The invention relates to a modular flying wing type layout vertical take-off and landing unmanned aerial vehicle with additional bionic suction cups. The modular flying wing type layout vertical take-off and landing unmanned aerial vehicle comprises a main vehicle body, wing assemblies, adsorption assemblies, power rotor assemblies, steering engine assemblies and auxiliary connecting plates. The main machine body is streamlined to reduce air resistance when the aircraft advances, and a flight control integrated system is installed in the main machine body. The wing assembly is in a flying wing type layout, and wings are installed on the two sides of the main body. The adsorption assembly is installed at the tail of the main machine body and completes bionic adsorption through nano glue. The rotor assemblies and the steering engine assemblies are installed at the two ends of the wings, and the flight requirements of vertical take-off and landing, forward turning and the like can be met through rotation of steering engines. The functions of vertical take-off and landing and pause adsorption of the flying wing type unmanned aerial vehicle are achieved, and the flying wing type unmanned aerial vehicle has the advantages of being reasonable in structural design, smaller in power consumption, higher in concealment, richer in modularization, high in stability and high in practicability, so that the problems and defects that an existing unmanned aerial vehicle is high in energy consumption and poor in concealment are effectively solved.

    本发明涉及一种附加仿生吸盘的模块化飞翼式布局垂直起降无人机,包括:主机体、机翼组件、吸附组件、动力转子组件、舵机组件及辅助连接板;主机体采用流线型以减少飞行器前进时的空气阻力,且在内部安装飞控集成系统;机翼组件为飞翼式布局,且机翼安装在主体的两侧;吸附组件安装在主机体尾部,且通过纳米胶完成仿生吸附;转子组件与舵机组件安装在机翼两端,且可以通过舵机转动满足垂直起降与前进转弯等飞行要求。本发明实现了飞翼式无人机的垂直起降以及暂停吸附节省能耗的功能,具有结构设计合理、功耗更小、隐蔽性更强、模块化更加丰富、稳定性强、实用性强的有点,从而有效解决了现有无人机耗能快,隐蔽性不强的问题和不足。


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    Titel :

    Modularized flying wing type layout vertical take-off and landing unmanned aerial vehicle additionally provided with bionic suction cups


    Weitere Titelangaben:

    一种附加仿生吸盘的模块化飞翼式布局垂直起降无人机


    Beteiligte:
    CHEN JIAOJIAO (Autor:in) / XIANG WEIYI (Autor:in) / LI ZHIKUN (Autor:in) / LI TONG (Autor:in) / CHEN WEIKE (Autor:in) / ZHANG SHIYAN (Autor:in)

    Erscheinungsdatum :

    26.05.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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