Question

In: Mechanical Engineering

A radial flow hydraulic turbine whose design is based on a power specific speed,

A radial flow hydraulic turbine whose design is based on a power specific speed, Ωsp=1.707 is to produce 25 MW from a total head, HE=25 m. The overall turbine efficiency ηo=0.92, the mechanical efficiency is 0.985, and the loss in head in the nozzles is 0.5 m. The ratio of the blade tip speed to jet speed is 0.90. Assuming the meridional velocity is constant and equal to 10 m/s and there is no swirl in the runner exit flow, determine

  1. The volume flow rate through the turbine;
  2. The rotational speed and diameter of the runner;
  3. The absolute and relative flow angles at entry to the runner.

Solutions

Expert Solution

Determine the volume flow rate through the turbine

Given:

        P = 25 × 106 W
        ηo = 0.92, ρ = 1000 kg/m3
        g = 9.81 m/s2, HE = 25 m
    

Flow rate calculation

Hence, the volume flow rate through the turbine is Q = 110.8 m3/s

Determine the rotational speed and diameter of the runner

Write expression for specific speed:

Specific speed expression

Calculate angular speed of turbine.

        Given:
        Ωsp = 1.707, g = 9.81 m/s2
        HE = 25 m, P = 25 × 106 W, ρ = 1000 kg/m3
    

Angular speed calculation

Calculate rotational speed:

Rotational speed calculation

Therefore, rotational speed is N = 100.0567 rpm

Calculate blade tip speed.

        Given:
        K = 0.9, g = 9.81 m/s2, HE = 25 m, h = 0.5 m
    

Blade tip speed calculation

Calculate diameter of runner.

        Given:
        U = 19.732 m/s, N = 100.0567 rpm
    

Diameter calculation

Therefore, the diameter is D = 3.766 m

Determine the absolute and relative flow angles at entry to the runner

Calculate hydraulic efficiency.

        Given:
        ηo = 0.92, ηm = 0.985
    

Hydraulic efficiency calculation

Calculate swirl velocity at runner exit.

        Given:
        ηh = 0.934, g = 9.81 m/s2, HE = 25 m, U = 19.732 m/s
    

Swirl velocity calculation

Radial velocity at runner exit is the meridional velocity.

Calculate absolute flow angle at runner exit.

        Given:
        cθ2 = 11.6087 m/s, cr2 = 10 m/s
    

Absolute flow angle calculation

Calculate relative flow angle at runner exit.

        Given:
        cθ2 = 11.6087 m/s, U = 19.732 m/s, cr2 = 10 m/s
    

Relative flow angle calculation

Hence, the absolute flow angle at runner exit is 49.26° and the relative flow angle at runner exit is -39.088°


There is the answer we calculate.

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