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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Gas turbine works on

Rankine cycle
Ericsson cycle
Carnot cycle
Brayton or Atkinson cycle

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Compressors, Gas Turbines and Jet Engines
Only rocket engines can be propelled to space because

These engines can work on several fuels
They are not air breathing engines
They have high propulsion efficiency
They can generate very high thrust

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Compressors, Gas Turbines and Jet Engines
The ratio of the increase in pressure in rotor blades to total increase in pressure in the stage is called

Degree of reaction
Pressure ratio
Slip factor
Pressure coefficient

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Compressors, Gas Turbines and Jet Engines
In axial flow compressor, exit flow angle deviation from the blade angle is a function of

Blade camber and space-chord ratio
Space-chord ratio
Blade camber
Blade camber and incidence angle

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Compressors, Gas Turbines and Jet Engines
After-cooler is used to

Reduce volume
Cause moisture and oil vapour to drop out
Decrease the delivery temperature for ease in handling
Cool the air

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Compressors, Gas Turbines and Jet Engines
More than one stage will be preferred for reciprocating compressor if the delivery pressure is more than

6 kg/cm²
10 kg/cm²
14.7 kg/cm²
2 kg/cm²

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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