公开(公告)号：US20240352558A1

公开(公告)日：2024-10-24

申请号：US18303254

申请日：2023-04-19

申请人： General Electric Company

发明人： Yan Cui ,  Jon C. Schaeffer ,  Michael Douglas Arnett ,  Matthew Joseph Laylock ,  Brian Lee Tollison

IPC分类号： C22C19/05

CPC分类号： C22C19/056

摘要： Described herein are compositions, and more particularly to alloy compositions, methods of using the alloy compositions, and articles formed from with the alloy compositions. The alloy compositions are broadly applicable in applications requiring superalloys, including welding processes, additive manufacturing processes, metal casting processes, coating processes, repairing processes, powder metallurgy, and/or combinations thereof.

公开(公告)号：US12121966B2

公开(公告)日：2024-10-22

申请号：US17095201

申请日：2020-11-11

申请人： Rolls-Royce Corporation ,  Rolls-Royce North American Technologies, Inc.

发明人： Quinlan Yee Shuck ,  Scott Nelson ,  Raymond Ruiwen Xu ,  Brandon David Ribic ,  Matthew R. Gold

IPC分类号： B22F10/18 ,  B22F3/10 ,  B22F10/00 ,  B29C64/112 ,  B29C64/393 ,  B33Y10/00 ,  B33Y30/00 ,  B33Y70/10 ,  B33Y80/00 ,  C22C19/05 ,  C22C30/02 ,  B29K101/12 ,  B29K505/08

CPC分类号： B22F10/18 ,  B22F3/1021 ,  B22F10/00 ,  B29C64/112 ,  B29C64/393 ,  B33Y10/00 ,  B33Y30/00 ,  B33Y70/10 ,  B33Y80/00 ,  C22C19/056 ,  C22C19/057 ,  C22C30/02 ,  B22F2301/15 ,  B29K2101/12 ,  B29K2505/08 ,  B22F2998/10 ,  B22F1/10 ,  B22F10/18 ,  B22F3/1021 ,  B22F3/1025 ,  B22F3/15

摘要： An additive manufacturing technique may include depositing, via a filament delivery device, a filament onto a surface of a substrate. The filament includes a binder and a powder including at least one metal or alloy and at least one braze alloy. The technique also includes sacrificing the binder to form a preform. The technique also includes sintering the preform to form a component including the at least one metal or alloy and the at least one braze alloy.

公开(公告)号：US20240344180A1

公开(公告)日：2024-10-17

申请号：US18573255

申请日：2022-06-10

申请人： SAFRAN ,  SAFRAN AIRCRAFT ENGINES

发明人： Jérémy RAME ,  Lorena MATAVELI SUAVE ,  Edern MENOU

IPC分类号： C22C19/05 ,  C23C28/00 ,  C30B29/52

CPC分类号： C22C19/057 ,  C23C28/347 ,  C30B29/52 ,  C22C2200/00

摘要： A nickel-based superalloy comprises in weight percentages: 5.4 to 6.0% of aluminium, 7.5 to 9.0% of tantalum, 0.10 to 0.25% of titanium, 5.5 to 7.5% of cobalt, 4.0 to 5.5% of chromium, 0.10 to 0.70% of molybdenum, 4.0 to 5.0% of tungsten, 4.8 to 6.2% of rhenium, 0.04 to 0.15% of hafnium, 0 to 0.15% of silicon, the remainder consisting of nickel and unavoidable impurities. The invention also relates to a single-crystal blade comprising such an alloy and to a turbomachine comprising such a blade.

