IGNITER ASSEMBLY FOR A GAS TURBINE ENGINE
    1.
    发明申请
    IGNITER ASSEMBLY FOR A GAS TURBINE ENGINE 审中-公开
    用于气体涡轮发动机的IGNITER组件

    公开(公告)号:US20160356223A1

    公开(公告)日:2016-12-08

    申请号:US14731524

    申请日:2015-06-05

    Abstract: In one aspect the present subject matter is directed to an igniter assembly for a gas turbine engine. The igniter assembly includes an outer housing and an igniter tube that extends radially through the outer housing. The igniter tube includes an ignition tip, a nut coupled to the igniter tube and disposed at least partially within the outer housing and a biasing member that extends between an inner surface of a top portion of the outer housing and the nut. A flexible seal extends radially inwardly from a bottom side of the nut and a retention collar is coupled to the igniter tube proximate to the ignition tip. The retention collar is configured to couple to a mounting ring connected to an outer liner of a combustor for the gas turbine engine.

    Abstract translation: 在一个方面,本主题涉及一种用于燃气涡轮发动机的点火器组件。 点火器组件包括外壳体和径向延伸穿过外壳体的点火管。 点火管包括点火头,联接到点火管并且至少部分地设置在外壳内的螺母和在外壳的顶部的内表面和螺母之间延伸的偏置构件。 柔性密封件从螺母的底侧径向向内延伸,并且保持套环与靠近点火头的点火器管连接。 保持套环构造成联接到连接到用于燃气涡轮发动机的燃烧器的外衬套的安装环。

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