ES2186184T3 - Procedimiento para realizar un laminado y laminado obtenido mediante dicho procedimiento. - Google Patents
Procedimiento para realizar un laminado y laminado obtenido mediante dicho procedimiento.Info
- Publication number
- ES2186184T3 ES2186184T3 ES98934904T ES98934904T ES2186184T3 ES 2186184 T3 ES2186184 T3 ES 2186184T3 ES 98934904 T ES98934904 T ES 98934904T ES 98934904 T ES98934904 T ES 98934904T ES 2186184 T3 ES2186184 T3 ES 2186184T3
- Authority
- ES
- Spain
- Prior art keywords
- metal sheet
- procedure
- rolling
- placing
- metal
- 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 - Lifetime
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B15/08—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/04—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B15/043—Layered products comprising a layer of metal comprising metal as the main or only constituent of a layer, which is next to another layer of the same or of a different material of metal
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/04—Layered products comprising a layer of synthetic resin as impregnant, bonding, or embedding substance
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/18—Layered products comprising a layer of synthetic resin characterised by the use of special additives
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
- B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
- B32B7/12—Interconnection of layers using interposed adhesives or interposed materials with bonding properties
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2250/00—Layers arrangement
- B32B2250/44—Number of layers variable across the laminate
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
- B32B2260/04—Impregnation, embedding, or binder material
- B32B2260/046—Synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/02—Synthetic macromolecular fibres
- B32B2262/0261—Polyamide fibres
- B32B2262/0269—Aromatic polyamide fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/101—Glass fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2262/00—Composition or structural features of fibres which form a fibrous or filamentary layer or are present as additives
- B32B2262/10—Inorganic fibres
- B32B2262/106—Carbon fibres, e.g. graphite fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B2605/00—Vehicles
- B32B2605/18—Aircraft
-
- 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
-
- 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
- Y10T156/1007—Running or continuous length work
- Y10T156/1008—Longitudinal bending
-
- 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
- Y10T156/1007—Running or continuous length work
- Y10T156/1008—Longitudinal bending
- Y10T156/101—Prior to or during assembly with 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
- Y10T156/10—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
- Y10T156/1007—Running or continuous length work
- Y10T156/1008—Longitudinal bending
- Y10T156/1011—Overedge bending or overedge folding
-
- 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
- Y10T156/1007—Running or continuous length work
- Y10T156/1023—Surface deformation only [e.g., embossing]
Landscapes
- Laminated Bodies (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Abstract
