The present application relates to an aircraft assembly. The aircraft assembly has a wing tip device connected to a wing tip of a wing by a first connector, a second connector and a third connector. The wing tip device includes a front device spar and a rear device spar. The first connector is associated with the rear device spar. The second connector is spaced apart in a chordwise direction forward of the first connector, and the third connector is spaced apart in a chordwise direction rearward of the first connector. The third connector comprises a spigot mounting formation.


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    Titel :

    An aircraft assembly including a wingtip device


    Beteiligte:
    RUTH PULLAN (Autor:in) / BEN SMITH (Autor:in) / DAVID LIVERSAGE (Autor:in) / CLIVE STEADMAN (Autor:in)

    Erscheinungsdatum :

    29.01.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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