The invention provides an unmanned aerial vehicle wing externally-hung structure and an unmanned aerial vehicle, and relates to the field of unmanned aerial vehicle mounting, and the unmanned aerial vehicle wing externally-hung structure comprises a first stiffening beam assembly, a second stiffening beam assembly, a plurality of supporting rods and a mounting connector; the first stiffening beam assembly is arranged on a front beam of a wing, the second stiffening beam assembly is arranged on a rear beam of the wing, the supporting rods are connected with the first stiffening beam assembly and the second stiffening beam assembly, and the two ends of the mounting connector are connected to the bottom of the first stiffening beam assembly and the bottom of the second stiffening beam assembly respectively. The front beam and the rear beam of the wing can be reinforced, the mounting capacity of the wing is improved, the stability of the unmanned aerial vehicle is improved, and the cargo carrying requirement is met.

    本发明提供一种无人机机翼外挂结构和无人机,涉及无人机挂载领域,包括第一加强梁组件、第二加强梁组件、多根支撑杆和挂载接头;第一加强梁组件设置在机翼的前梁上,第二加强梁组件设置在机翼的后梁上,多根支撑杆连接第一加强梁组件和第二加强梁组件,挂载接头的两端分别连接在第一加强梁组件的底部和第二加强梁组件的底部。本发明能够对机翼的前梁、后梁进行加强,增加机翼的挂载能力,提高无人机的稳定性,满足货物的搬运需求。


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    Titel :

    Unmanned aerial vehicle wing external hanging structure and unmanned aerial vehicle


    Weitere Titelangaben:

    一种无人机机翼外挂结构和无人机


    Beteiligte:

    Erscheinungsdatum :

    2024-04-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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