Gas turbine combustor and fuel manifold mounting arrangement

Details Gas turbine combustor and fuel manifold mounting arrangement Gas turbine combustor and fuel manifold mounting arrangement

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/60 (2006.01) F02C 3/14 (2006.01) F23R 3/46 (2006.01)

Patent

CA 2597592

A mounting system for locating a combustor and a fuel manifold of a gas turbine engine within a gas generator casing thereof is described. The mounting system comprises at least three support pin assemblies which extend radially inwardly from the gas generator casing. The support pin assemblies support both the fuel manifold and at least an upstream end of the combustor and maintaining engagement between the fuel manifold and the combustor during operation of the gas turbine engine.

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