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FR2869655B1 - Procede d'assemblage de pieces structurales et assemblage obtenu. - Google Patents

Procede d'assemblage de pieces structurales et assemblage obtenu.

Info

Publication number
FR2869655B1
FR2869655B1 FR0404495A FR0404495A FR2869655B1 FR 2869655 B1 FR2869655 B1 FR 2869655B1 FR 0404495 A FR0404495 A FR 0404495A FR 0404495 A FR0404495 A FR 0404495A FR 2869655 B1 FR2869655 B1 FR 2869655B1
Authority
FR
France
Prior art keywords
structural parts
assembly obtained
assembling structural
assembling
assembly
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 - Fee Related
Application number
FR0404495A
Other languages
English (en)
Other versions
FR2869655A1 (fr
Inventor
Maurice Prat
Gerard Navas
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR0404495A priority Critical patent/FR2869655B1/fr
Priority to US11/111,926 priority patent/US20050244215A1/en
Publication of FR2869655A1 publication Critical patent/FR2869655A1/fr
Application granted granted Critical
Publication of FR2869655B1 publication Critical patent/FR2869655B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B11/00Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding
    • F16B11/006Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00Joints and connections
    • Y10T403/47Molded joint
    • Y10T403/473Socket or open cup for bonding material

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
FR0404495A 2004-04-28 2004-04-28 Procede d'assemblage de pieces structurales et assemblage obtenu. Expired - Fee Related FR2869655B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0404495A FR2869655B1 (fr) 2004-04-28 2004-04-28 Procede d'assemblage de pieces structurales et assemblage obtenu.
US11/111,926 US20050244215A1 (en) 2004-04-28 2005-04-22 Assembly of structural parts

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0404495A FR2869655B1 (fr) 2004-04-28 2004-04-28 Procede d'assemblage de pieces structurales et assemblage obtenu.

Publications (2)

Publication Number Publication Date
FR2869655A1 FR2869655A1 (fr) 2005-11-04
FR2869655B1 true FR2869655B1 (fr) 2008-12-19

Family

ID=34946279

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0404495A Expired - Fee Related FR2869655B1 (fr) 2004-04-28 2004-04-28 Procede d'assemblage de pieces structurales et assemblage obtenu.

Country Status (2)

Country Link
US (1) US20050244215A1 (fr)
FR (1) FR2869655B1 (fr)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050199158A1 (en) * 2005-05-18 2005-09-15 Satco, Inc. Reinforced air cargo pallet
US8002332B2 (en) 2007-01-30 2011-08-23 Zephyros, Inc. Structural mounting insert
US8181327B2 (en) 2008-02-08 2012-05-22 Zephyros, Inc Mechanical method for improving bond joint strength
US9194408B2 (en) 2008-02-08 2015-11-24 Zephyros, Inc. Mechanical method for improving bond joint strength
GB0819159D0 (en) 2008-10-20 2008-11-26 Airbus Uk Ltd Joint between aircraft components
US7984919B2 (en) 2009-05-18 2011-07-26 Zephyros, Inc. Structural mounting insert having a non-conductive isolator
CA2736656C (fr) 2010-04-11 2019-03-05 Norduyn Inc. Mecanisme de fixation de pieces et methode d'utilisation
KR101830300B1 (ko) * 2010-12-30 2018-03-30 삼성디스플레이 주식회사 유기 발광 표시 장치 및 그 제조 방법
DE102012023717A1 (de) * 2012-12-05 2014-06-05 Eads Deutschland Gmbh Indikationsbolzen zur Überwachung von Klebeverbindungen in Strukturbauteilen
GB201318595D0 (en) 2013-10-21 2013-12-04 Zephyros Inc Improvements in or relating to laminates
CN109454957A (zh) 2013-12-17 2019-03-12 泽菲罗斯公司 一种局部纤维嵌入的载体及其制造方法
US9969441B2 (en) * 2015-04-21 2018-05-15 Honda Motor Co., Ltd. Joint for vehicle components
JP6354662B2 (ja) * 2015-05-27 2018-07-11 トヨタ自動車株式会社 車両用部材の接合構造及び車両用部材の接合方法
US10220935B2 (en) * 2016-09-13 2019-03-05 The Boeing Company Open-channel stiffener
US10852503B2 (en) * 2018-03-20 2020-12-01 Ricoh Company, Ltd. Joint structure
DE102018111857A1 (de) 2018-05-17 2019-11-21 Atlas Copco IAS UK Ltd. Verfahren zum Verbinden zweier Werkstücke

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4556592A (en) * 1981-09-25 1985-12-03 The Boeing Company Conductive joint seals for composite aircraft
US4729705A (en) * 1987-02-02 1988-03-08 Atr International, Inc. Insert fastener in a lightweight panel
US4980005A (en) * 1987-03-13 1990-12-25 The Boeing Company Method for producing an aerospace structure having a cast-in-place noncompressible void filler
GB2284031B (en) * 1987-11-27 1995-11-08 Gen Electric Composite fastener
NL8703076A (nl) * 1987-12-18 1989-07-17 Pieter De Jong Houtverbinding.
EP0329434B1 (fr) * 1988-02-19 1993-07-28 Mitsubishi Jukogyo Kabushiki Kaisha Structure textile pour le renforcement d'éléments de construction tels que poutres, en matériau composite, et procédé pour sa production
US5399052A (en) * 1993-04-08 1995-03-21 Volkmann; Josef F. Aerospace fastener with improved bonding relationship to other applications
GB2307287B (en) * 1995-11-16 1999-09-08 George William Ainscow A connection for connecting elements
US5928448A (en) * 1997-11-01 1999-07-27 Northrop Grumman Corporation Dowel adhesive method for repair of ceramic matrix composites
CA2494110A1 (fr) * 2002-07-31 2004-02-05 E.I. Du Pont De Nemours And Company Systemes de point de fixation pour verre feuillete et procede de realisation
US7017255B2 (en) * 2003-04-07 2006-03-28 General Motors Corporation Adhesive encapsulated blind rivet system

Also Published As

Publication number Publication date
US20050244215A1 (en) 2005-11-03
FR2869655A1 (fr) 2005-11-04

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Legal Events

Date Code Title Description
CA Change of address

Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

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Year of fee payment: 12

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Effective date: 20211205