Gas turbine engine combustor with cmc heat shield and...

F - Mech Eng,Light,Heat,Weapons – 23 – R

Patent

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Details

F23R 3/42 (2006.01) F02C 3/14 (2006.01) F02C 7/24 (2006.01)

Patent

CA 2738312

A combustor for a gas turbine engine is disclosed. The combustor is described as comprising a dome plate coupled to a liner thereof, with at least one heat shield comprised of a ceramic matrix composite coupled at the aft end of the dome plate. Also described is a method for assembling a combustor for a gas turbine engine, including releasing a metal alloy heat shield from a dome plate and providing a ceramic matrix composite heat shield as replacement.

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