DE602004025482D1 - Verfahren zur Herstellung eines gekrümmten Trägers aus Verbundwerkstoff - Google Patents
Verfahren zur Herstellung eines gekrümmten Trägers aus VerbundwerkstoffInfo
- Publication number
- DE602004025482D1 DE602004025482D1 DE602004025482T DE602004025482T DE602004025482D1 DE 602004025482 D1 DE602004025482 D1 DE 602004025482D1 DE 602004025482 T DE602004025482 T DE 602004025482T DE 602004025482 T DE602004025482 T DE 602004025482T DE 602004025482 D1 DE602004025482 D1 DE 602004025482D1
- Authority
- DE
- Germany
- Prior art keywords
- fiber composite
- flange
- male tool
- composite laminate
- contact
- 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
- B29C70/54—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 |
---|---|
DE602004025482D1 true DE602004025482D1 (de) | 2010-03-25 |
Family
ID=34927663
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602004025482T Active DE602004025482D1 (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 (40)
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 |
EP1775106B1 (de) * | 2005-10-17 | 2010-12-22 | Saab Ab | Verfahren zur Herstellung eines gekrümmten Gegenstands aus Verbundwerkstoff sowie durch dieses Verfahren hergestellter Gegenstand |
US10449736B2 (en) | 2006-02-02 | 2019-10-22 | The Boeing Company | Apparatus for fabricating thermoplastic composite parts |
US8491745B2 (en) | 2007-02-03 | 2013-07-23 | The Boeing Company | Method and material efficient tooling for continuous compression molding |
US8333858B2 (en) | 2006-02-02 | 2012-12-18 | The Boeing Company | Method for fabricating curved thermoplastic composite parts |
US7807005B2 (en) | 2006-02-02 | 2010-10-05 | The Boeing Company | Fabrication process for thermoplastic composite parts |
US10232532B1 (en) | 2006-02-02 | 2019-03-19 | The Boeing Company | Method for fabricating tapered 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 |
US8691137B2 (en) | 2009-03-04 | 2014-04-08 | The Boeing Company | Method of molding partus using a tool sleeve for mold die |
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 |
CN101910493B (zh) * | 2008-01-11 | 2013-07-24 | 东丽株式会社 | 弯曲形状强化纤维基材、及使用其的层合体、预成型体、纤维强化树脂复合材料和它们的制造方法 |
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. |
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 |
US9278484B2 (en) | 2008-04-17 | 2016-03-08 | The Boeing Company | Method and apparatus 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 |
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 |
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 |
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 |
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 |
US9314974B2 (en) | 2013-01-07 | 2016-04-19 | The Boeing Company | Method and apparatus for fabricating contoured laminate structures |
US10828846B2 (en) | 2013-01-07 | 2020-11-10 | The Boeing Company | Method and apparatus for fabricating contoured laminate structures |
US9782937B1 (en) | 2014-05-16 | 2017-10-10 | The Boeing Company | Apparatus for forming contoured composite laminates |
US10399284B2 (en) | 2014-05-16 | 2019-09-03 | The Boeing Company | Method and 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 |
CN110139742B (zh) * | 2017-03-17 | 2021-11-26 | 株式会社斯巴鲁 | 纤维材料的赋形装置和纤维材料的赋形方法 |
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 |
US11305498B2 (en) | 2018-12-21 | 2022-04-19 | The Boeing Company | System and method for fabricating a composite ply layup |
US11318689B2 (en) | 2018-12-21 | 2022-05-03 | The Boeing Company | Ply transporting and compacting apparatus and method therefor |
EP3822068B1 (de) * | 2019-11-13 | 2023-07-19 | Airbus Operations, S.L.U. | Vorrichtung und verfahren zur ausbildung eines verbundlaminats zur herstellung eines z-förmigen profils |
