Provided is a flight efficiency improving system for a compound helicopter with a rotor and fixed wings. In forward flight of the compound helicopter, the flight efficiency improving system does not perform a cyclic pitch control of the rotor so as to allow a difference in lift generated by the rotor between an advancing side and a retreating side of the rotor, or the flight efficiency improving system performs the cyclic pitch control to an extent that does not completely eliminate the difference. The fixed wings are provided respectively on left and right sides of a body and are asymmetric to each other so that influence of an aerodynamic interference between the rotor and the fixed wings is reduced.


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    Titel :

    FLIGHT EFFICIENCY IMPROVING SYSTEM FOR COMPOUND HELICOPTER


    Beteiligte:
    KOBAYASHI WATARU (Autor:in) / HAYASHI HIROTAKA (Autor:in) / NAKAMURA MIZUKI (Autor:in) / SASAKI MASAFUMI (Autor:in) / TANABE YASUTADA (Autor:in) / KOBIKI NOBORU (Autor:in)

    Erscheinungsdatum :

    2021-12-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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