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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
An air compressor may be controlled by

Throttle control
Any one of the above
Blow off control
Clearance control

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Compressors, Gas Turbines and Jet Engines
Maximum delivery pressure is a rotary air compressor is of the order of

6 kg/cm²
10 kg/cm²
25 kg/cm²
16 kg/cm²

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Compressors, Gas Turbines and Jet Engines
The advantage of multistage compression over single stage compression is

Lower power consumption per unit of air delivered
All of these
Decreased discharge temperature
Higher volumetric efficiency

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Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to steam turbine

Requires less space for installation
Has less efficiency
Has compressor and combustion chamber
All of these

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Compressors, Gas Turbines and Jet Engines
Cylinder clearance in a compressor should be

About 100% of swept volume
As small as possible
About 50% of swept volume
As large as possible

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Compressors, Gas Turbines and Jet Engines
Stalling of blades in axial flow compressor is the phenomenon of

Unsteady periodic and reversed flow
Air stream not able to follow the blade contour
Motion of air at sonic velocity
Air stream blocking the passage

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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