The present disclosure directed to an aircraft comprising one or more propulsion devices, a flexible wing, at least two tail booms having a proximal end and a distal end, the tail booms being secured to said flexible wing at the proximal end, wherein the tail booms comprise of a tail section connected at the distal end of said tail boom and wherein the tail section comprises of at least one control surface.


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    Titel :

    Wing-Twist Controlled Aircraft


    Beteiligte:
    UHLIG DANIEL (Autor:in) / KAYS CORY (Autor:in) / ULECK KEVIN (Autor:in) / CROUSE GIL (Autor:in)

    Erscheinungsdatum :

    2019-03-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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