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A simple turbine schematic of the Parsons type. Steam pressure drops by a fraction of the total across each pair of rotating and fixed blades, the stators grow larger as pressure drops.

Physics

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Answer

99.90 kW\text{99.90 kW}

24800.75 W\text{24800.75 W}

110.4 mm\text{110.4 mm}

Step-by-step solution

13 steps

5.1 Construct a velocity diagram.

As an AI, I cannot physically construct a diagram. However, I can provide all the necessary calculated values that would be entered onto the velocity diagram, using the given scale of 1 cm=30 m/s1 \text{ cm} = 30 \text{ m/s}.

  1. Calculate the blade velocity (UU).

    Diameter (DD) = 460 mm=0.460 m460 \text{ mm} = 0.460 \text{ m}
    Rotational speed (NN) = 116.267 rev/s116.267 \text{ rev/s}

    U=πDNU = \pi D N U=π×0.460 m×116.267 rev/sU = \pi \times 0.460 \text{ m} \times 116.267 \text{ rev/s} U≈168.39 m/sU \approx 168.39 \text{ m/s}
  2. Convert the absolute inlet velocity (V1V_1) to meters per second.

    Gas leaves at 1944 km/h1944 \text{ km/h}.

    V1=1944 km/h×1000 m1 km×1 h3600 sV_1 = 1944 \text{ km/h} \times \frac{1000 \text{ m}}{1 \text{ km}} \times \frac{1 \text{ h}}{3600 \text{ s}} V1=540 m/sV_1 = 540 \text{ m/s}
  3. Calculate the components of the inlet velocity triangle.

    Nozzle angle (α1\alpha_1) = 22∘22^\circ
    Inlet flow velocity (Vf1V_{f1}):

    Vf1=V1sin⁡α1=540 m/s×sin⁡22∘V_{f1} = V_1 \sin \alpha_1 = 540 \text{ m/s} \times \sin 22^\circ Vf1≈202.28 m/sV_{f1} \approx 202.28 \text{ m/s}

    Inlet whirl velocity (Vw1V_{w1}):

    Vw1=V1cos⁡α1=540 m/s×cos⁡22∘V_{w1} = V_1 \cos \alpha_1 = 540 \text{ m/s} \times \cos 22^\circ Vw1≈500.69 m/sV_{w1} \approx 500.69 \text{ m/s}

    Relative inlet velocity (Vr1V_{r1}):

    Vr1=Vf12+(Vw1−U)2V_{r1} = \sqrt{V_{f1}^2 + (V_{w1} - U)^2} Vr1=(202.28 m/s)2+(500.69 m/s−168.39 m/s)2V_{r1} = \sqrt{(202.28 \text{ m/s})^2 + (500.69 \text{ m/s} - 168.39 \text{ m/s})^2} Vr1=(202.28)2+(332.30)2=40917.1+110423.3V_{r1} = \sqrt{(202.28)^2 + (332.30)^2} = \sqrt{40917.1 + 110423.3} Vr1=151340.4≈389.02 m/sV_{r1} = \sqrt{151340.4} \approx 389.02 \text{ m/s}

    Inlet blade angle (β1\beta_1):

    tan⁡β1=Vf1Vw1−U=202.28332.30\tan \beta_1 = \frac{V_{f1}}{V_{w1} - U} = \frac{202.28}{332.30} β1=arctan⁡(0.6087)≈31.32∘\beta_1 = \arctan(0.6087) \approx 31.32^\circ
  4. Calculate the components of the outlet velocity triangle.

    No axial thrust means Vf2=Vf1=202.28 m/sV_{f2} = V_{f1} = 202.28 \text{ m/s}.
    15% loss of velocity due to friction means Vr2=0.85Vr1V_{r2} = 0.85 V_{r1}.

    Vr2=0.85×389.02 m/s≈330.67 m/sV_{r2} = 0.85 \times 389.02 \text{ m/s} \approx 330.67 \text{ m/s}

    Outlet blade angle (β2\beta_2):

    sin⁡β2=Vf2Vr2=202.28330.67\sin \beta_2 = \frac{V_{f2}}{V_{r2}} = \frac{202.28}{330.67} β2=arcsin⁡(0.6117)≈37.72∘\beta_2 = \arcsin(0.6117) \approx 37.72^\circ

    Exit whirl velocity (Vw2V_{w2}):

    Vw2=U−Vr2cos⁡β2V_{w2} = U - V_{r2} \cos \beta_2 Vw2=168.39 m/s−(330.67 m/s×cos⁡37.72∘)V_{w2} = 168.39 \text{ m/s} - (330.67 \text{ m/s} \times \cos 37.72^\circ) Vw2=168.39−(330.67×0.7910)=168.39−261.58≈−93.19 m/sV_{w2} = 168.39 - (330.67 \times 0.7910) = 168.39 - 261.58 \approx -93.19 \text{ m/s}

    Absolute exit velocity (V2V_2):

    V2=Vf22+Vw22=(202.28 m/s)2+(−93.19 m/s)2V_2 = \sqrt{V_{f2}^2 + V_{w2}^2} = \sqrt{(202.28 \text{ m/s})^2 + (-93.19 \text{ m/s})^2} V2=40917.1+8684.4=49601.5≈222.71 m/sV_2 = \sqrt{40917.1 + 8684.4} = \sqrt{49601.5} \approx 222.71 \text{ m/s}

