Engineering :: Heat Engines
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211. |
The pour point of diesel fuel oil must be |
A. |
More than the coldest atmospheric temperature at which oil is to be pumped |
B. |
Less than the coldest atmospheric temperature of which oil is to be pumped |
C. |
More than 100?C |
D. |
More than 0?C |
E. |
Less than 0?C |
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Answer: Option B
Explanation:
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212. |
In a compression ignition engine squish is |
A. |
Created at the beginning of suction stroke |
B. |
Created at the end of suction stroke |
C. |
Created during combustion |
D. |
Created towards the end of compression stroke |
E. |
None of the above |
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Answer: Option D
Explanation:
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213. |
For the same power and same speed, the flywheel of a two stroke engine as compared to that of a four stroke engine will be |
A. |
Bigger |
B. |
Small |
C. |
Same size |
D. |
Different shape |
E. |
There is no correlation |
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Answer: Option A
Explanation:
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214. |
Which statement is incorrect? |
A. |
Morse test can be conducted on petrol engines |
B. |
Morse test can also be conducted on diesel engines |
C. |
Morse test can be conducted only on multicylinder engines |
D. |
LH.P of engines can be determined by more test |
E. |
Morse test can be conducted on CFR engine. |
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Answer: Option E
Explanation:
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215. |
The efficiency of a jet engine is higher at |
A. |
Lower altitudes |
B. |
Higher altitudes |
C. |
Low speeds |
D. |
High speeds |
E. |
High speeds and low altitudes |
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Answer: Option B
Explanation:
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216. |
A jet engine has |
A. |
Propeller in front |
B. |
Propeller in back |
C. |
No propeller |
D. |
Propeller on the top |
E. |
None of the above |
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Answer: Option C
Explanation:
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217. |
In a jet propulsion unit the products of combustion after passing through the gas turbine are discharged into |
A. |
Atmosphere |
B. |
Recycled back to compressor |
C. |
Vacuum |
D. |
Discharge nozzle |
E. |
Compressor |
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Answer: Option D
Explanation:
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218. |
Air fuel ratio for a jet engine is of the order of |
Answer: Option D
Explanation:
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219. |
Samples of exhaust gases from following engines have been collected: |
A. |
Petrol engine |
B. |
Diesel engine |
C. |
Gas engine |
D. |
Jet propulsion unit |
Answer: Option D
Explanation:
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220. |
To augment the thrust of jet propulsion units part of the fuel is burned in the exhaust. How does this fuel burn |
A. |
Oxygen is also supplied along with fuel |
B. |
Some chemicals rich in oxygen are mixed with fuel |
C. |
Fuel finds oxygen from excess air supplied to engine |
D. |
Fuel is never burned in exhaust pipe |
Answer: Option C
Explanation:
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