According to the position and posture adjusting device and method for aircraft component installation, the position and posture adjusting device comprises a base, a driving mechanism and an installation mechanism, a main body of the installation mechanism is a C-shaped stabilizing ring, the C-shaped stabilizing ring is hinged to an installation base, and an aircraft component is fixed in the C-shaped stabilizing ring through a clamping hydraulic cylinder; the first servo motor drives the mounting mechanism to move up and down to adjust the posture through the screw rod, the two ends of the screw rod are connected to the base stand column, and the second servo motor drives the mounting mechanism to rotate horizontally to adjust the posture through the meshing fluted disc on the mounting base. And the third servo motor drives the C-shaped stable ring pin shaft to rotate up and down to adjust the posture through a driving gear on the mounting seat.

    一种飞机部件安装用位姿调整装置及调整方法,包括基座、驱动机构和安装机构,安装机构的主体为C型稳固环,C型稳固环铰接在安装座上,飞机部件通过夹持液压缸固定在C型稳固环内;第一伺服电机通过螺旋杆带动安装机构上下运动调姿,螺旋杆的两端连接在基座立柱上,第二伺服电机通过安装座上的啮合齿盘带动安装机构水平转动调姿,所述的第三伺服电机通过安装座上的驱动齿轮带动C型稳固环绕销轴上下转动调姿。


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    Title :

    Pose adjusting device and method for aircraft component installation


    Additional title:

    一种飞机部件安装用位姿调整装置及调整方法


    Contributors:
    XIE QIANLIANG (author) / ZOU FENG (author) / ZHANG HAO (author) / BAI YUNPENG (author) / LIAN CHAO (author)

    Publication date :

    2023-08-22


    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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