GAS TURBINE ENGINE FUEL INJECTOR WITH AN INNER HEAT SHIELD
    2.
    发明申请
    GAS TURBINE ENGINE FUEL INJECTOR WITH AN INNER HEAT SHIELD 有权
    燃气涡轮发动机燃油喷射器内置热风罩

    公开(公告)号:US20150253009A1

    公开(公告)日:2015-09-10

    申请号:US14199419

    申请日:2014-03-06

    CPC classification number: F23R3/28 F23R3/36 F23R2900/00004

    Abstract: A fuel injector for a combustor of a gas turbine engine is disclosed. The fuel injector includes a gas outer tube, a gas inner tube, a liquid tube, and a heat shield. The gas outer tube and the gas inner tube form a gas fuel annulus. The gas inner tube and the liquid tube form a liquid fuel annulus. The liquid tube forms an air cavity. The heat shield extends within the liquid tube forming an insulating gap between the heat shield and the liquid tube.

    Abstract translation: 公开了一种用于燃气涡轮发动机的燃烧器的燃料喷射器。 燃料喷射器包括气体外管,气体内管,液体管和隔热罩。 气体外管和气体内管形成气体燃料环。 气体内管和液体管形成液体燃料环。 液体管形成空气腔。 热屏蔽在液体管内延伸,形成隔热层与液体管之间的绝缘间隙。

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