The invention discloses an unmanned aerial vehicle assisted take-off and landing system. The system comprises a driving module, an adjusting module and an auxiliary lift module. With the driving module, lifting force can be provided for a middle part of the device so that the device can have enough lift force; by arranging the auxiliary lift module, lifting force is provided for the edge of the device, the device is not prone to being blown off by wind in the flying process, and the wind resistance of the device is enhanced accordingly; by arranging the adjusting module, swinging of a swingingplate can be controlled by controlling the adjusting motor, and therefore the flying direction of the device is controlled.

    本发明公开了一种无人机辅助起飞降落系统,包括驱动模块、调节模块和辅助升力模块。本发明通过设置驱动模块,可以为本装置的中部提供升力,从而保证本装置有足够的升力,通过设置辅助升力模块,为本装置边缘处提供升力,使得本装置在飞行时不容易被风吹偏,从而增强了本装置的抗风性,通过设置调节模块,可以通过控制调节电机来控制摆动板的摆动,从而控制本装置的飞行方向。


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    Titel :

    Unmanned aerial vehicle assisted take-off and landing system


    Weitere Titelangaben:

    一种无人机辅助起飞降落系统


    Beteiligte:
    SUN XIAOYU (Autor:in)

    Erscheinungsdatum :

    20.11.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / 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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