Igniter Port Retention System
AssigneeRolls-Royce North American Technologies Inc.
InventorKevin Sauer
Life of this patent
Estimating the term…
Loading patent…
AssigneeRolls-Royce North American Technologies Inc.
InventorKevin Sauer
Estimating the term…
A combustor igniter port assembly is disclosed. The assembly may be installed in a combustor section of a gas turbine engine. The combustor igniter port assembly may include a combustor tower positionable to project radially outward from a combustor outer wall forming a radially outer surface of the combustor section. The combustor tower may be positionable on the combustor outer wall to encircle an aperture included in the combustor wall. The combustor tower may include a keeper on an inner wall of the combustor tower. The assembly may include a ferrule disposed radially outward from at least a portion of the combustor tower. The assembly may include a retention ring disposed within the keeper of the combustor tower. The retention ring may have elasticity to vary the diameter of the retention ring.
A combustor igniter port assembly for a combustor section of a gas turbine engine, the combustor igniter port assembly comprising:
A method of installing a combustor igniter port retention ring, the method including:
A combustor igniter port assembly comprising:
Dependencies are inferred from the claim text.