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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The criterion of the thermodynamic efficiency for rotary compressor is

Polytropic compression
Isentropic compression
None of the listed here
Isothermal compression

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Compressors, Gas Turbines and Jet Engines
The material commonly used for air craft gas turbine is

Duralumin
Timken, Haste alloys
Stainless steel
High alloy steel

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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 allows maximum compression to be achieved
It greatly affects volumetric efficiency
It permits isothermal compression

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Compressors, Gas Turbines and Jet Engines
More than one stage will be preferred for reciprocating compressor if the delivery pressure is more than

14.7 kg/cm²
10 kg/cm²
2 kg/cm²
6 kg/cm²

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Compressors, Gas Turbines and Jet Engines
The advantage of multistage compression over single stage compression is

Lower power consumption per unit of air delivered
Higher volumetric efficiency
All of these
Decreased discharge temperature

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Compressors, Gas Turbines and Jet Engines
Gas turbines use following type of air compressor

Axial flow type
Lobe type
Reciprocating type
Centrifugal type

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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