ATE61970T1 - Schichtstoff aus metallschichten und aus durchgehendem faserverstaerktem synthetischem material. - Google Patents
Schichtstoff aus metallschichten und aus durchgehendem faserverstaerktem synthetischem material.Info
- Publication number
- ATE61970T1 ATE61970T1 AT88202179T AT88202179T ATE61970T1 AT E61970 T1 ATE61970 T1 AT E61970T1 AT 88202179 T AT88202179 T AT 88202179T AT 88202179 T AT88202179 T AT 88202179T AT E61970 T1 ATE61970 T1 AT E61970T1
- Authority
- AT
- Austria
- Prior art keywords
- poly
- laminate
- fiber reinforced
- metal layers
- synthetic material
- Prior art date
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
- B32B15/14—Layered products comprising a layer of metal next to 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
- B32B15/00—Layered products comprising a layer of metal
- B32B15/18—Layered products comprising a layer of metal comprising iron or steel
-
- 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
- B32B15/20—Layered products comprising a layer of metal comprising aluminium or copper
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/12—Construction or attachment of skin panels
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C13/00—Fibre or filament compositions
-
- 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
- B32B2260/02—Composition of the impregnated, bonded or embedded layer
- B32B2260/021—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
- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/51—Elastic
-
- 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
- B32B2307/00—Properties of the layers or laminate
- B32B2307/50—Properties of the layers or laminate having particular mechanical properties
- B32B2307/54—Yield strength; Tensile strength
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
-
- 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
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24942—Structurally defined web or sheet [e.g., overall dimension, etc.] including components having same physical characteristic in differing degree
- Y10T428/2495—Thickness [relative or absolute]
-
- 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
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31678—Of metal
-
- 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
- Y10T428/31504—Composite [nonstructural laminate]
- Y10T428/31678—Of metal
- Y10T428/31681—Next to polyester, polyamide or polyimide [e.g., alkyd, glue, or nylon, etc.]
-
- 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
- Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
- Y10T442/60—Nonwoven fabric [i.e., nonwoven strand or fiber material]
- Y10T442/654—Including a free metal or alloy constituent
- Y10T442/656—Preformed metallic film or foil or sheet [film or foil or sheet had structural integrity prior to association with the nonwoven fabric]
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- General Chemical & Material Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Materials Engineering (AREA)
- Organic Chemistry (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| NL8702453 | 1987-10-14 | ||
| EP88202179A EP0312151B1 (de) | 1987-10-14 | 1988-10-03 | Schichtstoff aus Metallschichten und aus durchgehendem faserverstärktem synthetischem Material |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE61970T1 true ATE61970T1 (de) | 1991-04-15 |
Family
ID=19850766
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT88202179T ATE61970T1 (de) | 1987-10-14 | 1988-10-03 | Schichtstoff aus metallschichten und aus durchgehendem faserverstaerktem synthetischem material. |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US5039571A (de) |
| EP (1) | EP0312151B1 (de) |
| JP (1) | JP2660563B2 (de) |
| AT (1) | ATE61970T1 (de) |
| CA (1) | CA1306936C (de) |
| DE (1) | DE3862185D1 (de) |
| ES (1) | ES2022602B3 (de) |
| GR (1) | GR3002178T3 (de) |
Families Citing this family (55)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5328744A (en) * | 1990-10-09 | 1994-07-12 | E. I. Du Pont De Nemours And Company | Panel having a core with thermoplastic resin facings |
| US5429326A (en) * | 1992-07-09 | 1995-07-04 | Structural Laminates Company | Spliced laminate for aircraft fuselage |
| US5906550A (en) * | 1993-10-18 | 1999-05-25 | Ticomp, Inc. | Sports bat having multilayered shell |
| US6194081B1 (en) | 1993-10-18 | 2001-02-27 | Ticomp. Inc. | Beta titanium-composite laminate |
