Method for avoiding pump surges in a compressor
A compressor and turbine technology, applied in the field of avoiding pump surge in compressors, to achieve the effect of reducing pressure ratio, avoiding indirect damage, and reducing compressor pressure ratio
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[0024] The fluid machine 1 partially shown in this drawing is designed as a gas turbine. Only the compressor 2 of the gas turbine is shown. The compressor 2 comprises guide vanes 6 fixed on the housing 4 and thus stationary, which are located in the flow channel 8 between the compressor inlet 10 and the compressor outlet 12 . The first guide vanes 6 in the flow direction of the air are designed as adjustable leading guide vanes 14 . As a result, the air quantity fed into the flow channel 8 can be adjusted and throttled.
[0025] Behind each guide blade 6 , 14 in the flow direction of the air, a rotor blade 18 is provided on the shaft 16 . The rotor blades 18 and the guide blades 6 , 14 are respectively arranged in a star-shaped ring in the flow channel 8 . The ring formed by the guide blades 6 , 14 together with the downstream ring formed by the rotor blades in the flow direction each form a stage of the compressor 2 .
[0026] In order to detect a threatening surge at an ...
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