An electrically distributed yaw control system for a helicopter having a tailboom includes a plurality of tail rotors rotatably coupled to the tailboom and a flight control computer implementing a tail rotor balancing module. The tail rotor balancing module includes a tail rotor balancing monitoring module configured to monitor one or more parameters of the helicopter and identify a first set of one or more tail rotors in the plurality of tail rotors based on the one or more parameters. The tail rotor balancing module also includes a tail rotor balancing command module configured to modify one or more operating parameters of the first set of tail rotors.


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    Titel :

    Tail rotor balancing systems for use on rotorcraft


    Beteiligte:
    KUANG CHEN (Autor:in) / BUSTAMANTE MARC (Autor:in) / SENTHILNATHAN THUVARAGAN (Autor:in) / BIRON GUILLAUME (Autor:in) / OUELLET MARC (Autor:in) / DUGRÉ ALEXIS (Autor:in)

    Erscheinungsdatum :

    25.10.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge