ATE456636T1 - Verfahren zum verbinden eines bauteils - Google Patents

Verfahren zum verbinden eines bauteils

Info

Publication number
ATE456636T1
ATE456636T1 AT03022314T AT03022314T ATE456636T1 AT E456636 T1 ATE456636 T1 AT E456636T1 AT 03022314 T AT03022314 T AT 03022314T AT 03022314 T AT03022314 T AT 03022314T AT E456636 T1 ATE456636 T1 AT E456636T1
Authority
AT
Austria
Prior art keywords
component
laminate
border
sheet
stiffness
Prior art date
Application number
AT03022314T
Other languages
English (en)
Inventor
Oerjan Arulf
Stefan Brick
Original Assignee
Ruag Aerospace Sweden Ab
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 Ruag Aerospace Sweden Ab filed Critical Ruag Aerospace Sweden Ab
Application granted granted Critical
Publication of ATE456636T1 publication Critical patent/ATE456636T1/de

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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054Fuselage structures substantially made from particular materials
    • B64C2001/0072Fuselage structures substantially made from particular materials from composite materials
    • 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
    • F16B19/00Bolts without screw-thread; Pins, including deformable elements; Rivets
    • F16B19/04Rivets; Spigots or the like fastened by riveting
    • F16B19/06Solid rivets made in one piece
    • 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Laminated Bodies (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Processing Of Terminals (AREA)
  • Mechanical Coupling Of Light Guides (AREA)
  • Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
AT03022314T 2003-10-03 2003-10-03 Verfahren zum verbinden eines bauteils ATE456636T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP03022314A EP1520895B1 (de) 2003-10-03 2003-10-03 Verfahren zum Verbinden eines Bauteils

Publications (1)

Publication Number Publication Date
ATE456636T1 true ATE456636T1 (de) 2010-02-15

Family

ID=34306822

Family Applications (1)

Application Number Title Priority Date Filing Date
AT03022314T ATE456636T1 (de) 2003-10-03 2003-10-03 Verfahren zum verbinden eines bauteils

Country Status (4)

Country Link
EP (1) EP1520895B1 (de)
AT (1) ATE456636T1 (de)
DE (1) DE60331146D1 (de)
ES (1) ES2338541T3 (de)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7393488B2 (en) 2005-05-25 2008-07-01 The Boeing Company Methods of joining structures and joints formed thereby
DE102011004775B4 (de) 2011-02-25 2012-10-25 Airbus Operations Gmbh Verfahren zum Herstellen einer Verbindung, Verbindung sowie Luft- oder Raumfahrzeug
DE102013222970B4 (de) 2013-11-12 2023-07-27 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zum Verbinden zweier Bauteile, Verbindungsabschnitt eines Bauteils und Bauteilverbund

Family Cites Families (3)

* 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
US4966802A (en) * 1985-05-10 1990-10-30 The Boeing Company Composites made of fiber reinforced resin elements joined by adhesive
SE516459C2 (sv) * 2000-11-24 2002-01-15 Saab Ericsson Space Ab Konstruktion och förfarande vid bärraket eller satellit

Also Published As

Publication number Publication date
EP1520895B1 (de) 2010-01-27
EP1520895A1 (de) 2005-04-06
ES2338541T3 (es) 2010-05-10
DE60331146D1 (de) 2010-03-18

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Legal Events

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RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties