The invention relates to a multi-constraint airfoil joint riveting device, belongs to the technical field of aircraft mounting and manufacturing, and solves the problem of inaccurate positioning of a main wing and an aileron during assembly of the main wing and the aileron. The device comprises a rudder shaft positioning device and an airfoil adjusting and riveting device, the rudder shaft positioning device comprises a positioning connector and a rudder shaft simulation piece. The positioning joint is used for positioning the main wing; the rudder shaft simulation piece is matched with the aileron and is used for positioning the aileron; the airfoil adjusting and riveting device comprises a pressing plate, a base plate and an adjusting assembly. The pressing plate and the base plate are hooped on the outer side of the main wing, the aileron is arranged between the pressing plate and the base plate, and the position of the aileron can be adjusted through the adjusting assembly; the pressing plate is provided with a joint riveting hole for reserving a space for riveting the adapter; after the main wing and the aileron are hooped and positioned through the multiple sets of wing face adjusting and riveting devices, the aileron and the main wing can be riveted at the joint riveting holes. According to the invention, the positioning of the main wing and the aileron of the aerospace craft is realized, and the installation precision of the wing surface is improved.
本发明涉及一种多约束翼面接头铆接装置,属于飞行器安装制造技术领域,解决了主翼和副翼装配时,二者定位不准确的问题。本发明包括舵轴定位装置和翼面调整铆接装置;舵轴定位装置包括:定位接头和舵轴模拟件;定位接头用于定位主翼;舵轴模拟件与副翼配合,用于定位副翼;翼面调整铆接装置包括:压板、垫板和调节组件;压板和垫板箍紧在主翼的外侧,副翼设置在压板和垫板之间,且通过能够通过调节组件进行位置调节;压板上设有接头铆接孔预留转接头铆接的空间;主翼和副翼均通过多组翼面调整铆接装置进行箍紧定位后,能够在接头铆接孔处将与副翼与主翼铆接。本发明实现了航天飞行器的主翼和副翼的位置定位,提升了翼面安装精度。
Multi-constraint airfoil joint riveting device and airfoil assembling method
一种多约束翼面接头铆接装置及翼面装配方法
2024-08-09
Patent
Electronic Resource
Chinese
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