The invention discloses a multifunctional engine starting system of an unmanned aerial vehicle. The output end of the motor is in transmission with an engine of the unmanned aerial vehicle; a motor control circuit; a power supply is provided for the operation of the motor; a rectification voltage stabilizing circuit; rectifying and stabilizing the electric energy generated by the motor; a switching circuit; the motor control circuit or the rectifying and voltage stabilizing circuit is selectively communicated with the motor; in addition, the invention further discloses starting steps of the unmanned aerial vehicle, and the problems that a traditional unmanned aerial vehicle structure is large in starting resistance and difficult to start, and the service life of a starting device is shortened are solved.

    本发明公开了一种无人机多功能发动机启动系统,包括电机;所述电机的输出端与无人机的发动机传动;电机控制电路;为所述电机运转提供电源;整流稳压电路;对所述电机产生的电能进行整流和稳压;切换电路;选择性的将所述电机控制电路或所述整流稳压电路与所述电机连通;此外,还公开了无人机的启动步骤,解决传统无人机结构启动时阻力大,启动困难,降低启动装置的寿命问题。


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    Titel :

    Multifunctional engine starting system of unmanned aerial vehicle


    Weitere Titelangaben:

    一种无人机多功能发动机启动系统


    Beteiligte:
    HUANG HAI (Autor:in) / LI YONGMING (Autor:in) / MIAO KEZUAN (Autor:in)

    Erscheinungsdatum :

    2022-09-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    F02N STARTING OF COMBUSTION ENGINES , Anlassen von Brennkraftmaschinen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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