    Absolute exit angle (α2\alpha_2):

    tan⁡α2=Vf2Vw2=202.28−93.19\tan \alpha_2 = \frac{V_{f2}}{V_{w2}} = \frac{202.28}{-93.19} α2=arctan⁡(−2.1706)≈−65.27∘\alpha_2 = \arctan(-2.1706) \approx -65.27^\circ

    The values to be entered onto the velocity diagram are:

    • Blade velocity (UU): 168.39 m/s168.39 \text{ m/s}
    • Absolute inlet velocity (V1V_1): 540 m/s540 \text{ m/s}
    • Absolute exit velocity (V2V_2): 222.71 m/s222.71 \text{ m/s}
    • Relative inlet velocity (Vr1V_{r1}): 389.02 m/s389.02 \text{ m/s}
    • Relative exit velocity (Vr2V_{r2}): 330.67 m/s330.67 \text{ m/s}
    • Inlet whirl velocity (Vw1V_{w1}): 500.69 m/s500.69 \text{ m/s}
    • Exit whirl velocity (Vw2V_{w2}): −93.19 m/s-93.19 \text{ m/s}
    • Inlet flow velocity (Vf1V_{f1}): 202.28 m/s202.28 \text{ m/s}
    • Exit flow velocity (Vf2V_{f2}): 202.28 m/s202.28 \text{ m/s}
    • Absolute inlet angle (α1\alpha_1): 22∘22^\circ
    • Absolute exit angle (α2\alpha_2): −65.27∘-65.27^\circ
    • Inlet blade angle (β1\beta_1): 31.32∘31.32^\circ
    • Exit blade angle (β2\beta_2): 37.72∘37.72^\circ

    5.2 Answer the following questions pertaining to the velocity diagram drawn in QUESTION 5.1.1 above:

    5.2.1 Calculate the power developed by the turbine if the mass flow rate of the gas is 1000 grams per second.

  5. Convert the mass flow rate to kilograms per second.

    Mass flow rate (m˙\dot{m}) = 1000 g/s=1 kg/s1000 \text{ g/s} = 1 \text{ kg/s}

  6. Use the formula for power developed by an impulse turbine.

    P=m˙U(Vw1−Vw2)P = \dot{m} U (V_{w1} - V_{w2})
  7. Substitute the calculated values and calculate the power.

    P=1 kg/s×168.39 m/s×(500.69 m/s−(−93.19 m/s))P = 1 \text{ kg/s} \times 168.39 \text{ m/s} \times (500.69 \text{ m/s} - (-93.19 \text{ m/s})) P=168.39×(500.69+93.19)P = 168.39 \times (500.69 + 93.19) P=168.39×593.88P = 168.39 \times 593.88 P≈99900.6 WP \approx 99900.6 \text{ W} P≈99.90 kWP \approx \boxed{\text{99.90 kW}}

    5.2.2 Calculate the kinetic energy that exits the blades.

  8. Identify the mass flow rate and absolute exit velocity.

    Mass flow rate (m˙\dot{m}) = 1 kg/s1 \text{ kg/s}
    Absolute exit velocity (V2V_2) = 222.71 m/s222.71 \text{ m/s}

  9. Use the formula for kinetic energy per second (power).

    KEexit=12m˙V22KE_{exit} = \frac{1}{2} \dot{m} V_2^2
  10. Substitute the values and calculate the kinetic energy.

    KEexit=12×1 kg/s×(222.71 m/s)2KE_{exit} = \frac{1}{2} \times 1 \text{ kg/s} \times (222.71 \text{ m/s})^2 KEexit=12×49601.5 J/sKE_{exit} = \frac{1}{2} \times 49601.5 \text{ J/s} KEexit≈24800.75 WKE_{exit} \approx \boxed{\text{24800.75 W}}

    5.3 Name THREE types of governors.

    • Watt governor
    • Porter governor
    • Proell governor

    5.4 Calculate the height of a Watt governor rotating at a speed of 90 r/min.

  11. Convert the rotational speed from revolutions per minute to radians per second.

    Speed (NN) = 90 r/min90 \text{ r/min}
    Angular velocity (ω\omega) = 2πN60\frac{2 \pi N}{60}

    ω=2π×9060=3π rad/s\omega = \frac{2 \pi \times 90}{60} = 3 \pi \text{ rad/s} ω≈9.4248 rad/s\omega \approx 9.4248 \text{ rad/s}
  12. Use the formula for the height (hh) of a Watt governor.

    h=gω2h = \frac{g}{\omega^2}

    where g=9.81 m/s2g = 9.81 \text{ m/s}^2 (acceleration due to gravity).

  13. Substitute the values and calculate the height.

    h=9.81 m/s2(9.4248 rad/s)2h = \frac{9.81 \text{ m/s}^2}{(9.4248 \text{ rad/s})^2} h=9.8188.8269h = \frac{9.81}{88.8269} h≈0.1104 mh \approx 0.1104 \text{ m} h≈110.4 mmh \approx \boxed{\text{110.4 mm}}
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