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US 2025/0052425 A1Published application
Combustor assembly
AssigneeROLLS-ROYCE plc
InventorsStephen C. HARDING, Paul A. HUCKER, Iain MORGAN
Life of this patent
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Abstract
The present disclosure relates to a combustor assembly for a gas turbine engine. The combustor assembly comprises a combustor liner, a combustor head, a cowl and a fastener. The combustor liner and the cowl define a cavity. The combustor liner has an integral lug that extends into the cavity from a wall of the combustor liner. The fastener extends into the combustor liner lug to fasten the combustor head to the combustor liner.
Claims16
A combustor assembly for a gas turbine engine, the combustor assembly comprising a combustor liner, a combustor head, a cowl and a fastener, wherein
- the combustor liner and the cowl define a cavity;
- the combustor liner has an integral lug that extends into the cavity from a wall of the combustor liner;
- and
- the fastener extends into the combustor liner lug to fasten the combustor head to the combustor liner.
1 more element
Dependencies are inferred from the claim text.