DE68909930D1 - Ermüdungsrissbeständige Nickelbasissuperlegierung und hergestelltes Erzeugnis. - Google Patents
Ermüdungsrissbeständige Nickelbasissuperlegierung und hergestelltes Erzeugnis.Info
- Publication number
- DE68909930D1 DE68909930D1 DE89111451T DE68909930T DE68909930D1 DE 68909930 D1 DE68909930 D1 DE 68909930D1 DE 89111451 T DE89111451 T DE 89111451T DE 68909930 T DE68909930 T DE 68909930T DE 68909930 D1 DE68909930 D1 DE 68909930D1
- Authority
- DE
- Germany
- Prior art keywords
- fatigue crack
- nickel base
- manufactured product
- super alloy
- resistant 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.)
- Expired - Fee Related
Links
Classifications
-
- 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%
-
- 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
- C22C19/057—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being less 10%
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/248,756 US5129971A (en) | 1988-09-26 | 1988-09-26 | Fatigue crack resistant waspoloy nickel base superalloys and product formed |
EP89111451A EP0403681B1 (de) | 1988-09-26 | 1989-06-23 | Ermüdungsrissbeständige Nickelbasissuperlegierung und hergestelltes Erzeugnis |
Publications (2)
Publication Number | Publication Date |
---|---|
DE68909930D1 true DE68909930D1 (de) | 1993-11-18 |
DE68909930T2 DE68909930T2 (de) | 1994-05-05 |
Family
ID=39952174
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE89111451T Expired - Fee Related DE68909930T2 (de) | 1988-09-26 | 1989-06-23 | Ermüdungsrissbeständige Nickelbasissuperlegierung und hergestelltes Erzeugnis. |
Country Status (5)
Country | Link |
---|---|
US (1) | US5129971A (de) |
EP (2) | EP0403681B1 (de) |
JP (1) | JPH03501980A (de) |
DE (1) | DE68909930T2 (de) |
WO (1) | WO1990003450A1 (de) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5372662A (en) * | 1992-01-16 | 1994-12-13 | Inco Alloys International, Inc. | Nickel-base alloy with superior stress rupture strength and grain size control |
FR2729675A1 (fr) * | 1995-01-19 | 1996-07-26 | Turbomeca | Procede perfectionne d'elaboration et de traitement thermique d'un superalliage polycristallin a base de nickel, resistant a chaud |
FR2737733B1 (fr) * | 1995-08-09 | 1998-03-13 | Snecma | Superalliages a base de nickel stables a hautes temperatures |
US6068714A (en) * | 1996-01-18 | 2000-05-30 | Turbomeca | Process for making a heat resistant nickel-base polycrystalline superalloy forged part |
GB9608617D0 (en) * | 1996-04-24 | 1996-07-03 | Rolls Royce Plc | Nickel alloy for turbine engine components |
US5980206A (en) * | 1996-05-31 | 1999-11-09 | Sikorsky Aircraft Corporation | Monolithic structure having improved flaw tolerance |
US5938863A (en) * | 1996-12-17 | 1999-08-17 | United Technologies Corporation | Low cycle fatigue strength nickel base superalloys |
US6551372B1 (en) | 1999-09-17 | 2003-04-22 | Rolls-Royce Corporation | High performance wrought powder metal articles and method of manufacture |
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 |
US8992700B2 (en) * | 2009-05-29 | 2015-03-31 | General Electric Company | Nickel-base superalloys and components formed thereof |
US8992699B2 (en) * | 2009-05-29 | 2015-03-31 | General Electric Company | Nickel-base superalloys and components formed thereof |
US8313593B2 (en) * | 2009-09-15 | 2012-11-20 | General Electric Company | Method of heat treating a Ni-based superalloy article and article made thereby |
RU2765297C1 (ru) * | 2021-02-25 | 2022-01-28 | Акционерное общество "Ступинская металлургическая компания" | Никелевый гранульный жаропрочный сплав для дисков газовых турбин |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL260545A (de) * | 1960-02-01 | |||
GB1075216A (en) * | 1963-12-23 | 1967-07-12 | Int Nickel Ltd | Nickel-chromium alloys |
FR1418583A (fr) * | 1964-12-22 | 1965-11-19 | Mond Nickel Co Ltd | Alliages de nickel-chrome |
BE712413A (de) * | 1967-04-04 | 1968-07-31 | ||
US3589893A (en) * | 1967-11-24 | 1971-06-29 | Martin Metals Co | Sulfidation resistant alloys and structures |
GB1261403A (en) * | 1968-04-29 | 1972-01-26 | Martin Marietta Corp | Cast alloys |
US3825420A (en) * | 1972-08-21 | 1974-07-23 | Avco Corp | Wrought superalloys |
US4207098A (en) * | 1978-01-09 | 1980-06-10 | The International Nickel Co., Inc. | Nickel-base superalloys |
GB2151659B (en) * | 1983-12-24 | 1987-03-18 | Rolls Royce | An alloy suitable for making single crystal castings |
US4888064A (en) * | 1986-09-15 | 1989-12-19 | General Electric Company | Method of forming strong fatigue crack resistant nickel base superalloy and product formed |
US4814023A (en) * | 1987-05-21 | 1989-03-21 | General Electric Company | High strength superalloy for high temperature applications |
-
1988
- 1988-09-26 US US07/248,756 patent/US5129971A/en not_active Expired - Fee Related
-
1989
- 1989-06-23 DE DE89111451T patent/DE68909930T2/de not_active Expired - Fee Related
- 1989-06-23 EP EP89111451A patent/EP0403681B1/de not_active Expired - Lifetime
- 1989-09-22 WO PCT/US1989/004171 patent/WO1990003450A1/en not_active Application Discontinuation
- 1989-09-22 JP JP1511740A patent/JPH03501980A/ja active Pending
- 1989-09-22 EP EP89912564A patent/EP0411067A1/de not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
JPH03501980A (ja) | 1991-05-09 |
WO1990003450A1 (en) | 1990-04-05 |
EP0411067A1 (de) | 1991-02-06 |
EP0403681B1 (de) | 1993-10-13 |
US5129971A (en) | 1992-07-14 |
EP0403681A1 (de) | 1990-12-27 |
DE68909930T2 (de) | 1994-05-05 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8320 | Willingness to grant licences declared (paragraph 23) | ||
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |