FR2393076A1 - Procede de fabrication d'articles faconnes en superalliage de nickel de resistance elevee et de faible ductilite - Google Patents
Procede de fabrication d'articles faconnes en superalliage de nickel de resistance elevee et de faible ductiliteInfo
- Publication number
- FR2393076A1 FR2393076A1 FR7815121A FR7815121A FR2393076A1 FR 2393076 A1 FR2393076 A1 FR 2393076A1 FR 7815121 A FR7815121 A FR 7815121A FR 7815121 A FR7815121 A FR 7815121A FR 2393076 A1 FR2393076 A1 FR 2393076A1
- Authority
- FR
- France
- Prior art keywords
- billet
- high strength
- low ductility
- superally
- 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.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/12—Both compacting and sintering
- B22F3/16—Both compacting and sintering in successive or repeated steps
Abstract
La présente invention concerne un procédé amélioré de fabrication d'articles façonnés en alliage de nickel de résistance mécanique élevée et faible ductilité. L'alliage sous forme de poudre pré-alliée est soumis à une compression isothermiquement à chaud pour réaliser une billette homogène solide qui est alors isothermiquement forgée pour obtenir la forme souhaitée dans des matrices à façonnage à chaud en une seule passe de forgeage qui comprend une étape initiale avec faible vitesse de transformation pour réaliser une réduction faible de l'épaisseur pour placer la billette dans un état temporaire superplastique suivi par une étape avec vitesse de transformation élevée pour effectuer une réduction importante de l'épaisseur alors que la billette est dans cet état temporaire superplastique. L'invention est utilisable pour la fabrication d'éléments des moteurs à turbine à gaz de forme complexe.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/802,926 US4081295A (en) | 1977-06-02 | 1977-06-02 | Fabricating process for high strength, low ductility nickel base alloys |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2393076A1 true FR2393076A1 (fr) | 1978-12-29 |
FR2393076B1 FR2393076B1 (fr) | 1983-07-08 |
Family
ID=25185108
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7815121A Granted FR2393076A1 (fr) | 1977-06-02 | 1978-05-22 | Procede de fabrication d'articles faconnes en superalliage de nickel de resistance elevee et de faible ductilite |
Country Status (17)
Country | Link |
---|---|
US (1) | US4081295A (fr) |
JP (1) | JPS542220A (fr) |
AR (1) | AR215710A1 (fr) |
BE (1) | BE867310A (fr) |
BR (1) | BR7803371A (fr) |
CA (1) | CA1108441A (fr) |
CH (1) | CH637426A5 (fr) |
DE (1) | DE2822153A1 (fr) |
DK (1) | DK153336C (fr) |
FR (1) | FR2393076A1 (fr) |
GB (1) | GB1564795A (fr) |
IL (1) | IL54801A (fr) |
IT (1) | IT1096611B (fr) |
NL (1) | NL7805975A (fr) |
NO (1) | NO781788L (fr) |
SE (1) | SE444584B (fr) |
ZA (1) | ZA782806B (fr) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4479833A (en) * | 1981-06-26 | 1984-10-30 | Bbc Brown, Boveri & Company, Limited | Process for manufacturing a semi-finished product or a finished component from a metallic material by hot working |
US4375375A (en) * | 1981-10-30 | 1983-03-01 | United Technologies Corporation | Constant energy rate forming |
US4613388A (en) * | 1982-09-17 | 1986-09-23 | Rockwell International Corporation | Superplastic alloys formed by electrodeposition |
US4529452A (en) * | 1984-07-30 | 1985-07-16 | United Technologies Corporation | Process for fabricating multi-alloy components |
JPS62134130A (ja) * | 1985-12-05 | 1987-06-17 | Agency Of Ind Science & Technol | 高強度・難加工材の超塑性ウオ−ムダイ・パツク鍛造法 |
US4769087A (en) * | 1986-06-02 | 1988-09-06 | United Technologies Corporation | Nickel base superalloy articles and method for making |
JPS6447828A (en) * | 1987-08-12 | 1989-02-22 | Agency Ind Science Techn | Turbin disk by super plastic forging of different alloys |
US5009704A (en) * | 1989-06-28 | 1991-04-23 | Allied-Signal Inc. | Processing nickel-base superalloy powders for improved thermomechanical working |
US5571345A (en) * | 1994-06-30 | 1996-11-05 | General Electric Company | Thermomechanical processing method for achieving coarse grains in a superalloy article |
US20060083653A1 (en) * | 2004-10-20 | 2006-04-20 | Gopal Das | Low porosity powder metallurgy produced components |
GB0918020D0 (en) * | 2009-10-15 | 2009-12-02 | Rolls Royce Plc | A method of forging a nickel base superalloy |
