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公开(公告)号:US12109618B2
公开(公告)日:2024-10-08
申请号:US17197266
申请日:2021-03-10
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Ibrahim Ucok , Yan Cui , Srikanth Chandrudu Kottilingam , Surinder Singh Pabla
IPC: B32B15/01 , B22F3/15 , B22F3/24 , B22F5/00 , B22F5/04 , B22F10/14 , B22F10/28 , B22F10/62 , B22F10/64 , B23K15/00 , B23K26/00 , B23K26/342 , B23K26/70 , B32B3/30 , B33Y10/00 , B33Y40/20 , B33Y70/00 , B33Y80/00 , C22C19/05 , C22C19/07 , C22C30/02 , C22C38/00 , C22C38/02 , C22C38/04 , C22C38/06 , C22C38/08 , C22C38/10 , C22C38/42 , C22C38/44 , C22C38/48 , C22C38/50 , C22C38/52 , C23C4/08 , C23C4/134 , C23C14/16 , C23C14/28 , C23C16/06 , C23C16/44 , C23C18/16 , C23C18/32 , F01D5/28 , F01D25/00 , F01D25/24 , B23K101/00
CPC classification number: B22F3/15 , B22F3/24 , B22F5/009 , B22F5/04 , B22F10/14 , B22F10/28 , B22F10/62 , B22F10/64 , B23K15/0086 , B23K15/0093 , B23K26/0006 , B23K26/342 , B23K26/70 , B32B3/30 , B32B15/01 , B33Y10/00 , B33Y40/20 , B33Y70/00 , B33Y80/00 , C22C19/055 , C22C19/056 , C22C19/057 , C22C19/07 , C22C30/02 , C22C38/002 , C22C38/02 , C22C38/04 , C22C38/06 , C22C38/08 , C22C38/105 , C22C38/42 , C22C38/44 , C22C38/48 , C22C38/50 , C22C38/52 , C23C4/08 , C23C4/134 , C23C14/16 , C23C14/28 , C23C16/06 , C23C16/44 , C23C18/1637 , C23C18/32 , F01D5/28 , F01D25/005 , F01D25/24 , B22F2003/242 , B22F2301/15 , B22F2301/35 , B22F2998/10 , B23K2101/001 , F05D2300/17 , Y02P10/25 , B22F2998/10 , B22F10/28 , B22F10/62 , B22F2003/242 , B22F10/64 , B22F3/15
Abstract: A process includes forming a printed article having an external surface and at least one microfeature with an internal surface by additive manufacture, coating the external surface and the internal surface of the printed article with a metallic microlayer to form a coated article, and densifying the coated article to form a component. After formation, the printed article has a porosity such that the printed article is not at full density. A densified component includes a printed article having an external surface and at least one microfeature with an internal surface and a metallic microlayer coating the external surface and the internal surface of the printed article. The printed article is formed by additive manufacture.
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公开(公告)号:US11766722B2
公开(公告)日:2023-09-26
申请号:US17061553
申请日:2020-10-01
Applicant: General Electric Company
Inventor: Srikanth Chandrudu Kottilingam , David Edward Schick , Jon Conrad Schaeffer , Steven J. Barnell , Brian Lee Tollison , Yan Cui
IPC: B23P15/04 , B23P19/10 , B22F10/10 , B33Y80/00 , B33Y99/00 , B23P6/00 , B22F3/24 , F01D5/00 , F01D9/04 , B33Y10/00 , B22F5/00 , B22F10/00 , B22F10/20 , B22F10/62 , B22F10/64 , B22F10/66
CPC classification number: B22F10/10 , B22F3/24 , B22F5/009 , B22F10/00 , B22F10/20 , B23P6/005 , B23P15/04 , B23P19/10 , B33Y10/00 , B33Y80/00 , B33Y99/00 , F01D5/005 , F01D9/041 , F01D9/042 , B22F10/62 , B22F10/64 , B22F10/66 , B22F2003/242 , B22F2003/247 , B22F2003/248 , B22F2207/20 , B22F2998/00 , F05D2230/20 , F05D2230/21 , F05D2230/22 , F05D2230/23 , F05D2230/31 , F05D2230/51 , F05D2230/60 , F05D2230/64 , F05D2230/70 , F05D2230/80 , Y02P10/25 , Y02T50/60
Abstract: A multi-piece part includes multiple pieces fabricated via different types of fabrication processes, wherein the multiple parts are configured to be coupled to one another to form the assembly. At least one of the multiple parts is fabricated via an additive manufacturing method. The multi-piece part also includes a holder assembly that couples and holds together the multiple pieces of the multi-piece part, wherein the holder assembly comprises a reversible, mechanical-type coupling.
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公开(公告)号:US20220372627A1
公开(公告)日:2022-11-24
申请号:US17816472
申请日:2022-08-01
Applicant: General Electric Company
Inventor: Yan Cui , Matthew Joseph Laylock , Brian Lee Tollison
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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公开(公告)号:US11426822B2
公开(公告)日:2022-08-30
申请号:US17110660
申请日:2020-12-03
Applicant: General Electric Company
Inventor: Yan Cui , Michael Douglas Arnett , Ethan Conrad Schaeffer , Brian Lee Tollison , Matthew Joseph Laylock
IPC: B23K1/00 , C22C19/00 , B23K35/30 , C22C19/05 , B23K101/00
Abstract: A composition includes the constituents, in approximate weight percentages: Chromium 15-17; Silicon 2.5-3.5; Cobalt 6.0-8.0; Aluminum 1.0-2.0; Tantalum 1.5-2.5; Boron 1.5-2.5; Yttrium 0.015-0.025; Nickel balance; and incidental impurities.
