ADVANCED STATIONARY SEALING COOLED CROSS-SECTION FOR AXIAL RETENTION OF CERAMIC MATRIX COMPOSITE SHROUDS
    12.
    发明申请
    ADVANCED STATIONARY SEALING COOLED CROSS-SECTION FOR AXIAL RETENTION OF CERAMIC MATRIX COMPOSITE SHROUDS 审中-公开
    陶瓷基复合材料的轴向保持高级静态密封冷却交叉部分

    公开(公告)号:US20170074111A1

    公开(公告)日:2017-03-16

    申请号:US14850383

    申请日:2015-09-10

    Abstract: In one aspect, the present subject matter is directed to a gas turbine sealing assembly that includes a first static gas turbine wall and a second static gas turbine wall. A seal is disposed between the first static gas turbine wall and the second static gas turbine wall. The seal includes a first seal layer defining a first seal layer aperture extending therethrough. A second seal layer defines an elongated slot extending therethrough. The elongated slot includes a first end and a second end. A third seal layer defines a third seal layer aperture extending therethrough. The second seal layer is positioned between the first seal layer and the third seal layer such that the first seal layer aperture is in fluid communication with the first end and the third seal layer aperture is in fluid communication with the second end.

    Abstract translation: 在一个方面,本主题涉及一种燃气轮机密封组件,其包括第一静态燃气涡轮机壁和第二静态燃气涡轮机壁。 密封件设置在第一静态燃气涡轮机壁和第二静态燃气涡轮机壁之间。 密封件包括限定延伸穿过其中的第一密封层孔的第一密封层。 第二密封层限定延伸穿过其中的细长槽。 细长槽包括第一端和第二端。 第三密封层限定延伸穿过其中的第三密封层孔。 第二密封层位于第一密封层和第三密封层之间,使得第一密封层孔与第一端流体连通,第三密封层孔与第二端流体连通。

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