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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The compressor efficiency is the

Compression work/motor input
Isothermal H.P/indicated H.R
Total output/air input
Isothermal H.P./shaft H.R

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

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

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

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

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Compressors, Gas Turbines and Jet Engines
The axial flow compressor is preferred in aircraft gas turbines because of

Higher thrust
High pressure rise
Low frontal area
None of the listed here

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Compressors, Gas Turbines and Jet Engines
In a double acting compressor, the air is compressed

In two cylinders
In one cylinder
In two cylinders on both sides of the piston
In a single cylinder on both sides of the piston

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Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to steam turbine

Requires less space for installation
Has less efficiency
Has compressor and combustion chamber
All of these

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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