DE602006012055D1 - Vorrichtung und verfahren zur herstellung von gekr - Google Patents
Vorrichtung und verfahren zur herstellung von gekrInfo
- Publication number
- DE602006012055D1 DE602006012055D1 DE602006012055T DE602006012055T DE602006012055D1 DE 602006012055 D1 DE602006012055 D1 DE 602006012055D1 DE 602006012055 T DE602006012055 T DE 602006012055T DE 602006012055 T DE602006012055 T DE 602006012055T DE 602006012055 D1 DE602006012055 D1 DE 602006012055D1
- Authority
- DE
- Germany
- Prior art keywords
- web
- compaction roller
- composite
- gekr
- 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.)
- Active
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
- B29C70/382—Automated fiber placement [AFP]
- B29C70/384—Fiber placement heads, e.g. component parts, details or accessories
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/0003—Producing profiled members, e.g. beams
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/545—Perforating, cutting or machining during or after moulding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/001—Profiled members, e.g. beams, sections
- B29L2031/003—Profiled members, e.g. beams, sections having a profiled transverse cross-section
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
-
- 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
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
- Y10T156/1089—Methods of surface bonding and/or assembly therefor of discrete laminae to single face of additional lamina
-
- 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
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/17—Surface bonding means and/or assemblymeans with work feeding or handling means
- Y10T156/1788—Work traversing type and/or means applying work to wall or static structure
- Y10T156/1795—Implement carried web supply
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Robotics (AREA)
- Moulding By Coating Moulds (AREA)
- Aerials With Secondary Devices (AREA)
- Bending Of Plates, Rods, And Pipes (AREA)
- Rod-Shaped Construction Members (AREA)
- Enzymes And Modification Thereof (AREA)
- Treatment Of Fiber Materials (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/195,786 US7469735B2 (en) | 2005-08-03 | 2005-08-03 | Composite structural element fabricating device and method |
PCT/US2006/027067 WO2007018935A1 (en) | 2005-08-03 | 2006-07-11 | Curved composite structural element fabricating device and method |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602006012055D1 true DE602006012055D1 (de) | 2010-03-18 |
Family
ID=37098596
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602006012055T Active DE602006012055D1 (de) | 2005-08-03 | 2006-07-11 | Vorrichtung und verfahren zur herstellung von gekr |
Country Status (10)
Country | Link |
---|---|
US (1) | US7469735B2 (de) |
EP (1) | EP1910062B1 (de) |
JP (1) | JP4987002B2 (de) |
KR (1) | KR100945565B1 (de) |
CN (1) | CN101277809B (de) |
AT (1) | ATE456445T1 (de) |
DE (1) | DE602006012055D1 (de) |
ES (1) | ES2339878T3 (de) |
HK (1) | HK1109601A1 (de) |
WO (1) | WO2007018935A1 (de) |
Families Citing this family (64)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7249943B2 (en) * | 2003-08-01 | 2007-07-31 | Alliant Techsystems Inc. | Apparatus for forming composite stiffeners and reinforcing structures |
US7943076B1 (en) * | 2005-05-03 | 2011-05-17 | The Boeing Company | Method of manufacturing curved composite structural elements |
US8632653B2 (en) | 2005-05-03 | 2014-01-21 | The Boeing Company | Method of manufacturing curved composite structural elements |
