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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
For perfect intercooling in a three stage compressor

p₁ p₃ = p₂ p₄
p₃/p₁ = p₄/p₂
p₁ p₂ = p₃ p₄
p₂/p₁ = p₃/p₂ = p₄/p₃

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Compressors, Gas Turbines and Jet Engines
Axial flow compressor resembles

Sliding vane compressor
Turbine
Centrifugal pump
Reciprocating pump

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Compressors, Gas Turbines and Jet Engines
Standard air is the air at ___ and relative humidity of 36 percent.

0.1 bar and 40°C
0.1 bar and 20°C
1 bar and 20°C
1 bar and 40°C

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Compressors, Gas Turbines and Jet Engines
The clearance volume of the air compressor is kept minimum because

It results in minimum work
It permits isothermal compression
It greatly affects volumetric efficiency
It allows maximum compression to be achieved

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Compressors, Gas Turbines and Jet Engines
Inter cooling in compressors

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

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Compressors, Gas Turbines and Jet Engines
The axial flow compressor is preferred in aircraft gas turbines because of

Higher thrust
High pressure rise
None of the listed here
Low frontal area

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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