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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The combustion efficiency of a gas turbine using perfect combustion chamber is of the order of

0.85
0.99
0.75
0.9

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

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

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Compressors, Gas Turbines and Jet Engines
More than one stage will be preferred for reciprocating compressor if the delivery pressure is more than

6 kg/cm²
2 kg/cm²
14.7 kg/cm²
10 kg/cm²

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor falls roughly as follows for every 100 m increase in elevation

1.0%
5%
0.5%
0.1%

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

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

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

In between isothermal and adiabatic
Better than isothermal and adiabatic
Same as adiabatic
Same as isothermal

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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