WO2005007507B1 - Composant structurel en aluminium soude et pourvu d'elements realises dans un materiau aluminium coule - Google Patents

Composant structurel en aluminium soude et pourvu d'elements realises dans un materiau aluminium coule

Info

Publication number
WO2005007507B1
WO2005007507B1 PCT/DE2004/001387 DE2004001387W WO2005007507B1 WO 2005007507 B1 WO2005007507 B1 WO 2005007507B1 DE 2004001387 W DE2004001387 W DE 2004001387W WO 2005007507 B1 WO2005007507 B1 WO 2005007507B1
Authority
WO
WIPO (PCT)
Prior art keywords
structural component
welded
aluminum
aluminium
connecting element
Prior art date
Application number
PCT/DE2004/001387
Other languages
German (de)
English (en)
Other versions
WO2005007507A1 (fr
Inventor
Frank Palm
Original Assignee
Eads Deutschland Gmbh
Frank Palm
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 Eads Deutschland Gmbh, Frank Palm filed Critical Eads Deutschland Gmbh
Publication of WO2005007507A1 publication Critical patent/WO2005007507A1/fr
Publication of WO2005007507B1 publication Critical patent/WO2005007507B1/fr

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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/14—Working by laser beam, e.g. welding, cutting or boring using a fluid stream, e.g. a jet of gas, in conjunction with the laser beam; Nozzles therefor
    • B23K26/1462—Nozzles; Features related to nozzles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/20—Bonding
    • B23K26/21—Bonding by welding
    • B23K26/211—Bonding by welding with interposition of special material to facilitate connection of the parts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/20—Bonding
    • B23K26/21—Bonding by welding
    • B23K26/24—Seam welding
    • B23K26/242—Fillet welding, i.e. involving a weld of substantially triangular cross section joining two parts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K26/00—Working by laser beam, e.g. welding, cutting or boring
    • B23K26/20—Bonding
    • B23K26/32—Bonding taking account of the properties of the material involved
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00—Articles made by soldering, welding or cutting
    • B23K2101/18—Sheet panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00—Materials to be soldered, welded or cut
    • B23K2103/08—Non-ferrous metals or alloys
    • B23K2103/10—Aluminium or alloys thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00—Materials to be soldered, welded or cut
    • B23K2103/18—Dissimilar materials

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Mechanical Engineering (AREA)
  • Plasma & Fusion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laser Beam Processing (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Arc Welding In General (AREA)

Abstract

La présente invention concerne un composant structurel (1) en aluminium soudé, pourvu d'éléments réalisés dans un matériau aluminium coulé et destiné notamment aux avions. Ce composant structurel comprend un champ de revêtement (2) et au moins un élément de renforcement (3b) auquel est fixé au moins un élément de liaison (4) qui permet de fixer par soudage l'élément de renforcement (3b) au champ revêtement (2). L'invention est caractérisée en ce que l'élément de liaison (4) est constitué d'un matériau aluminium coulé.
PCT/DE2004/001387 2003-07-14 2004-07-01 Composant structurel en aluminium soude et pourvu d'elements realises dans un materiau aluminium coule WO2005007507A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE10332003A DE10332003B3 (de) 2003-07-14 2003-07-14 Geschweißtes Aluminium-Strukturbauteil mit Aluminium-Guss-Werkstoffelementen
DE10332003.2 2003-07-14

Publications (2)

Publication Number Publication Date
WO2005007507A1 WO2005007507A1 (fr) 2005-01-27
WO2005007507B1 true WO2005007507B1 (fr) 2005-05-26

Family

ID=33441756

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/DE2004/001387 WO2005007507A1 (fr) 2003-07-14 2004-07-01 Composant structurel en aluminium soude et pourvu d'elements realises dans un materiau aluminium coule

Country Status (2)

Country Link
DE (1) DE10332003B3 (fr)
WO (1) WO2005007507A1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005033992B3 (de) 2005-07-21 2007-04-19 Airbus Deutschland Gmbh Verfahren zum Verbinden von mindestens zwei Flächengebilden, insbesondere von mindestens zwei Metallblechen für eine Leichtbaustruktur sowie Verbindung und Leichtbaustruktur
DE102006026918B4 (de) * 2006-06-09 2017-01-12 Airbus Operations Gmbh Rumpfstruktur
EP1880791A1 (fr) 2006-07-21 2008-01-23 Aleris Aluminum Koblenz GmbH Procédé et appareil pour l'assemblage par laser de deux composants utilisant un flux laminiare de gaz inert coaxial avec un fil d'apport métallique
DE102007048283A1 (de) 2007-10-08 2009-04-16 Eads Deutschland Gmbh Versteifungsprofil für Flugzeugstrukturen
US11613340B2 (en) * 2020-05-21 2023-03-28 North West Heli-Structures Incorporated Panel systems and methods for helicopters

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5576112A (en) * 1993-08-28 1996-11-19 Kabushiki Kaisha Kobe Seiko Sho Joint of aluminum alloy casting
FR2716896B1 (fr) * 1994-03-02 1996-04-26 Pechiney Recherche Alliage 7000 à haute résistance mécanique et procédé d'obtention.
DE19639667C1 (de) * 1996-09-27 1998-03-12 Daimler Benz Aerospace Airbus Verfahren zum Schweißen von Profilen auf großformatigen Aluminium-Strukturbauteilen mittels Laserstrahlen
US6766984B1 (en) * 1998-07-16 2004-07-27 Icom Engineering Corporation Stiffeners for aircraft structural panels
US6531004B1 (en) * 1998-08-21 2003-03-11 Eads Deutschland Gmbh Weldable anti-corrosive aluminium-magnesium alloy containing a high amount of magnesium, especially for use in aviation
DE19844035C1 (de) * 1998-09-25 1999-11-25 Daimler Chrysler Aerospace Schalenbauteil für ein Flugzeug und Verfahren zur Herstellung
DE19941924B4 (de) * 1999-09-03 2004-07-01 Airbus Deutschland Gmbh Großflächiges Flugzeugstrukturbauteil und Verfahren zur Herstellung des Flugzeugstrukturbauteils
FR2802946B1 (fr) * 1999-12-28 2002-02-15 Pechiney Rhenalu Element de structure d'avion en alliage al-cu-mg
US20020178583A1 (en) * 2001-03-14 2002-12-05 Holman Wrenn P. Modular monolithic bulkhead panel

Also Published As

Publication number Publication date
WO2005007507A1 (fr) 2005-01-27
DE10332003B3 (de) 2004-12-16

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