Disclosed is a method of enhancing aerodynamic performance of an aircraft wing assembly including a fixed section and a foldable section. The foldable section is hinged to the fixed section at a hinge axis. The method includes turning a torque box extending from the foldable section to rotate the foldable section about the hinge axis from a stowed position to a deployed position.


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    Titel :

    Enhancing aerodynamic performance of an aircraft wing assembly


    Beteiligte:
    GOOD MARK S (Autor:in) / WALKER STEVEN PAUL (Autor:in)

    Erscheinungsdatum :

    2018-04-03


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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