The technical problem to be solved by the invention is to provide the vector power coaxial double-propeller unmanned aerial vehicle which is compact in overall layout, relatively small in overall size, simpler and more reliable in structure and relatively light in structural weight. The unmanned aerial vehicle is controlled through vector power, the tilting mechanism is simple and reliable in structure, a complex pitch changing mechanism is omitted, the overall layout is more compact, the miniaturization size which cannot be achieved by other unmanned aerial vehicles under the condition of the same load and endurance can be achieved, the application requirements under the condition that the requirement for the boundary dimension is extremely strict are met, and the application range is wide. Compared with a conventional coaxial double-propeller unmanned aerial vehicle, the vector power coaxial double-propeller unmanned aerial vehicle is simpler in structure, higher in reliability and lighter in weight, the flight performance is improved under the same condition, in addition, the power cabin, the energy cabin and the load cabin of the vector power coaxial double-propeller unmanned aerial vehicle are connected through detachable structures, the sectional type modular design is adopted, configuration is flexible, and the vector power coaxial double-propeller unmanned aerial vehicle is suitable for large-scale popularization and application. And the task adaptability range is expanded. The method is suitable for popularization and application in the technical field of unmanned aerial vehicles.

    本发明所要解决的技术问题是提供一种整机布局紧凑、整体尺寸较小、结构更为简单可靠且结构重量也较轻的矢量动力共轴双桨无人机。该无人机通过矢量动力控制,且倾转机构结构简单可靠,省去了复杂的变距机构,使得总体布局更为紧凑,可以实现在同等载重和航时条件下其他无人机无法实现的微型化尺寸,满足某些对外形尺寸要求极为严苛的条件下的应用需要,而且相对常规共轴双桨无人机,结构更加简单,可靠性更高,重量更轻,在同等条件下提高了飞行性能,再者,本发明所述矢量动力共轴双桨无人机的动力舱、能源舱、载荷舱之间均采用了可拆卸结构连接,这种分段式模块化设计,配置灵活,增加了任务适应性范围。适合在无人机技术领域推广应用。


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    Titel :

    Vector power coaxial double-propeller unmanned aerial vehicle


    Weitere Titelangaben:

    一种矢量动力共轴双桨无人机


    Beteiligte:
    CHEN CHENG (Autor:in) / KANG NUAN (Autor:in)

    Erscheinungsdatum :

    2023-03-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64U



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