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Pelton turbine design (2 m³/s, 605 m, Ns 100)

Short answer

Given specific speed 100 is impossible for a Pelton wheel at this head. Using synchronous speed 500 rpm (12 poles) yields a single-jet design: power 10.33 MW, jet diameter 154 mm, wheel diameter 1.91 m, jet ratio 12.40, actual Ns 16.9, 22 buckets, bucket width 0.77 m, depth 0.19 m.

Design a Pelton turbine with the following data: Design discharge = 2 m³/s, Net head = 605 m, Overall efficiency = 87%, Specific speed = 100. Assume the ratios and coefficients from their standard range.

A Pelton wheel is designed by finding the jet velocity and jet diameter, choosing a synchronous speed that gives a suitable jet ratio m=D/dm = D/d (10 to 14 for good efficiency), and then sizing the wheel and buckets. The specific speed given in the data is checked first.

Data: Q=2Q = 2 m³/s, H=605H = 605 m, ηo=0.87\eta_o = 0.87, f=50f = 50 Hz. Assumed from the standard ranges: Cv=0.98C_v = 0.98 (0.97 to 0.99) and speed ratio ϕ=0.46\phi = 0.46 (0.43 to 0.47).

1. Power developed

P=ηoρgQH=0.87×9.81×2×605=10327.0 kWP = \eta_o \rho g Q H = 0.87 \times 9.81 \times 2 \times 605 = 10327.0\ \text{kW}

2. Jet velocity and bucket (peripheral) velocity

2gH=2×9.81×605=108.95 m/sV1=Cv2gH=0.98×108.95=106.77 m/su=ϕ2gH=0.46×108.95=50.12 m/s\begin{aligned} \sqrt{2gH} &= \sqrt{2 \times 9.81 \times 605} = 108.95\ \text{m/s} \\ V_1 &= C_v\sqrt{2gH} = 0.98 \times 108.95 = 106.77\ \text{m/s} \\ u &= \phi\sqrt{2gH} = 0.46 \times 108.95 = 50.12\ \text{m/s} \end{aligned}

3. Jet diameter (single jet)

Q=π4d2V1d=4×2π×106.77=0.1544 m≈154 mm\begin{aligned} Q &= \frac{\pi}{4} d^2 V_1 \\ d &= \sqrt{\frac{4 \times 2}{\pi \times 106.77}} = 0.1544\ \text{m} \approx 154\ \text{mm} \end{aligned}

4. Speed of the wheel

Trial with jet ratio m=12m = 12: D=12d=1.853D = 12d = 1.853 m, so

N=60uπD=60×50.12π×1.853=516.5 rpmN = \frac{60u}{\pi D} = \frac{60 \times 50.12}{\pi \times 1.853} = 516.5\ \text{rpm}

Nearest synchronous speed for 50 Hz: N=120f/p=6000/12=500N = 120f/p = 6000/12 = 500 rpm (12 poles).

Use of the given Ns=100N_s = 100: if the speed is taken from the given specific speed,

N=NsH5/4P=100×3000.5101.62=2953 rpm≈3000 rpmN = \frac{N_s H^{5/4}}{\sqrt{P}} = \frac{100 \times 3000.5}{101.62} = 2953\ \text{rpm} \approx 3000\ \text{rpm}

which gives D=60u/(πN)=0.319D = 60u/(\pi N) = 0.319 m and a jet ratio m=D/d=2.07m = D/d = 2.07, far below the minimum of about 10. A single jet Pelton has NsN_s of only about 8.5 to 30; even 6 jets raise this only by 6\sqrt{6} (to about 70). Reaching 100 would need about (100/16.9)2≈35(100/16.9)^2 \approx 35 jets, which is impossible. So Ns=100N_s = 100 cannot be met by a Pelton wheel at this head; the design below uses the practical speed of 500 rpm and the standard proportions, and the actual NsN_s is reported.

5. Wheel (pitch circle) diameter and jet ratio

D=60uπN=60×50.12π×500=1.914 mm=Dd=1.9140.1544=12.40\begin{aligned} D &= \frac{60u}{\pi N} = \frac{60 \times 50.12}{\pi \times 500} = 1.914\ \text{m} \\ m &= \frac{D}{d} = \frac{1.914}{0.1544} = 12.40 \end{aligned}

mm lies within 10 to 14, so a single-jet wheel is satisfactory.

6. Specific speed check

Ns=NPH5/4=500×101.623000.5=16.9N_s = \frac{N\sqrt{P}}{H^{5/4}} = \frac{500 \times 101.62}{3000.5} = 16.9

This is within the single-jet Pelton range (about 8.5 to 30), so the Pelton wheel is the correct choice.

7. Number of buckets (Tygun's formula)

z=15+D2d=15+12.402=21.20≈22z = 15 + \frac{D}{2d} = 15 + \frac{12.40}{2} = 21.20 \approx 22

8. Bucket size (usual proportions)

  • Bucket width B≈5d=0.772B \approx 5d = 0.772 m
  • Bucket depth T≈1.2d=0.185T \approx 1.2d = 0.185 m
  • Bucket radial length L≈2.5d=0.386L \approx 2.5d = 0.386 m

Summary of design

ItemValue
Power10.33 MW
Speed500 rpm
Number of jets1
Jet diameter dd154 mm
Wheel diameter DD1.91 m
Jet ratio mm12.40
Specific speed NsN_s16.9
Number of buckets22
Bucket width × depth0.77 m × 0.19 m

✓ Answer checked by Claude Opus 5.5 (high effort)

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