TURBINE MINIDISK BUMPER FOR GAS TURBINE ENGINE
    11.
    发明申请
    TURBINE MINIDISK BUMPER FOR GAS TURBINE ENGINE 审中-公开
    天然气涡轮发动机涡轮微型保险丝

    公开(公告)号:US20160069259A1

    公开(公告)日:2016-03-10

    申请号:US14783225

    申请日:2014-04-07

    Abstract: An assembly for a gas turbine engine includes a minidisk that includes an axial extension extending from a disc. The axial extension includes an inner diameter surface and a recess arranged radially opposite the inner diameter surface. The recess provides a radially outwardly extending flange and a bumper extending radially inward from and proud of the inner diameter surface. A method of working on a gas turbine engine section includes inserting a tool into a cavity beneath a seal assembly, and engaging a flange of a minidisk with the tool to manipulate first and second rotors with respect to one another.

    Abstract translation: 用于燃气涡轮发动机的组件包括包括从盘延伸的轴向延伸的小型磁盘。 轴向延伸部包括内径表面和径向相对于内径表面设置的凹部。 凹槽提供径向向外延伸的凸缘和从内径表面向内径向向内延伸的保险杠。 在燃气涡轮发动机部分上工作的方法包括将工具插入到密封组件下面的空腔中,并且将微型盘架的凸缘与工具接合以相对于彼此操纵第一和第二转子。

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