The invention belongs to the field of aviation, and discloses a wing movable surface structure and an assembly method.According to the wing movable surface structure and the assembly method, an inner flap, an outer flap, an aileron and a spoiler are installed on a wing and then adjusted to the mechanical zero position, and then the deflection angles of the inner flap and the outer flap are determined through a curve measuring device; and measuring the inner flap and the outer flap when the inner flap and the outer flap deflect from the mechanical zero position to 17 degrees and 35 degrees until the design requirements are met. Hinge points of the inner flap rocker arm, the inner flap support arm, the first outer flap support arm, the second outer flap support arm and the third outer flap support arm can be coaxially arranged quickly and effectively, so that the production efficiency of an airplane is improved, and the stability of the airplane is improved.

    本发明属于航空领域,公开了一种机翼活动面结构及装配方法,本发明将内襟翼、外襟翼、副翼和扰流板安装在机翼上后,调整至机械零位,再通过曲线测量装置确定内襟翼和外襟翼的偏转角度,进行内襟翼和外襟翼从机械零位偏转至17°和35°状态时的测量工作,直至满足设计要求。本发明能够快速有效的将内襟翼摇臂、内襟翼支臂、外襟翼第一支臂、外襟翼第二支臂和外襟翼第三支臂的铰接点同轴设置,从而提高飞机生产效率,提高飞机的稳定性。


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    Titel :

    Wing movable surface structure and assembling method


    Weitere Titelangaben:

    一种机翼活动面结构及装配方法


    Beteiligte:
    SHI SUIXIN (Autor:in) / HAN SHUANGBO (Autor:in) / YANG GAO (Autor:in)

    Erscheinungsdatum :

    2024-03-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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