The invention discloses an unmanned aerial vehicle motor tension-torque load loading test system and test method, and relates to the field of unmanned aerial vehicle motor propellers, and the system comprises a bottom plate which is provided with a motor support, and the motor support is used for placing a tested motor; the tension loading mechanism is arranged on one side of the motor support, the tension loading mechanism comprises a counterweight iron disc and at least two groups of electromagnets, the counterweight iron disc is used for being connected with a tested motor, and the electromagnets are uniformly distributed around the center of the counterweight iron disc; the torque loading mechanism is arranged on the other side of the motor support, the torque loading mechanism comprises a loading motor and a torque sensor, and the two ends of the torque sensor are connected with the loading motor and the tested motor respectively; the control unit is connected with the electromagnet and the loading motor; the test system solves the problems that existing test conditions are single and load loading cannot be fused, and meets the use requirements of most motor fields in the industry and aerospace.

    本发明公开了一种无人机用电机拉力‑扭矩载荷加载试验系统及试验方法,涉及无人机用电机螺旋桨领域,包括:底板,底板上设置有电机支架,电机支架用于放置被测电机;拉力加载机构,设置在电机支架的一侧,拉力加载机构包括配重铁盘和至少两组电磁铁,配重铁盘用于与被测电机连接,电磁铁以配重铁盘的圆心进行均布设置;扭矩加载机构,设置在电机支架的另一侧,扭矩加载机构包括加载电机和扭矩传感器,扭矩传感器的两端分别与加载电机和被测电机连接;控制单元,与电磁铁和加载电机连接;该试验系统解决现有试验条件单一,载荷加载不能融合的问题,满足工业界、航空航天大多数电动机领域使用需求。


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    Titel :

    Motor tension-torque load loading test system and test method for unmanned aerial vehicle


    Weitere Titelangaben:

    一种无人机用电机拉力-扭矩载荷加载试验系统及试验方法


    Beteiligte:
    CAI ZHIYING (Autor:in) / LI WEI (Autor:in) / CHEN DONGYANG (Autor:in)

    Erscheinungsdatum :

    2023-03-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    G01R Messen elektrischer Größen , MEASURING ELECTRIC VARIABLES / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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