The invention provides an unmanned aerial vehicle (UAV) stacked folding wing with a trailing edge control surface, and belongs to the field of novel UAVs, the unmanned aerial vehicle comprises a fuselage connecting structure, an inner side half wing, an outer side half wing, a compression nut, a torsion spring and a locker, the inner side half wing and the outer side half wing are sequentially connected to the fuselage connecting structure in a sleeving manner; the two half wings are coaxially stacked and connected with the fuselage connecting structure through the compression nut, the half wing close to the fuselage is an inner side half wing, the other half wing is an outer side half wing, the two half wings provide rotating force through the torsion spring, and position locking is achieved through the locker; according to the invention, the blank of special-layout patrol flight unmanned aerial vehicles, especially stacked folding wings with trailing edge control surfaces, is filled up.

    本发明提供一种带后缘舵面的巡飞无人机叠放式折叠机翼,属于新型无人机领域,机身连接结构、内侧半翼、外侧半翼、压紧螺帽、扭转弹簧和锁紧器,内侧半翼和外侧半翼依次套合连接在机身连接结构上,两个半翼共轴叠放并通过压紧螺帽与机身连接结构连接,靠近机身的半翼为内侧半翼,另一个为外侧半翼,两个半翼通过扭转弹簧提供旋转力,通过锁紧器实现位置锁定;本发明填补了特殊布局巡飞无人机,尤其是带后缘舵面的叠放式折叠机翼的空白。


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    Title :

    Stacked folding wing of patrol flight unmanned aerial vehicle with trailing edge control surface


    Additional title:

    一种带后缘舵面的巡飞无人机叠放式折叠机翼


    Contributors:
    ZHAO CHANGHUI (author) / LIU XU (author) / SONG KAI (author) / ZHANG QINZHI (author) / REN LULU (author) / QIAO ZHIBIN (author)

    Publication date :

    2025-01-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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