An aircraft 1 has a wing 3 and a wing tip device 4 at the tip of the wing 3. The wing tip device 4 has front and rear spars 14, 13. 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. Also disclosed is a method of making a wing tip device.


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    Titel :

    A spar arrangement in a wing tip device


    Beteiligte:

    Erscheinungsdatum :

    19.12.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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