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A fuel manifold and fuel injector arrangement for a gas turbine engine combustion chamber comprises an annular combustion chamber casing arranged around the combustion chamber. A plurality of circumferentially spaced fuel injectors supply fuel into the combustion chamber and a fuel manifold supplies

A fuel manifold and fuel injector arrangement for a gas turbine engine combustion chamber comprises an annular combustion chamber casing arranged around the combustion chamber. A plurality of 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 comprises a plurality of 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 at angles to the planes containing the axis of the casing and perpendicular to the axis of the casing respectively.

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1. 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 plurality of circumferentially spaced fuel injectors arranged to supply fuel into the at least

1. 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 plurality of circumferentially spaced fuel injectors arranged to supply fuel into the at least one combustion chamber, each fuel injector having a fuel feed arm extending through a corresponding aperture in the annular combustion chamber casing,a fuel manifold arranged to supply fuel to each of the fuel injectors, the fuel manifold comprising a plurality of flexible fuel pipes and a plurality of T piece connectors, each T piece connector comprising a stem and two parallel arms extending in opposite directions from the stem, the stem of each T piece connector being mounted on an outer end of a respective one of the fuel feed arms,each flexible fuel pipe interconnecting an arm of one T piece connector with an arm of an adjacent T piece connector,each T piece connector being arranged so that the adjacent arms of two adjacent T pieces are both angled inwards towards or both an led outwards from a plane perpendicular to the axis of the annular combustion chamber casing such that the fuel manifold extends around the combustion chamber casing sinusoidally. 2. A fuel manifold and fuel injector arrangement as claimed in claim 1 wherein each T piece connector being arranged such that the arms are arranged at an angle relative to a plane containing the axis of the annular combustion chamber casing and at an angle relative to a plane perpendicular to the axis of the annular combustion chamber casing and adjacent T piece connectors being arranged at opposite angles such that the fuel manifold extends around the combustion chamber casing sinusoidally. 3. A fuel manifold and fuel injector arrangement as claimed in claim 1 wherein the arms of the T piece connectors being arranged at an angle of 10° to 90° to the plane perpendicular to the axis of the annular combustion chamber casing. 4. A fuel manifold and fuel injector arrangement as claimed in claim 1 wherein the arms of the T piece connectors being arranged at an angle of 30° to 60° to the plane perpendicular to the axis of the annular combustion chamber casing. 5. A fuel manifold and fuel injector arrangement as claimed in claim 1 wherein all of the T piece connectors being arranged such that the arms are arranged at an angle of the same magnitude. 6. A fuel manifold and fuel injector arrangement as claimed in claim 1 wherein the T piece connectors being arranged such that the arms are arranged at angles of different magnitudes. 7. A fuel manifold and fuel injector arrangement as claimed in claim 1 wherein all of the T piece connectors being arranged such that the arms are arranged at an angle of 45° to the plane containing the axis of the annular combustion chamber casing and at an angle of 45° to the plane perpendicular to the axis of the annular combustion chamber casing. 8. A fuel manifold and fuel injector arrangement as claimed in claim 1 wherein the parallel arms of the T piece connector being arranged coaxially. 9. A fuel manifold and fuel injector arrangement as claimed in claim 1 comprising two L piece connectors, each L piece connector being arranged at a respective end of the fuel manifold, each L piece connector comprising a stem and an arm extending from the stem, the stem of each L piece connector being mounted on an outer end of a respective one of the fuel feed arms and one of the flexible fuel pipes interconnecting an arm of one T piece connector with an arm of an adjacent L piece connector. 10. A fuel manifold and fuel injector arrangement as claimed in claim 9 wherein the L piece connectors being arranged at an upper half of the annular combustion chamber casing. 11. A fuel manifold and fuel injector arrangement as claimed in claim 9 comprising a fuel inlet connector, the fuel inlet connector being interconnected with an arm of a T piece connector. 12. A fuel manifold and fuel injector arrangement as claimed in claim 11 wherein the fuel inlet connector being interconnected with an arm of a further T piece connector. 13. A fuel manifold and fuel injector arrangement as claimed in claim 11 wherein the fuel inlet connector being arranged at a lower half of the annular combustion chamber casing. 14. A fuel manifold and fuel injector arrangement as claimed in claim 1 wherein the at least one combustion chamber being an annular combustion chamber. 15. A fuel manifold and fuel injector arrangement as claimed in claim 1 wherein the at least one combustion chamber is a gas turbine engine combustion chamber. 16. A fuel manifold and fuel injector arrangement as claimed in claim 15 wherein the gas turbine engine is selected from the group consisting of an aero gas turbine engine, a marine gas turbine engine and an industrial gas turbine engine. 17. A fuel manifold and fuel injector arrangement as claimed in claim 1 wherein fuel injectors are lean burn fuel injectors, the fuel manifold comprising flexible fuel pipes having two fuel passages and the T piece connectors having two fuel passages. 18. A fuel manifold and fuel injector arrangement as claimed in claim 17 wherein the lean burn fuel injectors are selected from the group consisting of lean burn fuel injectors having a pilot fuel spray nozzle and a main fuel spray nozzle, lean burn fuel injectors having a pilot fuel prefilmer and a main fuel prefilmer and lean burn fuel injectors having a pilot fuel spray nozzle and a main fuel prefilmer. 19. A fuel manifold and fuel injector arrangement as claimed in claim 17 wherein fuel passages in the fuel pipes being coaxial and the main fuel flowing through an inner fuel passage. 20. 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 plurality of circumferentially spaced fuel injectors arranged to supply fuel into the at least one combustion chamber, each fuel injector having a fuel feed arm extending through a corresponding aperture in the annular combustion chamber casing,a fuel manifold arranged to supply fuel to each of the fuel injectors, the fuel manifold comprising a plurality of flexible fuel pipes and a plurality of T piece connectors,each T piece connector comprising a stem and two parallel arms extending in opposite directions from the stem, the stem of each T piece connector being mounted on an outer end of a respective one of the fuel feed arms,each flexible fuel pipe interconnecting an arm of one T piece connector with an arm of an adjacent T piece connector,each T piece connector being arranged so that the adjacent arms of two adjacent T pieces are both angled inwards towards or both angled outwards from a plane perpendicular to the axis of the annular combustion chamber casing such that the fuel manifold extends around the combustion chamber casing sinusoidally,the fuel manifold additionally comprising two L piece connectors, each L piece connector being arranged at a respective end of the fuel manifold, each L piece connector comprising a stem and an arm extending from the stem, the stem of each L piece connector being mounted on an outer end of a respective one of the fuel feed arms and one of the flexible fuel pipes interconnecting an arm of one T piece connector with an arm of an adjacent L piece connector, and the L piece connectors being arranged at an upper half of the annular combustion chamber casing.