Composite welding rods and associated cladded articles

    公开(公告)号:US11000921B2

    公开(公告)日:2021-05-11

    申请号:US16396123

    申请日:2019-04-26

    申请人: Kennametal Inc.

    IPC分类号: B23K35/30 C22C19/00 C22C29/08

    摘要: Welding rods and associated cladded articles are described herein. Briefly, a welding rod comprises a hard particle component dispersed in a nickel-based alloy matrix or cobalt-based alloy matrix, the hard particle component comprising tungsten carbide particles having an average size of less than 45 μm, and the nickel-based alloy matrix or the cobalt-based alloy matrix comprising at least one metal carbide forming element.

    Wear resistant articles and applications thereof

    公开(公告)号:US11376817B2

    公开(公告)日:2022-07-05

    申请号:US16931927

    申请日:2020-07-17

    申请人: Kennametal Inc.

    摘要: Wear resistant articles are described herein which, in some embodiments, mitigate CTE differences between wear resistant components and metallic substrates. In one aspect, an article comprises a layer of sintered cemented carbide bonded to a layer of iron-based alloy via a metal-matrix composite bonding layer, wherein coefficients of thermal expansion (CTE) of the sintered cemented carbide layer, metal matrix composite bonding layer, and iron-based alloy layer satisfy the relation: x = (  C ⁢ ⁢ T ⁢ ⁢ E ⁢ ⁢ WC - C ⁢ ⁢ T ⁢ ⁢ E ⁢ ⁢ M ⁢ ⁢ M ⁢ ⁢ C  ) (  C ⁢ ⁢ T ⁢ ⁢ E ⁢ ⁢ M ⁢ ⁢ M ⁢ ⁢ C - C ⁢ ⁢ T ⁢ ⁢ E ⁢ ⁢ Fe  ) wherein 0.5≤x≤2 and CTE WC, CTE MMC and CTE Fe are the CTE values for the sintered cemented carbide, metal matrix composite, and iron-based alloy in 1/K respectively at 900° C. to 1100° C.

    IMPARTING HIGH-TEMPERATURE WEAR RESISTANCE TO TURBINE BLADE Z-NOTCHES
    8.
    发明申请
    IMPARTING HIGH-TEMPERATURE WEAR RESISTANCE TO TURBINE BLADE Z-NOTCHES 审中-公开
    将高温耐磨损性提高到涡轮叶片Z型槽口

    公开(公告)号:US20160245099A1

    公开(公告)日:2016-08-25

    申请号:US14628912

    申请日:2015-02-23

    申请人: KENNAMETAL INC.

    IPC分类号: F01D5/28 B05D3/00

    摘要: A method of imparting wear-resistance to a contact face of a turbine blade Z-notch comprising applying a flexible cladding sheet comprising a Co-based cladding alloy and an organic binder to the contact face of the Z-notch, heating the turbine blade Z-notch with flexible cladding sheet thereon to volatilize the organic binder and remove it from the cladding sheet, and further heating the turbine blade Z-notch with flexible cladding sheet thereon to sinter the cladding sheet by liquid phase sintering, thereby cladding the cladding sheet to the contact face to produce a wear-resistant layer thereon.

    摘要翻译: 一种赋予涡轮叶片Z形切口的接触面的耐磨性的方法,包括将包含Co基包层合金和有机粘合剂的柔性包层片施加到Z形切口的接触面,加热涡轮叶片Z - 在其上具有柔性包覆片,使有机粘合剂挥发并将其从包覆片上除去,并且用柔性包覆片进一步加热涡轮叶片Z形切口,通过液相烧结烧结包覆片,从而将包覆片包覆 接触面以在其上产生耐磨层。