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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The compressed air may be used

For operating pneumatic drills
All of the listed here
In starting and supercharging of I.C. engines
In gas turbine plants

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine consists of a

All of these
Compressor
Heating chamber
Cooling chamber

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Compressors, Gas Turbines and Jet Engines
The maximum compression ratio in an actual single stage axial flow compressor is of the order of

0.048611111111111
0.00070833333333333
0.043055555555556
0.045138888888889

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Compressors, Gas Turbines and Jet Engines
Reheating in a gas turbine

Increases the turbine work
Increases the compressor work
Decreases the thermal efficiency
Increases the thermal efficiency

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Compressors, Gas Turbines and Jet Engines
The ratio of specific weight/h.p. of gas turbine and I.C engines may be typically of the order of

0.045833333333333
0.084027777777778
0.16736111111111
0.042361111111111

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Compressors, Gas Turbines and Jet Engines
The maximum combustion pressure in gas turbine as compared to I.C. engine is

Same
Depends on other factors
More
Less

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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