{\pi}{4}D^{2}=\tfrac{\pi}{4}(2.8)^2=6.16\ \text{m}^2$.
  4. Penstock velocity (b). $$V_b=\frac{Q_a}{A}=\frac{26.0}{6.16}=\boxed{4.2\ \text{m/s}}$$
  5. Effect of higher reservoir level (c). At normal high WL the head rises to $H_c=45.54-27.30=18.24\ \text{m}$. Because the power is fixed at 4 MW, a larger head requires a smaller flow ($Q=P/\rho g H$), hence a lower penstock velocity.
  6. Velocity at high water (d). $Q_c=\dfrac{4\times10^{6}}{1000\cdot 9.81\cdot 18.24}=22.4\ \text{m}^3/\text{s}$, so $$V_d=\frac{22.4}{6.16}=\boxed{3.6\ \text{m/s}}$$
Check: The penstock diameter is estimated from the sketch (D ≈ 2.8 m, roughly ±0.2 m). The velocities scale as 1/D², but the qualitative result in (c) and the ratio Vb/Vd = Qa/Qc = 1.16 are independent of the diameter estimate.

Part II — Kaplan turbine efficiency (Mactaquac)

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.

Given data
Water flow Q354 m³/sInlet dia Din6.4 m
Outlet dia Dout7.0 mInlet pressure226 kPa gauge
Outlet pressure−4.5 m H₂OElevation drop inlet→outlet5.0 m
Generator output110 MWSpeed112.5 rev/min

Find. Hydraulic (water) power delivered across the machine, the electrical output, and the overall turbine-generator efficiency.

Approach. Apply the steady-flow energy equation between the inlet and outlet gauges to get the total head H across the machine (pressure + velocity + elevation heads); water power is ρgQH; efficiency is electrical output over water power.

  1. Throat velocities. $V=\dfrac{Q}{\frac{\pi}{4}D^2}$: $$V_{in}=\frac{354}{\frac{\pi}{4}(6.4)^2}=11.0\ \text{m/s},\qquad V_{out}=\frac{354}{\frac{\pi}{4}(7.0)^2}=9.2\ \text{m/s}$$
  2. Head across the machine. With $p_{in}/\rho g = 226000/(1000\cdot 9.81)=23.04\ \text{m}$, $p_{out}=-4.5\ \text{m}$ (given as head), and the inlet 5.0 m above the outlet: $$H=\Big(\tfrac{p_{in}}{\rho g}+\tfrac{V_{in}^2}{2g}+z_{in}\Big)-\Big(\tfrac{p_{out}}{\rho g}+\tfrac{V_{out}^2}{2g}+z_{out}\Big)$$$$H=23.04+6.17+5.0-(-4.5)-4.31=\boxed{34.4\ \text{m}}$$
  3. (a) Hydraulic power. $$P_{hyd}=\rho g Q H=1000\cdot 9.81\cdot 354\cdot 34.4=\boxed{119.4\ \text{MW}}$$
  4. (b) Electrical output. Given directly: $P_{elec}=\boxed{110\ \text{MW}}$.
  5. (c) Overall efficiency. $$\eta=\frac{P_{elec}}{P_{hyd}}=\frac{110}{119.4}=\boxed{92.1\%}$$
Question 1 results
QuantityValue
Part I: Q at max power26.0 m³/s
Part I: penstock velocity (low water)4.2 m/s
Part I: penstock velocity (high water)3.6 m/s (lower)
Part II: head across machine34.4 m
Part II: hydraulic power119.4 MW
Part II: efficiency92.1%
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