Invention Grant
US08943835B2 Gas turbine engine combustor with CMC heat shield and methods therefor 有权
燃气轮机发动机燃烧器采用CMC隔热罩及其方法

Gas turbine engine combustor with CMC heat shield and methods therefor
Abstract:
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.
Information query
Patent Agency Ranking
0/0