The invention relates to an aircraft wing and fuselage assembly auxiliary system, belongs to the technical field of aircraft assembly, and solves the problems that the mounting position is difficult to accurately determine and the assembly efficiency is low in the aircraft assembly process. The system comprises a bracket supporting part, a visual guiding part, an industrial control center and a carrying assembly. The visual guiding part is mounted on the machine body mounting assembly; the bracket supporting component comprises a flexible supporting assembly and a bracket assembly. Two ends of the bracket assembly are connected with flexible supporting assemblies; the wing mounting assembly is clamped on the flexible supporting assembly; the carrying assembly comprises a carrying unit and a supporting frame adjusting unit. The lower end of the supporting frame adjusting unit is connected with the carrying unit, and the upper end of the supporting frame adjusting unit is connected with the lower end of the bracket assembly. The industrial control center can receive signals transmitted by the visual guiding component and the bracket supporting component and control the carrying assembly and the bracket supporting component to conduct displacement adjustment. The system is suitable for large component hole series butt joint assembly easy to deform, and the application range is wide.
本发明涉及一种飞行器机翼机身装配辅助系统,属于飞机装配技术领域,解决了飞行器装配过程中安装位置难以精确确定,装配效率低的问题。本发明的系统包括托架支撑部件、视觉引导部件、工控中心和运载组件;视觉引导部件安装在机身安装组件上;托架支撑部件包括柔性支撑组件和托架组件;托架组件两端连接柔性支撑组件;机翼安装组件装夹在柔性支撑组件上;运载组件包括运载单元和支撑架调整单元;支撑架调整单元下端连接所述运载单元,支撑架调整单元上端连接所述托架组件的下端;工控中心能够接收所述视觉引导部件和托架支撑部件传输的信号,控制运载组件和托架支撑部件做位移调整。本发明的系统适用于易于变形的大部件孔系对接装配,应用广泛。
Aircraft wing and fuselage assembly auxiliary system
一种飞行器机翼机身装配辅助系统
2023-12-08
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 |
Double-fuselage tandem rotor wing composite wing aircraft layout
European Patent Office | 2021
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