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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
Isothermal compression efficiency, even when running at high speed, can be approached by using

Multistage compression
Both (A) and (B) above
Cold water spray
Fully insulating the cylinder

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Compressors, Gas Turbines and Jet Engines
Which is false statement about advantages of multistage compressor in comparison to single stage compressor?

Better mechanical balance
Lower volumetric efficiency
Less power requirement
Less loss of air due to leakage past the cylinder

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Compressors, Gas Turbines and Jet Engines
The closed cycle in gas turbines

In never used
Provides lesser flexibility
Is used when gas is to be burnt
Provides greater flexibility

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Compressors, Gas Turbines and Jet Engines
In jet propulsion power unit, the inlet duct of diverging shape is used in order to

Provide robust structure
Beautify the shape
Collect more air
Convert kinetic energy of air into pressure energy

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Compressors, Gas Turbines and Jet Engines
The efficiency of the vane blower is (where W₁ = Workdone due to compression, and W₂ = Workdone due to back flow)

(W₁ + W₂)/W₁
W₂/(W₁ + W₂)
W₁/(W₁ + W₂)
(W₁ + W₂)/W₂

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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