The invention belongs to the technical field of unmanned aerial vehicle aileron mechanisms. The unmanned aerial vehicle aileron mechanism comprises a steering engine connector arranged in a vehicle body, a wing assembly and a wing assembly, the rear aileron is connected to the rear side of the wing; one end of the aileron transmission shaft is connected with the rear aileron, and the other end of the aileron transmission shaft penetrates through the fuselage longitudinal beam, extends into the fuselage and is connected with the steering engine connector; the aileron transmission shaft comprises a connector, one end of which is fixedly connected to one side, close to the fuselage, of the rear aileron; one end of the aileron rotating shaft is fixed to the connector, the other end of the aileron rotating shaft penetrates through the fuselage longitudinal beam to be connected with the steering engine connector, and the aileron rotating shaft is connected with the fuselage longitudinal beam through a first bearing. The aileron rotating mechanism and the steering engine can be placed in the fuselage through the aileron transmission shaft, the designable space of the aileron rotating mechanism is increased, and the requirement and influence of the aileron rotating mechanism on the aerodynamic configuration are avoided. And the device has the advantages of simplicity in installation, convenience in disassembly, stable structure, short manufacturing period and the like.

    本发明属于无人机副翼机构技术领域。公开一种无人机副翼机构及无人机,包括:舵机接头,布置在机身内;后副翼,连接在机翼后侧;副翼传动轴,一端与后副翼连接,另一端穿过机身纵梁并伸入机身内,副翼传动轴的另一端与舵机接头连接;副翼传动轴包括:连接头,一端连接固定在后副翼靠近机身的一侧;副翼转轴,一端与连接头固定,另一端穿过机身纵梁与舵机接头连接,副翼转轴通过第一轴承与机身纵梁连接。本发明能够实现通过副翼传动轴将副翼转动机构以及舵机放置于机身内,增加了副翼转动机构可设计空间,避免了其对气动外形的要求和影响。且具有安装简单、拆卸方便、结构稳定、制造周期短等诸多优点。


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    Titel :

    Unmanned aerial vehicle aileron mechanism and unmanned aerial vehicle


    Weitere Titelangaben:

    一种无人机副翼机构及无人机


    Beteiligte:
    CHEN JIAMING (Autor:in) / JU XIAOBIN (Autor:in) / GONG RUIJUN (Autor:in) / WANG ZHENYU (Autor:in) / CHEN MOYAN (Autor:in)

    Erscheinungsdatum :

    2023-12-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U



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