BRPI0415086A - estrutura de união em um laminado - Google Patents

estrutura de união em um laminado

Info

Publication number
BRPI0415086A
BRPI0415086A BRPI0415086-4A BRPI0415086A BRPI0415086A BR PI0415086 A BRPI0415086 A BR PI0415086A BR PI0415086 A BRPI0415086 A BR PI0415086A BR PI0415086 A BRPI0415086 A BR PI0415086A
Authority
BR
Brazil
Prior art keywords
metal layers
laminate
edges
pair
joining structure
Prior art date
Application number
BRPI0415086-4A
Other languages
English (en)
Inventor
Abdoel Faziel Rajabali
Willem Jan Nicolaas Ter Steeg
Original Assignee
Stork Fokker Aesp Bv
Airbus Gmbh
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
Application filed by Stork Fokker Aesp Bv, Airbus Gmbh filed Critical Stork Fokker Aesp Bv
Publication of BRPI0415086A publication Critical patent/BRPI0415086A/pt
Publication of BRPI0415086B1 publication Critical patent/BRPI0415086B1/pt

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
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • 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
    • B29C70/88—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
    • B29C70/882—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding
    • B29C70/885—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding with incorporated metallic wires, nets, films or plates
    • 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
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/02—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions
    • B32B3/08—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions characterised by added members at particular parts
    • 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
    • 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
    • Y10T428/12—All metal or with adjacent metals
    • Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12535—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.] with additional, spatially distinct nonmetal component
    • Y10T428/12556—Organic component
    • 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
    • Y10T428/19—Sheets or webs edge spliced or joined
    • 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.]
    • Y10T428/24777—Edge feature

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
  • Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)

Abstract

"ESTRUTURA DE UNIãO EM UM LAMINADO". é descrita uma estrutura de união em um laminado que compreende camadas de metal bem como pelo menos uma camada adesiva que é encerrada pelas camadas de metal, camadas de metal estas que compreendem cada qual partes de camadas de metal separadas que têm um par de bordas sobrepostas, pares de bordas estes que são deslocados uns em relação aos outros e que juntos definem uma região de união. O laminado compreende uma seção que é de construção padrão e uma seção que contém uma camada de metal de reforço interna adicional, a dita camada de metal de reforço compreendendo duas partes de camadas de metal de reforço com um par de bordas sobrepostas, o dito par de bordas sendo localizado fora da região da união.
BRPI0415086-4A 2003-10-07 2004-10-05 Estrutura de união em um laminado BRPI0415086B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
NL1024479A NL1024479C2 (nl) 2003-10-07 2003-10-07 Verbindingsconstructie in een laminaat met een plaatselijke versterking.
NL1024479 2003-10-07
PCT/NL2004/000700 WO2005032805A1 (en) 2003-10-07 2004-10-05 Joining structure in a laminate comprising a local reinforcement

Publications (2)

Publication Number Publication Date
BRPI0415086A true BRPI0415086A (pt) 2006-12-26
BRPI0415086B1 BRPI0415086B1 (pt) 2014-06-17

Family

ID=34420822

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0415086-4A BRPI0415086B1 (pt) 2003-10-07 2004-10-05 Estrutura de união em um laminado

Country Status (10)

