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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
A large clearance volume in a reciprocating compressor results in

Lower suction pressure
Increased volume flow rate
Reduced volume flow rate
Lower delivery pressure

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Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

500°C
700°C
200°C
1000°C

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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

Remain same
First increases and then decreases
Increases
Decreases

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Compressors, Gas Turbines and Jet Engines
Gas turbine blades are given a rake

Opposite to the direction of motion of blades
Depending on the velocity
In the direction of motion of blades
Equal to zero

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Compressors, Gas Turbines and Jet Engines
The net work input required for compressor with increase in clearance volume

Increases
Increases/decreases depending on compressor capacity
Decreases
Remains same

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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

5%
0.5%
1.0%
0.1%

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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