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

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Compressors, Gas Turbines and Jet Engines
Mining industry usually employs following motive power

Diesel engine
Petrol engine
C. electric motor
Compressed air

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

1000°C
700°C
2000°C
1500°C

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Compressors, Gas Turbines and Jet Engines
The ratio of the net work obtained from the gas turbine plant to the turbine work is known as

Pressure ratio
Compression ratio
None of these
Work ratio

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor falls roughly as follows for every 100 m increase in elevation

0.1%
5%
0.5%
1.0%

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Compressors, Gas Turbines and Jet Engines
For slow speed large capacity compressor, following type of valve will be best suited

Poppet valve
Mechanical valve of the Corliss, sleeve, rotary or semi rotary type
Any of the above
Disc or feather type

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