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RU2002132877A - UNITED DESIGN IN LAMINATED MATERIAL FROM METAL AND PLASTIC LAYERS - Google Patents

UNITED DESIGN IN LAMINATED MATERIAL FROM METAL AND PLASTIC LAYERS

Info

Publication number
RU2002132877A
RU2002132877A RU2002132877/02A RU2002132877A RU2002132877A RU 2002132877 A RU2002132877 A RU 2002132877A RU 2002132877/02 A RU2002132877/02 A RU 2002132877/02A RU 2002132877 A RU2002132877 A RU 2002132877A RU 2002132877 A RU2002132877 A RU 2002132877A
Authority
RU
Russia
Prior art keywords
metal
sections
overlay
laminated material
metal layer
Prior art date
Application number
RU2002132877/02A
Other languages
Russian (ru)
Other versions
RU2268820C2 (en
Inventor
Герардус Хюбертус Йоаннес Йозеф РУБРУКС
Original Assignee
Фоккер Эйростракчерс Б.В.
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from NL1015141A external-priority patent/NL1015141C2/en
Application filed by Фоккер Эйростракчерс Б.В. filed Critical Фоккер Эйростракчерс Б.В.
Publication of RU2002132877A publication Critical patent/RU2002132877A/en
Application granted granted Critical
Publication of RU2268820C2 publication Critical patent/RU2268820C2/en

Links

Claims (5)

1. Соединенная конструкция в слоистом материале из расположенных попеременно, по меньшей мере, двух металлических слоев (1-3) и, по меньшей мере, одного пластмассового слоя (6, 7), заключенного между ними, при этом каждый из металлических слоев (1-3) содержит, по меньшей мере, два участка (4’, 5’; 4’’, 5’’; 4’’’, 5’’’), а два участка (4’, 5’), по меньшей мере, одного внешнего металлического слоя (1) наложены друг на друга (8-10), причем эти два участка (4’, 5’) прикреплены друг к другу на местоположении наложения (8) посредством клея (6), отличающаяся тем, что каждый металлический слой (1-3) имеет наложенные друг на друга участки (4’, 5’; 4’’, 5’’; 4’’’, 5’’’), которые прикреплены друг к другу клеем (6).1. The connected structure in the layered material from alternately arranged at least two metal layers (1-3) and at least one plastic layer (6, 7), enclosed between them, with each of the metal layers (1 -3) contains at least two sections (4 ', 5'; 4 '', 5``; 4 '' ', 5' ''), and two sections (4 ', 5'), at least of at least one outer metal layer (1) are superimposed on each other (8-10), and these two sections (4 ', 5') are attached to each other at the location of the overlay (8) by means of glue (6), characterized in that ka Each metal layer (1-3) has overlapping sections (4 ’, 5’; 4 ’’, 5 ’’; 4 ’’ ’, 5’ ’’) that are glued to each other (6). 2. Конструкция по п.1, отличающаяся тем, что наложение (8) между двумя участками (4’, 5’) металлического слоя (1) смещено относительно наложения (9, 10) между двумя участками (4’’, 5’’; 4’’’, 5’’’) другого металлического слоя (2, 3).2. The construction according to claim 1, characterized in that the overlay (8) between the two sections (4 ', 5') of the metal layer (1) is offset from the overlay (9, 10) between the two sections (4 '', 5 '' ; 4 '' ', 5' '') of another metal layer (2, 3). 3. Конструкция по любому из пп.1 и 2, отличающаяся тем, что в каждом металлическом слое (1, 3) один участок (5’, 5’’, 5’’’) прямой, а другой участок (4’, 4’’, 4’’’) отогнут.3. Design according to any one of claims 1 and 2, characterized in that in each metal layer (1, 3) one section (5 ', 5``, 5' '') is straight and the other section (4 ', 4 ``, 4 '' ') is bent. 4. Конструкция по любому из пп.1-3, отличающаяся тем, что каждый пластмассовый слой (7, 8) отогнут на местоположении наложения (8, 10).4. Design according to any one of claims 1 to 3, characterized in that each plastic layer (7, 8) is bent at the location of the overlay (8, 10). 5. Конструкция по любому из пп.1-4, отличающаяся тем, что каждый пластмассовый слой (7, 8) является непрерывным на местоположении наложения (8, 10).5. Design according to any one of claims 1 to 4, characterized in that each plastic layer (7, 8) is continuous at the overlay location (8, 10).
RU2002132877/02A 2000-05-09 2001-05-09 Connected structure in sandwich material consisting of metal and plastic layers RU2268820C2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
NL1015141A NL1015141C2 (en) 2000-05-09 2000-05-09 Connecting construction in a laminate of metal and plastic layers.
NL1015141 2000-05-09

