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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Gas turbine works on

Brayton or Atkinson cycle
Rankine cycle
Ericsson cycle
Carnot cycle

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Compressors, Gas Turbines and Jet Engines
Adiabatic compression is one in which

No heat leaves or enters the compressor cylinder during compression
Temperature rise follows a linear relationship
Temperature during compression remains constant
Work done is maximum

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

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

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

Higher at high speed
Lower at low speed
Higher at high altitudes
Same at all altitudes

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Compressors, Gas Turbines and Jet Engines
A jet engine has

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

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Compressors, Gas Turbines and Jet Engines
The maximum compression ratio in an actual single stage axial flow compressor is of the order of

0.048611111111111
0.045138888888889
0.00070833333333333
0.043055555555556

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