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US 2026/0177010 A1Published application
Fuel injector for a gas turbine engine
AssigneeROLLS-ROYCE plc
InventorsAndrew WILKINSON, Eduardo ROMERO, Yannis HARDALUPAS
Life of this patent
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Abstract
A fuel injector for a combustor of a gas turbine engine is described. The fuel injector includes a fuel injection device having a fuel injection port configured to inject fuel into the combustor, wherein the fuel injection port includes an elongate aperture. A combustor for a gas turbine engine, a reheat assembly for a gas turbine engine, a gas turbine engine, and an aircraft.
Claims15
A reheat assembly for a gas turbine engine, the reheat assembly comprising:
- a fuel injector comprising a fuel injection device having a fuel injection port configured to inject fuel into the combustor, wherein the fuel injection port comprises an elongate aperture and wherein the aperture is elongate in a direction perpendicular to a direction of core airflow of the reheat assembly.
Dependencies are inferred from the claim text.