| US5733390A (en) * | 1993-10-18 | 1998-03-31 | Ticomp, Inc. | Carbon-titanium composites |
| US5578384A (en) * | 1995-12-07 | 1996-11-26 | Ticomp, Inc. | Beta titanium-fiber reinforced composite laminates |
| US5547735A (en) * | 1994-10-26 | 1996-08-20 | Structural Laminates Company | Impact resistant laminate |
| JPH08309926A (ja) * | 1995-05-17 | 1996-11-26 | Nitto Boseki Co Ltd | 積層板材及びそれから作製した織機の綜絖枠 |
| US5866272A (en) * | 1996-01-11 | 1999-02-02 | The Boeing Company | Titanium-polymer hybrid laminates |
| US5700347A (en) * | 1996-01-11 | 1997-12-23 | The Boeing Company | Thermoplastic multi-tape application head |
| US5651850A (en) * | 1996-01-11 | 1997-07-29 | The Boeing Company | Method of fabricating hybrid composite structures |
| ES2186184T3 (es) | 1997-05-28 | 2003-05-01 | Structural Laminates Co | Procedimiento para realizar un laminado y laminado obtenido mediante dicho procedimiento. |
| US6039832A (en) * | 1998-02-27 | 2000-03-21 | The Boeing Company | Thermoplastic titanium honeycomb panel |
| AU4901201A (en) * | 1999-10-25 | 2001-07-03 | Rolls-Royce Corporation | Erosion-resistant coatings for organic matric composites |
| RU2185964C1 (ru) * | 2001-01-19 | 2002-07-27 | Государственное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" | Слоистый композиционный материал и изделие, выполненное из него |
| SE517953C2 (sv) * | 2001-03-30 | 2002-08-06 | Saab Ab | Metallkompositlaminat samt sätt att framställa detsamma |
| US6648273B2 (en) | 2001-10-30 | 2003-11-18 | The Boeing Company | Light weight and high strength fuselage |
| NL1019601C2 (nl) * | 2001-12-18 | 2003-06-30 | Fokker Aerostructures Bv | Werkwijze voor het vervaardigen van een laminaat alsmede gekromd product bestaande uit laminaat. |
| US6758924B1 (en) | 2002-04-15 | 2004-07-06 | The United States Of America As Represented By The Secretary Of The Air Force | Method of repairing cracked aircraft structures |
| RU2314202C2 (ru) * | 2002-07-04 | 2008-01-10 | Анатолий Федорович Крутин | Способ изготовления композиционных отсеков изделий |
| FR2844742B1 (fr) * | 2002-09-25 | 2005-04-29 | Pechiney Rhenalu | Feuilles composites stratifiees aluminium-fibres de verre |
| US7192501B2 (en) * | 2002-10-29 | 2007-03-20 | The Boeing Company | Method for improving crack resistance in fiber-metal-laminate structures |
| NL1022237C2 (nl) * | 2002-12-20 | 2004-07-01 | Stork Fokker Aesp Bv | Laminaat met stompgelaste metaallagen. |
| RU2238850C1 (ru) * | 2003-03-12 | 2004-10-27 | Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" | Слоистый композиционный материал и изделие, выполненное из него |
| DE10330341B4 (de) * | 2003-07-05 | 2005-09-15 | Airbus Deutschland Gmbh | Metallischer Schichtwerkstoff, verstärkt mit langen Basaltfasern sowie dessen Erzeugnisse |
| DE10360808B4 (de) * | 2003-12-19 | 2005-10-27 | Airbus Deutschland Gmbh | Faserverstärkter metallischer Verbundwerkstoff |
| US20050142968A1 (en) * | 2003-12-24 | 2005-06-30 | The Boeing Company | Translucent, flame resistant composite materials |
| RU2270098C1 (ru) * | 2004-07-14 | 2006-02-20 | Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") | Слоистый композиционный материал и изделие, выполненное из него |
| FR2876655B1 (fr) * | 2004-10-19 | 2008-05-30 | Faurecia Interieur Ind Snc | Traverse pour vehicule automobile, et vehicule automobile correspondant |
| US7255916B2 (en) | 2005-01-04 | 2007-08-14 | Airbus Deutschland Gmbh | Metallic layer material, reinforced with basalt fibers, as well as products made thereof |
| NL1030029C2 (nl) * | 2005-09-26 | 2007-03-27 | Gtm Consulting B V | Werkwijze en inrichting voor het verlijmen van componenten tot een samengesteld vormdeel. |
| NL1030066C2 (nl) * | 2005-09-29 | 2007-03-30 | Gtm Consulting B V | Werkwijze voor het vervaardigen van een vormdeel uit een samengesteld materiaal. |
| US20100043939A1 (en) * | 2006-05-15 | 2010-02-25 | Alcoa, Inc. | Reinforced Hybrid Structures and Methods Thereof |
| NL2000100C2 (nl) | 2006-06-13 | 2007-12-14 | Gtm Consulting B V | Laminaat uit metaalplaten en kunststof. |
| NL2000232C2 (nl) * | 2006-09-12 | 2008-03-13 | Gtm Consulting B V | Huidpaneel voor een vliegtuigromp. |
| US7690164B2 (en) * | 2006-12-05 | 2010-04-06 | Lockheed Martin Corporation | System, method, and apparatus for structural lug formed from a combination of metal and composite laminate materials |
