An anti-torque system (10) for a helicopter (1) is described that comprises: an electric power supply unit (15); at least one first rotor (17), operatively connected to an electric power supply unit (15) and operable by the electric power supply unit (15) so as to rotate with a first variable angular speed; and at least one second rotor (25) operatively connected to electric power supply unit (15) and operable by the electric power supply unit (15) so as to rotate with a second variable angular speed.


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    Titel :

    HELICOPTER WITH AN ANTI-TORQUE SYSTEM


    Weitere Titelangaben:

    HUBSCHRAUBER MIT EINEM ANTI-DREHMOMENTSYSTEM
    HÉLICOPTÈRE AVEC UN SYSTÈME ANTICOUPLE


    Beteiligte:
    BRUNETTI MASSIMO (Autor:in) / BOTTASSO LUIGI MARIA (Autor:in) / GOH CHEE SU (Autor:in) / WELLER GARY (Autor:in)

    Erscheinungsdatum :

    28.09.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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