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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In which case the air-fuel ratio is likely to be maximum?

4-stroke petrol engine
4-stroke diesel engine
Gas turbine
Multi cylinder engine

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Compressors, Gas Turbines and Jet Engines
The inter-cooler pressure, for minimum work required, for a two stage reciprocating air compressor, is given by (where p₁ = Intake pressure of air, p₂ = Inter-cooler pressure, and p₃ = Delivery pressure of air)

p₂ = p₁/p₃
p₂ = p₁ × p₂
p₂ = p₃/p₁
p₂ = p₁ × p₃

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Compressors, Gas Turbines and Jet Engines
The compressor efficiency is the

Compression work/motor input
Isothermal H.P/indicated H.R
Total output/air input
Isothermal H.P./shaft H.R

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

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

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Compressors, Gas Turbines and Jet Engines
Rotary compressor is best suited for

Large quantity of air at low pressure
Large quantity of air at high pressure
Small quantity of air at low pressure
Small quantity of air at high pressure

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine gives ________ efficiency as compared to an open cycle gas turbine.

None of these
Higher
Lower
Same

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