ATE457265T1 - Verfahren zur herstellung eines gekrümmten trägers aus verbundwerkstoff - Google Patents
Verfahren zur herstellung eines gekrümmten trägers aus verbundwerkstoffInfo
- Publication number
- ATE457265T1 ATE457265T1 AT04028829T AT04028829T ATE457265T1 AT E457265 T1 ATE457265 T1 AT E457265T1 AT 04028829 T AT04028829 T AT 04028829T AT 04028829 T AT04028829 T AT 04028829T AT E457265 T1 ATE457265 T1 AT E457265T1
- Authority
- AT
- Austria
- Prior art keywords
- fiber composite
- flange
- male tool
- composite laminate
- contact
- Prior art date
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
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/541—Positioning reinforcements in a mould, e.g. using clamping means for the reinforcement
-
- 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
- B29C70/32—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 on a rotating mould, former or core
-
- 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
- B29C70/386—Automated tape laying [ATL]
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
-
- 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
- Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
- Y10T156/1036—Bending of one piece blank and joining edges to form article
-
- 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
- Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
- Y10T156/1043—Subsequent to assembly
-
- 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
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24058—Structurally defined web or sheet [e.g., overall dimension, etc.] including grain, strips, or filamentary elements in respective layers or components in angular relation
- Y10T428/24124—Fibers
-
- 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
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24628—Nonplanar uniform thickness material
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Catalysts (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP04028829A EP1666353B1 (de) | 2004-12-06 | 2004-12-06 | Verfahren zur Herstellung eines gekrümmten Trägers aus Verbundwerkstoff |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE457265T1 true ATE457265T1 (de) | 2010-02-15 |
Family
ID=34927663
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT04028829T ATE457265T1 (de) | 2004-12-06 | 2004-12-06 | Verfahren zur herstellung eines gekrümmten trägers aus verbundwerkstoff |
Country Status (5)
Country | Link |
---|---|
US (2) | US7670525B2 (de) |
EP (1) | EP1666353B1 (de) |
AT (1) | ATE457265T1 (de) |
DE (1) | DE602004025482D1 (de) |
ES (1) | ES2338551T3 (de) |
Families Citing this family (41)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
DE102005028765B4 (de) * | 2005-06-22 | 2016-01-21 | Airbus Operations Gmbh | Verfahren zur Herstellung eines Verstärkungsprofils |
DE602005025490D1 (de) * | 2005-10-17 | 2011-02-03 | Saab Ab | Verfahren zur Herstellung eines gekrümmten Gegenstands aus Verbundwerkstoff sowie durch dieses Verfahren hergestellter Gegenstand |
US7807005B2 (en) | 2006-02-02 | 2010-10-05 | The Boeing Company | Fabrication process for thermoplastic composite parts |
US10449736B2 (en) | 2006-02-02 | 2019-10-22 | The Boeing Company | Apparatus for fabricating thermoplastic composite parts |
US8691137B2 (en) | 2009-03-04 | 2014-04-08 | The Boeing Company | Method of molding partus using a tool sleeve for mold die |
US10232532B1 (en) | 2006-02-02 | 2019-03-19 | The Boeing Company | Method for fabricating tapered thermoplastic composite parts |
US8333858B2 (en) * | 2006-02-02 | 2012-12-18 | The Boeing Company | Method for fabricating curved thermoplastic composite parts |
US9102103B2 (en) | 2006-02-02 | 2015-08-11 | The Boeing Company | Thermoplastic composite parts having integrated metal fittings and method of making the same |
US8491745B2 (en) | 2007-02-03 | 2013-07-23 | The Boeing Company | Method and material efficient tooling for continuous compression molding |
CA2685481A1 (en) * | 2007-04-30 | 2008-11-06 | Airbus Operations S.L. | Complex geometries made of composite material and forming process for same |
