There is provided a rotorcraft (100, 200, 300), including a body (104), including a front portion (106) and a tail portion (102); a main rotor system (110) coupled to the front portion (106) of the body (104), the main rotor system (110) operable to provide a lifting force on the body (104); and an anti-torque system (120, 220, 320) coupled to the tail portion (102) of the body (104), the anti-torque system (120, 220, 320) including a primary tail rotor system (130, 330) and a secondary tail rotor system (140, 240); wherein the primary tail rotor system (130, 330) and the secondary tail rotor system (140, 240) are operable to provide a first anti-torque force and a second anti-torque force. In other aspects, there are methods of providing anti-torque force in a rotorcraft (100, 200, 300).


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    Titel :

    ROTORCRAFT ANTI-TORQUE SYSTEM


    Weitere Titelangaben:

    DREHMOMENTAUSGLEICHSSYSTEM FÜR DREHFLÜGLER
    SYSTÈME ANTI-COUPLE DE GIRAVION


    Beteiligte:
    HEFNER LEVI C (Autor:in) / STAMPS FRANK B (Autor:in)

    Erscheinungsdatum :

    2020-12-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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