Continuous ring composite turbine shroud
    1.
    发明授权
    Continuous ring composite turbine shroud 有权
    连续环复合涡轮机罩

    公开(公告)号:US08985944B2

    公开(公告)日:2015-03-24

    申请号:US13075740

    申请日:2011-03-30

    摘要: A composite annular shroud supported by a support assembly including at least two single piece full 360 degree rings and at least partially disposed within an innermost one of the rings. The shroud is biased against and in sealing engagement with an inner flange of the innermost ring. A three ring assembly includes the inner ring disposed radially inwardly of a middle ring disposed radially inwardly of an outer ring and the shroud at least partially disposed within the inner ring. At least three clocking pins extend radially inwardly from the middle ring through slots in the inner ring into notches in the shroud.The middle ring may be an aft end of a support ring fixedly connected to an engine backbone. Mounting pins may be press fitted into pin holes in the middle ring and extend radially outwardly from the middle ring through radial holes in the outer ring.

    摘要翻译: 一种由支撑组件支撑的复合环形罩,所述支撑组件包括至少两个单件全360度环并且至少部分地设置在所述环的最内一个环中。 护罩偏置在最内圈的内凸缘上并与之密封接合。 三环组件包括设置在外环的径向向内设置的中环的径向向内的内环,并且护罩至少部分地设置在内环内。 至少三个定时销从中间环径向向内延伸穿过内圈中的槽,使其处于护罩中的凹口。 中间环可以是固定地连接到发动机主干的支撑环的后端。 安装销可以压配合到中间环的销孔中,并从中间环径向向外延伸穿过外环的径向孔。

    CONTINUOUS RING COMPOSITE TURBINE SHROUD
    2.
    发明申请
    CONTINUOUS RING COMPOSITE TURBINE SHROUD 有权
    连续式复合涡轮机

    公开(公告)号:US20120247124A1

    公开(公告)日:2012-10-04

    申请号:US13075740

    申请日:2011-03-30

    IPC分类号: F01D11/00 F02C7/00

    摘要: A composite annular shroud supported by a support assembly including at least two single piece full 360 degree rings and at least partially disposed within an innermost one of the rings. The shroud is biased against and in sealing engagement with an inner flange of the innermost ring. A three ring assembly includes the inner ring disposed radially inwardly of a middle ring disposed radially inwardly of an outer ring and the shroud at least partially disposed within the inner ring. At least three clocking pins extend radially inwardly from the middle ring through slots in the inner ring into notches in the shroud.The middle ring may be an aft end of a support ring fixedly connected to an engine backbone. Mounting pins may be press fitted into pin holes in the middle ring and extend radially outwardly from the middle ring through radial holes in the outer ring.

    摘要翻译: 一种由支撑组件支撑的复合环形罩,所述支撑组件包括至少两个单件全360度环并且至少部分地设置在所述环的最内一个环中。 护罩偏置在最内圈的内凸缘上并与之密封接合。 三环组件包括设置在外环的径向向内设置的中环的径向向内的内环,并且护罩至少部分地设置在内环内。 至少三个定时销从中间环径向向内延伸穿过内圈中的槽,使其处于护罩中的凹口。 中间环可以是固定地连接到发动机主干的支撑环的后端。 安装销可以压配合到中间环的销孔中,并从中间环径向向外延伸穿过外环中的径向孔。