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公开(公告)号:US11117208B2
公开(公告)日:2021-09-14
申请号:US15465170
申请日:2017-03-21
Applicant: Kennametal Inc.
Inventor: Martin G. Perez , Michael Meyer , Robert W. Monds , Loretta M. Bell
IPC: B23K1/00 , B22F1/00 , B23K35/02 , B23K35/30 , C22C19/03 , C22C19/07 , C22C30/00 , F01D5/28 , B23K101/00
Abstract: In one aspect, composite preforms are provided for imparting wear resistance to superalloy articles. The composite preforms can be employed for metallurgically bonding alloy wear plates or pads to superalloy articles. A composite preform, in some embodiments, comprises a powder alloy composition comprising 1-30 wt. % nickel, 0.05-2 wt. % iron, 15-25 wt. % chromium, 10-30 wt. % molybdenum, 0-1 wt. % carbon, 1-5 wt. % silicon, 0.05-2 wt. % boron, 0-5 wt. % tungsten, 0-3 wt. % tantalum, 0-0.1 wt % manganese, 0-3 wt. % aluminum, 0-0.1 wt % yttrium and the balance cobalt.
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公开(公告)号:US20180272451A1
公开(公告)日:2018-09-27
申请号:US15465170
申请日:2017-03-21
Applicant: Kennametal Inc.
Inventor: Martin G. Perez , Michael Meyer , Robert W. Monds , Loretta M. Bell
CPC classification number: B23K1/0018 , B22F1/0059 , B22F5/04 , B22F7/08 , B22F2007/068 , B22F2301/15 , B23K35/0244 , B23K35/3046 , B23K2101/001 , C22C1/0433 , C22C19/03 , C22C19/07 , C22C30/00 , C22C32/0094 , F01D5/286 , F05D2300/175 , F05D2300/177 , F05D2300/603
Abstract: In one aspect, composite preforms are provided for imparting wear resistance to superalloy articles. The composite preforms can be employed for metallurgically bonding alloy wear plates or pads to superalloy articles. A composite preform, in some embodiments, comprises a powder alloy composition comprising 1-30 wt. % nickel, 0.05-2 wt. % iron, 15-25 wt. % chromium, 10-30 wt. % molybdenum, 0-1 wt. % carbon, 1-5 wt. % silicon, 0.05-2 wt. % boron, 0-5 wt. % tungsten, 0-3 wt. % tantalum, 0-0.1 wt % manganese, 0-3 wt. % aluminum, 0-0.1 wt % yttrium and the balance cobalt.
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公开(公告)号:US10967466B2
公开(公告)日:2021-04-06
申请号:US15492413
申请日:2017-04-20
Applicant: Kennametal Inc.
Inventor: Qingjun Zheng , Michael Meyer , Martin G. Perez , Abdelhakim Belhadjhamida
IPC: C22C19/05 , B23P6/04 , B23K1/00 , B23K35/02 , B23K35/30 , B23K101/00 , B23K103/08
Abstract: Methods of superalloy article repair are provided. In some embodiments, a method for repairing a nickel-based superalloy article comprises providing a layered assembly over a damaged region of the nickel-based superalloy article, the layered assembly comprising a nickel-based superalloy preform, an infiltration alloy preform and a melting point depressant component. The layered assembly is heated to form a nickel-based filler alloy metallurgically bonded to the damaged region, wherein primary carbide and secondary carbide phases are present in the nickel-based filler alloy in a combined amount of 0.5 to 10 vol. %.
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公开(公告)号:US10391557B2
公开(公告)日:2019-08-27
申请号:US15165877
申请日:2016-05-26
Applicant: Kennametal Inc.
Inventor: James A. Faust , Daniel Bourlotos , Qingjun Zheng , Michael Meyer
IPC: B22F7/00 , B22F7/04 , B32B15/01 , E21B43/26 , E21B34/06 , B22F1/00 , B22F7/08 , B22F5/10 , B22F7/06
Abstract: In one aspect, composite articles are described herein employing cobalt-based alloy claddings exhibiting high hardness and wear resistance while maintaining desirable integrity and adhesion to surfaces of metallic substrates. A composite article, in some embodiments, comprises a metallic substrate and a composite cladding metallurgically bonded to one or more surfaces of the metallic substrate, the composite cladding including cobalt-based alloy having a chromium gradient, wherein chromium content increases in a direction from the composite cladding surface to an interface of the composite cladding with the metallic substrate.
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