Compressor casing for a gas turbine engine

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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Details

F02C 7/00 (2006.01) F01D 11/08 (2006.01) F01D 25/24 (2006.01) F04D 29/16 (2006.01)

Patent

CA 2372325

The cylindrical compressor casing of a gas turbine engine has a plurality of radially inwardly and axially rearwardly opening anti-surge grooves disposed on a radially inner surface thereof whereby foreign objects ingested into said engine and entering said grooves are free to move axially rearwardly of the engine.

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