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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The mass of gas turbine per kW developed is about ________ as that of an I.C. engine.

One fourth
Same
One-half
One sixth

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Compressors, Gas Turbines and Jet Engines
Work ratio of a gas turbine plant is ratio of

Net work output and work done by turbine
Work done by turbine and heat supplied
Net work output and heat supplied
Work done by turbine and net work output

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Compressors, Gas Turbines and Jet Engines
Pressure ratio in gas turbines is the ratio of

Highest pressure to exhaust pressure
Compressor pressure ratio
Inlet pressure to exhaust pressure
Pressures across the turbine

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Compressors, Gas Turbines and Jet Engines
Work ratio of a gas turbine may be improved by

Decreasing the compression work
Both (A) and (C) above
Increasing the turbine work
Increasing the compression work

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Compressors, Gas Turbines and Jet Engines
Volumetric efficiency of air compressors is of the order of

20 - 30%
40 - 50%
70 - 90%
60 - 70%

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

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

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