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US 2006/0213203 A1Published application
Combustor
AssigneeROLLS-ROYCE plc
InventorStephen Cooper
Life of this patent
Estimating the term…
Abstract
A casing for a combustor of a gas turbine engine has a plurality of apertures, each aperture being reinforced with a band of material dividing the aperture. The casing and reinforcing member are forged simultaneously with the reinforcing member aligned with the direction of maximum stress field.
Claims10
A combustion casing for use in a gas turbine, the casing having an aperture extending therethrough, wherein the aperture has a reinforcing member extending across and dividing the aperture.
Dependencies are inferred from the claim text.