compressor stage

compressor stage

compressor stage
compressor stage
i. A pair of stator and rotor rings form one stage of an axial-flow compressor. The rotating airfoils increase air velocity, which then changes into pressure in the numerous diverging ducts formed by the stator vanes.
ii. Each section of a compressor during which the air pressure is progressively increased. A stage of compression consists of one row of blades and one row of stator vanes in an axial-flow compressor.
References in periodicals archive ?
Axial compressor stage performance is presented by the functional dependence of pressure ratio [[pi].
To withstand the high external forces of medium- and heavy-duty applications, the high-pressure compressor stage is equipped with a milled aluminium wheel.
This vented hot bleed air from the last compressor stage of the engine directly into the aft avionics bay, causing significant fire damage.
The off-design behaviour can be analysed by some design parameters such as fluid incidence on the wheel blades, the rotor and stator section ratio, the free space parameter, the reduced speed and position of the compressor stage on the Ns-Ds map.
The performance of a compressor is inherently deteriorated by different loses that occur at different sections of the compressor stage.
Team Hare has previously received praise from Formula Student judges for their engine designs, which last year featured a Cummins compressor stage, as well as the driver environment and control system design.
s CF6 engines installed in a total of 186 jet airliners in Japan to look for cracks at the high-pressure compressor stage that could cause serious engine failure.
The QF1Da512 SavFIRe[TM] (Simple and versatile FIR engine) is the industry's first audio applications-specific FIR filter to contain an integrated gain and compressor stage that directly addresses the issue of dynamic range loss in audio equalization applications.
If a lower turndown capacity is required with such a compressor, the problem can be solved by providing an additional bypassing line or compressor stage or cylinder.
025 on average bladed disk diameter), the loss ratio in the running disks of the compressor stage in abnormal modes is 10-20% lower than in the stage with the single-row bladed disks that have the same pressure in the design mode.
When they checked for freedom of rotation, they found the compressor stage made a grinding noise when rotated and did not rotate the turbine stage.

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