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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
When the outlet angle from the rotor of a centrifugal compressor is more than 90°, then the blades are said to be

Radial
None of the listed here
Forward curved
Backward curved

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Compressors, Gas Turbines and Jet Engines
The effective power of gas turbines is increased by adding the following in compressor

Carbon dioxide
Nitrogen
Ammonia and water vapour
Hydrogen

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Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

700°C
200°C
500°C
1000°C

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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
p₁/p₂
(p₁ - p₂)/2
(p₁ + p₂)/2

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

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

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Compressors, Gas Turbines and Jet Engines
Which is false statement about air receivers?

These are used to dampen pulsations
These knock out some oil and moisture
These increase compressor efficiency
These act as reservoir to take care of sudden demands

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