EP1775106B1 (de) * | 2005-10-17 | 2010-12-22 | Saab Ab | Verfahren zur Herstellung eines gekrümmten Gegenstands aus Verbundwerkstoff sowie durch dieses Verfahren hergestellter Gegenstand |
US8449709B2 (en) * | 2007-05-25 | 2013-05-28 | The Boeing Company | Method of fabricating fiber reinforced composite structure having stepped surface |
GB0712549D0 (en) * | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Improvements in elongate composite structural members |
GB0712553D0 (en) * | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Composite panel stiffener |
GB0712552D0 (en) * | 2007-06-29 | 2007-08-08 | Airbus Uk Ltd | Elongate composite structural members and improvements therein |
ITTO20070557A1 (it) * | 2007-07-27 | 2009-01-28 | Alenia Aeronautica Spa | Procedimento di fabbricazione di un elemento curvo in materiale composito |
WO2009058500A1 (en) * | 2007-11-01 | 2009-05-07 | Lockheed Martin Corporation | Highly tailored stiffening for advanced composites |
US7591294B2 (en) | 2007-11-29 | 2009-09-22 | Spirit Aerosystems, Inc. | Material placement method and apparatus |
US7717151B2 (en) * | 2007-11-29 | 2010-05-18 | Spirit Aerosystems, Inc. | Material placement method and apparatus |
US8152948B2 (en) * | 2008-01-09 | 2012-04-10 | The Boeing Company | Contoured composite parts |
EP2233625B1 (de) * | 2008-01-11 | 2019-03-13 | Toray Industries, Inc. | Verfahren für die herstellung von verstärkungsfaserbasis mit gekrümmter form |
US8088317B1 (en) | 2008-03-03 | 2012-01-03 | Abe Karem | Partially automated fabrication of composite parts |
US7858012B2 (en) * | 2008-03-03 | 2010-12-28 | Abe Karem | Automated prototyping of a composite airframe |
EP2268474B1 (de) * | 2008-03-07 | 2020-04-29 | Airbus Operations (S.A.S) | Aus verbundwerkstoff hergestelltes gekrümmtes strukturteil und verfahren zur herstellung solch eines teils |
FR2928294B1 (fr) * | 2008-03-07 | 2016-12-30 | Duqueine Rhone Alpes | Procede et dispositif de realisation d'un profil courbe en materiau composite,et profil correspondant. |
FR2928295B1 (fr) * | 2008-03-07 | 2017-12-08 | Duqueine Rhone Alpes | Procede et dispositif de moulage d'une piece courbe en materiau composite,et piece correspondante. |
US9278484B2 (en) * | 2008-04-17 | 2016-03-08 | The Boeing Company | Method and apparatus for producing contoured composite structures and structures produced thereby |
US8349105B2 (en) * | 2008-04-17 | 2013-01-08 | The Boeing Company | Curved composite frames and method of making the same |
US9090028B2 (en) * | 2008-04-17 | 2015-07-28 | The Boeing Company | Method for producing contoured composite structures and structures produced thereby |
US8932423B2 (en) * | 2008-04-17 | 2015-01-13 | The Boeing Company | Method for producing contoured composite structures and structures produced thereby |
US8540833B2 (en) * | 2008-05-16 | 2013-09-24 | The Boeing Company | Reinforced stiffeners and method for making the same |
DE102008028865B4 (de) * | 2008-06-19 | 2015-04-02 | Airbus Defence and Space GmbH | Verfahren zur Herstellung von Faserverbund-Profilbauteilen, sowie Verwendung derartig hergestellter Faserverbund-Profilbauteile |
GB0813161D0 (en) | 2008-07-18 | 2008-08-27 | Airbus Uk Ltd | Ramped stiffener and apparatus and method for forming the same |
GB0813146D0 (en) * | 2008-07-18 | 2008-08-27 | Airbus Uk Ltd | Ramped stiffener and apparatus and method for forming the same |
FR2934198B1 (fr) * | 2008-07-24 | 2012-12-21 | Eads Europ Aeronautic Defence | Pli et procede de metallisation d'une piece en materiau composite. |
EP2349686B1 (de) * | 2008-11-13 | 2018-08-08 | Saab AB | Verfahren zum bilden eines verbundartikels |
