FR2502042B1 - Procede de fabrication de structures metalliques armees de filaments - Google Patents

Procede de fabrication de structures metalliques armees de filaments

Info

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
Application number
FR8204856A
Other languages
English (en)
Other versions
FR2502042A1 (fr
Inventor
Leonard Angelo Ascani Jr
Billy Armond Burroughs
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing North American Inc
Original Assignee
Rockwell International Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Rockwell International Corp filed Critical Rockwell International Corp
Publication of FR2502042A1 publication Critical patent/FR2502042A1/fr
Application granted granted Critical
Publication of FR2502042B1 publication Critical patent/FR2502042B1/fr
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D26/00Shaping without cutting otherwise than using rigid devices or tools or yieldable or resilient pads, i.e. applying fluid pressure or magnetic forces
    • B21D26/02Shaping 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
    • B21D26/053Shaping 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
    • B21D26/055Blanks having super-plastic properties
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D47/00Making rigid structural elements or units, e.g. honeycomb structures
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/18Zonal welding by interposing weld-preventing substances between zones not to be welded
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12486Laterally 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)
FR8204856A 1981-03-23 1982-03-22 Procede de fabrication de structures metalliques armees de filaments Expired FR2502042B1 (fr)

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)

* Cited by examiner, † Cited by third party
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
US7533794B2 (en) * 2004-03-31 2009-05-19 The Boring Company Superplastic forming and diffusion bonding of fine grain titanium
US7850058B2 (en) 2004-03-31 2010-12-14 The Boeing Company Superplastic forming of titanium assemblies
RU2291019C2 (ru) * 2005-03-23 2007-01-10 Институт проблем сверхпластичности металлов РАН Способ изготовления изделия путем сверхпластической формовки и диффузионной сварки
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
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
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
CN108029214B (zh) * 2015-09-18 2020-07-24 东丽株式会社 壳体
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)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
GB2095137A (en) 1982-09-29
US4406393A (en) 1983-09-27
GB2095137B (en) 1985-07-03
FR2502042A1 (fr) 1982-09-24

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