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

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Compressors, Gas Turbines and Jet Engines
The thermodynamic efficiency of rotary compressor is based on

Polytropic compression
Isentropic compression
Adiabatic compression
Isothermal compression

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

Depends on other factors
Same
More
Less

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Compressors, Gas Turbines and Jet Engines
As the turbine inlet temperature increases, the thermal efficiency of gas turbine for the optimum pressure ratio

Decreases
First increases and then decreases
Remain same
Increases

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Compressors, Gas Turbines and Jet Engines
The axial flow compressor is preferred in aircraft gas turbines because of

Higher thrust
Low frontal area
High pressure rise
None of the listed here

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Compressors, Gas Turbines and Jet Engines
During base load operation, the best method of controlling compressor is

Constant speed unloader
Start-stop motor
Relief valve
Variable speed

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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