Flow directing assembly for a gas turbine engine

Details Flow directing assembly for a gas turbine engine Flow directing assembly for a gas turbine engine

F - Mech Eng,Light,Heat,Weapons

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170/53

F01D 1/04 (2006.01) F01D 25/24 (2006.01) F01D 25/26 (2006.01)

Patent

CA 1162148

Abstract of the Disclosure A non-rotating flow directing assembly for a gas turbine engine is disclosed. The flow directing assembly is formed of a circumferentially segmented inner case supported by an annular sleeve. The inner case is formed of a plurality of arcuate segments extending axially continuously through the engine. A method of assembling the circumferentially continuous annular sleeve about an axially continuous rotor is also disclosed. In an alternate embodiment the inner case is formed of several pluralities of arcuate segments.

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