Adjustable gaseous fuel injector
AssigneePratt & Whitney Canada Corp.
InventorsJakub Strzepek, Kian McCaldon, Anna Mamrol, Owen Wong, Maxime La Fleche
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AssigneePratt & Whitney Canada Corp.
InventorsJakub Strzepek, Kian McCaldon, Anna Mamrol, Owen Wong, Maxime La Fleche
Estimating the term…
A fuel injector for a gas turbine engine combustor is provided that includes a swirler, a mounting stage, and a distributor. The swirler has a shaft, a collar, a throat section, and first and second axial ends. The throat section includes an inner radial surface that defines a central passage that extends between the swirler inner bore and the collar. The collar includes a plurality of apertures extending therethrough disposed radially outside of the central passage. The mounting stage is disposed in the inner bore, and has an annular flange, a central hub, and at least one strut. The distributor has a stem attached to a head. The stem has a distal end opposite the head portion engaged with the central hub. The head portion has an end surface and a side surface. The distributor is selectively positionable relative to the throat section.
A fuel injector for a gas turbine engine combustor, the fuel injector having an axial centerline, comprising:
A fuel injector for a gas turbine engine combustor, the fuel injector having an axial centerline, comprising:
A method of calibrating a fuel injector within a gas turbine engine combustor, the method comprising:
Dependencies are inferred from the claim text.