Gas turbine internal manifold mounting arrangement

Details Gas turbine internal manifold mounting arrangement Gas turbine internal manifold mounting arrangement

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/28 (2006.01) F02C 3/14 (2006.01) F02C 7/22 (2006.01)

Patent

CA 2605220

A mounting system supporting and positioning an internal fuel manifold of a gas turbine engine includes at least a heat shield surrounding a fuel inlet of the fuel manifold, the heat shield bearing at least a portion of a load to support the fuel manifold.

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