LABYRINTH SEAL FOR TURBINES
    1.
    发明申请
    LABYRINTH SEAL FOR TURBINES 有权
    用于涡轮的LABYRINTH密封

    公开(公告)号:US20150001812A1

    公开(公告)日:2015-01-01

    申请号:US14490022

    申请日:2014-09-18

    IPC分类号: F01D11/02

    摘要: An improved labyrinth seal is described with the seal including a group of several fins forming circumferential barriers against the flow of a working fluid between stationary and rotating parts in a turbine, wherein within the group the volume between the penultimate fin and the last fin is altered compared to the average volume between other adjacent fins of the group.

    摘要翻译: 描述了改进的迷宫式密封件,密封件包括一组几个翅片,其形成围绕涡轮机中的静止部件和旋转部件之间的工作流体流动的周向障碍物,其中在该组内,倒数第二个翅片和最后的翅片之间的体积被改变 与该组其他相邻鳍片之间的平均体积相比。

    BLADE OF A ROTARY FLOW MACHINE WITH A RADIAL STRIP SEAL
    2.
    发明申请
    BLADE OF A ROTARY FLOW MACHINE WITH A RADIAL STRIP SEAL 有权
    具有径向条纹密封的旋转流动机的叶片

    公开(公告)号:US20150064012A1

    公开(公告)日:2015-03-05

    申请号:US14467752

    申请日:2014-08-25

    IPC分类号: F01D11/00 F01D5/30

    摘要: The invention refers to a blade of a rotary flow machine including an airfoil having a suction surface and a pressure surface joining each other along a trailing and a leading edge. A radially outward directed airfoil tip and a radially inward directed end joining an inner platform connect the airfoil to a shank at a radial end of the airfoil and providing, at least one shank pocket radially encircled by an axially extending portion of the platform. At least one radially extending rim extends from the trailing edge side of the shank and has an essentially radially orientated first slot for receiving a seal. A mount extends radially inwardly from said shank pocket. The first slot has a first aperture on a shank surface orientated in an axial direction.

    摘要翻译: 本发明涉及一种旋转流动机的叶片,其包括具有抽吸表面和沿着后缘和前缘彼此连接的压力表面的翼型件。 径向向外定向的翼型端头和连接内平台的径向向内的端部将翼型件在翼型件的径向端处连接到柄部,并且提供由平台的轴向延伸部分径向包围的至少一个柄袋。 至少一个径向延伸的边缘从柄的后缘侧延伸并且具有用于接收密封件的基本上径向定向的第一槽。 安装座从所述柄袋径向向内延伸。 第一槽具有在轴向方向上定向的柄表面上的第一孔。

    FLUID SEAL ARRANGEMENT AND METHOD FOR CONSTRICTING A LEAKAGE FLOW
THROUGH A LEAKAGE GAP
    3.
    发明申请
    FLUID SEAL ARRANGEMENT AND METHOD FOR CONSTRICTING A LEAKAGE FLOW THROUGH A LEAKAGE GAP 审中-公开
    流体密封装置和通过泄漏漏气约束泄漏流量的方法

    公开(公告)号:US20150050125A1

    公开(公告)日:2015-02-19

    申请号:US14341264

    申请日:2014-07-25

    IPC分类号: F01D11/10 F16J15/40

    摘要: The invention refers to a fluid seal arrangement for constricting a leakage flow directed through a leakage gap bordered by a rotational and a stationary component including at least one nozzle opening in the rotating and/or stationary component facing towards the rotating or stationary component of an opposite side of the leakage gap respectively in order for injecting a liquid or gaseous fluid flow through the nozzle opening into the leakage gap. The at least one nozzle opening is fluidly connected to a cooling channel inside said rotating and/or stationary component, so that said fluid flow emanating at the nozzle opening consists of a cooling fluid of the rotating and/or stationary component exclusively.

    摘要翻译: 本发明涉及一种流体密封装置,用于限制通过由旋转和静止部件界定的泄漏间隙的泄漏流动,所述泄漏间隙包括旋转和/或固定部件中的至少一个喷嘴开口,所述喷嘴开口面向相对的旋转部件或固定部件 以便将液体或气体流体流经喷嘴开口注入到泄漏间隙中。 至少一个喷嘴开口流体地连接到所述旋转和/或固定部件内的冷却通道,使得在喷嘴开口处发出的所述流体流由仅旋转和/或静止部件的冷却流体组成。