Low aspect ratio compressor casing treatment

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – Runner having full circular shroud for blades

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Details

415117, 415914, 4151731, 416181, 416189, F01D 900

Patent

active

061649112

ABSTRACT:
A compressor for a gas turbine engine, comprising a casing having an inner surface defining a plurality of circumferentially spaced-apart grooves adjacent the tips of a row of rotor blades. Each groove as a depth which is less than half the width thereof in order to increase surge margin at off design points without affecting the performance of the compressor under normal operating conditions.

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