RU2649103C1 (ru) * | 2017-04-18 | 2018-03-29 | Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") | Способ получения изделия из гранулируемого жаропрочного никелевого сплава |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2078603A5 (fr) * | 1970-02-16 | 1971-11-05 | Latrobe Steel Co | |
FR2095668A5 (en) * | 1970-06-10 | 1972-02-11 | Federal Mogul Corp | Superplastic alloy articles produced by powder metallurgical - and extrusion process |
FR2328538A1 (fr) * | 1975-10-20 | 1977-05-20 | Bbc Brown Boveri & Cie | Procede de realisation d'une piece en alliage resistant a des temperatures tres elevees par metallurgie des poudres |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3519503A (en) * | 1967-12-22 | 1970-07-07 | United Aircraft Corp | Fabrication method for the high temperature alloys |
SE421015B (sv) * | 1969-04-14 | 1981-11-16 | United Aircraft Corp | Forfarande vid framstellning av foremal av hogtemperaturlegeringar |
US3639179A (en) * | 1970-02-02 | 1972-02-01 | Federal Mogul Corp | Method of making large grain-sized superalloys |
NL171309C (nl) * | 1970-03-02 | 1983-03-01 | Hitachi Ltd | Werkwijze voor de vervaardiging van een halfgeleiderlichaam, waarbij een laag van siliciumdioxyde wordt gevormd op een oppervlak van een monokristallijn lichaam van silicium. |
US3702791A (en) * | 1970-04-20 | 1972-11-14 | Nasa | Method of forming superalloys |
US3655458A (en) * | 1970-07-10 | 1972-04-11 | Federal Mogul Corp | Process for making nickel-based superalloys |
US3698962A (en) * | 1971-04-30 | 1972-10-17 | Crucible Inc | Method for producing superalloy articles by hot isostatic pressing |
US3698219A (en) * | 1971-05-10 | 1972-10-17 | United Aircraft Corp | Apparatus for forging |
US3843421A (en) * | 1972-10-16 | 1974-10-22 | United Aircraft Corp | Wrought nickel-base alloy and products thereof |
US3987658A (en) * | 1975-12-12 | 1976-10-26 | United Technologies Corporation | Graphite forging die |
-
1977
- 1977-06-02 US US05/802,926 patent/US4081295A/en not_active Expired - Lifetime
-
1978
- 1978-05-09 CA CA302,904A patent/CA1108441A/fr not_active Expired
- 1978-05-16 ZA ZA00782806A patent/ZA782806B/xx unknown
- 1978-05-18 SE SE7805706A patent/SE444584B/sv not_active IP Right Cessation
- 1978-05-20 DE DE19782822153 patent/DE2822153A1/de active Granted
- 1978-05-22 FR FR7815121A patent/FR2393076A1/fr active Granted
- 1978-05-22 GB GB21043/78A patent/GB1564795A/en not_active Expired
- 1978-05-22 BE BE187896A patent/BE867310A/fr not_active IP Right Cessation
- 1978-05-23 NO NO781788A patent/NO781788L/no unknown
- 1978-05-24 CH CH565278A patent/CH637426A5/de not_active IP Right Cessation
- 1978-05-26 BR BR7803371A patent/BR7803371A/pt unknown
- 1978-05-26 JP JP6321478A patent/JPS542220A/ja active Granted
- 1978-05-29 DK DK236978A patent/DK153336C/da not_active IP Right Cessation
- 1978-05-29 IL IL54801A patent/IL54801A/xx unknown
- 1978-05-31 AR AR272399A patent/AR215710A1/es active
- 1978-05-31 IT IT24028/78A patent/IT1096611B/it active
- 1978-06-01 NL NL7805975A patent/NL7805975A/xx not_active Application Discontinuation
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2078603A5 (fr) * | 1970-02-16 | 1971-11-05 | Latrobe Steel Co | |
FR2095668A5 (en) * | 1970-06-10 | 1972-02-11 | Federal Mogul Corp | Superplastic alloy articles produced by powder metallurgical - and extrusion process |
FR2328538A1 (fr) * | 1975-10-20 | 1977-05-20 | Bbc Brown Boveri & Cie | Procede de realisation d'une piece en alliage resistant a des temperatures tres elevees par metallurgie des poudres |
Also Published As
Publication number | Publication date |
---|---|
SE444584B (sv) | 1986-04-21 |
JPS542220A (en) | 1979-01-09 |
NO781788L (no) | 1978-12-05 |
IT1096611B (it) | 1985-08-26 |
JPS6132387B2 (fr) | 1986-07-26 |
GB1564795A (en) | 1980-04-16 |
DK236978A (da) | 1978-12-03 |
DE2822153A1 (de) | 1978-12-14 |
FR2393076B1 (fr) | 1983-07-08 |
DK153336C (da) | 1988-11-14 |
SE7805706L (sv) | 1978-12-03 |
IL54801A (en) | 1981-01-30 |
DE2822153C2 (fr) | 1987-02-26 |
DK153336B (da) | 1988-07-04 |
BR7803371A (pt) | 1979-04-24 |
CA1108441A (fr) | 1981-09-08 |
BE867310A (fr) | 1978-09-18 |
ZA782806B (en) | 1979-05-30 |
AR215710A1 (es) | 1979-10-31 |
CH637426A5 (de) | 1983-07-29 |
AU3644078A (en) | 1979-11-29 |
IT7824028A0 (it) | 1978-05-31 |
NL7805975A (nl) | 1978-12-05 |
US4081295A (en) | 1978-03-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |