The feasibility of using an electromechanical actuator (EMA) as the primary flight control equipment in aerospace flight is examined. The EMA motor design is presented utilizing improved permanent magnet materials. The necessary equipment to complete a single channel EMA using the single channel power electronics breadboard is reported. The design and development of an improved rotor position sensor/tachometer is investigated.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Electromechanical Flight Control Actuator


    Erscheinungsdatum :

    1979


    Format / Umfang :

    129 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch







    AIRCRAFT FLIGHT CONTROL SYSTEM INCLUDING ELECTROMECHANICAL ACTUATOR

    MIYAZONO KOHEI / NISHIYAMA YOJI / SUGIURA HIDEYUKI | Europäisches Patentamt | 2020

    Freier Zugriff

    Aircraft flight control system including electromechanical actuator

    MIYAZONO KOHEI / NISHIYAMA YOJI / SUGIURA HIDEYUKI | Europäisches Patentamt | 2022

    Freier Zugriff