The invention belongs to the technical field of aircraft design, and particularly relates to a flaperon movement mechanism and an assembly compensation method thereof, the complex flaperon movement mechanism can be easily installed through the compensation structure, and additional stress caused by forced assembly can be avoided through adopted compensation measures; meanwhile, the position and the posture of the flaperon can be conveniently adjusted so as to meet the gap order difference requirement between the flaperon and the wing; in addition, the assembly compensation structural form is combined with control over free tolerance at the intersection point, the accumulative error of the mechanism is controlled within a small range, and the control precision of the mechanism is high.

    本申请属于飞机设计技术领域,特别涉及一种襟副翼运动机构及其装配补偿方法,该补偿结构可以使复杂的襟副翼运动机构易于安装,采取的补偿措施可避免强迫装配带来的附加应力;同时,可方便调整襟副翼的位置与姿态以满足襟副翼与机翼之间的间隙阶差要求;另外,该装配补偿结构形式结合交点处自由公差的控制,将机构累积误差控制在较小范围内,机构控制精度较高。


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    Title :

    Flaperon movement mechanism and assembly compensation method thereof


    Additional title:

    一种襟副翼运动机构及其装配补偿方法


    Contributors:
    WANG SHAOTONG (author) / FENG BIANBIAN (author) / CHENG PUQIANG (author) / GUO XIANG (author)

    Publication date :

    2025-02-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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