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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Open cycle gas turbine works on

Ericsson cycle
Carnot cycle
Rankine cycle
Brayton or Atkinson cycle

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Compressors, Gas Turbines and Jet Engines
In a double acting compressor, the air is compressed

In a single cylinder on both sides of the piston
In two cylinders
In two cylinders on both sides of the piston
In one cylinder

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Compressors, Gas Turbines and Jet Engines
Pick up the wrong statement about advantages of multistage compression

Mechanical balance is better
Better lubrication is possible advantages of multistage
More loss of air due to leakage past the cylinder
Air can be cooled perfectly in between

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Compressors, Gas Turbines and Jet Engines
Losses in a centrifugal compressor are due to

Diffuser losses
Inlet losses
Impeller channel losses
All of the listed here

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Compressors, Gas Turbines and Jet Engines
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

Higher
Lower
Equal
Can't be compared

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Compressors, Gas Turbines and Jet Engines
A compressor mostly used for supercharging of I.C. engines is

Radial flow compressor
Roots blower
Reciprocating compressor
Axial flow compressor

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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