Fuel manifold with jumper tubes
AssigneePratt & Whitney Canada Corp.
InventorsAleksandar Kojovic, Saeid Oskooel, Bryan Bond
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AssigneePratt & Whitney Canada Corp.
InventorsAleksandar Kojovic, Saeid Oskooel, Bryan Bond
Estimating the term…
A gas turbine engine fuel delivery system which includes an external fuel manifold fastened to the outer surface of a casing surrounding the combustor of the engine and which includes a plurality of inlet manifold tubes circumferentially disposed in serial flow communication. A plurality of fuel nozzles are mounted to the casing and are axially spaced apart from the fuel manifold on the outer surface of the casing. A plurality of jumper tubes are disposed outside the casing and feed fuel flow from the fuel manifold to the fuel nozzles. The jumper tubes have a rigidity that is less than that of the inlet manifold tubes of the fuel manifold such that the jumper tubes elastically deflect under load.
A fuel delivery system for a gas turbine engine having a combustor and a casing surrounding the combustor, the fuel delivery system comprising:
A gas turbine engine including a multi-stage compressor, a combustor and a multi-stage turbine, the gas turbine engine comprising:
Dependencies are inferred from the claim text.