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面向机身柔性装配的在线编程技术

武锋锋 李东升 王亮

武锋锋, 李东升, 王亮等 . 面向机身柔性装配的在线编程技术[J]. 北京航空航天大学学报, 2015, 41(4): 641-648. doi: 10.13700/j.bh.1001-5965.2014.0256
引用本文: 武锋锋, 李东升, 王亮等 . 面向机身柔性装配的在线编程技术[J]. 北京航空航天大学学报, 2015, 41(4): 641-648. doi: 10.13700/j.bh.1001-5965.2014.0256
WU Fengfeng, LI Dongsheng, WANG Lianget al. Online programming technique for flexible assembly of fuselage[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(4): 641-648. doi: 10.13700/j.bh.1001-5965.2014.0256(in Chinese)
Citation: WU Fengfeng, LI Dongsheng, WANG Lianget al. Online programming technique for flexible assembly of fuselage[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(4): 641-648. doi: 10.13700/j.bh.1001-5965.2014.0256(in Chinese)

面向机身柔性装配的在线编程技术

doi: 10.13700/j.bh.1001-5965.2014.0256
基金项目: 国防基础科研资助项目
详细信息
    作者简介:

    武锋锋(1983—),女,山西洪洞人,博士生,wffqll00@163.com

    通讯作者:

    李东升(1965—),男,甘肃静宁人,教授,lidongs@buaa.edu.cn,主要研究方向为现代飞机制造工艺与先进装备、航空钣金数字化制造与钛合金构件精密成形技术和超大型曲面的超精密柔性成形制造理论与应用技术.

  • 中图分类号: V262.1

Online programming technique for flexible assembly of fuselage

  • 摘要: 为满足机身数字化装配的“一架多型”和“一架多态”深层次柔性需求,使“桥架式”柔性工装具有更好的自主适应能力,必须建立相应的运动学模型,通过在线编程技术合理地规划运动控制策略.针对机身定位形式与柔性工装特点建立了柔性工装运动学模型,研究了基于仿真模型的在线编程原理、装配基准点构建方式和运动控制策略规划技术,提出了结构功能结合工艺需求驱动的仿真环境创建方法.为快速生成运动控制指令,开发了面向机身柔性装配的在线编程系统.以某飞机后机身装配为例,验证了系统的精准性、高效性和超强自主适应能力.

     

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出版历程
  • 收稿日期:  2014-05-08
  • 修回日期:  2014-08-25
  • 网络出版日期:  2015-04-20

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