Fuel manifold and fuel injector arrangement for a combustion chamber
AssigneeROLLS-ROYCE plc
InventorSimon FULLER
Life of this patent
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AssigneeROLLS-ROYCE plc
InventorSimon FULLER
Estimating the term…
A fuel manifold and fuel injector arrangement for a gas turbine engine combustion chamber includes an annular combustion chamber casing arranged around the combustion chamber. Circumferentially spaced fuel injectors supply fuel into the combustion chamber and a fuel manifold supplies fuel to each of the fuel injectors. The fuel manifold includes flexible fuel pipes and a plurality of T piece connectors. The stem of each connector is mounted on an outer end of a respective one of the fuel feed arms and each flexible fuel pipe interconnects an arm of one connector with an arm of an adjacent connector. Each connector is arranged such that the arms are arranged are at angles to the planes containing the axis of the casing and perpendicular to the axis of the casing respectively. Adjacent connectors are arranged at opposite angles such that the fuel manifold extends around the casing sinusoidally.
A fuel manifold and fuel injector arrangement for supplying fuel to at least one combustion chamber comprising an annular combustion chamber casing arranged around the at least one combustion chamber,
A fuel manifold and fuel injector arrangement for supplying fuel to at least one combustion chamber comprising an annular combustion chamber casing arranged around the at least one combustion chamber,
Dependencies are inferred from the claim text.