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作 者:崔兆杰[1] 金朝海[1] 武锋锋[1] 王亮[1]
机构地区:[1]北京航空航天大学机械工程及自动化学院,北京100191
出 处:《航空制造技术》2016年第17期56-61,共6页Aeronautical Manufacturing Technology
基 金:国防基础科研项目(A0520110016);国家自然科学基金项目(51205014);国际科技合作项目(2010DFB73280)
摘 要:针对机身部件"以骨架为基准"的装配特点,确定柔性工装的总体结构为桥架式,并划分了功能模块,研究了设备的"串-并"混合型调型模式。基于机型与装配状态不同,提出两类调型需求,分析基于测量反馈的调型数据传递流后,开发了专用规划仿真软件。应用表明,该调型方法可以辅助桥架式柔性工装稳定、可靠地完成调型运动。For the characteristics of fuselage assembly based on framework, the bridge-frame overall structure of fl exible tooling was ascertained, confi guration of which could be divided into several functional modules, and the parallel mixed type adjustment mode of the equipment was developed. Based on the different of aircraft types and assembly states, two kinds of adjustment requirements were put forward. Completing the analysis of the adjustment data transmission based on optical measurement feedback, the dedicated planning & simulation software was developed as well. The application show that this adjustment method could assist "bridge-frame" fl exible tooling to complete adjustment movement steadily and reliably.
分 类 号:V262.4[航空宇航科学与技术—航空宇航制造工程]
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