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. The absolute flow at runner exit is axial. Assuming that the hydraulic efficiency is 90% and the mechanical efficiency is 99%, determine:
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
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.