Combustor assembly and method

Details Combustor assembly and method Combustor assembly and method

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/46 (2006.01) F23R 3/28 (2006.01) F23R 3/60 (2006.01)

Patent

CA 2499258

An improved assembly and method is provided for attaching the inner and outer liner of a aircraft engine combustor, using heat shields located inside the combustor.

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