Fan case for turbofan engine

Details Fan case for turbofan engine Fan case for turbofan engine

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 9/04 (2006.01) F01D 21/00 (2006.01) F01D 21/14 (2006.01)

Patent

CA 2674061

A gas turbine engine rotor containment structure comprises an inner structurally supporting case having an inner surface positioned adjacent to a gas turbine engine rotor component to be contained. A layer of acoustic material is wrapped around and bounded to a radially outer surface of the inner case. A thin walled outer ring is bounded to a radially outer surface the layer of acoustic material. A layer of fibrous containment material surrounds a radially outer surface of the outer ring.

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