Procedimiento para realizar un laminado que consta de los siguientes pasos: - Colocar una primera capa de metal sobre una herramienta de moldeo o un sustrato, colocar una capa de adhesivo sobre la primera capa de metal, - Colocar una segunda capa de metal sobre la capa de adhesivo de tal manera que al menos una de las capas de metal solape al menos un borde de la otra capa de metal, aplicar calor y presión a la pila obtenida de este modo, caracterizado porque durante la aplicación de presión al menos una de las capas de metal se pliega hacia el plano de la otra capa de metal tras lo cual se fija la forma de las capas de metal.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP97201565 | 1997-05-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2186184T3 true ES2186184T3 (es) | 2003-05-01 |
Family
ID=8228358
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES98934904T Expired - Lifetime ES2186184T3 (es) | 1997-05-28 | 1998-05-22 | Procedimiento para realizar un laminado y laminado obtenido mediante dicho procedimiento. |
Country Status (8)
Country | Link |
---|---|
US (1) | US6736919B1 (es) |
EP (1) | EP0983141B1 (es) |
JP (1) | JP4262782B2 (es) |
AT (1) | ATE226512T1 (es) |
AU (1) | AU8435298A (es) |
DE (1) | DE69808903T2 (es) |
ES (1) | ES2186184T3 (es) |
WO (1) | WO1998053989A1 (es) |
Families Citing this family (51)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050154567A1 (en) * | 1999-06-18 | 2005-07-14 | President And Fellows Of Harvard College | Three-dimensional microstructures |
CA2396570A1 (en) | 2000-01-07 | 2001-07-19 | President And Fellows Of Harvard College | Fabrication of metallic microstructures via exposure of photosensitive composition |
NL1015141C2 (nl) * | 2000-05-09 | 2001-11-13 | Fokker Aerostructures Bv | Verbindingsconstructie in een laminaat uit metalen en kunststof lagen. |
NL1018120C2 (nl) * | 2001-05-21 | 2002-12-03 | Fokker Aerostructures Bv | Werkwijze voor het vervaardigen van een gevormd laminaat. |
NL1019574C2 (nl) * | 2001-12-14 | 2003-06-17 | Stichting Fmlc | Metaalvezellaminaatsamenstel ingericht voor het weerstaan van een het samenstel vervormende locale impact. |
NL1019957C2 (nl) | 2002-02-13 | 2003-10-03 | Stork Fokker Aesp Bv | Gelamineerd paneel met discontinue inwendige laag. |
DE10238460B3 (de) * | 2002-08-22 | 2004-03-11 | Airbus Deutschland Gmbh | Leichtbaustruktur aus dünnen Metallblechlagen |
FR2844742B1 (fr) * | 2002-09-25 | 2005-04-29 | Pechiney Rhenalu | Feuilles composites stratifiees aluminium-fibres de verre |
NL1023811C2 (nl) * | 2003-07-03 | 2005-01-04 | Stork Fokker Aesp Bv | Laminaat met plaatselijke versterking. |
EP1495858B1 (de) | 2003-07-08 | 2019-08-07 | Airbus Operations GmbH | Leichtbaustruktur aus metallischen schichtwerkstoffen |
NL1023854C2 (nl) * | 2003-07-08 | 2005-01-11 | Stork Fokker Aesp Bv | Laminaat met vullaag. |
DE502004007968D1 (de) | 2003-07-08 | 2008-10-16 | Airbus Gmbh | Leichtbaustruktur |
NL1024076C2 (nl) | 2003-08-08 | 2005-02-10 | Stork Fokker Aesp Bv | Werkwijze voor het vormen van een laminaat met een uitsparing. |
NL1024077C2 (nl) | 2003-08-08 | 2005-02-10 | Stork Fokker Aesp Bv | Werkwijze voor het vervaardigen van een laminaat met onderling versprongen lagen. |
NL1024479C2 (nl) * | 2003-10-07 | 2005-04-08 | Stork Fokker Aesp Bv | Verbindingsconstructie in een laminaat met een plaatselijke versterking. |
US20050175813A1 (en) * | 2004-02-10 | 2005-08-11 | Wingert A. L. | Aluminum-fiber laminate |
DK200401225A (da) * | 2004-08-13 | 2006-02-14 | Lm Glasfiber As | Metode til afskæring af laminatlag, eksempelvis et glasfiber- eller kulfiber-laminatlag i en vindmöllevinge |
NL1029088C2 (nl) * | 2005-05-20 | 2006-11-21 | Netherlands Inst For Metals Re | Vezel-metaal laminaten en constructies voorzien daarvan. |
