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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The maximum delivery pressure in a rotary air compressor is

10 bar
50 bar
20 bar
30 bar

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Compressors, Gas Turbines and Jet Engines
The air-fuel ratio in gas turbines is of the order of

7: 1
50: 1.
15: 1
30: 1

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

Maximum work output
High thermal efficiency
Reduction in compressor work
Decrease of heat loss in exhaust

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

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

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Compressors, Gas Turbines and Jet Engines
The ratio of the discharge pressure to the inlet pressure of air is called

Expansion ratio
Compressor efficiency
Volumetric efficiency
Compression ratio

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Compressors, Gas Turbines and Jet Engines
The efficiency of a jet engine is higher at

High altitudes
Low altitudes
Low speeds
High speeds

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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