F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
F02C 7/22 (2006.01) F02C 7/24 (2006.01) F23R 3/28 (2006.01)
Patent
CA 2603619
An internal fuel manifold assembly for a gas turbine engine comprises a fuel manifold ring and a fuel inlet assembly fastened thereto. The fuel inlet assembly providing fluid flow communication with the fuel manifold ring and being joined to the fuel manifold ring at an inlet region thereon. The inlet region of the fuel manifold ring is reinforced relative to the remainder of the circumference of the fuel manifold ring.
Norton Rose Or S.e.n.c.r.l. S.r.l./llp
Pratt & Whitney Canada Corp.
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