The invention relates to a multi-constraint airfoil assembly method, belongs to the technical field of aircraft installation and manufacturing, and solves the problem of inconvenience in airfoil assembly in the prior art. The airfoil assembly method comprises the following steps: S1, fixing an adapter and an aileron; after being combined with the adapter, the aileron and the main wing are pre-mounted but not connected; s2, the rudder shaft positioning device and the main wing are positioned in a matched mode; the wing surface joint riveting device is arranged outside the main wing and the aileron in a covering mode, the main wing is fixed, and at the moment, the position of the aileron can be adjusted; s3, the rudder shaft simulation piece is matched with the aileron, the relative position of the aileron and the main wing is adjusted through the adjusting assembly, and the main wing and the aileron are hooped and positioned through the wing surface connector riveting device; and S4, after the aileron and the main wing are matched in place, the adapter and the main wing are riveted and fixed, and connection of the main wing and the aileron is completed. According to the method, the orientation adjustment of the airfoil of the aerospace craft is realized, the airfoil is restrained and fixed, and the installation precision and the assembly efficiency of the airfoil are improved.
本发明涉及一种多约束翼面装配方法,属于飞行器安装制造技术领域,解决了现有技术中翼面装配不方便的问题。本发明的翼面装配方法,包括步骤S1:将转接头与副翼固定;副翼与转接头组合后与主翼预安装但不连接;步骤S2:将舵轴定位装置与主翼配合定位;将翼面接头铆接装置罩设在主翼和副翼的外部,并将主翼固定,此时副翼位置可调节;步骤S3:通过舵轴模拟件与副翼配合,通过调节组件调节副翼与主翼的相对位置,通过翼面接头铆接装置将主翼和副翼箍紧定位;步骤S4:副翼与主翼配合到位后,将转接头与主翼铆接固定,完成主翼和副翼的连接。本发明实现了航天飞行器的翼面的方位调整,并对翼面进行约束固定,提升了翼面安装精度和装配效率。
Multi-constraint airfoil assembly method
一种多约束翼面装配方法
2024-07-19
Patent
Electronic Resource
Chinese
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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