The present application relates to an aircraft assembly and, in particular, a wing leading edge wing assembly. The assembly includes a structural component, such as a leading edge panel, and a cover panel located over the structural component. The cover panel has a thermoplastic layer with an inner surface. A thermoplastic fastening member extends through the structural component and is welded to the inner surface so that the structural component is fastened between the inner surface and the fastening member.


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    Titel :

    AIRCRAFT ASSEMBLY, METHOD OF ASSEMBLING AN AIRCRAFT ASSEMBLY, AND KIT OF PARTS


    Weitere Titelangaben:

    FLUGZEUGBAUGRUPPE, VERFAHREN ZUR ZUSAMMENBAU EINER FLUGZEUGBAUGRUPPE UND KIT VON TEILEN
    ASSEMBLAGE DANS UN AÉRONEF, PROCÉDÉ D'ASSEMBLAGE D'UN ASSEMBLAGE DANS UN AÉRONEF ET KIT DE PIÈCES


    Beteiligte:
    EVANS RODNEY (Autor:in) / PHIPPS DAVID (Autor:in)

    Erscheinungsdatum :

    13.10.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B29L INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES , Index-Schema für besondere Gegenstände in Verbindung mit Unterklasse B29C / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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