Bleed holes oriented with gaspath and flared for noise...

Details Bleed holes oriented with gaspath and flared for noise... Bleed holes oriented with gaspath and flared for noise...

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 9/18 (2006.01) F01D 25/24 (2006.01) F02C 7/24 (2006.01) F02K 3/075 (2006.01)

Patent

CA 2604367

A gas turbine engine has a compressor assembly and a turbine assembly rotationally mounted on a shaft, the turbine assembly being driven by hot gases discharged from a combustion chamber disposed between the compressor and turbine assemblies and an engine case encasing a portion of the engine, the case having an oblong bleed hole having a major axis parallel to a gaspath direction and a minor axis perpendicular to the gaspath direction.

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