US8118959B2 (en) * | 2007-06-27 | 2012-02-21 | The Boeing Company | Method and apparatus for contouring composite pre-preg articles |
CA2711928A1 (en) | 2008-01-11 | 2009-07-16 | Tomoyuki Shinoda | Reinforcing fiber substrate of curved shape, layered product using the same, preform, fiber-reinforced resin composite material, and processes for producing those |
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. |
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 |
US8349105B2 (en) | 2008-04-17 | 2013-01-08 | The Boeing Company | Curved composite frames and method of making the same |
US9278484B2 (en) | 2008-04-17 | 2016-03-08 | The Boeing Company | Method and apparatus for producing contoured composite structures and structures produced thereby |
US10821653B2 (en) | 2010-02-24 | 2020-11-03 | Alexander M. Rubin | Continuous molding of thermoplastic laminates |
GB2484476B (en) * | 2010-10-11 | 2012-12-12 | Gkn Aerospace Services Ltd | Composite structure |
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 |
US9387657B2 (en) | 2010-11-12 | 2016-07-12 | The Boeing Company | Method of fabricating a curved composite structure using composite prepreg tape |
ITTO20110421A1 (it) * | 2011-05-12 | 2012-11-13 | Alenia Aeronautica Spa | Elemento strutturale con ala avente bordo netto, e suo processo di fabbricazione |
US9545757B1 (en) * | 2012-02-08 | 2017-01-17 | Textron Innovations, Inc. | Composite lay up and method of forming |
US10828846B2 (en) | 2013-01-07 | 2020-11-10 | The Boeing Company | Method and apparatus for fabricating contoured laminate structures |
US9314974B2 (en) | 2013-01-07 | 2016-04-19 | The Boeing Company | Method and apparatus for fabricating contoured laminate structures |
US10399284B2 (en) | 2014-05-16 | 2019-09-03 | The Boeing Company | Method and apparatus for forming contoured composite laminates |
US9782937B1 (en) | 2014-05-16 | 2017-10-10 | The Boeing Company | Apparatus for forming contoured composite laminates |
ES2731210T3 (es) | 2014-09-26 | 2019-11-14 | Airbus Operations Sl | Método para la fabricación de una pieza de material compuesto que comprende un alma y al menos un reborde |
DE102016106258B4 (de) | 2015-04-08 | 2021-11-18 | Cotesa Gmbh | Faserlage für gekrümmte Faserverbundwerkstoff-Laminate und Verfahren zur Ablage aufgefächerter Faserlagen |
DE102015110195A1 (de) * | 2015-06-24 | 2016-12-29 | Airbus Operations Gmbh | Vorrichtung und Verfahren zum Umformen eines Faserhalbzeugs |
US10005267B1 (en) | 2015-09-22 | 2018-06-26 | Textron Innovations, Inc. | Formation of complex composite structures using laminate templates |
EP3597412B1 (de) * | 2017-03-17 | 2022-10-05 | Subaru Corporation | Formvorrichtung für fasermaterial und formverfahren für fasermaterial |
FR3081369B1 (fr) | 2018-05-28 | 2020-05-08 | Stelia Aerospace | Dispositif et procede de mise en forme d'une piece d'ebauche pour la formation d'une piece thermoplastique structurelle |
US11014314B2 (en) | 2018-06-28 | 2021-05-25 | The Boeing Company | End effector for forming prepreg plies on highly contoured surfaces |
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 |
ES2958761T3 (es) * | 2019-11-13 | 2024-02-14 | Airbus Operations Slu | Dispositivo y método de formación de un laminado compuesto para obtener un perfil en forma de Z |
WO2021157082A1 (ja) * | 2020-02-07 | 2021-08-12 | 三菱重工業株式会社 | 複合材構造体の製造方法及び積層体の製造方法並びに積層体及び積層型 |
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US2593714A (en) * | 1943-06-30 | 1952-04-22 | Roy H Robinson | Method of making cellular structures |
GB1258456A (de) * | 1969-03-27 | 1971-12-30 | ||
US3913290A (en) * | 1974-03-25 | 1975-10-21 | Avco Corp | Fire insulation edge reinforcements for structural members |
DE3003552C2 (de) * | 1980-01-31 | 1982-06-24 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Flächenbauteil, insbesondere für ein Luftfahrzeug |
GB2105254B (en) * | 1981-06-24 | 1984-05-10 | Permabond Adhesives | Top-hat stiffeners for grp and other panels of synethetic plastics materials |
DE3248856T1 (de) * | 1981-06-30 | 1984-10-18 | The Boeing Co., Seattle, Wash. | Verfahren zum Herstellen einer Vorform aus faserverstärktem Verbundmaterial |
FR2544050A1 (fr) * | 1983-04-11 | 1984-10-12 | Lombard Gerard | Profile leger en plastique arme avec armature interne rigidificatrice |
DK92684D0 (da) | 1983-04-20 | 1984-02-23 | Itt | Profil eller konstruktionselement af et armeret kompositmateriale samt maskine og fremgangsmade til fremstilling heraf |
US4512835A (en) * | 1983-06-06 | 1985-04-23 | Hercules Incorporated | Method of making a curved composite beam |
US4576849A (en) * | 1983-06-06 | 1986-03-18 | Hercules Incorporated | Curved composite beam |
US4475976A (en) * | 1983-12-23 | 1984-10-09 | The Boeing Company | Method and apparatus for forming composite material articles |
US4955803A (en) * | 1986-02-03 | 1990-09-11 | The Board Of Trustees Of The Leland Stanford Junior University | Apparatus for forming fiber composite materials |
FR2635484B1 (fr) * | 1988-08-18 | 1991-04-05 | Aerospatiale | Procede et dispositifs de fabrication de pieces planes incurvees en materiau composite |
FR2635714B1 (fr) * | 1988-08-26 | 1991-02-01 | Brisard Machines Outils | Dispositif de nappage pour la mise en place automatique d'une nappe de fibres sur un moule et machine comportant un tel dispositif |
JP2554063Y2 (ja) * | 1989-10-17 | 1997-11-12 | 財団法人日本航空機開発協会 | 胴体壁内装板 |
US5223067A (en) * | 1990-02-28 | 1993-06-29 | Fuji Jukogyo Kabushiki Kaisha | Method of fabricating aircraft fuselage structure |
DE4137649C2 (de) * | 1991-11-15 | 1997-11-20 | Gerhard Dingler | Bauelement |
US6017048A (en) * | 1992-06-05 | 2000-01-25 | Fritschen; Thomas M. | Aero bicycle frame |
US5648109A (en) * | 1995-05-03 | 1997-07-15 | Massachusetts Institute Of Technology | Apparatus for diaphragm forming |
FR2766407B1 (fr) * | 1997-07-22 | 1999-10-15 | Aerospatiale | Procede de fabrication de pieces de grandes dimensions en materiau composite a matrice thermoplastique, telles que des troncons de fuselage d'aeronefs |
US6054197A (en) * | 1997-09-19 | 2000-04-25 | State University Of New York At Albany | Structural elements |
GB9828368D0 (en) * | 1998-12-22 | 1999-02-17 | British Aerospace | Forming reinforcing components |
US6655633B1 (en) * | 2000-01-21 | 2003-12-02 | W. Cullen Chapman, Jr. | Tubular members integrated to form a structure |
WO2002042044A1 (de) * | 2000-11-21 | 2002-05-30 | Eads Deutschland Gmbh | Konfektionstechnisches verfahren, ein spannmodul und ein nähguthalter zur gestaltung von textilen vorformlingen zur herstellung von faserverstärkten kunststoff-bauteilen |
KR100427405B1 (ko) * | 2001-03-07 | 2004-04-17 | 박재만 | 피에스에스씨 합성거더 |
EP1342553B1 (de) * | 2002-03-08 | 2016-05-18 | Airbus Operations GmbH | Verfahren zum Herstellen eines Fensterrahmens für Flugzeuge aus faserverstärktem Kunststoff und Vorrichtung zur Durchführung des Verfahrens |
US20050210820A1 (en) * | 2004-03-24 | 2005-09-29 | Shinmaywa Industries, Ltd. | Frame and method for fabricating the same |
US7434366B2 (en) * | 2005-01-11 | 2008-10-14 | A. Zahner Company | I-beam with curved flanges |
AT501521B1 (de) * | 2005-01-27 | 2013-07-15 | Krestel Stefan | Trägerartiges, aus einzelteilen zusammengesetztes bauelement sowie verfahren zur herstellung des bauelements |
US7673433B2 (en) * | 2005-04-29 | 2010-03-09 | The Boeing Company | Damage-tolerant monolithic structures |
US8632653B2 (en) * | 2005-05-03 | 2014-01-21 | The Boeing Company | Method of manufacturing curved composite structural elements |
-
2004
- 2004-12-06 AT AT04028829T patent/ATE457265T1/de not_active IP Right Cessation
- 2004-12-06 DE DE602004025482T patent/DE602004025482D1/de active Active
- 2004-12-06 EP EP04028829A patent/EP1666353B1/de active Active
- 2004-12-06 ES ES04028829T patent/ES2338551T3/es active Active
-
2005
- 2005-12-01 US US11/164,672 patent/US7670525B2/en not_active Expired - Fee Related
-
2010
- 2010-02-26 US US12/713,549 patent/US8151529B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
ES2338551T3 (es) | 2010-05-10 |
US8151529B2 (en) | 2012-04-10 |
DE602004025482D1 (de) | 2010-03-25 |
US20060216480A1 (en) | 2006-09-28 |
EP1666353B1 (de) | 2010-02-10 |
US7670525B2 (en) | 2010-03-02 |
US20100148005A1 (en) | 2010-06-17 |
EP1666353A1 (de) | 2006-06-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |