CONTACTLESS SEALS FOR GAS TURBINE ENGINES
    31.
    发明申请
    CONTACTLESS SEALS FOR GAS TURBINE ENGINES 审中-公开
    气体涡轮发动机接头密封件

    公开(公告)号:US20160053623A1

    公开(公告)日:2016-02-25

    申请号:US14809894

    申请日:2015-07-27

    Inventor: Ioannis Alvanos

    Abstract: A seal for a gas turbine engine includes a first seal structure and a second seal structure. The first seal structure is separated from the second seal structure by a gap. The first seal structure includes an injector extending into the gap with an outlet that is in fluid communication with a fluid source. Fluid issuing from the outlet and against the second seal structure magnifies a vortex formed within the gap by fluid traversing the gap.

    Abstract translation: 燃气涡轮发动机的密封件包括第一密封结构和第二密封结构。 第一密封结构通过间隙与第二密封结构分离。 第一密封结构包括延伸到具有与流体源流体连通的出口的间隙中的喷射器。 从出口排出并抵靠第二密封结构的流体通过流过该间隙的流体放大在间隙内形成的涡流。

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