GAS TURBINE TRANSITION PIECE AFT FRAME ASSEMBLIES WITH COOLING CHANNELS AND METHODS FOR MANUFACTURING THE SAME
    65.
    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。

    METHODS OF FORMING DESIRED GEOMETRY ON SUPERALLOY PART USING POWDER MIXTURE OF LOW AND HIGH MELT TEMPERATURE SUPERALLOYS

    公开(公告)号:US20220372627A1

    公开(公告)日:2022-11-24

    申请号:US17816472

    申请日:2022-08-01

    Abstract: Methods of forming a desired geometry at a location on a superalloy part are disclosed. The method may include directing particles of a powder mixture including a low melt temperature superalloy powder and a high melt temperature superalloy powder to the location on the superalloy part at a velocity sufficient to cause the superalloy powders to deform and to form a mechanical bond but not a metallurgical bond to the superalloy part. The directing of particles continues until the desired geometry is formed. Heat is applied to the powder mixture on the repair location. The heat causes the low melt temperature superalloy powder to melt, creating the metallurgical bonding at the location. Another method uses the same directing to form a preform for repairing the location on the part. The low melt temperature superalloy powder melts at less than 1287° C., and the high melt temperature superalloy powder melts at greater than 1287° C.

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