The invention discloses an unmanned aerial vehicle parachute throwing device and an unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles. The unmanned aerial vehicle parachute throwing device comprises a base mechanism, the base mechanism comprises a base, a middle concave part is formed in the middle of the upper surface of the base, four clamping holes are formed in the outer sides of the front, rear, left and right peripheries of the upper surface of the base, rotating grooves are formed in the peripheries of the side walls of the lower end of the middle concave part, and the rotating grooves are fan-shaped; the number of the rotating grooves is four, the four rotating grooves correspond to the four clamping holes in a one-to-one mode, the lower ends of the clamping holes are correspondingly communicated with the rotating grooves, throwing grooves are formed in the two sides of the upper inner wall of each rotating groove, the throwing grooves upwards penetrate through the base, plate grooves are evenly formed in the periphery of the upper surface of the base at equal intervals, the number of the plate grooves is four, and the four plate grooves are in an arc shape. According to the unmanned aerial vehicle parachute throwing device and the unmanned aerial vehicle, parachute throwing movement of parachute opening failure is automatically completed, and it is guaranteed that the unmanned aerial vehicle cannot be influenced by a parachute and lose maneuverability.

    本发明公开了一种无人机抛伞装置及无人机,涉及无人机技术领域。该一种无人机抛伞装置及无人机,包括底座机构,底座机构包括底座,底座的上表面中部开设有中凹,底座的上表面前后左右四周外侧均开设有卡孔,卡孔的数量为四个,中凹的下端侧壁四周均开设有转动槽,转动槽呈现扇形,转动槽的数量为四个,四个转动槽与四个卡孔一一对应,卡孔的下端对应连通转动槽,每个转动槽的上内壁两侧均开设有抛槽,抛槽向上贯穿底座,底座的上表面四周等距均与的开设有板槽,板槽的数量为四个,四个板槽呈现圆弧形,该一种无人机抛伞装置及无人机自动的完成开伞失败的抛伞运动,保证无人机可以不被降落伞影响失去操纵性。


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    Titel :

    Unmanned aerial vehicle parachute throwing device and unmanned aerial vehicle


    Weitere Titelangaben:

    一种无人机抛伞装置及无人机


    Beteiligte:
    HE JUAN (Autor:in) / LUO DELIAN (Autor:in) / YANG SHA (Autor:in) / ZENG LIJUAN (Autor:in) / KANG SHUAI (Autor:in)

    Erscheinungsdatum :

    2022-06-24


    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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