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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The pressure ratio of an ideal vaned compressor with increase in mass flow rate

Remain constant
Decreases
First decreases and then increases
Increases

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Compressors, Gas Turbines and Jet Engines
Diffuser in a compressor is used to

Make the flow streamline
Convert kinetic energy into pressure energy
Convert pressure energy into kinetic energy
Increase velocity

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Compressors, Gas Turbines and Jet Engines
Gas turbine cycle with regenerator

Allows high compression ratio
Decreases heat loss is exhaust
Allows operation at very high altitudes
Increases thermal efficiency

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Compressors, Gas Turbines and Jet Engines
For maximum work, the reheating should be done to an intermediate pressure of (Where p₁ = Maximum pressure, and p₂ = Minimum pressure)

(p₁ - p₂)/2
p₁ p₂
p₁/p₂
(p₁ + p₂)/2

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Compressors, Gas Turbines and Jet Engines
Turbofan engine employs

One air stream
Solid fuel firing
Two or more air streams
No air stream

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Compressors, Gas Turbines and Jet Engines
Phenomenon of choking in compressor means

Increased inclination of chord with air steam
Fixed mass flow rate regardless of pressure ratio
No flow of air
Reducing mass flow rate with increase in pressure ratio

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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