The invention discloses an unmanned aerial vehicle front flap control surface structure which is characterized in that a front flap control surface is divided into an active front flap control surface and a follow-up front flap control surface, the active front flap control surface and the follow-up front flap control surface are connected through a control surface upper connecting piece and a control surface lower connecting piece, and a control surface deflection rudder angle seat is mounted on the active front flap control surface; a control surface deflection rudder angle seat is installed on the front flap control surface, a control surface deflection rudder angle is connected between the control surface deflection rudder angle seat and the wing stabilizer, a follow-up rudder angle seat is installed on the front flap control surface, a follow-up rudder angle is connected between the follow-up rudder angle seat and the wing stabilizer, and the deflection axis position of the front flap control surface is close to the bottom of the control surface of the front flap control surface. The front flap control surface is easy to disassemble, assemble, install and position quickly, and facilitates transportation of a scaling unmanned aerial vehicle applying the front flap control surface and quick assembly of the unmanned aerial vehicle after transportation.

    本发明公开了一种无人机前襟翼舵面结构,前襟翼舵面分割为主动前襟翼舵面和随动前襟翼舵面,主动前襟翼舵面和随动前襟翼舵面通过舵面上连接件、舵面下连接件连接,主动前襟翼舵面安装有舵面偏转舵角座,舵面偏转舵角座和机翼安定面之间连接有舵面偏转舵角,随动前襟翼舵面安装有随动舵角座,随动舵角座和机翼安定面之间连接有随动舵角,前襟翼舵面的偏转轴线位置靠近其舵面底部。本发明的前襟翼舵面易于快速拆装与安装定位,便于其应用的缩比无人机运输以及运输后无人机的快速组装。


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    Titel :

    Front flap control surface structure of unmanned aerial vehicle


    Weitere Titelangaben:

    一种无人机前襟翼舵面结构


    Beteiligte:
    LUO WEI (Autor:in) / ZHU ZHUANG (Autor:in) / LIU JINLONG (Autor:in) / MA YUE (Autor:in) / ZHOU YIDONG (Autor:in) / GUO SHUAI (Autor:in) / YANG SHUAI (Autor:in) / WEI JIANFENG (Autor:in) / HE JUHENG (Autor:in)

    Erscheinungsdatum :

    2022-07-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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