COOLED FUEL INJECTOR SYSTEM FOR A GAS TURBINE ENGINE
    2.
    发明申请
    COOLED FUEL INJECTOR SYSTEM FOR A GAS TURBINE ENGINE 审中-公开
    用于燃气涡轮发动机的冷却燃料喷射器系统

    公开(公告)号:US20160201917A1

    公开(公告)日:2016-07-14

    申请号:US14912117

    申请日:2014-08-14

    Abstract: A fuel injector is provided for a gas turbine engine. The fuel injector includes a fuel conduit and a cooling fluid circuit through a strut. A gas turbine engine is provided that includes a multiple of fuel injectors in communication with a combustor and a cooling system in communication with each of the multiple of fuel injectors.

    Abstract translation: 燃气喷射器设置用于燃气涡轮发动机。 燃料喷射器包括通过支柱的燃料管道和冷却流体回路。 提供了一种燃气涡轮发动机,其包括与燃烧器连通的多个燃料喷射器和与多个燃料喷射器中的每一个连通的冷却系统。

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