CN102301050B (zh) * | 2009-02-02 | 2014-01-29 | 东丽株式会社 | 具有圆弧状部的带状增强纤维基材的制造方法及制造装置、及使用该基材的层合体、预成型体及纤维增强树脂复合材料 |
IT1395892B1 (it) * | 2009-09-15 | 2012-10-26 | Alenia Aeronautica Spa | Procedimento per la fabbricazione di un'ordinata di fusoliera in materiale composito |
US8282757B2 (en) * | 2009-11-10 | 2012-10-09 | Alliant Techsystems Inc. | Automated composite annular structure forming |
US9662841B2 (en) | 2009-11-10 | 2017-05-30 | Orbital Atk, Inc. | Radially extending composite structures |
DE102010013713A1 (de) | 2010-04-02 | 2011-10-06 | Airbus Operations Gmbh | Verfahren und Vorrichtung zur Herstellung eines faserverstärkten thermoplastischen Verbundbauteils |
US9266279B2 (en) | 2010-07-08 | 2016-02-23 | Orbital Atk, Inc. | Variable material stretch-forming apparatus and methods |
US8795567B2 (en) * | 2010-09-23 | 2014-08-05 | The Boeing Company | Method for fabricating highly contoured composite stiffeners with reduced wrinkling |
US9387657B2 (en) | 2010-11-12 | 2016-07-12 | The Boeing Company | Method of fabricating a curved composite structure using composite prepreg tape |
US9701067B2 (en) | 2010-11-12 | 2017-07-11 | The Boeing Company | Method of laying up prepreg plies on contoured tools using a deformable carrier film |
US8551380B2 (en) | 2010-11-12 | 2013-10-08 | The Boeing Company | Method of laying up prepreg plies on contoured tools using a deformable carrier film |
US9604417B2 (en) | 2011-04-05 | 2017-03-28 | The Boeing Company | Method for making contoured composite stiffeners |
US9180960B2 (en) | 2011-06-10 | 2015-11-10 | The Boeing Company | Boron fiber reinforced structural components |
US8900391B2 (en) | 2011-06-26 | 2014-12-02 | The Boeing Company | Automated resin and fiber deposition for resin infusion |
US9308692B2 (en) * | 2011-09-28 | 2016-04-12 | The Boeing Company | Material placement system |
US8721316B2 (en) | 2012-01-26 | 2014-05-13 | Alliant Techsystems Inc. | Automated material delivery system |
FR2989619B1 (fr) * | 2012-04-23 | 2014-06-13 | Airbus Operations Sas | Procede de realisation d'un profile courbe en materiau composite a partir d'une preforme rectiligne de nappes de fibres |
US8826957B2 (en) * | 2012-08-31 | 2014-09-09 | General Electric Company | Methods and systems for automated ply layup for composites |
EP2808158A1 (de) * | 2013-05-31 | 2014-12-03 | Siemens Aktiengesellschaft | Verfahren und Vorrichtug zum Verlegen eines Fasermaterials auf einer Formoberfläche |
DE102013017450A1 (de) * | 2013-10-22 | 2015-04-23 | Airbus Defence and Space GmbH | Verfahren zur Herstellung von Faserverbund-Halbzeugen |
CN103692663B (zh) * | 2013-12-30 | 2015-09-23 | 中国科学院自动化研究所 | 一种对纤维丝束进行重送剪切导向压紧的方法 |
US9579875B2 (en) | 2014-02-04 | 2017-02-28 | The Boeing Company | Bonded tab and tooling device |
US10112349B2 (en) * | 2014-03-20 | 2018-10-30 | The Boeing Company | Placement of prepreg tows in high angle transition regions |
WO2016018194A1 (en) * | 2014-08-01 | 2016-02-04 | Gök Gökhan Vargin | Fiber placement head having double roller system and a fiber placement head application method |
US9545759B2 (en) * | 2015-01-30 | 2017-01-17 | CGTech | Automated fiber placement with course trajectory compensation |
JP6732101B2 (ja) * | 2017-03-17 | 2020-07-29 | 株式会社Subaru | 繊維材の賦形装置及び繊維材の賦形方法 |
CN110461918B (zh) | 2017-03-31 | 2022-06-28 | 三菱化学株式会社 | 预浸料片及其制造方法、带表皮材的单元层、纤维增强复合材料成型品及其制造方法 |
WO2020067478A1 (ja) * | 2018-09-27 | 2020-04-02 | 三菱ケミカル株式会社 | テーププリプレグ、テーププリプレグの配置方法、繊維強化複合材料及び繊維強化複合材料の製造方法 |
US11318689B2 (en) | 2018-12-21 | 2022-05-03 | The Boeing Company | Ply transporting and compacting apparatus and method therefor |
