Back to results
US 2017/0248312 A1Published application
Combustor Assembly
AssigneeGeneral Electric Company
InventorsDavid Andrew Hannwacker, Stephen John Howell
Life of this patent
Estimating the term…
Abstract
A combustor assembly for a gas turbine engine includes a combustor dome and a combustion chamber liner formed integrally of a ceramic matrix composite material. The combustor dome defines a plurality of openings for receiving a respective plurality of fuel air injector hardware assemblies and may extend continuously along a circumferential direction.
Claims20
A combustor assembly for a gas turbine engine defining a circumferential direction, the combustor assembly comprising:
- a combustor dome and combustion chamber liner formed integrally of a ceramic matrix composite material, the combustor dome defining a plurality of openings for receiving a respective plurality of fuel-air injector hardware assemblies.
A combustor assembly for a gas turbine engine defining a circumferential direction, the combustor assembly comprising:
- a combustor dome and combustion chamber liner formed integrally of a ceramic matrix composite material, the combustor dome and combustion chamber liner at least in part defining a combustion chamber and extending continuously along the circumferential direction.
Dependencies are inferred from the claim text.