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公开(公告)号:US20220176499A1
公开(公告)日:2022-06-09
申请号:US17110660
申请日:2020-12-03
Applicant: General Electric Company
Inventor: Yan Cui , Michael Douglas Arnett , Ethan Conrad Schaeffer , Brian Lee Tollison , Matthew Joseph Laylock
Abstract: A composition includes the constituents, in approximate weight percentages: Chromium 15-17; Silicon 2.5-3.5; Cobalt 6.0-8.0; Aluminum 1.0-2.0; Tantalum 1.5-2.5; Boron 1.5-2.5; Yttrium 0.015-0.025; Nickel balance; and incidental impurities.
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公开(公告)号:US20220127727A1
公开(公告)日:2022-04-28
申请号:US17079829
申请日:2020-10-26
Applicant: General Electric Company
Inventor: Yan Cui , Matthew Joseph Laylock , Brian Lee Tollison
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 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 1287° C.
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公开(公告)号:US20210205910A1
公开(公告)日:2021-07-08
申请号:US16737469
申请日:2020-01-08
Applicant: General Electric Company
Inventor: Yan Cui , Michael Douglas Arnett , Matthew Joseph Laylock , Brian Lee Tollison , Jeffrey Michael Breznak
Abstract: A method for repairing a part and the resulting is disclosed. The method includes positioning a plug having an inner braze element coupled thereto into a cavity defined by an internal surface of a component. The cavity has a circular cross-section at the external surface of the component. The plug completely fills the circular cross-section and the inner braze element is within the cavity. A braze paste is positioned at least partially around the plug at the external surface. The component is positioned such that the inner braze element is above the plug. The component is subjected to a thermal cycle to melt the inner braze element around the plug, completely sealing the cavity by forming a metallurgical bond with the plug and the internal surface of the component. During the thermal cycle the braze paste is melted to form a metallurgical bond with the plug and external surface.
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公开(公告)号:US20210017868A1
公开(公告)日:2021-01-21
申请号:US17061553
申请日:2020-10-01
Applicant: General Electric Company
Inventor: Srikanth Chandrudu Kottilingam , David Edward Schick , Jon Conrad Schaeffer , Steven J. Barnell , Brian Lee Tollison , Yan Cui
IPC: F01D9/04 , B22F3/00 , B33Y80/00 , B33Y99/00 , B22F3/105 , B23P6/00 , B22F3/24 , F01D5/00 , B23P15/04 , B33Y10/00 , B22F5/00
Abstract: A multi-piece part includes multiple pieces fabricated via different types of fabrication processes, wherein the multiple parts are configured to be coupled to one another to form the assembly. At least one of the multiple parts is fabricated via an additive manufacturing method. The multi-piece part also includes a holder assembly that couples and holds together the multiple pieces of the multi-piece part, wherein the holder assembly comprises a reversible, mechanical-type coupling.
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公开(公告)号:US10786878B2
公开(公告)日:2020-09-29
申请号:US15657921
申请日:2017-07-24
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Yan Cui , Srikanth Chandrudu Kottilingam , Brian Lee Tollison
IPC: B23P6/00 , B23K9/23 , B23K9/04 , B23K101/00
Abstract: A method of welding a component and a treated component are provided. The method comprises an initial heat-treating of the component comprising a substrate. The method further comprises removing a portion of the substrate to form a treatment region comprising an exposed surface. The method further comprises buttering the exposed surface with a first filler additive to form a weld metal adjacent to the fusion line comprising an easy-to-weld alloy. The method further comprises welding the component with the easy-to-weld alloy and a second filler additive. The first filler additive comprises a sufficient amount of each of Co, Cr, Mo, Fe, Al, Ti, Mn, C and Ni to form the easy-to-weld alloy, when welded with the hard-to-weld base alloy.
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公开(公告)号:US10598030B2
公开(公告)日:2020-03-24
申请号:US15402725
申请日:2017-01-10
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Srikanth Chandrudu Kottilingam , Yan Cui , Brian Lee Tollison
IPC: F01D5/22 , B23K1/00 , B23K35/02 , C22C19/07 , B23K35/30 , C21D1/78 , C21D9/00 , C22F1/10 , B23P6/00 , F01D5/00 , B23K20/02 , F01D5/28 , B23K101/00
Abstract: In some embodiments, a process treats a turbine component. The turbine component includes an article and a wear component brazed to the article. The process includes applying a braze tape on at least a portion of the wear component and thermal processing the turbine component while the braze tape is on the at least a portion of the wear component to treat the turbine component. In some embodiments, an assembly includes a turbine component. The turbine component includes an article and a pre-sintered preform brazed to a surface of the article. The assembly also includes a braze tape on at least a portion of the pre-sintered preform. In some embodiments, a treated turbine component includes a treated article and a pre-sintered preform brazed to a surface of the treated article. The treated turbine component has been thermally processed with the pre-sintered preform being substantially free of re-flow.
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