Inter compressor duct variable geometry annular...

Details Inter compressor duct variable geometry annular... Inter compressor duct variable geometry annular...

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/228 (2006.01) F01D 17/10 (2006.01) F02C 9/18 (2006.01) F02K 1/78 (2006.01) F04D 27/02 (2006.01) F04D 29/08 (2006.01)

Patent

CA 2133793

A method and apparatus are disclosed which allows the bleed-off requirement from the Inter Compressor Duct of a multi spool gas turbine engine, which is recognized as a flow bifurcation with two significant features, to be achieved in a controlled fashion with both minimal distortion to, and controlled diffusion of, the flow remaining within the Inter Compressor Duct.

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