The present invention belongs to the field of aircraft, and in particular, it relates to fittings and joints intended to be attached to a removable aircraft panel and/or to a fuselage section of an aircraft. More specifically, the invention relates to joints for a removable structural panel of an aircraft, such as a panel or a door that provides accessibility to a fuel tank and associated systems of an aircraft, for improved industrialisation, operability and maintenance.


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    Titel :

    STRUCTURAL JOINT FOR ATTACHING A REMOVABLE AIRCRAFT PANEL TO A FUSELAGE SECTION


    Weitere Titelangaben:

    STRUKTURELLE VERBINDUNG ZUR BEFESTIGUNG EINER ABNEHMBAREN FLUGZEUGPLATTE AN EINEM RUMPFABSCHNITT
    JOINT STRUCTUREL POUR LA FIXATION D'UN PANNEAU AMOVIBLE D'AÉRONEF À UNE SECTION DE FUSELAGE



    Erscheinungsdatum :

    18.06.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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