Method and apparatus for a structural outlet guide vane

Details Method and apparatus for a structural outlet guide vane Method and apparatus for a structural outlet guide vane

F - Mech Eng,Light,Heat,Weapons

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F01D 9/02 (2006.01) B23P 15/04 (2006.01) F01D 5/14 (2006.01) F01D 5/28 (2006.01) F01D 25/28 (2006.01) F02K 3/06 (2006.01)

Patent

CA 2697292

An outlet guide vane (62,100) for a gas turbine engine is provided. The outlet guide vane (62,100) includes a first flange (64), a second flange (66) positioned radially outwardly from the first flange, an airfoil (102) extending between the first and second flanges and coupled thereto, the airfoil including a leading edge portion (130) and a trailing edge portion (132), the leading edge portion and the trailing edge portion fabricated from a first material, a filler portion (150) coupled in a gap formed by the leading edge portion and the trailing edge portion, the filler portion including a first side (203) and a second side (204), the filler portion fabricated from a second material, the second material different from the first material, a first skin coupled to the first side, the first skin fabricated from a composite material, and a second skin coupled to the second side, the second skin fabricated from a composite material.

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