NEAR FLOW PATH SEAL FOR A TURBOMACHINE
    1.
    发明申请
    NEAR FLOW PATH SEAL FOR A TURBOMACHINE 审中-公开
    涡轮机附近的流路密封

    公开(公告)号:US20130186103A1

    公开(公告)日:2013-07-25

    申请号:US13354625

    申请日:2012-01-20

    IPC分类号: F02C7/28 F16J15/44

    摘要: A near flow path seal for a turbomachine includes a support member having a first end portion that extends to a second end portion through an intermediate portion, and an arm member extending from the first end portion of the support member. The arm member includes a first end that extends to a second end, a first surface extending between the first and second ends, and a second, opposing surface extending between the first and second ends. The second surface includes a plurality of surface features that extend from about the first end toward the second end.

    摘要翻译: 用于涡轮机的近流路密封件包括支撑构件,该支撑构件具有通过中间部分延伸到第二端部的第一端部和从支撑构件的第一端部延伸的臂构件。 臂构件包括延伸到第二端的第一端,在第一和第二端之间延伸的第一表面和在第一和第二端之间延伸的第二相对表面。 第二表面包括从大约第一端向第二端延伸的多个表面特征。

    TIP SHROUDED BLADE
    2.
    发明申请
    TIP SHROUDED BLADE 审中-公开
    TIP SHROUDED刀片

    公开(公告)号:US20130209258A1

    公开(公告)日:2013-08-15

    申请号:US13397296

    申请日:2012-02-15

    IPC分类号: F01D5/20

    CPC分类号: F01D5/225 F05D2250/314

    摘要: A tip shrouded blade includes an airfoil rotatable about an axial centerline. Also included is a tip shroud connected at a radially outer tip of the airfoil, wherein the tip shroud includes at least one portion angled about a tangential axis defined by the radially outer tip of the airfoil.

    摘要翻译: 尖端覆盖的叶片包括可围绕轴向中心线旋转的翼型件。 还包括连接在翼型件的径向外部末端处的尖端罩,其中尖端护罩包括围绕由翼型件的径向外部末端限定的切向轴线成角度的至少一个部分。