Family Cites Families (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
EP0082202B1 (de) * | 1981-06-30 | 1987-09-30 | The Boeing Company | Verfahren zur herstellung einer vorform aus faserverstärktem kompositmaterial |
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 |
US4576849A (en) * | 1983-06-06 | 1986-03-18 | Hercules Incorporated | Curved composite beam |
US4512835A (en) * | 1983-06-06 | 1985-04-23 | Hercules Incorporated | Method of making a 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 EP EP04028829A patent/EP1666353B1/de active Active
- 2004-12-06 ES ES04028829T patent/ES2338551T3/es active Active
- 2004-12-06 DE DE602004025482T patent/DE602004025482D1/de active Active
- 2004-12-06 AT AT04028829T patent/ATE457265T1/de not_active IP Right Cessation
-
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 |
---|---|
ATE457265T1 (de) | 2010-02-15 |
ES2338551T3 (es) | 2010-05-10 |
EP1666353A1 (de) | 2006-06-07 |
US20060216480A1 (en) | 2006-09-28 |
EP1666353B1 (de) | 2010-02-10 |
US8151529B2 (en) | 2012-04-10 |
US7670525B2 (en) | 2010-03-02 |
US20100148005A1 (en) | 2010-06-17 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE602004025482D1 (de) | Verfahren zur Herstellung eines gekrümmten Trägers aus Verbundwerkstoff | |
SE0102411L (sv) | Stamp med antividhäftningsskikt samt sätt att framställa och sätt att reparera en sådan stamp | |
WO2006119002A3 (en) | Method of manufacturing curved composite structural elements | |
ATE461025T1 (de) | Verfahren und vorrichtung zur herstellung einer rohrförmigen verbundstruktur | |
ATE316835T1 (de) | Verfahren zur herstellung eines formkörpers durch metallpulverschmelzverfahren | |
ATE545499T1 (de) | Verfahren zur herstellung eines beschichteten verbundproduktes | |
ATE473089T1 (de) | Verfahren zur herstellung einer dreidimensional geformten sandwichstruktur | |
DE60335354D1 (de) | Laminatfussbodenpaneel | |
ATE481232T1 (de) | Verfahren und vorrichtung zur herstellung einer felge | |
WO2006127291A3 (en) | Method for making a semiconductor device including a superlattice having at least one group of substantially undoped layers | |
DE69840845D1 (de) | Verfahren zur herstellung eines verstärkten fasersubstrats für einen verbundwerkstoff | |
ATE516938T1 (de) | Verfahren zur herstellung von bodenplatten und auf diese weise hergestellte bodenplatte | |
DE602006013107D1 (de) | Verfahren zur herstellung eines laminats aus polymerbändern sowie laminat und dessen verwendung | |
WO2008064985A3 (de) | Leichtbau-formteil und entsprechendes herstellungsverfahren | |
EA200800405A1 (ru) | Способ производства рулонного материала | |
ATE372208T1 (de) | Verfahren zur herstellung von dekorativem verbundschichtstoff | |
EP1262596A3 (de) | Blattbildungsvorrichtung und Verfahren zur Blattbildung | |
ATE136843T1 (de) | Verfahren zur herstellung eines gegenstandes aus thermoplastischem verbund-material | |
ATE389534T1 (de) | Thermoplastisches material, verfahren zur herstellung von orthopädischen vorrichtungen und daraus hergestellte orthopädische vorrichtungen | |
ATE503054T1 (de) | Bespannung für eine maschine zur herstellung von bahnmaterial und verfahren zur herstellung einer derartigen bespannung | |
DE502004004996D1 (de) | Verbundbauteil, sowie Verfahren zu dessen Herstellung | |
WO2007056664A3 (en) | Blow-molded composite compositions and methods | |
ATE340547T1 (de) | Verfahren zur herstellung einer elastischen verbundfolie | |
ATE556265T1 (de) | Verfahren zur herstellung von verbundrohren durch pultrusion und damit hergestellte rohre | |
SE0100232L (sv) | Metod för tillverkning av ett krökt sandwichelement och ett krökt sandwichelement |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |