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Compressors, Gas Turbines and Jet Engines

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

To increase the output
To reduce the exit temperature
To save fuel
To increase the efficiency

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Compressors, Gas Turbines and Jet Engines
The advantage of multistage compression over single stage compression is

Lower power consumption per unit of air delivered
Higher volumetric efficiency
Decreased discharge temperature
All of these

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Compressors, Gas Turbines and Jet Engines
During peak load periods, the best method of controlling compressors is

Relief valve
Variable speed
Constant speed unloader
Start-stop motor

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

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

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

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

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor falls roughly as follows for every 5°C increase in atmospheric temperature

0.01
0.001
0.005
0.05

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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