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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The area of actual indicator diagram on an air compressor as compared to area of ideal indicator diagram is

Less
More
Same
More/less depending on compressor capacity

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Compressors, Gas Turbines and Jet Engines
Water is injected in gas turbine cycle to

Increase efficiency
Control temperature
Control output of turbine
Control fire hazards

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Compressors, Gas Turbines and Jet Engines
A jet engine has

Propeller in front
Propeller on the top
No propeller
Propeller at back

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Compressors, Gas Turbines and Jet Engines
The hottest point in a gas turbine is

between ~ to i of the blade height
at the base
in the center
at the tip

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Compressors, Gas Turbines and Jet Engines
The following property is most important for material used for gas turbine blade

Corrosion resistance
Toughness
Creep
Fatigue

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Compressors, Gas Turbines and Jet Engines
Gas turbine cycle with regenerator

Increases thermal efficiency
Allows high compression ratio
Allows operation at very high altitudes
Decreases heat loss is exhaust

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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