US11305498B2 (en) | 2018-12-21 | 2022-04-19 | The Boeing Company | System and method for fabricating a composite ply layup |
CN111203996B (zh) * | 2019-12-13 | 2022-04-19 | 中国航空工业集团公司基础技术研究院 | 一种带有弯折截面预制体的制备设备及方法 |
EP4082769B1 (de) * | 2020-02-28 | 2024-02-21 | Mitsubishi Heavy Industries, Ltd. | Schichtkörper und schichtungsverfahren |
NL2027395B1 (en) * | 2021-01-26 | 2022-08-12 | Boeing Co | Frame fabrication line |
EP4000909A1 (de) * | 2020-11-18 | 2022-05-25 | The Boeing Company | Rahmenfertigungslinie |
US11845566B2 (en) | 2020-11-18 | 2023-12-19 | The Boeing Company | Frame fabrication line |
US11577814B2 (en) | 2020-12-18 | 2023-02-14 | The Boeing Company | Composite structure and method of forming |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3259021A (en) * | 1961-05-05 | 1966-07-05 | North American Aviation Inc | Multiple purpose fabrication apparatus and method |
JPS5839845U (ja) * | 1981-09-11 | 1983-03-16 | 東芝機械株式会社 | テ−プ自動貼付装置 |
US4720255A (en) * | 1984-06-28 | 1988-01-19 | The Boeing Company | Apparatus for planar forming of zero degree composite tape |
US4726924A (en) * | 1984-06-28 | 1988-02-23 | The Boeing Company | Method of planar forming of zero degree composite tape |
FR2590069B1 (fr) * | 1985-11-14 | 1987-12-11 | Alsthom | Enrubanneuse pour l'enrubannage a chaud d'un conducteur electrique |
US4867834A (en) * | 1986-04-07 | 1989-09-19 | Hercules | Filament winding system |
JPH0639133B2 (ja) * | 1990-06-27 | 1994-05-25 | 川崎重工業株式会社 | ロービング材自動積層装置 |
JPH0483713U (de) * | 1990-11-30 | 1992-07-21 | ||
JP2501497B2 (ja) * | 1991-08-27 | 1996-05-29 | 川崎重工業株式会社 | ロ―ビング材積層装置 |
CA2308615A1 (en) * | 1997-11-05 | 1999-05-14 | Sikorsky Aircraft Corporation | Feed control system for fiber placement machines |
JP3999031B2 (ja) * | 2002-04-26 | 2007-10-31 | 東京特殊電線株式会社 | 角形断面マグネットワイヤの製造方法 |
US7249943B2 (en) * | 2003-08-01 | 2007-07-31 | Alliant Techsystems Inc. | Apparatus for forming composite stiffeners and reinforcing structures |
JP3742082B2 (ja) * | 2003-08-08 | 2006-02-01 | 株式会社ジャムコ | 曲率を有した繊維強化プラスチック部材の連続成形方法及び装置 |
US7134629B2 (en) * | 2004-04-06 | 2006-11-14 | The Boeing Company | Structural panels for use in aircraft fuselages and other structures |
-
2005
- 2005-08-03 US US11/195,786 patent/US7469735B2/en active Active
-
2006
- 2006-07-11 ES ES06787029T patent/ES2339878T3/es active Active
- 2006-07-11 AT AT06787029T patent/ATE456445T1/de not_active IP Right Cessation
- 2006-07-11 JP JP2008524977A patent/JP4987002B2/ja active Active
- 2006-07-11 KR KR1020087002950A patent/KR100945565B1/ko active IP Right Grant
- 2006-07-11 WO PCT/US2006/027067 patent/WO2007018935A1/en active Application Filing
- 2006-07-11 DE DE602006012055T patent/DE602006012055D1/de active Active
- 2006-07-11 EP EP06787029A patent/EP1910062B1/de not_active Not-in-force
- 2006-07-11 CN CN2006800369058A patent/CN101277809B/zh not_active Expired - Fee Related
-
2008
- 2008-04-17 HK HK08104364.2A patent/HK1109601A1/xx not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
EP1910062B1 (de) | 2010-01-27 |
WO2007018935A1 (en) | 2007-02-15 |
KR20080031942A (ko) | 2008-04-11 |
CN101277809B (zh) | 2010-09-29 |
EP1910062A1 (de) | 2008-04-16 |
KR100945565B1 (ko) | 2010-03-08 |
US7469735B2 (en) | 2008-12-30 |
CN101277809A (zh) | 2008-10-01 |
US20070029038A1 (en) | 2007-02-08 |
JP4987002B2 (ja) | 2012-07-25 |
HK1109601A1 (en) | 2008-06-13 |
ATE456445T1 (de) | 2010-02-15 |
JP2009502585A (ja) | 2009-01-29 |
ES2339878T3 (es) | 2010-05-26 |
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