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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Maximum temperature in a gas turbine is of the order of

2000°C
1500°C
1000°C
700°C

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Compressors, Gas Turbines and Jet Engines
A jet engine has

Propeller in front
Propeller on the top
No propeller
Propeller at back

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Compressors, Gas Turbines and Jet Engines
In a single stage, single acting reciprocating air compressor, without clearance volume, the work-done is minimum during

Isentropic compression
Isothermal compression
Polytropic compression
None of these

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

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

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Compressors, Gas Turbines and Jet Engines
Gas turbines for power generation are normally used

In emergency
To supply base load requirements
To supply peak load requirements
To enable start thermal power plant

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Compressors, Gas Turbines and Jet Engines
Which is false statement about air receivers?

These increase compressor efficiency
These act as reservoir to take care of sudden demands
These are used to dampen pulsations
These knock out some oil and moisture

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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