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Compressors, Gas Turbines and Jet Engines

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

Carbon dioxide
Hydrogen
Ammonia and water vapour
Nitrogen

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Compressors, Gas Turbines and Jet Engines
The pressure ratio for an open cycle gas turbine compared to closed cycle gas turbine of same h.p. is

High
Low/high depending on make and type
Same
Low

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Compressors, Gas Turbines and Jet Engines
Separators are generally used in air compressor installations

Between the after-cooler and receiver
Before the inter-cooler
Before first stage suction
After the inter-cooler

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Compressors, Gas Turbines and Jet Engines
The compression ratio in a gas turbine is of the order of

0.50069444444444
0.33402777777778
3.5 : 1
0.20902777777778

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

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

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Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to steam turbine

Requires less space for installation
Has less efficiency
Has compressor and combustion chamber
All of these

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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