NL2000100C2 (nl) | 2006-06-13 | 2007-12-14 | Gtm Consulting B V | Laminaat uit metaalplaten en kunststof. |
DE102006031436B4 (de) * | 2006-07-07 | 2012-12-06 | Airbus Operations Gmbh | Strukturelement, Verfahren zur Herstellung eines derartigen Strukturelements und Flugzeug mit einem derartigen Strukturelement |
NL2000232C2 (nl) * | 2006-09-12 | 2008-03-13 | Gtm Consulting B V | Huidpaneel voor een vliegtuigromp. |
DE102007018753B4 (de) * | 2007-04-20 | 2012-11-08 | Airbus Operations Gmbh | Brandschutzraum für Flugzeugpassagiere mit Hilfe von Rumpfbehäutung aus Faser-Metall-Laminaten |
DE102007019716A1 (de) * | 2007-04-26 | 2008-10-30 | Airbus Deutschland Gmbh | Faser-Metall-Laminat-Panel |
DE102007063608B4 (de) * | 2007-05-23 | 2011-04-21 | Airbus Operations Gmbh | Verbund und Rumpfzellenabschnitt mit einem derartigen Verbund |
DE102007046478B4 (de) * | 2007-05-23 | 2012-08-02 | Airbus Operations Gmbh | Blechlaminat, insbesondere für Rumpfhautbleche für Flugzeuge |
DE102007025818A1 (de) * | 2007-06-02 | 2008-12-04 | Voith Patent Gmbh | Blechformbaueinheit, insbesondere Gehäuse oder Verkleidung für Maschinen und Anlagen, Verfahren zur Fertigung derartiger Blechformbaueinheiten und Verwendung in Gehäusen oder Verkleidungen von Papiermaschinen |
DE102008010228A1 (de) * | 2008-02-21 | 2009-09-03 | Airbus Deutschland Gmbh | Verfahren und Vorrichtung zur Herstellung faserverstärkter Kunststoffprofilteile |
GB0805268D0 (en) * | 2008-03-25 | 2008-04-30 | Airbus Uk Ltd | Composite joint protection |
FR2932106B1 (fr) * | 2008-06-06 | 2010-05-21 | Airbus France | Procede de depose d'un revetement visant a ameliorer l'ecoulement laminaire |
EP2177352A1 (de) * | 2008-10-08 | 2010-04-21 | Hydro Aluminium Deutschland GmbH | Verbundwerkstoff für die Schall- und Wärmeisolation sowie Verfahren zu dessen Herstellung |
US8282042B2 (en) | 2009-06-22 | 2012-10-09 | The Boeing Company | Skin panel joint for improved airflow |
US9821538B1 (en) * | 2009-06-22 | 2017-11-21 | The Boeing Company | Ribbed caul plate for attaching a strip to a panel structure and method for use |
US20110143081A1 (en) * | 2010-06-29 | 2011-06-16 | General Electric Company | Modified ply drops for composite laminate materials |
US20110143082A1 (en) * | 2010-06-29 | 2011-06-16 | General Electric Company | Ply drops modifications for composite laminate materials and related methods |
US9522512B2 (en) * | 2010-08-17 | 2016-12-20 | The Boeing Company | Methods for making composite structures having composite-to-metal joints |
US8652606B2 (en) * | 2010-08-17 | 2014-02-18 | The Boeing Company | Composite structures having composite-to-metal joints and method for making the same |
US8993084B2 (en) | 2010-08-17 | 2015-03-31 | The Boeing Company | Multi-layer metallic structure and composite-to-metal joint methods |
CA2862610A1 (en) * | 2011-02-21 | 2012-08-30 | Productive Research Llc | Composite materials including regions differing in properties and methods |
NL2007603C2 (en) * | 2011-10-14 | 2013-04-16 | Univ Delft Tech | Fiber metal laminate. |
US9233526B2 (en) | 2012-08-03 | 2016-01-12 | Productive Research Llc | Composites having improved interlayer adhesion and methods thereof |
US9302349B2 (en) | 2012-10-31 | 2016-04-05 | Productive Research Llc | Edge joint of light weight composites |
WO2015060837A1 (en) * | 2013-10-23 | 2015-04-30 | Hewlett-Packard Development Company, L.P. | Multi-layered metal |
