The invention relates to an aircraft wing and fuselage assembly control method, belongs to the technical field of aircraft assembly, and solves the problems of complicated adjustment of poses of wings relative to a fuselage, difficulty in accurate centering of assembly connection positions and low assembly efficiency in an aircraft assembly process. The control method comprises the steps that preparation work is conducted, the wing installation assembly is clamped to the aircraft wing and fuselage assembly auxiliary system, the carrying assembly drives the wing installation assembly to enter the assembly position, multi-point-position assembly is conducted on the wing installation assembly through the fastening device, the wing installation assembly is connected with the fuselage installation assembly, and the auxiliary tool is withdrawn. Comprising the steps that an industrial control center receives and processes data collected by a sensing part, control information of an execution element is generated, and assembly from a wing installation assembly to a fuselage installation assembly is completed. According to the control method, the automation degree is high, integrated execution element linkage can be achieved, the assembly precision and efficiency are greatly improved, and the aircraft can be prevented from generating unreasonable assembly stress. The method is wide in application.
本发明涉及一种飞行器机翼机身装配控制方法,属于飞机装配技术领域,解决了飞行器装配过程机翼相对机身位姿调整繁复、装配连接位置难以精确对中、装配效率低的问题。本发明的控制方法包括准备工作、将机翼安装组件装夹到飞行器机翼机身装配辅助系统上、运载组件带动机翼安装组件进入装配位置、通过紧固装置将机翼安装组件进行多点位装配,与机身安装组件连接、撤出辅助工装的步骤,其中,包括工控中心接受并处理传感部件采集的数据、生成对执行元件的控制信息,完成机翼安装组件向机身安装组件的装配。本发明控制方法自动化程度高,能实现集成化的执行元件联动,大幅提高了装配精度和效率,可避免飞行器产生不合理装配应力。本发明方法应用广泛。
Aircraft wing and fuselage assembly control method
一种飞行器机翼机身装配控制方法
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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