An aircraft (1) having a wing (3) and a wing tip device (4) at the tip of the wing (3), the wing tip device (4) having front and rear spars (14, 13), wherein the wing tip device (4) has a cross-brace spar (18) that links the front and rear spars and is oriented such that it is oblique to the front and rear spars (14, 13). A wing assembly (2) of the aircraft (1). A wing tip device (4) of the aircraft (1). A method of manufacture of the aircraft (1), wing assembly (2) and wing tip device (4).


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    Titel :

    A spar arrangement in a wing tip device


    Erscheinungsdatum :

    02.08.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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