公开(公告)号：US20240336998A1

公开(公告)日：2024-10-10

申请号：US18575622

申请日：2023-08-11

申请人： GAONA AERO MATERIAL CO., LTD

发明人： Shaoming ZHANG ,  Zhongnan BI ,  Ming ZHANG ,  Jiantao LIU ,  Mingdong LIU

IPC分类号： C22C19/05 ,  B22F3/15 ,  B22F3/20 ,  B22F9/08 ,  C22C1/02

CPC分类号： C22C19/056 ,  B22F3/15 ,  B22F3/20 ,  B22F9/082 ,  C22C1/023 ,  C22C19/057 ,  B22F2003/208

摘要： The present disclosure relates to the technical field of nickel-based superalloys, and in particular to a nickel-based superalloy and preparation method therefor, and a structural component. The alloy includes the following components in mass percentage: Co 17%-22%, Cr 9%-13%, Ta 2.95%-3.95%, Al 2.5%-3.5%, Ti 2.5%-3.5%, W 2.1%-3.5%, Mo 2.1%-3.5%, Nb 1.65%-1.95%, Hf 0.2%-0.7%, C 0.03%-0.08%, B 0.01%-0.06%, Zr 0.03%-0.07% and Ni. The nickel-based superalloys of the present disclosure, in the creep process at 780° C., produces specific Suzuki atmosphere in certain positions, and locks dislocations to improve creep resistance, such that the operating temperature can be raised to more than 780° C., which meets the requirements on the materials for the advanced aero-engines.

公开(公告)号：US12109618B2

公开(公告)日：2024-10-08

申请号：US17197266

申请日：2021-03-10

申请人： GENERAL ELECTRIC COMPANY

发明人： Ibrahim Ucok ,  Yan Cui ,  Srikanth Chandrudu Kottilingam ,  Surinder Singh Pabla

IPC分类号： 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分类号： 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

摘要： 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.

公开(公告)号：US12104508B1

公开(公告)日：2024-10-01

申请号：US18710730

申请日：2022-11-15

申请人： COSCO SHIPPING MARINE EQUIPT & SPARES (NJ) CO., LTD

发明人： Hong Lu ,  Weiwei Dai ,  Lihe Jiang ,  Guozheng Quan ,  Xiaolin Zhang

IPC分类号： C22C19/05 ,  B21J5/02 ,  C22F1/10 ,  F01L3/02

CPC分类号： F01L3/02 ,  B21J5/02 ,  C22C19/058 ,  C22F1/10

摘要： Provided are a large-size diesel exhaust valve and a manufacturing method thereof, which relate to the technical field of manufacturing of large-size diesel exhaust valves for ships. The large-size diesel exhaust valve includes an exhaust valve disc portion made of a 3J40 alloy, and the large-size diesel exhaust valve has the following microstructure: there are ultra-fine grains with a grain size of 10 grade or more, α-Cr lamellar phases are evenly distributed at grain boundaries of the ultra-fine grains, nickel-lean Cr—Al—Ce particle phases are evenly distributed in a matrix, a single lamella of the α-Cr lamellar phases has a thickness of less than 140 nm, and the nickel-lean Cr—Al—Ce particle phases have a diameter of less than 10 μm. The present application solves the technical problem of how to improve the comprehensive mechanical properties and the vibration-damping performance of a large-size diesel exhaust valve simultaneously.

公开(公告)号：US12098446B2

公开(公告)日：2024-09-24

申请号：US18505145

申请日：2023-11-09

申请人： Hainan University

发明人： Wenchao Ma ,  Terrence Wenga ,  Sixuan Zeng ,  Xingcai Chen ,  Lingyu Tai

IPC分类号： C22C19/05 ,  C22C1/02

CPC分类号： C22C19/055 ,  C22C1/023

摘要： A corrosion-resistant nickel alloy is provided. The alloy includes the following components in percentage by mass: 4.68-5.35% of B, 5.69-6.41% of W, 27.68-28.39% of Cr, 12.65-13.42% of Al, and the balance of Ni and inevitable impurities. The corrosion-resistant nickel alloy is a Ni—W—B ternary alloy with main components of Ni, W and B, wherein the three elements have strong high-temperature corrosion resistance at a temperature of about 600° C., and have the potential of solid solution hardening and precipitate formation because all belong to solid solution forming elements, so that a creep strength of a nickel alloy matrix is improved. Meanwhile, Al and Cr are further added in the alloy formula, so that Al2O3 and Cr2O3 oxide layers can be formed, which play a role as a physical diffusion barrier against chlorine gas and other corrosive gases.

公开(公告)号：US20240254578A1

公开(公告)日：2024-08-01

申请号：US18162860

申请日：2023-02-01

申请人： Raytheon Technologies Corporation

发明人： Masoud Anahid ,  Matthew D. Mordasky ,  Anthony Patrick Ventura ,  David U. Furrer

IPC分类号： C21D1/42 ,  C21D11/00 ,  C22C19/05

CPC分类号： C21D1/42 ,  C21D11/00 ,  C22C19/05

摘要： The present disclosure provides assemblies, systems and methods for a single-step process for selective heat treatment of metals. More particularly, the present disclosure provides assemblies, systems and methods for a single-step process for selective heat treatment of metals using multiple induction heating coils. A hybrid modeling-test approach can be used in the design process to improve or optimize the process parameters to achieve location specific and improved/optimal microstructure and residual stress to enhance the part performance. It is also noted that performing the selective heat treatment in a single step can reduce the cycle time significantly. Moreover, large thermal gradients can be avoided in the part as different volumes of the part are heated to their desired temperature simultaneously.

公开(公告)号：US12018394B1

公开(公告)日：2024-06-25

申请号：US18300105

申请日：2023-04-13

申请人： HRL Laboratories, LLC

发明人： Tobias A. Schaedler ,  John H. Martin

IPC分类号： F02K9/97 ,  B32B3/12 ,  B32B15/01 ,  B32B15/04 ,  C22C19/00 ,  C22C19/03 ,  C22C19/05 ,  C22F1/10 ,  C23C10/38 ,  C23C10/48 ,  C23C28/02 ,  C25D1/02 ,  C25D3/12 ,  C25D3/56

CPC分类号： C25D1/02 ,  B32B3/12 ,  B32B15/01 ,  B32B15/043 ,  C22C19/002 ,  C22C19/03 ,  C22C19/058 ,  C22F1/10 ,  C23C10/38 ,  C23C10/48 ,  C23C28/023 ,  C25D3/12 ,  C25D3/56 ,  F02K9/97

摘要： A thin-walled metal part, and a method to fabricate such a part out of various alloys. A plurality of layers are formed, each of the layers being formed on a polymer template or on a previously formed layer. A homogenizing heat treatment is used to cause chemical elements in the layers to interdiffuse, to form a single continuous layer with a substantially uniform alloy composition.

公开(公告)号：US11999000B2

公开(公告)日：2024-06-04

申请号：US16733430

申请日：2020-01-03

申请人： Rolls-Royce Corporation

发明人： Joseph Peter Henderkott

IPC分类号： B23K1/00 ,  B22F5/00 ,  B22F7/00 ,  B22F7/04 ,  B22F7/08 ,  B23K1/008 ,  B23K31/02 ,  B23K103/02 ,  B23K103/08 ,  C22C19/05 ,  F17C1/02

CPC分类号： B23K1/0018 ,  B22F5/009 ,  B22F7/008 ,  B22F7/08 ,  B23K31/025 ,  C22C19/05 ,  C22C19/056 ,  C22C19/057 ,  C22C19/058 ,  F17C1/02 ,  B22F2007/042 ,  B22F2301/15 ,  B22F2301/35 ,  B22F2303/30 ,  B23K1/008 ,  B23K2103/02 ,  B23K2103/08

摘要： The disclosure describes assemblies, systems, and techniques for reinforcing complex geometries of pressure vessels using a pre-sintered preform (PSP) braze material that includes a low-melt powder and a high-melt powder. An example technique includes positioning a PSP reinforcement on a surface of a substrate. The technique includes heating the PSP reinforcement to soften or melt at least one constituent metal or alloy of the low-melt powder. During heating, the PSP reinforcement is configured to conform to a contour of the surface of the substrate. The technique also includes cooling the PSP reinforcement to define a reinforced component.