Guide vane and method of fabricating the same

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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F01D 9/02 (2006.01) F01D 5/28 (2006.01) F01D 9/04 (2006.01)

Patent

CA 2602314

An outlet guide vane (100), for a gas turbine engine (10), comprises an airfoil (102) comprising a leading edge portion (130) and a trailing edge portion (132) each fabricated from a first material. A filler portion (202) is positioned between the leading and trailing edge portions and is fabricated from a second material that is different than said first material.

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