JOINING PROCESS, JOINED ARTICLE, AND PROCESS OF FABRICATING A JOINED ARTICLE
    21.
    发明申请
    JOINING PROCESS, JOINED ARTICLE, AND PROCESS OF FABRICATING A JOINED ARTICLE 审中-公开
    加工过程,加工文章和制作加工文章的过程

    公开(公告)号:US20140335373A1

    公开(公告)日:2014-11-13

    申请号:US13889489

    申请日:2013-05-08

    Abstract: Joining process, joined article, and process of fabricating a joined article are disclosed. The joining process includes providing a consumable electrode comprising a first material and a second material, melting the consumable electrode by a current-induced melting or remelting, and re-solidifying the first material and the second material to form a dissimilar ingot having a first region being a re-solidification of the first material and a second region being a re-solidification of the second material. The joined article includes the first region and the second region; the dissimilar ingot at least partially defines the joined article. The process of fabricating includes providing the dissimilar ingot, positioning the dissimilar ingot within a die, and applying force from the die to compress the dissimilar ingot, thereby forming the joined article.

    Abstract translation: 公开了加工过程,连结件和制造连接件的过程。 接合工艺包括提供包括第一材料和第二材料的消耗电极,通过电流感应熔化或再熔化来熔化可消耗电极,并重新固化第一材料和第二材料,以形成具有第一区域的不同锭 是第一材料的再凝固,第二区域是第二材料的再凝固。 所述接合制品包括所述第一区域和所述第二区域; 不同的锭至少部分地限定了连接的物品。 制造过程包括提供不同的锭,将不同的锭定位在模具内,并且从模具施加力以压缩不同的锭,从而形成连接的制品。

    METHOD FOR HARDFACING A METAL ARTICLE
    22.
    发明申请

    公开(公告)号:US20190022786A1

    公开(公告)日:2019-01-24

    申请号:US15653069

    申请日:2017-07-18

    Inventor: Dechao LIN

    Abstract: A method for hardfacing a metal article is disclosed including applying a first pass of a metal composition to a surface of the metal article along a first application path, applying a second pass of the metal composition to the surface along a second application path, and applying a third pass of the metal composition to the surface along a third application path between the first application path and the second application path. The first pass and the second pass form a hardfacing perimeter, and the third pass fills in the hardfacing perimeter.

    METHOD FOR CLOSING A PLURALITY OF HOLES IN A METAL ARTICLE

    公开(公告)号:US20190022785A1

    公开(公告)日:2019-01-24

    申请号:US15652953

    申请日:2017-07-18

    Inventor: Dechao LIN

    Abstract: A method for closing a plurality of holes penetrating from a first surface of a metal article through a second surface of the metal article is disclosed including applying the metal composition to the first surface along a bridging application path. The bridging application path passes over the plurality of holes between a first edge of each of the plurality of holes and a second edge of each of the plurality of holes. Applying the metal composition along the bridging application path closes the plurality of holes.

    METHOD FOR CLOSING A HOLE IN A METAL ARTICLE
    24.
    发明申请

    公开(公告)号:US20190022784A1

    公开(公告)日:2019-01-24

    申请号:US15652857

    申请日:2017-07-18

    Inventor: Dechao LIN

    Abstract: A method for closing a hole penetrating a hole height from a first surface of a metal article through a second surface of the metal article is disclosed including removing a portion of the metal article surrounding the hole from the metal article. The portion includes a depth extending from the first surface into the metal article and terminating prior to the second surface. Removing the portion forms a support surface within the hole adjacent and opposite to the second surface. A metal support structure is disposed within the hole on the support surface, and a metal composition is applied into the hole and onto the metal support structure. The metal support structure, the metal composition, and the metal article are fused together.

    METHOD FOR FORMING A TURBINE COMPONENT
    25.
    发明申请

    公开(公告)号:US20190022783A1

    公开(公告)日:2019-01-24

    申请号:US15653015

    申请日:2017-07-18

    Inventor: Dechao LIN

    Abstract: A method for forming a turbine component is disclosed, including applying a metal composition to a structure by an additive manufacturing technique and lengthening the structure by the additive manufacturing technique. The structure is a transition piece or a combustion liner-transition piece assembly. Lengthening the structure forms a structure extension. A picture frame is formed on an outer surface of the structure extension by the additive manufacturing technique.

    METHODS OF WELDING AND WELDED ARTICLES
    26.
    发明申请

    公开(公告)号:US20180236583A1

    公开(公告)日:2018-08-23

    申请号:US15435932

    申请日:2017-02-17

    Inventor: Dechao LIN

    Abstract: In some embodiments, a method of welding includes welding at least one fill bead to fill at least one gap on a substrate with arc scanning by an arc welder. The gap is defined by at least one weld bead on the substrate. The weld beads are non-overlapping. A welded article includes a substrate including a crack-prone superalloy and at least one weld bead and at least one fill bead welded on the substrate. The fill bead, the weld bead, and a heat-affected zone of the substrate are micro-crack-free and macro-crack-free. In some embodiments, a method of welding includes welding weld beads on a substrate and welding fill beads on the substrate with an arc welder while arc scanning. The fill beads fill the gaps between neighboring pairs of weld beads. The fill beads are welded in a non-sequential order.

    METHOD OF TREATING A BRUSH SEAL, TREATED BRUSH SEAL, AND BRUSH SEAL ASSEMBLY

    公开(公告)号:US20170260868A1

    公开(公告)日:2017-09-14

    申请号:US15067253

    申请日:2016-03-11

    Abstract: A method treats a brush seal at a tip end of the brush seal. The method includes contacting the tip end of the brush seal to an oxidation-resistant, wear-resistant coating composition and heat-treating a distal portion of the bristles to form an oxidation-resistant, wear-resistant coating on the distal portion from the oxidation-resistant, wear-resistant coating composition. A brush seal includes a brush support and bristles extending from the brush support with a distal portion coated by an aluminide diffusion coating. A brush seal assembly includes a non-rotary component and a rotary component. The non-rotary component includes a brush seal including a bristle pack. The bristle pack includes bristles extending from a brush support with a distal portion coated by an aluminide diffusion coating. The rotary component has a sealing surface contacting the distal portion of the brush seal to form a turbine seal between the rotary component and the non-rotary component.

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