DE602005000586D1 - Laschenverbandvorrichtung zwischen komposite und metallischen Strukturelementen - Google Patents

Laschenverbandvorrichtung zwischen komposite und metallischen Strukturelementen

Info

Publication number
DE602005000586D1
DE602005000586D1 DE602005000586T DE602005000586T DE602005000586D1 DE 602005000586 D1 DE602005000586 D1 DE 602005000586D1 DE 602005000586 T DE602005000586 T DE 602005000586T DE 602005000586 T DE602005000586 T DE 602005000586T DE 602005000586 D1 DE602005000586 D1 DE 602005000586D1
Authority
DE
Germany
Prior art keywords
composite
structural elements
metallic structural
lashing device
panel
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.)
Active
Application number
DE602005000586T
Other languages
English (en)
Other versions
DE602005000586T2 (de
Inventor
Jean-Marc Durand
Bruno Sarpy
Gilles Bazerque
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
Publication of DE602005000586D1 publication Critical patent/DE602005000586D1/de
Application granted granted Critical
Publication of DE602005000586T2 publication Critical patent/DE602005000586T2/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B64C1/26—Attaching the wing or tail units or stabilising surfaces
    • 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
    • Y10T403/00—Joints and connections
    • Y10T403/44—Three or more members connected at single locus
    • 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
    • Y10T403/00—Joints and connections
    • Y10T403/75—Joints and connections having a joining piece extending through aligned openings in plural members

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Superconductors And Manufacturing Methods Therefor (AREA)
  • Joining Of Building Structures In Genera (AREA)
DE602005000586T 2004-07-22 2005-07-20 Laschenverbandvorrichtung zwischen komposite und metallischen Strukturelementen Active DE602005000586T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0451614A FR2873347B1 (fr) 2004-07-22 2004-07-22 Dispositif d'eclissage d'elements de structure composite avec des elements de structure metallique
FR0451614 2004-07-22

Publications (2)

Publication Number Publication Date
DE602005000586D1 true DE602005000586D1 (de) 2007-04-05
DE602005000586T2 DE602005000586T2 (de) 2007-10-25

Family

ID=34947570

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005000586T Active DE602005000586T2 (de) 2004-07-22 2005-07-20 Laschenverbandvorrichtung zwischen komposite und metallischen Strukturelementen

Country Status (6)

Country Link
US (1) US7195418B2 (de)
EP (1) EP1619116B1 (de)
AT (1) ATE354516T1 (de)
CA (1) CA2511847C (de)
DE (1) DE602005000586T2 (de)
FR (1) FR2873347B1 (de)

