GAS TURBINE ENGINE PREMIX INJECTORS
    3.
    发明申请
    GAS TURBINE ENGINE PREMIX INJECTORS 审中-公开
    燃气涡轮发动机喷油器

    公开(公告)号:WO2007119115A2

    公开(公告)日:2007-10-25

    申请号:PCT/IB2006004251

    申请日:2006-12-14

    CPC classification number: F23R3/346 F23R3/14 F23R3/286 F23R3/36 Y02T50/675

    Abstract: One embodiment is a gas turbine engine premix injector including a mixing duct, a plurality of air inlet slots leading to the duct, a plurality of gaseous fuel inlet apertures leading to the duct, a plurality of vanes positioned in the duct downstream from said air inlets, a plurality of liquid fuel inlet apertures leading to the duct, and a plurality of discharge windows positioned between the vanes.

    Abstract translation: 一个实施例是一种燃气涡轮发动机预混喷射器,其包括混合管道,通向管道的多个空气入口狭槽,通向管道的多个气体燃料入口孔,多个叶片,其位于管道下游的所述空气入口 ,多个通向管道的液体燃料入口孔和位于叶片之间的多个排出窗口。

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