HOT GAS PATH COMPONENT TRAILING EDGE HAVING NEAR WALL COOLING FEATURES
    94.
    发明申请
    HOT GAS PATH COMPONENT TRAILING EDGE HAVING NEAR WALL COOLING FEATURES 有权
    具有近壁式冷却功能的热气路径组件拖车边缘

    公开(公告)号:US20160362985A1

    公开(公告)日:2016-12-15

    申请号:US14739944

    申请日:2015-06-15

    Abstract: A hot gas path component includes a substrate having an outer surface and an inner surface. The inner surface defines an interior space. The outer surface defines a pressure side surface and a suction side surface. The pressure and suction side surfaces are joined together at a leading edge and at a trailing edge. A first cooling passage is formed in the suction side surface of the substrate. It is coupled in flow communication to the interior space. A second cooling passage, separate from the first cooling passage, is formed in the pressure side surface. The second cooling passage is coupled in flow communication to the interior space. A cover is disposed over at least a portion of the first and second cooling passages. The interior space channels a cooling fluid to the first and second cooling passages, which channel the cooling fluid therethrough to remove heat from the component.

    Abstract translation: 热气体路径部件包括具有外表面和内表面的基板。 内表面限定了内部空间。 外表面限定了压力侧表面和吸力侧表面。 压力和吸力侧表面在前缘和后缘处连接在一起。 第一冷却通道形成在基板的吸力侧表面上。 它与流动通信耦合到内部空间。 与第一冷却通道分开的第二冷却通道形成在压力侧表面上。 第二冷却通道与内部空间流动联接。 盖子设置在第一和第二冷却通道的至少一部分上。 内部空间将冷却流体引导到第一和第二冷却通道,第一和第二冷却通道将冷却流体通过其中以从部件移除热量。

    GAS TURBINE TRANSITION PIECE AFT FRAME ASSEMBLIES WITH COOLING CHANNELS AND METHODS FOR MANUFACTURING THE SAME
    100.
    发明申请
    GAS TURBINE TRANSITION PIECE AFT FRAME ASSEMBLIES WITH COOLING CHANNELS AND METHODS FOR MANUFACTURING THE SAME 有权
    具有冷却通道的气体涡轮转换丝杠组合框架及其制造方法

    公开(公告)号:US20150369068A1

    公开(公告)日:2015-12-24

    申请号:US14090832

    申请日:2013-11-26

    Abstract: Aft frame assemblies for a gas turbine transition pieces include a body comprising an exterior surface and a plurality of interior surfaces, one or more exterior cooling holes disposed on the exterior surface of the body for capturing compressor discharge air outside of the transition piece, and a supplemental component bonded to at least one of the plurality of interior surfaces of the body. At least one cooling channel is at least partially defined by the supplemental component and the interior surface that the supplemental component is bonded to, wherein the at least one cooling channel fluidly connects at least one of the one or more exterior cooling holes to one or more interior cooling outlets that discharge the compressor discharge air captured from the at least one of the one or more exterior cooling holes.

    Abstract translation: 用于燃气涡轮机过渡件的后框架组件包括:主体,其包括外表面和多个内表面;一个或多个外部冷却孔,设置在主体的外表面上,用于捕获过渡件外部的压缩机排出空气;以及 补充部件结合到身体的多个内表面中的至少一个。 至少一个冷却通道至少部分地由补充部件和附加部件结合到的内表面限定,其中至少一个冷却通道将一个或多个外部冷却孔中的至少一个流体连接到一个或多个 内部冷却出口,其排出从一个或多个外部冷却孔中的至少一个捕获的压缩机排放空气。

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