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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    Title :

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


    Additional title:

    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


    Contributors:
    EVANS RODNEY (author) / PHIPPS DAVID (author)

    Publication date :

    2021-10-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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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