The invention discloses a support method for assembling, adjusting and positioning an aircraft body component. An integral tool bracket is used for supporting the aircraft body component, a three-coordinate positioning system is cross-linked with the integral tool bracket, the three-coordinate positioning system is used for adjusting the posture of the aircraft body component by adjusting the integral tool bracket, and the integral tool bracket replaces a traditional independently installed supporting joint, so that assembly stress generated by posture adjustment caused by a supporting mode isavoided, product quality is improved, a process is simple and convenient to operate, rapid transfer of the aircraft body component is achieved, and the support method has universality in posture adjustment and positioning of the aircraft body component.

    一种飞机机体部件装配调姿定位的支撑方法,通过一个整体式工装托架支撑飞机机体部件,有一个三坐标定位系统与整体式工装托架交联,通过三坐标定位系统调整整体式工装托架实现对飞机机体部件的姿态调整,通过整体式工装托架代替传统的独立安装的支撑接头,避免了支撑方式导致调姿产生的装配应力,提高产品质量,工艺过程简单,操作方便,实现飞机机体部件的快速转站,对飞机机体部件的调姿定位具有普遍的推广性。


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    Titel :

    Support method for assembling, adjusting and positioning aircraft body component


    Weitere Titelangaben:

    一种飞机机体部件装配调姿定位的支撑方法


    Beteiligte:
    MAO XINYU (Autor:in) / GE XIAODONG (Autor:in) / HAN JIAWEI (Autor:in)

    Erscheinungsdatum :

    24.11.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    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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