A rotorcraft has a frame and a plurality of rotors connected to the frame. The frame has a roll axis and a pitch axis. Each of the rotors includes a rotor shaft. The rotor shaft of each of the rotors is canted with respect to at least one of the roll axis and the pitch axis. The rotor shaft of each of the rotors may be canted between 3 and 15 degrees. Each of the rotors may be a co-axial co-rotating rotor. The rotors may be oriented in opposing pairs across the frame. Both rotors in each opposing pair rotate in the same direction. The rotorcraft may include at least two additional rotors, each having a forward cant. Each of the additional rotors may be a co-axial contra-rotating rotor.


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    Titel :

    CANTED CO-AXIAL ROTORS FOR A ROTORCRAFT


    Weitere Titelangaben:

    GENEIGTE KOAXIALROTOREN FÜR EIN DREHFLÜGELFLUGZEUG
    ROTORS COAXIAUX INCLINÉS POUR GIRAVION


    Beteiligte:
    LACY ROGER W (Autor:in) / DUFFY MICHAEL J (Autor:in) / MASON DAVID H (Autor:in)

    Erscheinungsdatum :

    2022-06-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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