The invention discloses an unmanned aerial vehicle refueling mechanism and method. A front oil filler cap and a rear oil filler cap are arranged at the top of a head of an unmanned aerial vehicle; the near-rear end of the front oil filler cap is connected to the wall of a refueling cabin through a front hydraulic supporting rod, and the near-front end of the rear oil filler cap is connected to the wall of the refueling cabin through a rear hydraulic supporting rod; a refueling connector is fixed to the inner side of the rear oil filler cap, and the front hydraulic supporting rod and the rear hydraulic supporting rod are controlled by the refueling controller. When the unmanned aerial vehicle is refueled, the refueling controller firstly opens the front oil filler cap and then opens the rear oil filler cap, so that the refueling connector extends out of the refueling cabin together with the oil filler cap for refueling.

    一种无人机受油机构及受油方法,在无人机的机头顶部设有前加油口盖和后加油口盖,前加油口盖的近后端通过前液压支杆连接在加油舱的舱壁上,后加油口盖的近前端通过后液压支杆连接在加油舱的舱壁上,受油接头固定在后加油口盖的内侧,所述的前液压支杆、后液压支杆受加油控制器控制。无人机受油时,加油控制器首先将前加油口盖打开,再将后加油口盖打开,使受油接头随后加油口盖一起伸出加油舱受油。


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    Titel :

    Unmanned aerial vehicle refueling mechanism and oil receiving method


    Weitere Titelangaben:

    一种无人机受油机构及受油方法


    Beteiligte:
    LI CHEN (Autor:in) / CUI YAN (Autor:in) / LU LU (Autor:in) / SUN WEITAO (Autor:in)

    Erscheinungsdatum :

    2021-07-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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