The invention discloses an aircraft large component linkage involution attitude-adjusting assembly device and attitude-adjusting assembly method.The aircraft large component linkage involution attitude-adjusting assembly device comprises a chassis framework, a front fuselage linkage attitude-adjusting device, a middle fuselage linkage attitude-adjusting device and a rear fuselage linkage attitude-adjusting device are arranged at the top of the chassis framework, and the front fuselage linkage attitude-adjusting device, the middle fuselage linkage attitude-adjusting device and the rear fuselage linkage attitude-adjusting device are matched according to the superposition principle of space rotation and translation vectors. Through linkage posture adjusting cooperation of the posture adjusting device, the machine body large component is translated and rotated in the axial direction, the radial direction and the vertical direction of the machine body, unified posture adjustment of the machine body large component in the space is achieved, operation is more convenient and rapid, and the posture adjusting position precision is more accurate; the middle fuselage, the front fuselage and the rear fuselage are assembled after working time sequence decomposition, adjustment and positioning, so that attitude adjustment and subsequent assembly and connection of large components of the aircraft can be completed by one person, and the problem of mismatching of overall attitude adjustment operation through cooperation of multiple persons in a traditional attitude adjustment fixture is solved; and meanwhile, the problems that a traditional involution posture adjusting assembly fixture is difficult to operate and the posture adjusting and aligning precision is not high are solved.

    本发明公开了一种飞机大部件联动对合调姿装配装置及调姿装配方法,包括底盘骨架,所述底盘骨架的顶部设置有前机身联动调姿装置、中机身联动调姿装置、后机身联动调姿装置,根据空间旋转、平移矢量的叠加原理,通过调姿装置的联动调姿配合,将机身大部件空间调姿按机身轴向、机身径向、竖直方向进行平移及旋转,实现对机身大部件在空间中的统一姿态调节,操作更加方便快捷,且调姿位置精度更加准确;通过中机身、前机身、后机身的工作时序分解调资定位后再进行装配,可以一人即可完成对飞机大部件的调姿以及后续装配连接,避免传统调姿型架多人协作整体调姿操作不匹配问题,同时也改善了传统对合调姿装配型架难以操作、调姿对位精度不高的问题。


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    Title :

    Linkage involution posture-adjusting assembly device and posture-adjusting assembly method for large components of airplane


    Additional title:

    一种飞机大部件联动对合调姿装配装置及调姿装配方法


    Contributors:
    PENG WENWU (author) / MAO CHAODONG (author) / LUO YONG (author) / BI XIUWEN (author) / DENG JUN (author) / DENG ZHENBO (author) / ZHAO JIANWEI (author) / ZHU JINSONG (author) / ZHANG LIN (author)

    Publication date :

    2024-10-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    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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