FR2502042B1 - Procede de fabrication de structures metalliques armees de filaments - Google Patents
Procede de fabrication de structures metalliques armees de filamentsInfo
- Publication number
- FR2502042B1 FR2502042B1 FR8204856A FR8204856A FR2502042B1 FR 2502042 B1 FR2502042 B1 FR 2502042B1 FR 8204856 A FR8204856 A FR 8204856A FR 8204856 A FR8204856 A FR 8204856A FR 2502042 B1 FR2502042 B1 FR 2502042B1
- Authority
- FR
- France
- Prior art keywords
- filaments
- metal structures
- reinforced metal
- producing reinforced
- producing
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D26/00—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
- B21D26/02—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure
- B21D26/053—Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces by applying fluid pressure characterised by the material of the blanks
- B21D26/055—Blanks having super-plastic properties
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D47/00—Making rigid structural elements or units, e.g. honeycomb structures
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
- B23K20/18—Zonal welding by interposing weld-preventing substances between zones not to be welded
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12486—Laterally noncoextensive components [e.g., embedded, etc.]
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Shaping Metal By Deep-Drawing, Or The Like (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/246,490 US4406393A (en) | 1981-03-23 | 1981-03-23 | Method of making filamentary reinforced metallic structures |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2502042A1 FR2502042A1 (fr) | 1982-09-24 |
FR2502042B1 true FR2502042B1 (fr) | 1987-06-05 |
Family
ID=22930897
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8204856A Expired FR2502042B1 (fr) | 1981-03-23 | 1982-03-22 | Procede de fabrication de structures metalliques armees de filaments |
Country Status (3)
Country | Link |
---|---|
US (1) | US4406393A (fr) |
FR (1) | FR2502042B1 (fr) |
GB (1) | GB2095137B (fr) |
Families Citing this family (46)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4588651A (en) * | 1983-02-16 | 1986-05-13 | Rockwell International Corporation | Accordion expansion process |
US4811890A (en) * | 1983-05-07 | 1989-03-14 | Rockwell International Corporation | Method of eliminating core distortion in diffusion bonded and uperplastically formed structures |
US4509671A (en) * | 1983-07-25 | 1985-04-09 | Rockwell International Corporation | Method of producing diffusion bonded superplastically formed structures |
US4691857A (en) * | 1985-11-07 | 1987-09-08 | Trw Inc. | Method of shaping a workpiece |
US4809903A (en) * | 1986-11-26 | 1989-03-07 | United States Of America As Represented By The Secretary Of The Air Force | Method to produce metal matrix composite articles from rich metastable-beta titanium alloys |
US4807798A (en) * | 1986-11-26 | 1989-02-28 | The United States Of America As Represented By The Secretary Of The Air Force | Method to produce metal matrix composite articles from lean metastable beta titanium alloys |
US4733816A (en) * | 1986-12-11 | 1988-03-29 | The United States Of America As Represented By The Secretary Of The Air Force | Method to produce metal matrix composite articles from alpha-beta titanium alloys |
US4882823A (en) * | 1988-01-27 | 1989-11-28 | Ontario Technologies Corp. | Superplastic forming diffusion bonding process |
US5024369A (en) * | 1989-05-05 | 1991-06-18 | The United States Of America As Represented By The Secretary Of The Air Force | Method to produce superplastically formed titanium alloy components |
US4893743A (en) * | 1989-05-09 | 1990-01-16 | The United States Of America As Represented By The Secretary Of The Air Force | Method to produce superplastically formed titanium aluminide components |
GB8912025D0 (en) * | 1989-05-25 | 1989-07-12 | British Aerospace | Diffusion bonding |
US5385204A (en) * | 1989-08-25 | 1995-01-31 | Rolls-Royce Plc | Heat exchanger and methods of manufacture thereof |
US5287918A (en) * | 1990-06-06 | 1994-02-22 | Rolls-Royce Plc | Heat exchangers |
US5505256A (en) * | 1991-02-19 | 1996-04-09 | Rolls-Royce Plc | Heat exchangers and methods of manufacture thereof |
US5118026A (en) * | 1991-04-05 | 1992-06-02 | Rockwell International Corporation | Method for making titanium aluminide metallic sandwich structures |
GB9111954D0 (en) * | 1991-06-04 | 1991-07-24 | Rolls Royce Plc | A method of manufacturing an article by superplastic forming and diffusion bonding and a vacuum chamber for use in processing workpieces |
US5263638A (en) * | 1991-06-04 | 1993-11-23 | Rolls-Royce Plc | Method of manufacturing an article by superplastic forming and diffusion bonding and a vacuum chamber for use in processing workpieces for superplastic forming and diffusion bonding |
US5141146A (en) * | 1991-06-06 | 1992-08-25 | Mcdonnell Douglas Corporation | Fabrication of superplastically formed trusscore structure |
US5262220A (en) * | 1991-06-18 | 1993-11-16 | Chem-Tronics, Inc. | High strength structure assembly and method of making the same |
GB9117546D0 (en) * | 1991-08-14 | 1992-02-19 | British Aerospace | Manufacture of structures by diffusion bonding and superplastic forming |
GB9121107D0 (en) * | 1991-10-04 | 1991-11-20 | British Aerospace | Improvements relating to diffusion bonded/superplastically formed cellular structures |
