A Francis turbine with an overall efficiency of 70% is required to produce 147.15 kW. It is working under a head of 8 m. The wheel runs at 200 r.p.m. and the hydraulic losses in the turbine are 20% of the available energy. Assume radial discharge, determine : (i) The guide blade angle, (ii) The wheel vane angle at inlet, (iii) Diameter of the wheel at inlet, and (iv) Width of the wheel at inlet.

Francis Turbine Design Calculation

Problem Statement

A Francis turbine with an overall efficiency of 70% is required to produce 147.15 kW. It is working under a head of 8 m. The peripheral velocity = \(0.30\sqrt{2gH}\) and the radial velocity of flow at inlet is \(0.96\sqrt{2gH}\). The wheel runs at 200 r.p.m. and the hydraulic losses in the turbine are 20% of the available energy. Assume radial discharge, determine : (i) The guide blade angle, (ii) The wheel vane angle at inlet, (iii) Diameter of the wheel at inlet, and (iv) Width of the wheel at inlet.

Given Data & Constants

  • Overall efficiency, \(\eta_o = 70\% = 0.70\)
  • Shaft Power, \(P_s = 147.15 \, \text{kW} = 147150 \, \text{W}\)
  • Head, \(H = 8 \, \text{m}\)
  • Peripheral velocity, \(u_1 = 0.30\sqrt{2gH}\)
  • Velocity of flow, \(V_{f1} = 0.96\sqrt{2gH}\)
  • Speed, \(N = 200 \, \text{r.p.m.}\)
  • Hydraulic efficiency, \(\eta_h = 1 - 0.20 = 0.80\)
  • Radial discharge: \(V_{w2} = 0\)
  • Density of water, \(\rho = 1000 \, \text{kg/m}^3\)
  • Acceleration due to gravity, \(g = 9.81 \, \text{m/s}^2\)

Solution

1. Calculate Key Velocities

First, we calculate the base velocity term from the head.

$$ \sqrt{2gH} = \sqrt{2 \times 9.81 \times 8} \approx 12.53 \, \text{m/s} $$ $$ \text{Peripheral Velocity, } u_1 = 0.30 \times 12.53 = 3.759 \, \text{m/s} $$ $$ \text{Velocity of Flow, } V_{f1} = 0.96 \times 12.53 = 12.029 \, \text{m/s} $$

(iii) Diameter of the Wheel at Inlet (\(D_1\))

The diameter is calculated from the peripheral velocity and the rotational speed.

$$ u_1 = \frac{\pi D_1 N}{60} \implies D_1 = \frac{60 u_1}{\pi N} $$ $$ D_1 = \frac{60 \times 3.759}{\pi \times 200} \approx 0.359 \, \text{m} $$

2. Determine Whirl Velocity at Inlet (\(V_{w1}\))

Using the hydraulic efficiency and the Euler turbine equation (with \(V_{w2}=0\)).

$$ \eta_h = \frac{\text{Work Done per Unit Weight}}{H} = \frac{(V_{w1} u_1)/g}{H} $$ $$ V_{w1} = \frac{\eta_h \cdot g \cdot H}{u_1} $$ $$ V_{w1} = \frac{0.80 \times 9.81 \times 8}{3.759} \approx 16.71 \, \text{m/s} $$

(i) The Guide Blade Angle (\(\alpha\))

This is found from the components of the absolute velocity at the inlet.

$$ \tan(\alpha) = \frac{V_{f1}}{V_{w1}} = \frac{12.029}{16.71} \approx 0.7199 $$ $$ \alpha = \arctan(0.7199) \approx 35.75^\circ $$

(ii) The Wheel Vane Angle at Inlet (\(\theta\))

This is found from the components of the relative velocity at the inlet.

$$ \tan(\theta) = \frac{V_{f1}}{V_{w1} - u_1} $$ $$ \tan(\theta) = \frac{12.029}{16.71 - 3.759} = \frac{12.029}{12.951} \approx 0.9288 $$ $$ \theta = \arctan(0.9288) \approx 42.89^\circ $$

(iv) Width of the Wheel at Inlet (\(b_1\))

First, calculate the required discharge (Q) using the overall efficiency and shaft power.

$$ P_w = \frac{P_s}{\eta_o} = \frac{147150}{0.70} = 210214 \, \text{W} $$ $$ Q = \frac{P_w}{\rho g H} = \frac{210214}{1000 \times 9.81 \times 8} \approx 2.678 \, \text{m}^3/\text{s} $$ $$ \text{Now, find the width from the discharge formula:} $$ $$ Q = \pi D_1 b_1 V_{f1} \implies b_1 = \frac{Q}{\pi D_1 V_{f1}} $$ $$ b_1 = \frac{2.678}{\pi \times 0.359 \times 12.029} \approx 0.197 \, \text{m} $$
Final Design Parameters:

(i) Guide blade angle: \( \alpha \approx 35.75^\circ \)

(ii) Wheel vane angle at inlet: \( \theta \approx 42.89^\circ \)

(iii) Diameter of the wheel at inlet: \( D_1 \approx 0.359 \, \text{m} \) or \(359 \, \text{mm}\)

(iv) Width of the wheel at inlet: \( b_1 \approx 0.197 \, \text{m} \) or \(197 \, \text{mm}\)

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