EP2907654B1 (en) | 2014-02-13 | 2024-06-26 | Airbus Operations GmbH | Joints in fibre metal laminates |
NL2012458B1 (en) * | 2014-03-17 | 2016-01-08 | Gtm-Advanced Products B V | Laminate of mutually bonded adhesive layers and metal sheets, and method to obtain such laminate. |
NL2012692B1 (nl) | 2014-04-25 | 2016-07-18 | Fokker Aerostructures Bv | Paneel uit laminaten, alsmede werkwijze voor het vervaardigen daarvan. |
CN104015917A (zh) * | 2014-06-16 | 2014-09-03 | 上海飞机制造有限公司 | 一种用作飞机壁板的纤维铝锂合金层板及其制备方法 |
NL2015437B1 (en) | 2015-09-15 | 2017-04-03 | Gtm-Advanced Products B V | Laminate of mutually bonded adhesive layers and metal sheets, and method to obtain such laminate. |
GB2545655A (en) | 2015-12-18 | 2017-06-28 | Airbus Operations Ltd | A structure formed from composite material |
DE102016012691A1 (de) * | 2016-10-25 | 2018-04-26 | Hydro Aluminium Rolled Products Gmbh | Mehrschichtiges Strukturbauteil, Verfahren zu dessen Herstellung und Verwendungen dafür |
NL2017850B1 (en) | 2016-11-23 | 2018-05-28 | Gtm Advanced Products B V | Laminate of mutually bonded adhesive layers and spliced metal sheets |
EP4283095A1 (en) | 2022-05-27 | 2023-11-29 | RTX Corporation | Cmc laminate airfoil with ply drops |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL8100087A (nl) | 1981-01-09 | 1982-08-02 | Tech Hogeschool Delft Afdeling | Laminaat uit metalen platen en daarmede verbonden draden. |
NL8100088A (nl) | 1981-01-09 | 1982-08-02 | Tech Hogeschool Delft Afdeling | Laminaat uit metalen platen en daarmede verbonden draden, alsmede werkwijzen ter vervaardiging daarvan. |
EP0312151B1 (en) | 1987-10-14 | 1991-03-27 | Akzo N.V. | Laminate of metal sheets and continuous glass filaments-reinforced synthetic material |
EP0312150B1 (en) | 1987-10-14 | 1992-12-02 | Structural Laminates Company | Laminate of metal sheets and continuous filaments-reinforced thermoplastic synthetic material, as well as a process for the manufacture of such a laminate |
GB9103804D0 (en) | 1991-02-23 | 1991-04-10 | British Aerospace | Improvements relating to diffusion bonded/superplastically formed cellular structures |
US5429326A (en) * | 1992-07-09 | 1995-07-04 | Structural Laminates Company | Spliced laminate for aircraft fuselage |
US5567535A (en) * | 1992-11-18 | 1996-10-22 | Mcdonnell Douglas Corporation | Fiber/metal laminate splice |
US5547735A (en) | 1994-10-26 | 1996-08-20 | Structural Laminates Company | Impact resistant laminate |
-
1998
- 1998-05-22 DE DE69808903T patent/DE69808903T2/de not_active Expired - Lifetime
- 1998-05-22 JP JP50024999A patent/JP4262782B2/ja not_active Expired - Fee Related
- 1998-05-22 ES ES98934904T patent/ES2186184T3/es not_active Expired - Lifetime
- 1998-05-22 AT AT98934904T patent/ATE226512T1/de not_active IP Right Cessation
- 1998-05-22 US US09/424,598 patent/US6736919B1/en not_active Expired - Lifetime
- 1998-05-22 EP EP19980934904 patent/EP0983141B1/en not_active Expired - Lifetime
- 1998-05-22 WO PCT/EP1998/003173 patent/WO1998053989A1/en active IP Right Grant
- 1998-05-22 AU AU84352/98A patent/AU8435298A/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
DE69808903T2 (de) | 2003-08-07 |
JP4262782B2 (ja) | 2009-05-13 |
US6736919B1 (en) | 2004-05-18 |
EP0983141B1 (en) | 2002-10-23 |
EP0983141A1 (en) | 2000-03-08 |
JP2001526601A (ja) | 2001-12-18 |
AU8435298A (en) | 1998-12-30 |
WO1998053989A1 (en) | 1998-12-03 |
ATE226512T1 (de) | 2002-11-15 |
DE69808903D1 (de) | 2002-11-28 |
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