F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
F02C 7/04 (2006.01) B64D 29/00 (2006.01) F02C 7/20 (2006.01) F02K 1/72 (2006.01) F02K 3/06 (2006.01)
Patent
CA 2726503
An assembly includes a unitary nacelle structure and an integrated fan housing for a gas turbine engine assembly. The unitary nacelle structure includes an inlet region and a fan cowl region, and is configured to at least partially circumscribe the integrated fan housing. The integrated fan housing comprises an integral composite structure and includes a fan case sized and configured for encircling a fan blade assembly of an associated gas turbine engine, a fan hub, and a plurality of fan outlet guide vanes. The unitary nacelle structure cooperates with the integrated fan housing to transfer static and dynamic loads directly to a support structure, rather than through the engine core, to minimize backbone bending.
Gardner Donald Lee
Glynn Christopher Charles
Lachapelle Donald George
Mitchell Stephen Craig
Pennekamp David Lance
Company General Electric
Craig Wilson And Company
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