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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The air is delivered ________ in one revolution in case of a three lobbed rotor.

Three times
Four times
Two times
Six times

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Compressors, Gas Turbines and Jet Engines
High air-fuel ratio in gas turbines

Increases power output
Improves thermal efficiency
Do not damage turbine blades
Reduces exhaust temperature

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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

0.043055555555556
0.048611111111111
0.00070833333333333
0.045138888888889

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Compressors, Gas Turbines and Jet Engines
In a four stage compressor, if the pressure at the first and third stage is 1 bar and 16 bar, then the delivery pressure at the fourth stage will be

256 bar
64 bar
1 bar
16 bar

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Compressors, Gas Turbines and Jet Engines
If infinite number of heaters be used in a gas turbine, then expansion process in turbine approaches

Isothermal
Isentropic
Isochoric
Adiabatic

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine gives ________ efficiency as compared to an open cycle gas turbine.

None of these
Same
Higher
Lower

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