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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
An air compressor may be controlled by

Throttle control
Any one of the above
Blow off control
Clearance control

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Compressors, Gas Turbines and Jet Engines
Propulsive efficiency is defined as ratio of

Thrust power and fuel energy
Engine output and propulsive power
Propulsive power and fuel input
Thrust power and propulsive power

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Compressors, Gas Turbines and Jet Engines
The most efficient method of compressing air is to compress it

Isothermally
Isochronically
Isentropically
Adiabatically

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Compressors, Gas Turbines and Jet Engines
Inter cooling in compressors

Is the standard practice for big compressors
Cools the delivered air
Results in saving of power in compressing a given volume to given pressure
Enables compression in two stages

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Compressors, Gas Turbines and Jet Engines
In a high pressure compressor, the delivery pressure is

10 to 15 bar
1 to 5 bar
8 to 10 bar
5 to 8 bar

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

Improves thermal efficiency
Do not damage turbine blades
Reduces exhaust temperature
Increases power output

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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