Publications (2)

Publication Number Publication Date
RU2002132877A true RU2002132877A (en) 2004-06-27
RU2268820C2 RU2268820C2 (en) 2006-01-27

Family

ID=19771340

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2002132877/02A RU2268820C2 (en) 2000-05-09 2001-05-09 Connected structure in sandwich material consisting of metal and plastic layers

Country Status (12)

Country Link
US (2) US20040013826A1 (en)
EP (1) EP1296822B1 (en)
JP (1) JP4986371B2 (en)
KR (1) KR20030005323A (en)
CN (1) CN1236911C (en)
AT (1) ATE367917T1 (en)
BR (1) BR0110644B1 (en)
CA (1) CA2407406C (en)
DE (1) DE60129560T2 (en)
NL (1) NL1015141C2 (en)
RU (1) RU2268820C2 (en)
WO (1) WO2002078950A1 (en)

Families Citing this family (15)

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Publication number Priority date Publication date Assignee Title
NL1019957C2 (en) * 2002-02-13 2003-10-03 Stork Fokker Aesp Bv Laminated panel with discontinuous inner layer.
NL1023811C2 (en) * 2003-07-03 2005-01-04 Stork Fokker Aesp Bv Laminate with local reinforcement.
NL1023854C2 (en) * 2003-07-08 2005-01-11 Stork Fokker Aesp Bv Laminate with filling layer.
NL1024479C2 (en) * 2003-10-07 2005-04-08 Stork Fokker Aesp Bv Connection construction in a laminate with a local reinforcement.
DE102007003357A1 (en) * 2007-01-17 2008-07-24 Airbus Deutschland Gmbh Method for bonding a thermoplastic material to a fiber composite material
DE102007019716A1 (en) * 2007-04-26 2008-10-30 Airbus Deutschland Gmbh Fiber metal laminate panel
DE102007036510B3 (en) * 2007-08-01 2009-01-02 Deutsches Zentrum für Luft- und Raumfahrt e.V. Composite material for optimized high-strength coupling of stringer to aerofoil of aircraft, has intermediate layer exhibiting small rigidity than adjacent non-continuous fiber composite layer and reinforcement material layer
DE102008007545A1 (en) * 2008-02-05 2009-08-27 Airbus Deutschland Gmbh Load-bearing and damage tolerant laminate airplane window
US20090235604A1 (en) * 2008-03-20 2009-09-24 Xxentria Technology Materials Co., Ltd Architectural material
DE102009009491A1 (en) * 2009-02-18 2010-09-09 Airbus Deutschland Gmbh Method for producing a shell body
EP2907654B1 (en) * 2014-02-13 2024-06-26 Airbus Operations GmbH Joints in fibre metal laminates
NL2012692B1 (en) * 2014-04-25 2016-07-18 Fokker Aerostructures Bv Panel from laminates, as well as method for manufacturing them.
RU2570469C1 (en) * 2014-09-10 2015-12-10 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") Method for glass laminate aluminium reinforced epoxy junction
RU2618072C1 (en) * 2015-11-05 2017-05-02 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") Method for producing laminated metal fiberglass
CN107323022B (en) * 2017-07-24 2020-03-06 北京汽车集团有限公司 Adhesive joint structure of composite material and metal material and preparation method thereof

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS60120047A (en) * 1983-12-01 1985-06-27 マツダ株式会社 Method of joining composite board
JPS63231932A (en) * 1987-03-20 1988-09-28 株式会社神戸製鋼所 Metal laminated plate
DE3876371T2 (en) * 1987-10-14 1993-05-13 Structural Laminates Co LAMINATE FROM METAL LAYERS AND FROM CONTINUOUS, FIBER REINFORCED, SYNTHETIC, THERMOPLASTIC MATERIAL AND METHOD FOR THE PRODUCTION THEREOF.
US5160771A (en) * 1990-09-27 1992-11-03 Structural Laminates Company Joining metal-polymer-metal laminate sections
DE4301564A1 (en) * 1993-01-21 1994-07-28 Emitec Emissionstechnologie Electrically insulating support structure with the possibility of a metallic connection, process for its production and its application
JP4262782B2 (en) * 1997-05-28 2009-05-13 ストラクチユアル・ラミネイツ・カンパニー LAMINATE MANUFACTURING METHOD AND LAMINATE OBTAINED BY THE METHOD

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