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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Separators in compressor installations are located

Between after-cooler and air receiver
Before inter-cooler
After receiver
After inter-cooler

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Compressors, Gas Turbines and Jet Engines
The main purpose of reheating in gas turbine is to

Increase speed
Reduce turbine size
Increase power output
Increase temperature

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Compressors, Gas Turbines and Jet Engines
The volume of air delivered by the compressor is called

Compressor capacity
None of the listed here
Swept volume
Free air delivery

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Compressors, Gas Turbines and Jet Engines
Separators are generally used in air compressor installations

Before first stage suction
Between the after-cooler and receiver
Before the inter-cooler
After the inter-cooler

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Compressors, Gas Turbines and Jet Engines
Pressure ratio in gas turbines is the ratio of

Pressures across the turbine
Highest pressure to exhaust pressure
Inlet pressure to exhaust pressure
Compressor pressure ratio

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Compressors, Gas Turbines and Jet Engines
The ratio of outlet whirl velocity to blade velocity in case of centrifugal compressor is called

None of these
Velocity factor
Slip factor
Velocity coefficient

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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