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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
Reheating in a gas turbine

Increases the turbine work
Increases the thermal efficiency
Decreases the thermal efficiency
Increases the compressor work

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

To increase the output
To save fuel
To increase the efficiency
To reduce the exit temperature

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Compressors, Gas Turbines and Jet Engines
The maximum delivery pressure in a rotary air compressor is

10 bar
20 bar
30 bar
50 bar

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Compressors, Gas Turbines and Jet Engines
It is not possible to use closed gas turbine cycle in aeronautical engines because

It is inefficient
None of these
It is bulky
It requires cooling water for its operation

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of compressor with increase in compression ratio will

Increase
Decrease
May increase or decrease depending on clearance volume
Remain same

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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