Question

In: Mechanical Engineering

A Kaplan turbine designed with a shape factor (power specific speed) of 3.0 (rad), a runner tip diameter of 4.4 m, and a hub diameter of 2.0 m, operates with a net head of 20 m and a shaft speed of 150 rev/min.

A Kaplan turbine designed with a shape factor (power specific speed) of 3.0 (rad), a runner tip diameter of 4.4 m, and a hub diameter of 2.0 m, operates with a net head of 20 m and a shaft speed of 150 rev/min. The absolute flow at runner exit is axial. Assuming that the hydraulic efficiency is 90% and the mechanical efficiency is 99%, determine:

  1. The volume flow rate and shaft power output;
  2. The relative flow angles at the runner inlet and outlet at the hub, at the mean radius and at the tip.

Solutions

Expert Solution

 

Determine The Volume Flow Rate and Shaft Power Output

Calculate the rotational speed of the shaft.

Given: N=150rpm

Ω=π30N=π30×150=15.70rad/s

Calculate the power delivered to the rotor.

Given: ρ=1000 kg/m3,Ωsp=3.0rad,Ω=15.70rad/s,g=9.18 m/s2,HE=20 m

P=ρ(ΩpΩ)2(gHE)52=1000(315.70)(9.81×20)52=1000×0.036×539197.05=19.67×106 W

Calculate the shaft power delivered to the external device.

Given: ηshaft =0.99,P=19.67×105 W

Pshaft =ηmP=0.99×19.67×105=19.47MW

Hence, the power delivered to the shaft is 19.47 MW.

Calculate the volume flow rate.

Given: P=19.67×105 W,ρ=1000 kg/m3,g=9.18 m/s2,HE=20 m

Q=PηHρgHE=19.67×1060.9×9.81×1000×20=111.4 m3/s

Hence, the volume flow rate Q=111.4 m3/s

Determine The Relative Flow Angles at the Runner Inlet and Outlet at the Hub, at the Mean Radius, and at the Tip

Calculate the specific work done.

Given: P=19.67×105 W,ρ=1000 kg/m3,Q=111.4 m3/s

ΔW=PρQ=19.67×1061000×111.4=176.6 m2/s2

Calculate the axial velocity.

Given: Q=111.4 m3/s,D1=4.4 m,Dh=2 m

cx=4Qπ(D12−Dh2)=4×111.4π(4.42−22)=9.234 m/s

Calculate the blade tip speed.

Given: Ω=15.07rad/s,D1=4.4 m

U1=ΩD12=15.07×4.42=34.56 m/s

Consider the expression for the relative flow angle at various radii at the runner inlet.

Given: U1=34.56 m/s,cx=9.234 m/s,ΔW=176.6 m2/s2

β2=tan−1⁡[(rr1)U1cx−(r1r)ΔWcxU1]=tan−1⁡[(rr1)34.569.234−(r1r)176.69.234×34.56]=tan−1⁡[3.743(rr1)−0.5534(r1r)](∗)

Consider the expression for the relative flow angle at various radii at the runner outlet.

Given: U1=34.56 m/s,cx=9.234 m/s

β3=tan−1⁡(rr1U1cx)=tan−1⁡(3.743×rr1)(∗∗)

Tabulate the value of equation (*) and (**) in the table below.

Position Hub Mean Tip
Radius/Ratio 0.4545 0.7273 1
β2∘ 25.81 62.99 72.59
β3∘ 59.55 69.83 75.04

There is the answer.

 

Related Solutions

A vertical shaft Kaplan turbine operating under a head of 9.8 m has a runner diameter...
A vertical shaft Kaplan turbine operating under a head of 9.8 m has a runner diameter of 9.3 m. At the maximum optimum point, the turbine runs at 51.7 rpm and develops 45,000 kW power discharging 535 m 3 /s water. Determine the values of unit speed, unit discharge, unit power and specific speed of the turbine. If the critical value of cavitation coefficient for the runner is 0.95, determine the location of the runner with respect to the tail...
A small-scale Kaplan turbine has a power output of 8MW, an available head at turbine entry of 13.4 m, and a rotational speed of 200rev/min.
A small-scale Kaplan turbine has a power output of $8 \mathrm{MW}$, an available head at turbine entry of $13.4 \mathrm{~m}$, and a rotational speed of $200 \mathrm{rev} / \mathrm{min}$. The inlet guide vanes have a length of $1.6 \mathrm{~m}$ and the diameter at the trailing edge surface is $3.1 \mathrm{~m}$. The runner diameter is $2.9 \mathrm{~m}$ and the hub-tip ratio is 0.4. Assuming the hydraulic efficiency is $92 \%$ and the runner design is "free-vortex," determineThe radial and tangential components...
ADVERTISEMENT
ADVERTISEMENT
ADVERTISEMENT