The invention discloses an unmanned aerial vehicle wing driving mechanism. The unmanned aerial vehicle wing driving mechanism comprises a driving motor fixed in a vehicle body, the output end of the driving motor is provided with a first rotating rod, the first rotating rod is connected with a third rotating rod through a length-adjustable second rotating rod, and the end of the third rotating rodis provided with a lantern ring used for being connected with a rotating shaft; and threads are arranged at the two ends of the second rotating rod, the rotating directions of the threads located atthe two ends of the second rotating rod are opposite, threaded sleeves are connected to the two ends of the second rotating rod in a threaded mode, one threaded sleeve is rotationally connected with the first rotating rod, and the other threaded sleeve is rotationally connected with the third rotating rod. One thread sleeve is rotationally connected with the first rotating rod through a first bearing, and the other thread sleeve is rotationally connected with the third rotating rod through a second bearing; and the middle part of the second rotating rod bulges outwards to form a polygonal prism. The unmanned aerial vehicle has the advantages that the driving motor is not easy to damage, flight accidents are not easy to cause, the wind resistance is small, the maintenance is easy, the application range is wide, and the service life is long.

    本发明公开了一种无人机机翼驱动机构,包括固定在机身内的驱动电机,驱动电机输出端设有第一转杆,第一转杆通过长度可调的第二转杆连接第三转杆,第三转杆的端部设有用于与转轴连接的套环;所述第二转杆的两端均设有螺纹,位于第二转杆两端的螺纹旋向相反,第二转杆的两端均螺接有螺套,其中一个螺套与第一转杆转动连接,另一个螺套与第三转杆转动连接;所述的其中一个螺套通过第一轴承与第一转杆转动连接,所述的另一个螺套通过第二轴承与第三转杆转动连接;所述第二转杆的中部向外侧鼓出形成多棱柱。本发明具有驱动电机不易损坏、不易引发飞行事故、风阻较小、维护较为容易、适用范围较广、使用寿命较长的优点。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Unmanned aerial vehicle wing driving mechanism


    Weitere Titelangaben:

    无人机机翼驱动机构


    Beteiligte:
    CHEN CHAO (Autor:in) / ZHOU YONGTAO (Autor:in)

    Erscheinungsdatum :

    23.02.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



    Unmanned aerial vehicle wing limiting mechanism, unmanned aerial vehicle wing and unmanned aerial vehicle

    ZHANG KE / ZHANG XIAOPAN / ZHANG YING et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Unmanned aerial vehicle wing folding mechanism and unmanned aerial vehicle

    GUO YITING / WANG JUN / KANG CHUANMING et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Wing folding mechanism, unmanned aerial vehicle and wing folding method of unmanned aerial vehicle

    LI ZESHI / MA PENGKE / YAN FEI et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Integrated unmanned aerial vehicle wing rotating mechanism and integrated unmanned aerial vehicle

    WANG YANWEI / YANG LIGONG / WEN XI et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Unmanned aerial vehicle wing and unmanned aerial vehicle

    WANG KUN / QU HUMIN / WANG CHAO et al. | Europäisches Patentamt | 2024

    Freier Zugriff