JOINT PART
    6.
    发明申请
    JOINT PART 审中-公开
    联合部分

    公开(公告)号:US20140321905A1

    公开(公告)日:2014-10-30

    申请号:US14361539

    申请日:2012-11-19

    发明人: Takashi Arai

    IPC分类号: B23K1/19

    摘要: Provided is joint part capable of suppressing diffusion of carbon and nitrogen contained in the steel member to the TiAl-based alloy member and suppressing formation of voids, titanium carbide or a nitride due to diffusion of carbon and nitrogen contained in the steel member, and thereby suppressing decrease in the brazing strength. A joint part comprises a steel member containing alloy elements including C and Cr, a TiAl-based alloy member, and a Ni-based brazing filler metal via which the steel member and the TiAl-based alloy member are joined to each other, wherein the steel member has a carbide and a nitride each forming a bond with at least one of the alloy elements at least on a side of a boundary with the Ni-based brazing filler metal, and diffusion of C and N to the Ni-based brazing filler metal adjacent to the TiAl-based alloy member is suppressed by the carbide and the nitride. The joint part may be a turbine body 1 comprising a turbine wheel 2 and a shaft 3, and a structural steel material of the shaft 3 is structural steel material containing 0.30 to 0.45 wt % of C and 0.85 to 1.25 wt % of Cr, or a martensitic stainless steel material containing at most 15 wt % of C and 11.5 to 13 wt % of Cr.

    摘要翻译: 提供了能够抑制钢构件中所含的碳氮的扩散到TiAl基合金构件并抑制由于钢构件中包含的碳和氮的扩散而导致的空隙,碳化钛或氮化物的形成的接合部, 抑制钎焊强度的降低。 接合部包括包含C和Cr的合金元素的钢构件,TiAl基合金构件和Ni基钎料,钢构件和TiAl基合金构件通过该Ni基钎料彼此接合,其中 钢构件具有碳化物和氮化物,其至少在与Ni基钎料的边界一侧与至少一个合金元素形成结合,并且将C和N扩散到Ni基钎料 与TiAl基合金构件相邻的金属被碳化物和氮化物抑制。 接头部分可以是包括涡轮机叶轮2和轴3的涡轮机体1,轴3的结构钢材料是含有0.30-0.45重量%的C和0.85-1.25重量%的Cr的结构钢材料,或者 含有至多15重量%C和11.5〜13重量%Cr的马氏体不锈钢材料。

    Methods for manufacturing porous orthopaedic implants
    7.
    发明授权
    Methods for manufacturing porous orthopaedic implants 有权
    制造多孔整形外科植入物的方法

    公开(公告)号:US08727203B2

    公开(公告)日:2014-05-20

    申请号:US12883447

    申请日:2010-09-16

    IPC分类号: B23K20/02 B23K26/00

    摘要: A method of manufacturing an orthopaedic implant device having a porous outer surface is described. In one embodiment, the implant device includes a porous layer, an intermediate layer, and a solid substrate. The porous layer is preferably bonded to the intermediate layer by cold isostatic pressing. The intermediate layer is preferably bonded by vacuum welding to the solid substrate such that the porous layer forms at least a portion of the outer surface of the orthopaedic implant device. Preferably, a diffusion bond is created between the bonded intermediate layer and the solid substrate by hot isostatic pressing. In another embodiment, a porous layer is created on an outer surface of a solid layer by selective melting. Preferably, the solid layer is bonded to the solid substrate such that the porous layer forms at least a portion of the outer surface of the orthopaedic implant device.

    摘要翻译: 描述了一种制造具有多孔外表面的矫形植入装置的方法。 在一个实施例中,植入装置包括多孔层,中间层和固体基底。 多孔层优选通过冷等静压来结合到中间层。 中间层优选通过真空焊接粘结到固体基底上,使得多孔层形成整形外科植入装置的外表面的至少一部分。 优选地,通过热等静压法在接合的中间层和固体基材之间产生扩散接合。 在另一个实施方案中,通过选择性熔融在固体层的外表面上形成多孔层。 优选地,固体层结合到固体基质上,使得多孔层形成整形外科植入装置的外表面的至少一部分。

    METHOD AND DEVICE FOR PRODUCING A COMPONENT OF A TURBOMACHINE
    10.
    发明申请
    METHOD AND DEVICE FOR PRODUCING A COMPONENT OF A TURBOMACHINE 审中-公开
    用于生产涡轮分子的组分的方法和装置

    公开(公告)号:US20120213659A1

    公开(公告)日:2012-08-23

    申请号:US13504888

    申请日:2010-09-30

    摘要: A method for producing a component of a turbomachine is disclosed. The method includes a) layer-by-layer deposition of a powder component material onto a component platform in a region of a buildup and joining zone, where the deposition takes place in accordance with layer information of the component to be produced; b) local layer-by-layer fusion or sintering of the powder component material by energy supplied in the region of the buildup and joining zone, where the buildup and joining zone is heated to a temperature just below a melting point of the powder component material; c) layer-by-layer lowering of the component platform by a predefined layer thickness; and d) repetition of steps a) to c) until the component is finished. A device for producing a component of a turbomachine is also disclosed.

    摘要翻译: 公开了一种涡轮机组件的制造方法。 该方法包括:a)在堆积和接合区域的区域中将粉末成分材料逐层沉积到部件平台上,其中根据要生产的部件的层信息进行沉积; b)通过在积聚和接合区域的区域供应的能量对粉末成分材料进行局部逐层融合或烧结,其中将积聚和接合区域加热到刚好低于粉末组分材料熔点的温度 ; c)将组件平台逐层降低预定层厚度; 和d)重复步骤a)至c)直到组分完成。 还公开了一种用于生产涡轮机的部件的装置。