DE3870957D1 - Werkstuecke aus superlegierung von hoher festigkeit mit gradierten eigenschaften. - Google Patents
Werkstuecke aus superlegierung von hoher festigkeit mit gradierten eigenschaften.Info
- Publication number
- DE3870957D1 DE3870957D1 DE8888104065T DE3870957T DE3870957D1 DE 3870957 D1 DE3870957 D1 DE 3870957D1 DE 8888104065 T DE8888104065 T DE 8888104065T DE 3870957 T DE3870957 T DE 3870957T DE 3870957 D1 DE3870957 D1 DE 3870957D1
- Authority
- DE
- Germany
- Prior art keywords
- workpieces
- high strength
- super alloy
- graded properties
- graded
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 229910000601 superalloy Inorganic materials 0.000 title 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/10—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt or alloys based thereon
Landscapes
- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/032,661 US4820358A (en) | 1987-04-01 | 1987-04-01 | Method of making high strength superalloy components with graded properties |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3870957D1 true DE3870957D1 (de) | 1992-06-17 |
Family
ID=21866123
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8888104065T Expired - Lifetime DE3870957D1 (de) | 1987-04-01 | 1988-03-15 | Werkstuecke aus superlegierung von hoher festigkeit mit gradierten eigenschaften. |
Country Status (6)
Families Citing this family (40)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5143563A (en) * | 1989-10-04 | 1992-09-01 | General Electric Company | Creep, stress rupture and hold-time fatigue crack resistant alloys |
US5161950A (en) * | 1989-10-04 | 1992-11-10 | General Electric Company | Dual alloy turbine disk |
US5080734A (en) * | 1989-10-04 | 1992-01-14 | General Electric Company | High strength fatigue crack-resistant alloy article |
FR2680522A1 (fr) * | 1991-08-21 | 1993-02-26 | Snecma | Procede de traitement thermique de pieces en superalliages avec mise en place d'une barriere thermique avant trempe. |
US5312497A (en) * | 1991-12-31 | 1994-05-17 | United Technologies Corporation | Method of making superalloy turbine disks having graded coarse and fine grains |
US5527402A (en) * | 1992-03-13 | 1996-06-18 | General Electric Company | Differentially heat treated process for the manufacture thereof |
DE4235303A1 (de) * | 1992-10-20 | 1994-04-21 | Wieland Werke Ag | Rotationssymmetrisches Halbzeug mit über den Querschnitt variierenden Eigenschaften |
FR2707092B1 (fr) * | 1993-06-28 | 1995-08-25 | Pechiney Rhenalu | Produit métallurgique en alliage d'Al à durcissement structural présentant une variation continue des propriétés d'emploi suivant une direction donnée et un procédé et dispositif d'obtention de celui-ci. |
US5571345A (en) * | 1994-06-30 | 1996-11-05 | General Electric Company | Thermomechanical processing method for achieving coarse grains in a superalloy article |
US5593519A (en) * | 1994-07-07 | 1997-01-14 | General Electric Company | Supersolvus forging of ni-base superalloys |
US5547523A (en) * | 1995-01-03 | 1996-08-20 | General Electric Company | Retained strain forging of ni-base superalloys |
RU2134175C1 (ru) * | 1997-07-14 | 1999-08-10 | Институт проблем сверхпластичности металлов РАН | Стан для изготовления осесимметричных деталей |
US6158261A (en) * | 1997-07-14 | 2000-12-12 | General Electric Company | Mill for producing axially symmetric parts |
US6287644B1 (en) | 1999-07-02 | 2001-09-11 | General Electric Company | Continuously-graded bond coat and method of manufacture |
JP4674932B2 (ja) * | 2000-03-01 | 2011-04-20 | 株式会社小松製作所 | 履帯ブッシュおよびその製造方法並びに製造装置 |
CN100460528C (zh) * | 2001-06-07 | 2009-02-11 | 株式会社小松制作所 | 履带轴套及其制造方法和制造装置 |
US6660110B1 (en) | 2002-04-08 | 2003-12-09 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Heat treatment devices and method of operation thereof to produce dual microstructure superalloy disks |
US6974508B1 (en) | 2002-10-29 | 2005-12-13 | The United States Of America As Represented By The United States National Aeronautics And Space Administration | Nickel base superalloy turbine disk |
US8266800B2 (en) | 2003-09-10 | 2012-09-18 | Siemens Energy, Inc. | Repair of nickel-based alloy turbine disk |
WO2005073515A1 (ja) * | 2004-01-30 | 2005-08-11 | Ishikawajima-Harima Heavy Industries Co., Ltd. | ディスク材 |
US7316057B2 (en) * | 2004-10-08 | 2008-01-08 | Siemens Power Generation, Inc. | Method of manufacturing a rotating apparatus disk |
US20080124210A1 (en) * | 2006-11-28 | 2008-05-29 | Peter Wayte | Rotary assembly components and methods of fabricating such components |
US7891952B2 (en) * | 2006-11-28 | 2011-02-22 | General Electric Company | Rotary machine components and methods of fabricating such components |
US7967570B2 (en) * | 2007-07-27 | 2011-06-28 | United Technologies Corporation | Low transient thermal stress turbine engine components |
US8083872B2 (en) | 2007-08-03 | 2011-12-27 | Rolls-Royce Plc | Method of heat treating a superalloy component and an alloy component |
CN101815804B (zh) * | 2007-10-04 | 2013-07-24 | 阿勒里斯铝业科布伦茨有限公司 | 制造在工程性质上具有梯度的锻造金属板产品的方法 |
US20100233504A1 (en) * | 2009-03-13 | 2010-09-16 | Honeywell International Inc. | Method of manufacture of a dual microstructure impeller |
MX2012008682A (es) | 2010-01-29 | 2012-11-12 | Tata Steel Nederland Technology Bv | Proceso para un tratamiento termico de material de tira metalica, y material de tira metalica producida de esta manera. |
US8480368B2 (en) | 2010-02-05 | 2013-07-09 | General Electric Company | Welding process and component produced therefrom |
DE102010043837A1 (de) * | 2010-11-12 | 2012-05-16 | Hilti Aktiengesellschaft | Schlagwerkskörper, Schlagwerk und Handwerkzeugmaschine mit einem Schlagwerk |
US8918996B2 (en) | 2011-05-04 | 2014-12-30 | General Electric Company | Components and processes of producing components with regions having different grain structures |
US9156113B2 (en) | 2011-06-03 | 2015-10-13 | General Electric Company | Components and processes of producing components with regions having different grain structures |
US20130167979A1 (en) * | 2011-12-29 | 2013-07-04 | General Electric Company | Method of predicting quench cracking in components formed by high deformation processes |
US9188514B1 (en) * | 2013-05-23 | 2015-11-17 | The United States Of America As Represented By The Secretary Of The Navy | System and method for producing a sample having a monotonic doping gradient of a diffusive constituent or interstitial atom or molecule |
EP3394295A4 (en) * | 2015-12-22 | 2019-11-13 | Ecole de Technologie Supérieure | METHOD FOR HEAT TREATMENT BY INDUCTION OF AN ALLOY COMPONENT FOR GENERATING MICROSTRUCTURE GRADIENTS AND METHOD OF HEAT-TREATED ALLOY COMPONENTS |
US12297525B2 (en) | 2019-11-28 | 2025-05-13 | Proterial, Ltd. | Manufacturing method for nickel-based alloy product or titanium-based alloy product |
JP7068673B2 (ja) | 2019-11-28 | 2022-05-17 | 日立金属株式会社 | ニッケル基合金製品またはチタン基合金製品の製造方法 |
CN112642504B (zh) * | 2020-11-27 | 2022-05-27 | 中国航发四川燃气涡轮研究院 | 一种可持续实现轮盘径向梯度温差的加温装置 |
US20240254611A1 (en) * | 2023-02-01 | 2024-08-01 | Raytheon Technologies Corporation | Single-step process for selective heat treatment of metals using multiple heating sources |
US20240254589A1 (en) * | 2023-02-01 | 2024-08-01 | Raytheon Technologies Corporation | Selective heat treatment of metals using a coil-in-furnace system |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3741821A (en) * | 1971-05-10 | 1973-06-26 | United Aircraft Corp | Processing for integral gas turbine disc/blade component |
EP0115092B1 (de) * | 1983-02-01 | 1987-08-12 | BBC Brown Boveri AG | Bauteil mit hoher Korrosions- und Oxydationsbeständigkeit, bestehend aus einer dispersionsgehärteten Superlegierung und Verfahren zu dessen Herstellung |
US4529452A (en) * | 1984-07-30 | 1985-07-16 | United Technologies Corporation | Process for fabricating multi-alloy components |
US4608094A (en) * | 1984-12-18 | 1986-08-26 | United Technologies Corporation | Method of producing turbine disks |
-
1987
- 1987-04-01 US US07/032,661 patent/US4820358A/en not_active Expired - Lifetime
-
1988
- 1988-03-09 IL IL85674A patent/IL85674A/xx unknown
- 1988-03-15 EP EP88104065A patent/EP0284876B1/en not_active Expired
- 1988-03-15 DE DE8888104065T patent/DE3870957D1/de not_active Expired - Lifetime
- 1988-04-01 JP JP63078337A patent/JPS63310947A/ja active Pending
-
1992
- 1992-06-23 GR GR910402262T patent/GR3005001T3/el unknown
Also Published As
Publication number | Publication date |
---|---|
GR3005001T3 (GUID-C5D7CC26-194C-43D0-91A1-9AE8C70A9BFF.html) | 1993-05-24 |
US4820358A (en) | 1989-04-11 |
IL85674A0 (en) | 1988-08-31 |
EP0284876B1 (en) | 1992-05-13 |
IL85674A (en) | 1990-11-05 |
EP0284876A1 (en) | 1988-10-05 |
JPS63310947A (ja) | 1988-12-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8128 | New person/name/address of the agent |
Representative=s name: SIEB, R., DIPL.-CHEM. DR.RER.NAT., PAT.-ANW., 6947 |
|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |