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Compressors, Gas Turbines and Jet Engines

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

Lobe type
Axial flow type
Centrifugal type
Reciprocating type

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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
The axial flow compressor is preferred in aircraft gas turbines because of

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

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Compressors, Gas Turbines and Jet Engines
The weight per horse power ratio for gas in Turbine as compared to I.C. engine and steam turbine is

Higher
Lower
None of these
Same

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Compressors, Gas Turbines and Jet Engines
The hottest point in a gas turbine is

at the base
in the center
between ~ to i of the blade height
at the tip

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Compressors, Gas Turbines and Jet Engines
Gas turbines for power generation are normally used

In emergency
To supply peak load requirements
To supply base load requirements
To enable start thermal power plant

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