Problem Statement
The following data is given for a Francis turbine : Net head = 70 m, speed = 600 r.p.m., shaft power = 367.875 kW, overall efficiency = 85% , hydraulic efficiency = 95%, flow ratio = 0.25, breadth ratio = 0.1, outer diameter of the runner = 2 x inner diameter of runner. The thickness of vanes occupy 10% of the circumferential area of the runner. Velocity of flow is constant at inlet and outlet and discharge is radial at outlet. Determine : (i) Guide blade angle, (ii) Runner vane angles at inlet and outlet, (iii) Diameters of runner at inlet and outlet, and (iv) Width of wheel at inlet.
Given Data & Constants
- Net Head, \(H = 70 \, \text{m}\)
- Speed, \(N = 600 \, \text{r.p.m.}\)
- Shaft Power, \(P_s = 367.875 \, \text{kW} = 367875 \, \text{W}\)
- Overall efficiency, \(\eta_o = 85\% = 0.85\)
- Hydraulic efficiency, \(\eta_h = 95\% = 0.95\)
- Flow ratio, \(K_f = 0.25\)
- Breadth ratio, \(n = 0.1\)
- Diameter ratio, \(D_1 = 2 D_2\)
- Area blockage = 10% (Effective Area Factor = 0.90)
- Constant flow velocity: \(V_{f1} = V_{f2}\)
- 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 Velocities and Discharge
First, we calculate the velocity of flow based on the head and flow ratio.
Next, find the required discharge (Q) using the overall efficiency and shaft power.
(iii) & (iv) Diameters and Width of Runner
The discharge is related to the effective flow area at the inlet.
2. Calculate Peripheral Velocities and Whirl Velocity
Using the hydraulic efficiency and Euler's equation (with \(V_{w2}=0\)):
(i) Guide Blade Angle (\(\alpha\))
(ii) Runner Vane Angles at Inlet (\(\theta\)) and Outlet (\(\phi\))
(i) Guide blade angle: \( \alpha \approx 12.33^\circ \)
(ii) Runner vane angles: Inlet \( \theta \approx 18.96^\circ \), Outlet \( \phi \approx 50.25^\circ \)
(iii) Diameters of runner: Inlet \( D_1 \approx 0.49 \, \text{m} \), Outlet \( D_2 \approx 0.245 \, \text{m} \)
(iv) Width of wheel at inlet: \( b_1 \approx 0.049 \, \text{m} \) or \(49 \, \text{mm}\)


