公开(公告)号：US12103267B2

公开(公告)日：2024-10-01

申请号：US17978470

申请日：2022-11-01

Applicant: Pratt & Whitney Canada Corp.

Inventor： Joel Larose ,  Alan D. Cetel ,  David A. Litton ,  Brian S. Tryon

IPC: B32B15/01 ,  B32B15/04 ,  C22C5/04 ,  C22C19/03 ,  C22C19/05 ,  C22C30/00 ,  C23C14/02 ,  C23C14/14 ,  C23C14/16 ,  C23C14/58 ,  C23C28/00 ,  C23C28/02 ,  C23C30/00 ,  F01D5/28

CPC classification number: B32B15/01 ,  B32B15/04 ,  B32B15/043 ,  C22C5/04 ,  C22C19/03 ,  C22C19/05 ,  C22C19/051 ,  C22C19/057 ,  C22C30/00 ,  C23C14/025 ,  C23C14/14 ,  C23C14/16 ,  C23C14/165 ,  C23C14/58 ,  C23C14/5806 ,  C23C28/022 ,  C23C28/32 ,  C23C28/321 ,  C23C28/3215 ,  C23C28/3455 ,  C23C30/00 ,  C23C30/005 ,  F01D5/28 ,  F01D5/288 ,  Y10T428/12875 ,  Y10T428/12931 ,  Y10T428/12937 ,  Y10T428/12944

Abstract: A coating-substrate combination includes: a Ni-based superalloy substrate comprising, by weight percent: 2.0-5.1 Cr; 0.9-3.3 Mo; 3.9-9.8 W; 2.2-6.8 Ta; 5.4-6.5 Al; 1.8-12.8 Co; 2.8-5.8 Re; 2.8-7.2 Ru; and a coating comprising, exclusive of Pt group elements, by weight percent: Ni as a largest content; 5.8-9.3 Al; 4.4-25 Cr; 3.0-13.5 Co; up to 6.0 Ta, if any; up to 6.2 W, if any; up to 2.4 Mo, if any; 0.3-0.6 Hf; 0.1-0.4 Si; up to 0.6 Y, if any; up to 0.4 Zr, if any; up to 1.0 Re, if any.

公开(公告)号：US20240227006A1

公开(公告)日：2024-07-11

申请号：US18405157

申请日：2024-01-05

Applicant: UT-Battelle, LLC

Inventor： Rishi R. PILLAI ,  Soumya NAG ,  Thomas FELDHAUSEN

IPC: B22F7/02 ,  B22F10/28 ,  B33Y10/00 ,  B33Y80/00 ,  C22C1/04 ,  C22C19/05

CPC classification number: B22F7/02 ,  B22F10/28 ,  B33Y10/00 ,  B33Y80/00 ,  C22C1/0433 ,  C22C19/056 ,  C22C19/057 ,  B22F2998/10 ,  B22F2999/00

Abstract: An alloy construction for separating a low oxygen content corrosive environment from a high oxygen content oxidizing environment includes a wall having a wall thickness and a first surface segment for contacting the low oxygen content corrosive environment, and a second surface segment for contacting the high oxygen content oxidizing environment. The alloy comprises, in weight percent: 0 to 5 Al; 5 to 30 Cr; 0 to 20 Co; 0 to 70 Fe; 0 to 2 Nb; 0 to 2 Ta; 0 to 3 Ti; 0 to 1 Si; 0 to 1 V; 0 to 2 Mn; 0 to 5 Cu; 0 to 30 Mo; 0 to 30 W; 0 to 0.1 P; 0 to 1 Zr; 0 to 1 Hf; 0 to 0.1 Y; 0.05 to 0.5 C; 0 to 0.1 N; and balance Ni. The alloy is compositionally graded from the first surface segment to the second surface segment. The wall composition has a stable FCC austenitic matrix microstructure, with strengthening phases comprising gamma prime with a volume fraction of 0 to 30% and carbides with a volume fraction of 0 to 5%.

公开(公告)号：US20240124957A1

公开(公告)日：2024-04-18

申请号：US17966965

申请日：2022-10-17

Applicant: Liburdi Engineering Limited

Inventor： Alexander B. GONCHAROV ,  Paul LOWDEN

IPC: C22C19/05 ,  B23K35/30 ,  B33Y70/00

CPC classification number: C22C19/057 ,  B23K35/3033 ,  B33Y70/00 ,  C22C19/056 ,  B23K2101/001

Abstract: The high gamma prime (γ′) nickel based welding material for repair and 3D additive manufacturing of turbine engine components containing from 9.0 to 11.0% Cr, from 16.0 to 24.0% Co, from 1.0 to 1.4% Mo, from 5.0 to 5.8% W, from 1.5 to 1.9% Ta, from 4.5 to 5.5 Al %, from 0.1 to 0.3% Hf, up to 0.02% B, from 0.05 to 0.12% C, from 0.2 to 0.8% Fe, from 1.5 to 2.5% Re, and nickel with impurities to balance.

