INSERT ELEMENT FOR CLOSING AN OPENING INSIDE A WALL OF A HOT GAS PATH COMPONENT OF A GAS TURBINE AND METHOD FOR ENHANCING OPERATIONAL BEHAVIOUR OF A GAS TURBINE
    1.
    发明申请
    INSERT ELEMENT FOR CLOSING AN OPENING INSIDE A WALL OF A HOT GAS PATH COMPONENT OF A GAS TURBINE AND METHOD FOR ENHANCING OPERATIONAL BEHAVIOUR OF A GAS TURBINE 有权
    用于封闭气体涡轮机的热气道组件内的开启的插入元件和用于增强气体涡轮机的操作行为的方法

    公开(公告)号:US20140147251A1

    公开(公告)日:2014-05-29

    申请号:US14087569

    申请日:2013-11-22

    Abstract: The invention refers an insert element for closing an opening inside a wall of a hot gas path component of a gas turbine. The insert includes a plate like body with an opening sided surface. The surface provides at least one first area which projects beyond at least one second area of said surface which surrounds the at least one first area frame-like. The at least one first area is encompassed by a circumferential edge corresponding in form and size to the opening such that the circumferential edge and the opening contour limit a gap at least in some areas, while the at least one second area contacts directly or indirectly the wall of the hot gas path component at a rear side facing away from the hot gas path. The plate like body provides at least a first functional layer-system, providing at least one layer made of heat resistant material, defining the first area of the surface (S).

    Abstract translation: 本发明涉及一种用于关闭燃气轮机的热气路径部件的壁内的开口的插入元件。 插入件包括具有开口侧表面的板状主体。 所述表面提供至少一个第一区域,其突出超过所述表面的至少一个第二区域,所述至少一个第二区域围绕所述至少一个第一区域框架状。 所述至少一个第一区域被围绕所述开口的形式和尺寸对应的圆周边缘包围,使得所述周边边缘和所述开口轮廓至少在一些区域中限制间隙,而所述至少一个第二区域直接或间接地接触 所述热气体路径部件的壁位于远离热气体路径的后侧。 板状体提供至少第一功能层系统,提供限定表面(S)的第一区域的至少一层由耐热材料制成的层。

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