The invention relates to the technical field of aircrafts, in particular to a high-speed unmanned aerial vehicle and an empennage thereof. Wherein the inner side of the stabilizer is used for being fixed to a fuselage, and the inner side of the control plane is attached to the outer side of the stabilizer; the control surface control system is rotationally connected to the upper surface of the stabilizer, the outer end of the control surface control system is fixedly connected to the portion, close to the inner side, of the upper surface of the control surface, the inner end of the control surface control system is fixedly connected to the output end of the torsion steering engine, and the torsion steering engine is located in the unmanned aerial vehicle body. The aerodynamic characteristic and the control characteristic of the unmanned aerial vehicle during high-speed flight are improved.

    本申请涉及飞行器技术领域,尤其涉及一种高速无人机及其尾翼,包括:扭转舵机、安定面、舵面和舵面操纵系统;其中,安定面的内侧用于固定至机身,舵面的内侧贴至安定面的外侧;舵面操纵系统转动连接于安定面的上表面,并且舵面操纵系统的外端固定连接于舵面的上表面靠近内侧的部分,舵面操纵系统的内端固定连接于扭转舵机的输出端,并且扭转舵机位于无人机机身内。本申请提高了无人机在高速飞行时候的气动特性和操纵特性。


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    Titel :

    High-speed unmanned aerial vehicle and empennage thereof


    Weitere Titelangaben:

    一种高速无人机及其尾翼


    Beteiligte:
    HANEDUN BILLIG CO LTD (Autor:in) / JIA HAO (Autor:in) / LI YUECONG (Autor:in) / LIU HONGBIAO (Autor:in) / LIANG XIAO (Autor:in) / WANG HONGGUANG (Autor:in)

    Erscheinungsdatum :

    14.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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