The invention relates to an aileron cabin structure for an aircraft. The aileron cabin structure is at least composed of an aileron cabin upper wall plate (7) and an aileron suspension support arm (6). The aileron cabin structure is not provided with an aileron cabin supporting partition plate fixedly connected with the aileron cabin upper wall plate (7). The aileron cabin upper wall plate (7) isdivided into a plurality of sections in the extending direction of wings of the aircraft, and an outward-extending cantilever beam with double fulcrums is formed through aileron suspension supportingarms (6). The aileron cabin structure for the aircraft is easy to assemble and low in maintenance cost, and the problem that the aileron cabin supporting partition plate is broken due to structural fatigue is solved from the source.

    本发明涉及一种用于飞行器的副翼舱结构。该副翼舱结构至少由副翼舱上壁板(7)和副翼悬挂支臂(6)组成。副翼舱结构未配备有固接副翼舱上壁板(7)的副翼舱支撑隔板。副翼舱上壁板(7)沿飞行器的机翼的伸展方向分为多个段并且利用副翼悬挂支臂(6)构成具有双支点的外伸悬臂梁。上述用于飞行器的副翼舱结构装配简单、维护成本低,并且从源头上解决了副翼舱支撑隔板因结构疲劳而断裂的问题。


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    Titel :

    Aileron cabin structure for aircraft


    Weitere Titelangaben:

    用于飞行器的副翼舱结构


    Beteiligte:
    HUA WENZHONG (Autor:in) / WENG CHENTAO (Autor:in) / KE ZHIQIANG (Autor:in) / LI XIAOJUN (Autor:in) / XU PEI (Autor:in) / YANG XUERUI (Autor:in)

    Erscheinungsdatum :

    05.06.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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