FUEL INJECTOR FOR A GAS TURBINE ENGINE COMBUSTION CHAMBER

    公开(公告)号:US20170089582A1

    公开(公告)日:2017-03-30

    申请号:US15247340

    申请日:2016-08-25

    Abstract: A fuel injector includes a central member arranged on axis of fuel injector and a first member arranged around central member. A first swirler is arranged between central member and first member. A pilot fuel injector is arranged to supply fuel onto inner surface of first member. A second member is arranged between downstream end of first member and downstream end of shroud. A second swirler is arranged between upstream end of first member and upstream end of shroud and between downstream end of first member and upstream end of second member. A third swirler is arranged between downstream end of shroud and second member. A main fuel injector is arranged to supply fuel into an annular passage between first member and second member and a fourth swirler extends through first member.

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