Families Citing this family (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2883548B1 (fr) * 2005-03-23 2007-06-15 Airbus France Sas Dispositif et procede d'eclissage mixte carbone-metal dissymetrique
US20070051851A1 (en) * 2005-09-02 2007-03-08 The Boeing Company Multi-piece fastener for limited clearance applications
US8142126B2 (en) 2005-09-02 2012-03-27 The Boeing Company Multi-piece fastener with self-indexing nut
CN100482517C (zh) * 2006-04-29 2009-04-29 中国国际海运集装箱(集团)股份有限公司 一种连接接头及带有该连接接头的车架主梁
US7546979B1 (en) * 2006-09-15 2009-06-16 The Boeing Company Trapezoidal panel pin joint allowing free deflection between fuselage and wing
GB0619512D0 (en) * 2006-10-03 2006-11-15 Airbus Uk Ltd Fitting
AU2007316403B2 (en) 2006-11-06 2011-02-03 Qualcomm Incorporated MIMO transmission with layer permutation in a wireless communication system
ES2378702B1 (es) * 2009-04-21 2013-02-28 Airbus Operations, S.L. Herrajes para la cogida del estabilizador vertical de cola de una aeronave.
FR2948155A1 (fr) * 2009-07-16 2011-01-21 Astrium Sas Procede de dimensionnement de liaisons mecaniques
ES2372849B1 (es) * 2010-03-25 2012-12-13 Airbus Operations, S.L. Estructura de unión de cajones de torsión en una aeronave mediante un herraje triforme de materiales compuestos no metálicos.
DE102010014301A1 (de) 2010-04-09 2011-10-13 Premium Aerotec Gmbh Befestigungsanordnung und Verbindungselement für eine Befestigungsanordnung
US8333345B2 (en) * 2010-08-26 2012-12-18 The Boeing Company Composite aircraft joint
FR2970463B1 (fr) * 2011-01-17 2013-02-15 Airbus Operations Sas Dispositif d'eclissage a tenue mecanique amelioree.
FR2970942B1 (fr) * 2011-01-28 2013-02-22 Airbus Operations Sas Raccordement des cadres de raidissage entre un fuselage d'aeronef et un caisson de voilure
US9574587B2 (en) 2011-11-04 2017-02-21 The Boeing Company Preloading a fastener of a mechanical fitting
US20130114994A1 (en) * 2011-11-04 2013-05-09 Robert Erik Grip Truss end pad fitting
CN102501965A (zh) * 2011-11-08 2012-06-20 中国商用飞机有限责任公司 用于飞机外翼翼肋上缘条的型材
US8684311B2 (en) * 2012-03-07 2014-04-01 The Boeing Company Bonded splice joint
US9180956B1 (en) 2012-04-11 2015-11-10 The Boeing Company Methods and apparatus for attaching an aircraft wing assembly to an aircraft body
US8857765B2 (en) * 2012-10-16 2014-10-14 The Boeing Company Method and apparatus for attaching an aircraft fuselage frame to a wing box
US9272769B2 (en) 2012-11-13 2016-03-01 The Boeing Company Joint for composite wings
US9227718B2 (en) 2013-06-07 2016-01-05 The Boeing Company Lower joints between outboard wing boxes and center wing sections of aircraft wing assemblies
US9580164B2 (en) 2013-07-10 2017-02-28 The Boeing Company Apparatus and methods for joining aircraft composite structures
US9475570B2 (en) 2013-08-23 2016-10-25 The Boeing Company Upper joints between outboard wing boxes and wing center sections of aircraft wing assemblies
FR3015433B1 (fr) 2013-12-23 2016-02-12 Airbus Operations Sas Ensemble pour aeronef comprenant un mat d'accrochage integre a la nacelle et agence en partie arriere du fuselage
US9399507B2 (en) 2014-01-22 2016-07-26 The Boeing Company Joints between a composite skin and a load-bearing component and methods of forming same
CN104176228B (zh) * 2014-02-26 2017-07-11 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种复合材料机身、机翼接头
US9586667B2 (en) * 2014-12-02 2017-03-07 The Boeing Company Splice assembly for joining structural components
GB2538097A (en) * 2015-05-07 2016-11-09 Airbus Operations Ltd Composite structures
US9926066B2 (en) * 2015-10-14 2018-03-27 The Boeing Company Corner tension fitting
US20200189714A1 (en) * 2017-05-01 2020-06-18 Bombardier Inc. Aircraft wing-to-fuselage interface permitting positional adjustment
FR3074143A1 (fr) * 2017-11-29 2019-05-31 Airbus Operations Nervure de jonction voilure-caisson de voilure pour aeronef et procede de fabrication d'un aeronef au moyen d'une telle nervure
PL241373B1 (pl) * 2017-12-13 2022-09-19 Flaris Spolka Z Ograniczona Odpowiedzialnoscia Połączenie struktur metalowo-kompozytowych samolotu
CN110406657B (zh) * 2019-07-31 2021-06-01 中国商用飞机有限责任公司北京民用飞机技术研究中心 民用飞机机翼上壁板根部连接角盒、连接结构及机翼
US11305862B2 (en) * 2019-12-20 2022-04-19 The Boeing Company Joint joining an aircraft wing to an aircraft body

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1523404A (fr) * 1967-03-22 1968-05-03 Sud Aviation Perfectionnement aux raccordements entre fuselage et voilure d'un aérodyne
US3724153A (en) * 1971-01-19 1973-04-03 Budd Co Joint construction
US4760493A (en) * 1985-09-30 1988-07-26 The Boeing Company Lightning protection system for composite material aircraft structures
FR2675563B1 (fr) * 1991-04-22 1993-08-27 Aerospatiale Procede d'assemblage mecanique d'un tube en materiau composite et d'une piece metallique et assemblage ainsi realise.
GB9215827D0 (en) * 1992-07-24 1992-09-09 British Aerospace A lightning shield
GB9411006D0 (en) * 1994-06-02 1994-07-20 British Aerospace Method of fastening composite aircraft skins
US5467570A (en) * 1994-10-12 1995-11-21 Simpson Strong-Tie Co., Inc. Tension tie
US6073405A (en) * 1995-12-22 2000-06-13 Icf Kaiser Engineers, Inc. Fitting for effecting bolted connection between a beam and a column in a steel frame structure
AU2584497A (en) * 1996-03-22 1997-10-10 Boeing Company, The Determinant spar assembly
US6766984B1 (en) * 1998-07-16 2004-07-27 Icom Engineering Corporation Stiffeners for aircraft structural panels
US6311449B1 (en) * 1999-08-06 2001-11-06 Michael G. Morse Securing decks to houses with “L”-shaped brackets
US6374570B1 (en) * 2000-08-25 2002-04-23 Lockheed Martin Corporation Apparatus and method for joining dissimilar materials to form a structural support member

Also Published As

Publication number Publication date
CA2511847A1 (fr) 2006-01-22
US20060018710A1 (en) 2006-01-26
US7195418B2 (en) 2007-03-27
DE602005000586T2 (de) 2007-10-25
CA2511847C (fr) 2013-08-27
FR2873347A1 (fr) 2006-01-27
ATE354516T1 (de) 2007-03-15
FR2873347B1 (fr) 2006-11-17
EP1619116B1 (de) 2007-02-21
EP1619116A1 (de) 2006-01-25

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