Engineering :: Hydraulics Machines
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41. |
The overall efficiency of a reaction turbine is the ratio of |
A. |
power produced by the turbine to the energy actually suppied by the turbine |
B. |
actual work available at the turbine to the energy imparted to the wheel |
C. |
workdone on the wheel to the energy (or head of water) actually supplied to the turbine |
D. |
none of the above |
Answer: Option A
Explanation:
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42. |
A Kaplan turbine is an axial flow reaction turbine. |
Answer: Option A
Explanation:
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43. |
In a Francis turbine runner, the number of blades are generally between |
A. |
2 to 4 |
B. |
4 to 8 |
C. |
8 to 16 |
D. |
16 to 24 |
Answer: Option D
Explanation:
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44. |
In a Kaplan turbine runner, the number of blades are generally between |
A. |
2 to 4 |
B. |
4 to 8 |
C. |
8 to 16 |
D. |
16 to 24 |
Answer: Option B
Explanation:
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45. |
Which of the following is not a reaction turbine? |
A. |
Furneyron turbine |
B. |
Jonval turbine |
C. |
Thomson's turbine |
D. |
Pelton wheel |
Answer: Option D
Explanation:
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46. |
The Furneyron turbine is |
A. |
an axial flow |
B. |
an inward flow |
C. |
an outward flow |
D. |
a mixed flow |
Answer: Option C
Explanation:
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47. |
The Thomson's turbine is |
A. |
an axial flow |
B. |
an inward flow |
C. |
an outward flow |
D. |
a mixed flow |
Answer: Option C
Explanation:
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48. |
In a Francis turbine, the pressure at inlet is |
A. |
less than |
B. |
more than |
Answer: Option B
Explanation:
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49. |
The flow ratio of Francis turbine is defined as the ratio of the |
A. |
velocity of flow at inlet to the theoretical jet velocity |
B. |
theoretical velocity of jet to the velocity of flow at inlet |
C. |
velocity of runner at inlet to the velocity of flow at inlet |
D. |
none of the above |
Answer: Option A
Explanation:
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50. |
The flow ratio in case of Francis turbine varies from |
A. |
0.15 to 0.3 |
B. |
0.4 to 0.5 |
C. |
0.6 to 0.9 |
D. |
1 to 15 |
Answer: Option A
Explanation:
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