Country Link
US (1) US7560152B2 (pt)
EP (1) EP1670633B1 (pt)
JP (1) JP4938455B2 (pt)
CN (1) CN100540280C (pt)
BR (1) BRPI0415086B1 (pt)
CA (1) CA2541820C (pt)
DE (1) DE602004027060D1 (pt)
NL (1) NL1024479C2 (pt)
RU (1) RU2358877C2 (pt)
WO (1) WO2005032805A1 (pt)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006031436B4 (de) * 2006-07-07 2012-12-06 Airbus Operations Gmbh Strukturelement, Verfahren zur Herstellung eines derartigen Strukturelements und Flugzeug mit einem derartigen Strukturelement
DE102007019716A1 (de) * 2007-04-26 2008-10-30 Airbus Deutschland Gmbh Faser-Metall-Laminat-Panel
FR2922516B1 (fr) * 2007-10-18 2010-04-16 Airbus France Eclissage de raidisseurs en omega au niveau d'une jonction circonferentielle d'un fuselage d'avion
DE102008010228A1 (de) * 2008-02-21 2009-09-03 Airbus Deutschland Gmbh Verfahren und Vorrichtung zur Herstellung faserverstärkter Kunststoffprofilteile
US8220745B2 (en) * 2008-04-14 2012-07-17 Airbus Deutschland Gmbh Connection arrangement for connecting a first and second reinforcing element for an aircraft or spacecraft, and a shell component
US8857128B2 (en) * 2009-05-18 2014-10-14 Apple Inc. Reinforced device housing
US8372495B2 (en) 2010-05-26 2013-02-12 Apple Inc. Electronic device enclosure using sandwich construction
US9120272B2 (en) 2010-07-22 2015-09-01 Apple Inc. Smooth composite structure
US8333345B2 (en) * 2010-08-26 2012-12-18 The Boeing Company Composite aircraft joint
US9011623B2 (en) 2011-03-03 2015-04-21 Apple Inc. Composite enclosure
DE102011108167B4 (de) * 2011-07-20 2014-02-13 Airbus Operations Gmbh Fenstertrichter sowie Fensterbereich für ein Flugzeug
US10407955B2 (en) 2013-03-13 2019-09-10 Apple Inc. Stiff fabric
CN204608330U (zh) 2013-12-20 2015-09-02 苹果公司 编织纤维带
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.
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
NL2017850B1 (en) 2016-11-23 2018-05-28 Gtm Advanced Products B V Laminate of mutually bonded adhesive layers and spliced metal sheets
US10864686B2 (en) 2017-09-25 2020-12-15 Apple Inc. Continuous carbon fiber winding for thin structural ribs
JP2020064488A (ja) * 2018-10-18 2020-04-23 レノボ・シンガポール・プライベート・リミテッド 筐体用部材及び電子機器

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5160771A (en) * 1990-09-27 1992-11-03 Structural Laminates Company Joining metal-polymer-metal laminate sections
GB9107766D0 (en) * 1991-04-12 1991-06-05 Short Brothers Plc A structural component
RU2027555C1 (ru) * 1991-07-17 1995-01-27 Точилин Евгений Афанасьевич Многослойный композиционный материал и способ его изготовления
US6736919B1 (en) * 1997-05-28 2004-05-18 Structural Laminates Company Method for making a laminate and laminate obtainable by said method
NL1015141C2 (nl) * 2000-05-09 2001-11-13 Fokker Aerostructures Bv Verbindingsconstructie in een laminaat uit metalen en kunststof lagen.
NL1023854C2 (nl) * 2003-07-08 2005-01-11 Stork Fokker Aesp Bv Laminaat met vullaag.

Also Published As

Publication number Publication date
WO2005032805A1 (en) 2005-04-14
NL1024479C2 (nl) 2005-04-08
CA2541820A1 (en) 2005-04-14
EP1670633B1 (en) 2010-05-05
DE602004027060D1 (de) 2010-06-17
CN100540280C (zh) 2009-09-16
JP2007507373A (ja) 2007-03-29
BRPI0415086B1 (pt) 2014-06-17
JP4938455B2 (ja) 2012-05-23
US7560152B2 (en) 2009-07-14
RU2006115617A (ru) 2007-11-20
CN1863668A (zh) 2006-11-15
EP1670633A1 (en) 2006-06-21
CA2541820C (en) 2012-12-04
US20070042214A1 (en) 2007-02-22
RU2358877C2 (ru) 2009-06-20

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Legal Events

Date Code Title Description
B25D Requested change of name of applicant approved

Owner name: AIRBUS DEUTSCHLAND GMBH (DE) , FOKKER AEROSTRUCTUR

Free format text: NOME ALTERADO DE: STORK FOKKER AESP B.V.

B25D Requested change of name of applicant approved

Owner name: FOKKER AEROSTRUCTURES B.V. (NL) , AIRBUS OPERATION

Free format text: NOME ALTERADO DE: AIRBUS DEUTSCHLAND GMBH

B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 05/10/2004, OBSERVADAS AS CONDICOES LEGAIS.

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 15A ANUIDADE.

B24D Patent annual fee: restoration after fee payment
B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 16A ANUIDADE.

B24D Patent annual fee: restoration after fee payment
B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 17A ANUIDADE.

B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)

Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2640 DE 10-08-2021 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.