Device for extending the performances of a radial compressor

Rotary kinetic fluid motors or pumps – With means for re-entry of working fluid to blade set – Re-entry working fluid joins inlet working fluid upstream of...

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415143, 415914, F04D 2944

Patent

active

049900536

ABSTRACT:
In a radial compressor the device for extending the performance at small throughputs by stabilizing the impeller flow in the inlet region comprises a recess (5) in the form of a groove which is oriented in the circumferential direction of the inlet duct (6) of the compressor, whereas in the flow direction it extends with a given axial width to the impeller (2). A stabilization ring (3) is integrated into said recess (5), being arranged in front of the impeller (2) and outside the principal flow (7) of the transported medium. A plurality of blades (4,4a), which are placed on the outer circumference of the stabilization ring (3), are in turn anchored to the inner contour of the recess (5).

REFERENCES:
patent: 4212585 (1980-07-01), Swarden et al.
patent: 4375937 (1983-03-01), Cooper
patent: 4630993 (1986-12-01), Jensen
patent: 4673331 (1987-06-01), Kolb
patent: 4743161 (1988-05-01), Fisher et al.
patent: 4781530 (1988-11-01), Lauterbach
patent: 4871294 (1989-10-01), Ivanov et al.
patent: 4930978 (1990-06-01), Khanna et al.

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