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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The efficiency of the vane blower is (where W₁ = Workdone due to compression, and W₂ = Workdone due to back flow)

W₁/(W₁ + W₂)
(W₁ + W₂)/W₁
W₂/(W₁ + W₂)
(W₁ + W₂)/W₂

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Compressors, Gas Turbines and Jet Engines
A closed gas turbine in which fuel is burnt directly in the air is not possible because of

High specific volume
Paucity of O2
High friction losses
Increasing gas temperature

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Compressors, Gas Turbines and Jet Engines
In multistage compressor, the isothermal compression is achieved by

By running compressor at very slow speed
By constantly cooling the cylinder
By insulating the cylinder
Employing inter-cooler

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Compressors, Gas Turbines and Jet Engines
Inter cooling in compressors

Cools the delivered air
Results in saving of power in compressing a given volume to given pressure
Is the standard practice for big compressors
Enables compression in two stages

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Compressors, Gas Turbines and Jet Engines
1 m of air at atmospheric condition weighs approximately

1.3 kg
1.0 kg
0.5 kg
2.2 kg

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Compressors, Gas Turbines and Jet Engines
Volumetric efficiency of a compressor decreases with ________ in compression ratio.

Remain same
Decrease
Does not change
Increase

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