A rotorcraft (101) includes a fight control computer (FCC) (205), a first rotor system (110), and a second rotor system (112). The first rotor system (110) includes a first swashplate (122) coupled to a first rotor (118) and a first plurality of actuators (231) configured to move the first swashplate (122). The second rotor system (112) includes a second swashplate (124) coupled to a second rotor (120) and a second plurality of actuators (233) configured to move the second swashplate (124). The rotorcraft also includes a first communications channel coupled between the FCC, a first actuator of the first multiple actuators (231), and a second actuator of the second multiple actuators (233). The rotorcraft also includes a second communications channel coupled between the FCC and a third actuator of the first multiple actuators.


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    Titel :

    ROTORCRAFT SWASHPLATE ACTUATOR CONTROL


    Weitere Titelangaben:

    DREHFLÜGLERTAUMELSCHEIBENAKTUATORSTEUERUNG
    COMMANDE D'ACTIONNEUR DE PLATEAU OSCILLANT D'UN GIRAVION


    Beteiligte:
    TRANTHAM MICHAEL (Autor:in) / ATKINS BRADY (Autor:in) / COVINGTON CHARLES (Autor:in)

    Erscheinungsdatum :

    20.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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