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Pelton wheel power with penstock losses

Short answer

Net head H = H_g − f L V_p²/(2g D) = 441.50 m. Jet velocity V₁ = C_v√(2gH) = 91.21 m/s, jet diameter d = 83.5 mm. Bucket speed u = 0.46√(2gH) = 42.81 m/s, N = 584 rpm. Euler power P = ρQ u (V_w₁ − V_w₂) = 1986.7 kW, η_h = 91.7%, shaft power = 1927.1 kW.

A Pelton wheel is supplied with 0.5 m³/s of water through a penstock 2000 m long and 0.6 m in diameter from a reservoir whose surface is 450 m above the nozzle. Take the Darcy friction factor of the penstock as 0.016 and the minor losses as negligible. The nozzle velocity coefficient is 0.98, the speed ratio is 0.46, the wheel (pitch circle) diameter is 1.4 m, the buckets deflect the jet through 165 degrees, and the relative velocity is reduced by 5 % while passing over the bucket. Mechanical efficiency is 97 %. Calculate (a) the net head, (b) the jet diameter, (c) the speed of the wheel, (d) the power developed by the runner and its hydraulic efficiency, and (e) the shaft power.

Given: Hg=450H_g=450 m, L=2000L=2000 m, D=0.6D=0.6 m, f=0.016f=0.016, Q=0.5Q=0.5 m³/s, Cv=0.98C_v=0.98, ϕ=0.46\phi=0.46, Dw=1.4D_w=1.4 m, deflection 165∘165^\circ, k=0.95k=0.95 (Vr2=kVr1V_{r2}=kV_{r1}), ηm=0.97\eta_m=0.97.

(a) Net head

Velocity in penstock: Vp=Qπ4D2=0.50.2827=1.768V_p=\dfrac{Q}{\frac{\pi}{4}D^2}=\dfrac{0.5}{0.2827}=1.768 m/s.

hf=fLVp22gD=0.016×2000×1.76822×9.81×0.6=8.50 mh_f=\frac{fLV_p^2}{2gD}=\frac{0.016\times2000\times1.768^2}{2\times9.81\times0.6}=8.50\ \text{m} H=Hg−hf=450−8.50=441.50 mH = H_g - h_f = 450 - 8.50 = 441.50\ \text{m}

(b) Jet diameter

V1=Cv2gH=0.98×2×9.81×441.50=0.98×93.07=91.21 m/sV_1 = C_v\sqrt{2gH} = 0.98\times\sqrt{2\times9.81\times441.50} = 0.98\times93.07 = 91.21\ \text{m/s} a=QV1=5.482×10−3 m2,d=4aπ=83.5 mma=\frac{Q}{V_1}=5.482\times10^{-3}\ \text{m}^2,\qquad d=\sqrt{\frac{4a}{\pi}}=83.5\ \text{mm}

(c) Speed of wheel

u=ϕ2gH=0.46×93.07=42.81 m/s,N=60uπDw=60×42.81π×1.4=584 rpmu=\phi\sqrt{2gH}=0.46\times93.07=42.81\ \text{m/s},\qquad N=\frac{60u}{\pi D_w}=\frac{60\times42.81}{\pi\times1.4}=584\ \text{rpm}

(d) Power developed and hydraulic efficiency

Velocity triangles: Vw1=V1=91.21V_{w1}=V_1=91.21 m/s; Vr1=V1−u=48.40V_{r1}=V_1-u=48.40 m/s; Vr2=0.95Vr1=45.98V_{r2}=0.95V_{r1}=45.98 m/s.

The bucket turns the jet by 165∘165^\circ, so the relative exit velocity makes 180−165=15∘180-165=15^\circ with the direction opposite to the bucket motion.

Vw2=u−Vr2cos⁡15∘=42.81−44.41=−1.60 m/s (backwards)V_{w2}=u-V_{r2}\cos15^\circ=42.81-44.41=-1.60\ \text{m/s (backwards)} Vw1+∣Vw2∣=91.21+1.60=92.81 m/sV_{w1}+|V_{w2}|=91.21+1.60=92.81\ \text{m/s} P=ρQ u (Vw1+∣Vw2∣)=1000×0.5×42.81×92.81=1986.7 kWWater power=ρgQH=2165.6 kWηh=1986.72165.6=91.7%\begin{aligned} P&=\rho Q\,u\,(V_{w1}+|V_{w2}|)=1000\times0.5\times42.81\times92.81=1986.7\ \text{kW}\\ \text{Water power}&=\rho g Q H=2165.6\ \text{kW}\\ \eta_h&=\frac{1986.7}{2165.6}=91.7\% \end{aligned}

(e) Shaft power

Ps=ηmP=0.97×1986.7=1927.1 kWP_s=\eta_m P=0.97\times1986.7=1927.1\ \text{kW}

Answer: (a) 441.50 m; (b) 83.5 mm; (c) 584 rpm; (d) 1986.7 kW, ηh=91.7%\eta_h=91.7\%; (e) 1927.1 kW.

✓ Answer checked by Claude Sonnet 5.5

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