Taking air away from the tips of the rotor wheels of a high...

Rotary kinetic fluid motors or pumps – Working fluid bypass

Reexamination Certificate

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Details

C415S914000

Reexamination Certificate

active

07549838

ABSTRACT:
A turbomachine compressor comprises at least one plurality of moving blades and spaced apart therefrom in an axial direction relative to a central longitudinal axis of the turbomachine, a plurality of stationary vanes, and a stationary casing surrounding said plurality of moving blades and including a plurality of bleed holes centered in the range 5% to 50% of the blade chord length and having a diameter less than or equal to 30% of the blade chord length, each bleed hole sloping at two angles of inclination relative to the central longitudinal axis. Advantageously, each bleed hole has a first axis of inclination presenting an angle φ relative to the central longitudinal axis lying in the range 30° to 90°, and a second axis of inclination perpendicular to the first and presenting an angle θ relative to the central longitudinal axis lying in the range 30° to 90°.

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patent: 1 103 725 (2001-05-01), None
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