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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In a jet propulsion unit, the products of combustion after passing through the gas turbine are discharged into

Back to the compressor
Atmosphere
Vacuum
Discharge nozzle

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Compressors, Gas Turbines and Jet Engines
Gas turbines use following type of air compressor

Reciprocating type
Lobe type
Axial flow type
Centrifugal type

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Compressors, Gas Turbines and Jet Engines
In jet propulsion power unit, the inlet duct of diverging shape is used in order to

Convert kinetic energy of air into pressure energy
Beautify the shape
Provide robust structure
Collect more air

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Compressors, Gas Turbines and Jet Engines
The ratio of work done per cycle to the swept volume in case of compressor is called

Mean effective pressure
Compressor efficiency
Compression ratio
Compression index

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Compressors, Gas Turbines and Jet Engines
The maximum combustion pressure in gas turbine as compared to I.C. engine is

Same
Depends on other factors
Less
More

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine consists of a

All of these
Heating chamber
Cooling chamber
Compressor

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