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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
Diffuser in a compressor is used to

Convert kinetic energy into pressure energy
Convert pressure energy into kinetic energy
Increase velocity
Make the flow streamline

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Compressors, Gas Turbines and Jet Engines
The ratio of isentropic work to Euler’s work is known as

Compressor efficiency
Isentropic efficiency
Euler
Pressure coefficient

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Compressors, Gas Turbines and Jet Engines
As the turbine inlet temperature increases, the thermal efficiency of gas turbine for the optimum pressure ratio

Decreases
First increases and then decreases
Remain same
Increases

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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
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

Can't be compared
Equal
Higher
Lower

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