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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Compression efficiency is compared against

Ideal compression
Isothermal compression
Isentropic compression
Adiabatic compression

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

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

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Compressors, Gas Turbines and Jet Engines
Which of the following fuels can be used in turbojet engines?

High speed diesel oil
Kerosene
Methyl alcohol
Liquid hydrogen

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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)

W₂/(W₁ + W₂)
(W₁ + W₂)/W₂
(W₁ + W₂)/W₁
W₁/(W₁ + W₂)

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Compressors, Gas Turbines and Jet Engines
Volumetric efficiency is

The ratio of the air actually delivered to the amount of piston displacement
Index of compressor performance
The ratio of stroke volume to clearance volume
Reciprocal of compression ratio

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine consists of a

Compressor
All of these
Cooling chamber
Heating chamber

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