Tail rotor control system is described for helicopters. A pedal position sensor operable by a pilot yields greater tail rotor RPM relative to the main rotor RPM, giving the pilot increased control over the vehicle. This proves especially useful in certain situations, such as high altitude, where increasing tail rotor speed from main rotor speed can give a pilot increased maneuverability and stability.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Helicopter Tail Rotor Drive System on Demand Speed Control


    Beteiligte:
    LAVALLEE YANN (Autor:in) / POSTER SCOTT D (Autor:in)

    Erscheinungsdatum :

    2023-11-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Helicopter tail rotor drive system on demand speed control

    LAVALLEE YANN / POSTER SCOTT D | Europäisches Patentamt | 2023

    Freier Zugriff

    Helicopter Tail Rotor Drive System on Demand Speed Control

    LAVALLEE YANN / POSTER SCOTT D | Europäisches Patentamt | 2022

    Freier Zugriff

    Vector ducted tail rotor high-speed helicopter

    JIANG CHONGWEN / HE XIN / LI ZHIHAO et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Drive of a tail rotor of a helicopter

    HAMANN JENS / KÖPKEN HANS-GEORG / STOIBER DIETMAR | Europäisches Patentamt | 2017

    Freier Zugriff

    Helicopter rotor tail rotor failure protection system and helicopter

    CHEN XI / GAO XUAN / FEI ZHONGYANG et al. | Europäisches Patentamt | 2023

    Freier Zugriff