COATED SEAL SLOT SYSTEMS FOR TURBOMACHINERY AND METHODS FOR FORMING THE SAME
    5.
    发明申请
    COATED SEAL SLOT SYSTEMS FOR TURBOMACHINERY AND METHODS FOR FORMING THE SAME 审中-公开
    用于涡轮机的涂层密封槽系统及其形成方法

    公开(公告)号:US20170058686A1

    公开(公告)日:2017-03-02

    申请号:US14834866

    申请日:2015-08-25

    IPC分类号: F01D11/00 F01D25/00

    摘要: A coated seal slot system for turbomachinery includes a first turbine component comprising a first groove having at least one first coating attached to at least a portion of the first groove of the first turbine component, a second turbine component comprising a second groove having at least one second coating attached to at least a portion of the second groove of the second turbine component. The first and the second turbine components are disposable adjacent to each other with the first groove having the first coating and the second groove having the second coating together forming a coated seal slot extending across a gap between the first turbine component and the second turbine component. A seal is disposable in the coated seal slot and extendable across the gap between the first and the second turbine components and engageable with the first coating and the second coating to inhibit leakage of gas through the gap.

    摘要翻译: 一种用于涡轮机械的涂覆密封槽系统包括第一涡轮机部件,该第一涡轮机部件包括第一凹槽,该第一凹槽具有连接到第一涡轮机部件的第一凹槽的至少一部分的至少一个第一涂层,第二涡轮部件,其包括具有至少一个 第二涂层附着到第二涡轮机部件的第二凹槽的至少一部分。 第一和第二涡轮机部件是彼此相邻的,第一凹槽具有第一涂层,第二凹槽具有第二涂层,一起形成延伸穿过第一涡轮机部件和第二涡轮机部件之间的间隙的涂覆的密封槽。 密封件在涂覆的密封槽中是一次性的,并且可以跨越第一和第二涡轮机部件之间的间隙延伸并且可与第一涂层和第二涂层接合以抑制气体通过间隙的泄漏。