The invention relates to an unmanned aerial vehicle system, in particular to a temperature control protection system of an unmanned aerial vehicle rudder blade driving motor. The protection system comprises a main control system, a propelling system, a rudder system and a feedback system; the rudder system comprises a rudder sheet driving transmission mechanism, the rudder sheet driving transmission mechanism comprises at least one heat conduction and heat insulation path formed by a plurality of transmission parts connected in series or in parallel, and each heat conduction and heat insulation path comprises at least two heat insulation connecting nodes formed by connecting the transmission parts. At least two heat insulation connecting nodes comprise heat insulation pieces arranged between the adjacent transmission parts. One end of the heat conduction and heat insulation path is a rudder sheet, and the other end is a rudder sheet driving motor. By adopting the temperature control protection system of the unmanned aerial vehicle rudder sheet driving motor, the temperature is gradually reduced from the rudder sheet end through multi-stage echelon heat insulation of the plurality of connecting nodes, so that the stable and safe operation of the rudder sheet driving motor is ensured, and the reliable operation of the whole rudder system is ensured.

    本发明涉及无人飞行器系统,尤其涉及一种无人飞行器舵片驱动电机的温控保护系统,包括主控系统,推进系统,舵系统,反馈系统,舵系统包含舵片驱动传动机构,包括所述舵片驱动传动机构包含至少一条由多个串联或并联的传动部件形成的热传导隔热路径,每个所述热传导隔热路径包含至少两个由传动部件之间的连接形成的隔热连接节点,至少有两个隔热连接节点包含有设置于相邻传动部件之间的隔热件;所述热传导隔热路径一端为舵片,另一端为舵片驱动电机。采用本无人飞行器舵片驱动电机的温控保护系统,通过多个连接节点的多级梯次隔热,将温度从舵片端逐渐降温,保障了舵片驱动电机的稳定和安全的运行,保障了整个舵系统的可靠运转。


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    Title :

    Temperature control protection system of unmanned aerial vehicle rudder sheet driving motor


    Additional title:

    无人飞行器舵片驱动电机的温控保护系统


    Contributors:
    TANG BING (author) / LIU YIJIAN (author)

    Publication date :

    2021-01-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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