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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
In which case the air-fuel ratio is likely to be maximum?

4-stroke petrol engine
Multi cylinder engine
4-stroke diesel engine
Gas turbine

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

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

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Compressors, Gas Turbines and Jet Engines
Reheating in gas turbine results in

Both (A) and (B) above
Increase of work ratio
Decrease of work ratio
Decrease of thermal efficiency

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Compressors, Gas Turbines and Jet Engines
The reason for volumetric efficiency of reciprocating compressor being less than 100 percent is

All of these
Clearance volume and leakages
Superheating in compressor
Pressure drop across the valves

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Compressors, Gas Turbines and Jet Engines
Reheating in a multistage expansion gas turbine ________ compressor work.

None of these
Increases
Decreases
Has no effect on

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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