GB9123818D0 (en) * | 1991-11-08 | 1992-01-02 | British Aerospace | Forming of gas injection/exhaustion channels in diffusion bonded materials |
JPH05185169A (ja) * | 1992-01-10 | 1993-07-27 | Mitsubishi Heavy Ind Ltd | サンドイッチパネルの製作方法 |
GB9209464D0 (en) * | 1992-05-01 | 1992-06-17 | Rolls Royce Plc | A method of manufacturing an article by superplastic forming and diffusion bonding |
US5479705A (en) * | 1992-05-01 | 1996-01-02 | Rolls-Royce Plc | Method of manufacturing an article by superplastic forming and diffusion bonding |
IL108337A0 (en) * | 1994-01-14 | 1994-04-12 | Univ Ramot | Structural members with predetermined thermal expansivity |
JP3398246B2 (ja) * | 1995-02-24 | 2003-04-21 | 日本飛行機株式会社 | 金属サンドイッチ構造体およびその製造方法 |
US5850722A (en) * | 1996-09-27 | 1998-12-22 | Mcdonnell Douglas Corporation | Lightweight superplastically formed, diffusion bonded panel structure and process of manufacture |
RU2233683C1 (ru) * | 2003-01-29 | 2004-08-10 | ООО "Специальные материалы и технологии" | Лицевая пластина головки клюшки для игры в гольф и способ ее изготовления |
GB0327043D0 (en) | 2003-11-18 | 2004-04-07 | Rolls Royce Plc | A method of manufacturing an article by applying heat and pressure, a method of connecting a pipe to a sealed assembly and a connector for use therein |
DE102004001666A1 (de) * | 2004-01-12 | 2005-08-04 | Mtu Aero Engines Gmbh | Verfahren zur Herstellung von Hohlschaufeln |
US7850058B2 (en) | 2004-03-31 | 2010-12-14 | The Boeing Company | Superplastic forming of titanium assemblies |
US7533794B2 (en) * | 2004-03-31 | 2009-05-19 | The Boring Company | Superplastic forming and diffusion bonding of fine grain titanium |
RU2291019C2 (ru) * | 2005-03-23 | 2007-01-10 | Институт проблем сверхпластичности металлов РАН | Способ изготовления изделия путем сверхпластической формовки и диффузионной сварки |
US20070261463A1 (en) * | 2006-05-11 | 2007-11-15 | Rti International Metals, Inc. | Method and apparatus for creep forming of and relieving stress in an elongated metal bar |
US20070261462A1 (en) * | 2006-05-11 | 2007-11-15 | Rti International Metals, Inc. | Method and apparatus for creep forming of and relieving stress in an elongated metal bar |
FR2913107B1 (fr) * | 2007-02-23 | 2009-05-08 | Pierre Vironneau | Procede pour realiser un echangeur thermique et echangeur thermique obtenu selon ce procede |
GB0911416D0 (en) * | 2009-07-02 | 2009-08-12 | Rolls Royce Plc | A method of forming an internal structure within a hollow component |
CN102069368B (zh) * | 2010-12-07 | 2012-05-23 | 苏州和林精密科技有限公司 | 一种精密器件加工方法 |
FR2997644B1 (fr) * | 2012-11-08 | 2015-05-15 | Technicatome | Procede de soudage par diffusion |
RU2529259C1 (ru) * | 2013-03-15 | 2014-09-27 | Федеральное Государственное Унитарное Предприятие "Научно-Производственное Объединение "Техномаш" | Штамп для формообразования изделий из листовых заготовок |
JP6168242B1 (ja) * | 2015-09-18 | 2017-07-26 | 東レ株式会社 | 筐体 |
RU2613003C1 (ru) * | 2015-09-30 | 2017-03-14 | Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" | Способ изготовления деталей из титановых сплавов |
CN106363375B (zh) * | 2016-08-26 | 2018-07-13 | 北京普惠三航科技有限公司 | 一种制造栅格翼舵的方法 |
RU178662U1 (ru) * | 2017-05-30 | 2018-04-16 | федеральное государственное бюджетное образовательное учреждение высшего образования "Московский государственный технический университет имени Н.Э. Баумана (национальный исследовательский университет)" (МГТУ им. Н.Э. Баумана) | Штамп для изготовления сферических, эллиптических и других куполообразных днищ |
RU189518U1 (ru) * | 2018-10-17 | 2019-05-24 | Анвар Юсуфович Боташев | Импульсная машина для обработки давлением листового материала |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3711936A (en) * | 1970-12-28 | 1973-01-23 | United Aircraft Corp | Method for forming composite articles from alloy in temporary condition of superplasticity |
JPS547509B2 (fr) * | 1974-05-13 | 1979-04-07 | ||
US3991928A (en) * | 1974-08-22 | 1976-11-16 | United Technologies Corporation | Method of fabricating titanium alloy matrix composite materials |
US3927817A (en) * | 1974-10-03 | 1975-12-23 | Rockwell International Corp | Method for making metallic sandwich structures |
US4010884A (en) * | 1974-11-20 | 1977-03-08 | United Technologies Corporation | Method of fabricating a filament-reinforced composite article |
US4087037A (en) * | 1976-07-09 | 1978-05-02 | Mcdonnell Douglas Corporation | Method of and tools for producing superplastically formed and diffusion bonded structures |
US4163380A (en) * | 1977-10-11 | 1979-08-07 | Lockheed Corporation | Forming of preconsolidated metal matrix composites |
US4217397A (en) * | 1978-04-18 | 1980-08-12 | Mcdonnell Douglas Corporation | Metallic sandwich structure and method of fabrication |
US4197977A (en) * | 1978-04-20 | 1980-04-15 | The Boeing Company | Method of making an actively-cooled titanium structure |
-
1981
- 1981-03-23 US US06/246,490 patent/US4406393A/en not_active Expired - Lifetime
-
1982
- 1982-03-22 FR FR8204856A patent/FR2502042B1/fr not_active Expired
- 1982-03-23 GB GB8208377A patent/GB2095137B/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR2502042A1 (fr) | 1982-09-24 |
GB2095137A (en) | 1982-09-29 |
US4406393A (en) | 1983-09-27 |
GB2095137B (en) | 1985-07-03 |
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