FR2953860B1 - Procede de fabrication de superaillages de nickel de type inconel 718 - Google Patents
Procede de fabrication de superaillages de nickel de type inconel 718Info
- Publication number
- FR2953860B1 FR2953860B1 FR0958815A FR0958815A FR2953860B1 FR 2953860 B1 FR2953860 B1 FR 2953860B1 FR 0958815 A FR0958815 A FR 0958815A FR 0958815 A FR0958815 A FR 0958815A FR 2953860 B1 FR2953860 B1 FR 2953860B1
- Authority
- FR
- France
- Prior art keywords
- superborts
- inconel
- manufacturing
- type nickel
- nickel
- 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.)
- Active
Links
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 title 2
- 229910000816 inconels 718 Inorganic materials 0.000 title 1
- 238000004519 manufacturing process Methods 0.000 title 1
- 238000000034 method Methods 0.000 title 1
- 229910052759 nickel 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
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
- C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
- C22C19/056—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 10% but less than 20%
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Forging (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Priority Applications (9)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0958815A FR2953860B1 (fr) | 2009-12-10 | 2009-12-10 | Procede de fabrication de superaillages de nickel de type inconel 718 |
CN201080056172.0A CN102652179B (zh) | 2009-12-10 | 2010-12-09 | 一种制造铬镍铁耐热蚀合金718型镍超级合金的方法 |
CA2782460A CA2782460A1 (fr) | 2009-12-10 | 2010-12-09 | Procede de fabrication de superalliages de nickel de type inconel 718 |
RU2012128876/02A RU2567968C2 (ru) | 2009-12-10 | 2010-12-09 | Способ изготовления никелевых суперсплавов типа inconel 718 |
US13/514,891 US20120247626A1 (en) | 2009-12-10 | 2010-12-09 | Method of fabricating inconel 718 type nickel superalloys |
BR112012013752A BR112012013752A2 (pt) | 2009-12-10 | 2010-12-09 | processo de fabricação de superligas de níquel de tipo inconel 718. |
PCT/FR2010/052658 WO2011070302A1 (fr) | 2009-12-10 | 2010-12-09 | Procede de fabrication de superalliages de nickel de type inconel 718 |
EP10801646.0A EP2510131B1 (fr) | 2009-12-10 | 2010-12-09 | Procede de fabrication de superalliages de nickel de type inconel 718 |
JP2012542604A JP5951499B2 (ja) | 2009-12-10 | 2010-12-09 | インコネル718型ニッケル超合金を製造する方法 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0958815A FR2953860B1 (fr) | 2009-12-10 | 2009-12-10 | Procede de fabrication de superaillages de nickel de type inconel 718 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2953860A1 FR2953860A1 (fr) | 2011-06-17 |
FR2953860B1 true FR2953860B1 (fr) | 2015-05-15 |
Family
ID=42313893
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0958815A Active FR2953860B1 (fr) | 2009-12-10 | 2009-12-10 | Procede de fabrication de superaillages de nickel de type inconel 718 |
Country Status (9)
Country | Link |
---|---|
US (1) | US20120247626A1 (fr) |
EP (1) | EP2510131B1 (fr) |
JP (1) | JP5951499B2 (fr) |
CN (1) | CN102652179B (fr) |
BR (1) | BR112012013752A2 (fr) |
CA (1) | CA2782460A1 (fr) |
FR (1) | FR2953860B1 (fr) |
RU (1) | RU2567968C2 (fr) |
WO (1) | WO2011070302A1 (fr) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9310081B2 (en) * | 2012-05-14 | 2016-04-12 | Delavan Inc. | Methods of fabricating fuel injectors using laser additive deposition |
WO2016013433A1 (fr) | 2014-07-23 | 2016-01-28 | 株式会社Ihi | PROCÉDÉ DE PRODUCTION D'UN COMPOSANT D'ALLIAGE DE Ni |
CN104625607B (zh) * | 2014-12-09 | 2017-07-14 | 抚顺特殊钢股份有限公司 | 闪光焊环用inco718型材制造方法 |
US10077714B2 (en) | 2015-11-06 | 2018-09-18 | Rolls-Royce Plc | Repairable fuel injector |
CN111118423B (zh) * | 2019-11-27 | 2020-12-15 | 北京钢研高纳科技股份有限公司 | 一种gh4282镍基高温合金棒材及其制备方法 |
CN115323298B (zh) * | 2022-08-11 | 2023-03-03 | 江苏大学 | 一种镍基高温合金锻造过程的物理模拟方法 |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3660177A (en) * | 1970-05-18 | 1972-05-02 | United Aircraft Corp | Processing of nickel-base alloys for improved fatigue properties |
JP3369627B2 (ja) * | 1993-04-08 | 2003-01-20 | 日立金属株式会社 | 微細結晶粒超耐熱合金部材の製造方法 |
JPH08311626A (ja) * | 1995-05-17 | 1996-11-26 | Japan Steel Works Ltd:The | 超合金材の製造方法 |
FR2745588B1 (fr) * | 1996-02-29 | 1998-04-30 | Snecma | Procede de traitement thermique d'un superalliage a base de nickel |
JP3909406B2 (ja) * | 2002-02-06 | 2007-04-25 | 大同特殊鋼株式会社 | Ni基合金材の製造方法 |
US6730264B2 (en) * | 2002-05-13 | 2004-05-04 | Ati Properties, Inc. | Nickel-base alloy |
US7531054B2 (en) * | 2005-08-24 | 2009-05-12 | Ati Properties, Inc. | Nickel alloy and method including direct aging |
FR2937654A1 (fr) * | 2008-10-28 | 2010-04-30 | Snecma | Procede de traitement de pieces metalliques pour en ameliorer la tenue en fatigue |
-
2009
- 2009-12-10 FR FR0958815A patent/FR2953860B1/fr active Active
-
2010
- 2010-12-09 EP EP10801646.0A patent/EP2510131B1/fr active Active
- 2010-12-09 CA CA2782460A patent/CA2782460A1/fr active Pending
- 2010-12-09 CN CN201080056172.0A patent/CN102652179B/zh active Active
- 2010-12-09 BR BR112012013752A patent/BR112012013752A2/pt not_active Application Discontinuation
- 2010-12-09 JP JP2012542604A patent/JP5951499B2/ja active Active
- 2010-12-09 US US13/514,891 patent/US20120247626A1/en not_active Abandoned
- 2010-12-09 WO PCT/FR2010/052658 patent/WO2011070302A1/fr active Application Filing
- 2010-12-09 RU RU2012128876/02A patent/RU2567968C2/ru active
Also Published As
Publication number | Publication date |
---|---|
WO2011070302A1 (fr) | 2011-06-16 |
JP5951499B2 (ja) | 2016-07-13 |
CN102652179A (zh) | 2012-08-29 |
RU2567968C2 (ru) | 2015-11-10 |
FR2953860A1 (fr) | 2011-06-17 |
BR112012013752A2 (pt) | 2016-03-15 |
JP2013513728A (ja) | 2013-04-22 |
EP2510131B1 (fr) | 2021-03-24 |
CA2782460A1 (fr) | 2011-06-16 |
EP2510131A1 (fr) | 2012-10-17 |
RU2012128876A (ru) | 2014-01-20 |
US20120247626A1 (en) | 2012-10-04 |
CN102652179B (zh) | 2015-11-25 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 7 |
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Year of fee payment: 9 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170717 |
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Year of fee payment: 11 |
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