公开(公告)号：US11859273B2

公开(公告)日：2024-01-02

申请号：US18095403

申请日：2023-01-10

Applicant: Halliburton Energy Services, Inc.

Inventor： Shashwat Shukla ,  Arpana Singh ,  Michael Linley Fripp

IPC: C22F1/10 ,  B32B15/01 ,  C22C19/05

CPC classification number: C22F1/10 ,  B32B15/01 ,  C22C19/057 ,  Y10T428/12944

Abstract: The disclosure provides for a layered metal with resistance to hydrogen induced cracking and method of production thereof, comprising a core metal alloy and a skin metal alloy. The core metal alloy comprises twinned boundaries. The core metal alloy has undergone plastic deformation and a heat treatment. The core metal alloy comprises nickel and cobalt. The skin metal alloy is disposed on the core metal alloy, wherein the skin metal alloy comprises an entropy greater than the core metal alloy. The core metal alloy comprises a greater density of twinned boundaries than the skin metal alloy. The skin metal alloy comprises a stacking fault energy of at least about 50 mJ/m2, and the skin metal alloy comprises iron, aluminum, and boron.

公开(公告)号：US20230332276A1

公开(公告)日：2023-10-19

申请号：US18245645

申请日：2021-09-16

Applicant: voestalpine Metal Forming GmbH ,  Mogema BV

Inventor： Bas-Jan Hoogenberg ,  Robert Vehof ,  Brian Brady ,  Guillermo Domínguez ,  Karl Radlmayr

IPC: C22C19/05 ,  C22F1/10 ,  C22C38/02 ,  C22C38/04 ,  C22C38/06 ,  C22C38/30 ,  C22C38/28 ,  C22C38/26 ,  C22C38/24 ,  C22C38/22 ,  C21D9/46 ,  C21D8/12 ,  C21D6/00 ,  B33Y10/00 ,  B33Y80/00 ,  B22F5/00 ,  B33Y40/20 ,  B22F10/64 ,  H05K9/00 ,  B21D22/02

CPC classification number: C22C19/057 ,  C22F1/10 ,  C22C38/02 ,  C22C38/04 ,  C22C38/06 ,  C22C38/30 ,  C22C38/28 ,  C22C38/26 ,  C22C38/24 ,  C22C38/22 ,  C21D9/46 ,  C21D8/1216 ,  C21D8/1244 ,  C21D6/002 ,  C21D6/005 ,  C21D6/007 ,  C21D6/008 ,  B33Y10/00 ,  B33Y80/00 ,  B22F5/006 ,  B33Y40/20 ,  B22F10/64 ,  H05K9/0075 ,  B21D22/022 ,  C22C2202/02 ,  B22F2998/10

Abstract: A method for producing three-dimensional magnetic shields with a sufficient permeability from unannealed, soft-annealed, or magnetization annealed magnetically soft metal sheets, wherein the metal sheet is either cold formed into the three-dimensional component in a one-step or multi-step process, then is subjected to a (magnetization) annealing to increase the permeability, and is then transferred to a forming tool, in which it is held and/or pressed in a tool, which has the desired contour of the component, and is optionally shape-corrected or calibrated by the tool, and allowed to cool in the tool, or a sheet is heated and then formed to the desired geometry in a hot-forming tool and held in it, and is allowed to cool in the tool, or the three-dimensional component is generated by additive production and then is subjected to a (magnetization) annealing to increase the permeability; the invention also relates to a shielding device.

公开(公告)号：US11718897B2

公开(公告)日：2023-08-08

申请号：US17714518

申请日：2022-04-06

Applicant: CRS HOLDINGS, LLC

Inventor： Stephane Forsik ,  Alberto Polar-Rosas ,  Tao Wang ,  Samuel Kernion ,  Mario Epler ,  Ning Zhou

IPC: C22C19/07 ,  C22C30/00 ,  C22C19/05

CPC classification number: C22C19/07 ,  C22C19/056 ,  C22C19/057 ,  C22C30/00

Abstract: A precipitation hardenable, cobalt-nickel base superalloy is disclosed. The is characterized by the following weight percent composition.















C
about 0.01 to about 0.15



Cr
about 6.00 to about 15.00



Ni
about 30.00 to about 45.00



W
about 3.00 to about 15.00



Ti
about 0.50 to about 4.00



Al
about 3.00 to about 7.00



Nb
up to about 2.50



Ta
up to about 6.00



Hf
up to about 1.50



Zr
up to about 1.50



B
up to about 0.20



Mo
up to about 2.50



Si
up to about 1.50









The balance of the alloy is cobalt and usual impurities. The alloy provides a novel combination of strength and ductility after long-term exposure to elevated operating temperatures as found in gas turbines and jet engines. A fine-grain steel article made from the alloy is also disclosed. The steel article is also characterized by a continuous surface layer of Al2O3 and Cr2O3 that protects the alloy from oxidation at the elevated operating temperatures.

公开(公告)号：US20230220518A1

公开(公告)日：2023-07-13

申请号：US18009417

申请日：2021-06-17

Applicant: Siemens Energy Global GmbH & Co. KG

Inventor： Christoph Heinze ,  Yves Küsters ,  Michael Ott

IPC: C22C19/05 ,  C22C1/04 ,  B22F10/28

CPC classification number: C22C19/056 ,  C22C19/057 ,  C22C1/0433 ,  B22F10/28 ,  B33Y10/00

Abstract: A nickel-based alloy which includes at least the following alloy elements in wt. %: cobalt (Co) 10.3-10.7, chromium (Cr) 9.8-10.2, tungsten (W) 9.3-9.7, aluminum (Al) 5.2-5.7, hafnium (Hf) 1.8-2.2, tantalum (Ta) 1.9-2.1, molybdenum (Mo) 0.4-0.6, the remainder being nickel and impurities.

公开(公告)号：US20180305792A1

公开(公告)日：2018-10-25

申请号：US15958454

申请日：2018-04-20

Applicant: CRS HOLDINGS, INC.

Inventor： Stephane Forsik ,  Alberto Polar-Rosas ,  Tao Wang ,  Samuel Kernion ,  Mario Epler ,  Ning Zhou

IPC: C22C19/07 ,  C22C19/05 ,  C22C30/00

CPC classification number: C22C19/07 ,  C22C19/056 ,  C22C19/057 ,  C22C30/00

Abstract: A precipitation hardenable, cobalt-nickel base superalloy is disclosed. The is characterized by the following weight percent composition. C about 0.01 to about 0.15 Cr about 6.00 to about 15.00 Ni about 30.00 to about 45.00 W about 3.00 to about 15.00 Ti about 0.50 to about 4.00 Al about 3.00 to about 7.00 Nb up to about 2.50 Ta up to about 6.00 Hf up to about 1.50 Zr up to about 1.50 B up to about 0.20 Mo up to about 2.50 Si up to about 1.50 The balance of the alloy is cobalt and usual impurities. The alloy provides a novel combination of strength and ductility after long-term exposure to elevated operating temperatures as found in gas turbines and jet engines. A fine-grain steel article made from the alloy is also disclosed. The steel article is also characterized by a continuous surface layer of Al2O3 and Cr2O3 that protects the alloy from oxidation at the elevated operating temperatures.

公开(公告)号：US20180304420A1

公开(公告)日：2018-10-25

申请号：US15492413

申请日：2017-04-20

Applicant: Kennametal Inc.

Inventor： Qingjun ZHENG ,  Michael MEYER ,  Martin G. PEREZ ,  Abdelhakim BELHADJHAMIDA

IPC: B23P6/04 ,  C22C19/05 ,  B23K35/30 ,  B23K35/02 ,  B23K1/00

CPC classification number: B23P6/045 ,  B23K1/0018 ,  B23K35/0238 ,  B23K35/0244 ,  B23K35/304 ,  B23K2101/001 ,  B23K2103/08 ,  C22C19/056 ,  C22C19/057

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. %.

公开(公告)号：US20180245188A1

公开(公告)日：2018-08-30

申请号：US15900460

申请日：2018-02-20

Applicant: DAIDO STEEL CO., LTD.

Inventor： Kyohei Yokota ,  Yoshinori Sumi ,  Yoshihiko Koyanagi ,  Hiroyuki Takabayashi

IPC: C22C19/05

CPC classification number: C22C19/057 ,  C22C19/05 ,  C22C19/056

Abstract: The present invention relates to an Ni-based superalloy having a composition containing, in terms of % by mass, C: from 0.1 to 0.3%, Cr: from 8.0 to 12.0%, Mo: from 1.0 to 5.0%, Co: from 10.0 to 20.0%, Ta: from 0.01 to 1.50%, Ti: from 2.0 to 4.2%, Al: from 5.0 to 8.0%, V: from 0 to 1.5%, B: from 0.005 to 0.030%, and Zr: from 0.05 to 0.15%, with the balance being Ni and unavoidable impurities, and satisfying, in terms of atom %, Ti+Al being from 16.0 to 20.3% and Ti/Al being 0.3 or less.