In order to reduce the weight of a hybrid propulsion system for a multi-rotor rotary-wing aircraft, the system comprises at least one inverter configured to supply power in parallel to multiple electric motors intended to drive the corresponding propellers of the system.


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    Title :

    ГИБРИДНАЯ СИЛОВАЯ УСТАНОВКА ДЛЯ МНОГОВИНТОВОГО ВИНТОКРЫЛОГО ВОЗДУШНОГО СУДНА, СОДЕРЖАЩАЯ УЛУЧШЕННОЕ СРЕДСТВО ПРЕОБРАЗОВАНИЯ ПОСТОЯННЫЙ ТОК/ПЕРЕМЕННЫЙ ТОК


    Publication date :

    2020-10-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge