The invention belongs to the field of unmanned aerial vehicle structures, and discloses an unmanned aerial vehicle and a fuselage fairing structure thereof, the unmanned aerial vehicle comprises a cover body, the top of the cover body is provided with a hinge joint connected with a fuselage of the unmanned aerial vehicle, the cover body is also provided with a quick release lock connected with the fuselage of the unmanned aerial vehicle, and the cover body is internally provided with an air support rod connected with the fuselage of the unmanned aerial vehicle; when the quick-release lock releases the connection between the cover body and the fuselage of the unmanned aerial vehicle, the air supporting rod can upwards support the cover body, and when the air supporting rod upwards supports the cover body, the cover body rotates around the hinge joint. The fuselage fairing structure of the unmanned aerial vehicle is convenient to open, and then maintenance of the large freight unmanned aerial vehicle is facilitated.

    本发明属于无人机结构领域,公开了一种无人机及其机身整流罩结构,包括罩体,罩体的顶部设有与无人机的机身连接的铰链接头,罩体上还设有与无人机的机身连接的快卸锁,罩体的内部设有与无人机的机身连接的气撑杆;当快卸锁解除罩体与无人机的机身连接后,所述气撑杆能够向上撑起罩体,当气撑杆向上撑起罩体过程中,罩体绕所述铰链接头转动。本发明无人机的机身整流罩结构便于开启,进而有利于大型货运无人机的维护。


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    Title :

    Unmanned aerial vehicle and fuselage fairing structure thereof


    Additional title:

    一种无人机及其机身整流罩结构


    Contributors:
    MA JIN (author) / FENG SIDONG (author) / WANG ZHANHU (author)

    Publication date :

    2025-02-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



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