| US20090211697A1 (en) * | 2007-05-15 | 2009-08-27 | Heinimann Markus B | Reinforced hybrid structures and methods thereof |
| EP2085215B1 (de) * | 2008-01-29 | 2013-03-27 | GTM Holding B.V. | Hochfeste Fasermetallbeschichtung |
| RU2381904C1 (ru) * | 2008-09-04 | 2010-02-20 | Валентин Александрович Жабрев | Слоистый композиционный материал |
| JP5392465B2 (ja) * | 2008-11-25 | 2014-01-22 | 住友電気工業株式会社 | マグネシウム合金部材 |
| CN102470627B (zh) * | 2009-07-31 | 2014-09-10 | 新日铁住金株式会社 | 层叠钢板 |
| ES2541631T3 (es) * | 2010-11-29 | 2015-07-22 | Gtm-Advanced Structures B.V. | Laminado de material compuesto reforzado fibra-lámina metálica |
| NL2007683C2 (en) | 2011-10-31 | 2013-05-06 | Gtm Advanced Products B V | Improved fiber-metal laminate. |
| WO2013124001A1 (en) | 2012-02-25 | 2013-08-29 | Adamco Ag | Self stabilizing halloysite aluminum metal matrix compound |
| WO2013127368A1 (zh) | 2012-03-02 | 2013-09-06 | 中航复合材料有限责任公司 | 一种含有植物纤维织物的复合材料及其制备方法 |
| CN102991009B (zh) * | 2012-11-16 | 2015-02-11 | 中国航空工业集团公司北京航空材料研究院 | 一种层间增韧的碳纤维-金属层合板 |
| KR101455834B1 (ko) * | 2013-04-01 | 2014-11-03 | 채경남 | 그래핀의 피에조 저항 특성을 이용한 스마트 복합재 |
| CN105522788B (zh) | 2014-11-24 | 2017-11-21 | 比亚迪股份有限公司 | 一种纤维金属层合板及其制备方法 |
| DE102015108307A1 (de) * | 2015-05-27 | 2016-12-01 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Werkstoffverbund |
| US11273622B2 (en) | 2016-12-14 | 2022-03-15 | The Boeing Company | Stiffening elements that comprise integral current flowpaths |
| US11014337B2 (en) | 2016-12-14 | 2021-05-25 | The Boeing Company | Laminate structures comprising fiber-reinforced thermoplastic prepreg plies |
| US11077644B2 (en) | 2016-12-14 | 2021-08-03 | The Boeing Company | Material systems and methods of manufacturing material systems |
| RU2641744C1 (ru) * | 2017-03-02 | 2018-01-22 | Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") | Слоистый гибридный композиционный материал и изделие, выполненное из него |
| US11584041B2 (en) * | 2018-04-20 | 2023-02-21 | Pella Corporation | Reinforced pultrusion member and method of making |
| US11371280B2 (en) | 2018-04-27 | 2022-06-28 | Pella Corporation | Modular frame design |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1357393A (fr) * | 1962-05-25 | 1964-04-03 | Owens Corning Fiberglass Corp | Compositions de verre à très haute résistance mécanique et à la température |
| JPS5045372U (de) * | 1973-08-22 | 1975-05-07 | ||
| US4110147A (en) * | 1976-03-24 | 1978-08-29 | Macdermid Incorporated | Process of preparing thermoset resin substrates to improve adherence of electrolessly plated metal deposits |
| JPS5498877U (de) * | 1977-12-26 | 1979-07-12 | ||
| ES487112A1 (es) * | 1978-12-22 | 1980-10-01 | Monsanto Co | Un procedimiento para la preparacion de un estratificado de metal-termoplastico-metal |
| 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. |
| NL8100087A (nl) * | 1981-01-09 | 1982-08-02 | Tech Hogeschool Delft Afdeling | Laminaat uit metalen platen en daarmede verbonden draden. |
| JPS6060797A (ja) * | 1983-09-13 | 1985-04-08 | 松下電工株式会社 | 積層板用ガラス布および積層板 |
| JPS621337A (ja) * | 1985-06-27 | 1987-01-07 | Meidensha Electric Mfg Co Ltd | デイジタル保護継電装置のデ−タ収集方法 |
| JPS629951A (ja) * | 1985-07-08 | 1987-01-17 | 新日本製鐵株式会社 | 成形性に優れたラミネ−ト鋼板 |
-
1988
- 1988-10-03 EP EP88202179A patent/EP0312151B1/de not_active Expired - Lifetime
- 1988-10-03 AT AT88202179T patent/ATE61970T1/de not_active IP Right Cessation
- 1988-10-03 ES ES88202179T patent/ES2022602B3/es not_active Expired - Lifetime
- 1988-10-03 DE DE8888202179T patent/DE3862185D1/de not_active Expired - Lifetime
- 1988-10-11 US US07/255,435 patent/US5039571A/en not_active Expired - Lifetime
- 1988-10-13 CA CA000580022A patent/CA1306936C/en not_active Expired - Lifetime
- 1988-10-14 JP JP63257432A patent/JP2660563B2/ja not_active Expired - Lifetime
-
1991
- 1991-06-25 GR GR91400862T patent/GR3002178T3/el unknown
Also Published As
| Publication number | Publication date |
|---|---|
| JPH01136736A (ja) | 1989-05-30 |
| CA1306936C (en) | 1992-09-01 |
| JP2660563B2 (ja) | 1997-10-08 |
| US5039571A (en) | 1991-08-13 |
| EP0312151B1 (de) | 1991-03-27 |
| ES2022602B3 (es) | 1991-12-01 |
| DE3862185D1 (de) | 1991-05-02 |
| GR3002178T3 (en) | 1992-12-30 |
| EP0312151A1 (de) | 1989-04-19 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| UEP | Publication of translation of european patent specification | ||
| EELA | Cancelled due to lapse of time |