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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
During peak load periods, the best method of controlling compressors is

Variable speed
Constant speed unloader
Relief valve
Start-stop motor

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Compressors, Gas Turbines and Jet Engines
The temperature of air at the beginning of the compression stroke is ________ the atmospheric temperature.

More than
Equal to
None of these
Less than

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Compressors, Gas Turbines and Jet Engines
The overall thermal efficiency of an ideal gas turbine plant is (where r = Pressure ratio)

1 - (1/r) ɣ-1/ɣ
r ɣ-1
1 - (1/r) ɣ/ɣ-1
1 - r ɣ-1

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Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

700°C
500°C
200°C
1000°C

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

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

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Compressors, Gas Turbines and Jet Engines
If the clearance ratio for a reciprocating air compressor is 'K', then its volumetric efficiency is given by

1 - k + k (p₁/p₂)1/n
1 - k + k (p₁/p₂) n- 1/n
1 + k - k (p₂/p₁) n-1/n
1 + k - k (p₂/p₁)1/n

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