Examples of 'compressor stage' in a sentence
Meaning of "compressor stage"
A compressor stage is a section within a compressor that performs a specific function in the compression of gas or air. It is one of the sequential stages required for efficient compression
How to use "compressor stage" in a sentence
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compressor stage
Turbine or compressor stage for a turbojet.
Include additional axial compressor stage.
Turbine or compressor stage for a turbomachine.
An array of movable blades and an array of fixed blades form a compressor stage.
Each walled passage enables a single compressor stage to be inspected by endoscopy.
Each of the second and third stages may comprise a single acting reciprocating piston compressor stage.
Compressor with at least one compressor stage and a moisture separator.
Each rotor is followed by a stator, so as to form a compressor stage.
The configuration of the compressor stage means the lips seals can be shortened.
Each impeller-diffuser set is a compressor stage.
The choice of compressor stage depends on the pressure required for bleeding the gas.
The bleed air may be supplied by a compressor stage of an aircraft engine.
However, a compressor stage can also operate in a state known as an unstable working range.
The channels may be channels communicating with a compressor stage to pressurize the chamber directly.
Conveniently, the first stage comprises a double acting reciprocating piston compressor stage.
See also
The inlet air may be bleed air from the compressor stage of an airplane 's engine.
Modifying the compressor stage number can then be performed without significant re-designing work.
In this case, a corresponding aftercooler is not necessarily provided downstream of the first compressor stage.
A first compressor stage performs a first compression, which normally leads to overheating of the vapor.
Once again, manually rotate the compressor module compressor stage in the rotation direction several times.
Stream of impure carbon monoxide 1 at a low pressure is sent to a compressor stage V 1.
The second compressor stage 9 also consists of vanes fitted with a pitch control mechanism 50.
FIG . 8 is a fragmentary diagrammatic view in perspective of a turbine or compressor stage of a turbine engine.
The gas entering the first compressor stage 15 from evaporator 13 is compressed.
As of the Astazou X, the engine received a second axial compressor stage.
Particular problem with such a compressor stage 1 is shown in FIG . 2.
The rotor comprises a series of blades 10 fixed on its circumference, corresponding to a compressor stage.
FIG . 1 is a diagrammatic perspective view of a compressor stage of a turbine engine of the invention ;.
A row of rotor blades 10 and the downstream array of stator blades 6 comprise one compressor stage.
The pressure Pu at the outlet of compressor stage 4 ; and.
Here the compressed air is cooled and passed on to the output compressor stage 110.
The pressure Pi at the inlet of compressor stage 4 ;.
Compressing a gas mixture of the first and second gas through the second compressor stage ( 1B ) ;.
The turbine stage 24 also provides the necessary power to drive the compressor stage 22.
Detecting a pressure parameter of the first compressor stage ( 1A ) ;.
In Fig . 1 these streams are combined in the suction of final compressor stage 107.
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