Combustor attachment with rotational joint

Details Combustor attachment with rotational joint Combustor attachment with rotational joint

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/60 (2006.01) F02C 3/14 (2006.01) F23R 3/50 (2006.01)

Patent

CA 2471328

A gas turbine engine with: a compressor section; a turbine section; a combustor, disposed between the compressor and turbine sections, having at least one combustor mounting assembly connecting the combustor to the engine. Each combustor mounting assembly has: a longitudinal axis; and an articulating joint having a first and second portion constrained from relative translation transverse to the longitudinal axis, and where said first and second portion have a multiple rotational degrees of freedom relative to each other about axes transverse to the longitudinal axis.

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