The invention relates to a device for assembling a plurality of panels of an aircraft fuselage, said device comprising at least one anvil body, comprising a surface for supporting the said plurality of panels, the said anvil body comprising at least one anvil rail mounted movably in a cavity of the anvil body and configured to move between a top position in which the upper surface of the anvil rail extends into the extension of the support surface and a bottom position in which a workspace is created between the upper surface of the anvil rail and the support surface so as to allow a machining and/or stripping tool to pass through.


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    Titel :

    PROCEDE, DISPOSITIF ET SYSTEME D'ASSEMBLAGE D'UNE PLURALITE DE PANNEAUX


    Beteiligte:
    DARRAS FRANCK (Autor:in) / WATTIER YANNICK (Autor:in)

    Erscheinungsdatum :

    20.05.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B23P Sonstige Metallbearbeitung , OTHER WORKING OF METAL / B23K Löten , SOLDERING OR UNSOLDERING / B64C AEROPLANES , Flugzeuge



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