A vertical take-off and landing aircraft and method which uses fixed rotors for both VTOL and forward flight operations. The rotors are positioned to achieve a high span efficiency. The rotors are positioned to even out the lift across the span of the wing. The wing may also have narrow front and rear airfoils which may provide structural support as well as providing lift during forward flight, or may have a single center wing. The wing rotors are tilted forward and provide some forward propulsion during horizontal flight.


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    Titel :

    VTOL AIRCRAFT USING FIXED FORWARD CANTED ROTORS TO SIMULATE RIGID WING DYNAMICS


    Weitere Titelangaben:

    VERTIKAL STARTENDES UND LANDENDES FLUGZEUG (VTOL) MIT FESTEN, NACH VORNE GENEIGTEN ROTOREN ZUR SIMULIERUNG DER DYNAMIK STARRER FLÜGEL
    AÉRONEF ADAV FAISANT APPEL À DES ROTORS PENCHÉS EN AVANT, FIXES, POUR SIMULER UNE DYNAMIQUE D'AILE RIGIDE


    Beteiligte:
    BEVIRT JOEBEN (Autor:in) / STOLL ALEX (Autor:in) / MIKIC GREGOR VEBLE (Autor:in)

    Erscheinungsdatum :

    2023-02-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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    VTOL AIRCRAFT USING FIXED FORWARD CANTED ROTORS TO SIMULATE RIGID WING DYNAMICS

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