TURBOMACHINE SEALING ELEMENT
    1.
    发明申请

    公开(公告)号:US20190010819A1

    公开(公告)日:2019-01-10

    申请号:US16027819

    申请日:2018-07-05

    IPC分类号: F01D11/12 F01D11/00 F16J15/44

    摘要: The present invention relates to sealing element for sealing a radial gap relative to a counter element of a turbomachine, wherein the sealing element has a number of adjacent cells in the peripheral direction and/or in the axial direction, which are joined to one another by common walls, wherein an extension of a least one, in particular front-side, cross section of at least one cell in a first axial section of the sealing element in the peripheral direction and/or in the axial direction for sealing against a radial flange of the counter element is smaller than that in a second axial section of the sealing element that adjoins the first axial section upstream and/or in a second axial section that adjoins the first axial section downstream.