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基于非正交干涉矩阵的飞机装配序列规划方法

孙占磊 赵罡 韩鹏飞 郭春英

孙占磊, 赵罡, 韩鹏飞, 等 . 基于非正交干涉矩阵的飞机装配序列规划方法[J]. 北京航空航天大学学报, 2013, 39(5): 615-620.
引用本文: 孙占磊, 赵罡, 韩鹏飞, 等 . 基于非正交干涉矩阵的飞机装配序列规划方法[J]. 北京航空航天大学学报, 2013, 39(5): 615-620.
Sun Zhanlei, Zhao Gang, Han Pengfei, et al. Assembly sequence planning for aircraft based on non-orthogonalinterference matrix[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(5): 615-620. (in Chinese)
Citation: Sun Zhanlei, Zhao Gang, Han Pengfei, et al. Assembly sequence planning for aircraft based on non-orthogonalinterference matrix[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(5): 615-620. (in Chinese)

基于非正交干涉矩阵的飞机装配序列规划方法

基金项目: 国家"863"计划重点资助项目(2009AA043302,2009AA043306)
详细信息
  • 中图分类号: V262.4

Assembly sequence planning for aircraft based on non-orthogonalinterference matrix

  • 摘要: 针对飞机装配中外形曲面特征多、装配关系复杂、连接方式多样等带来的装配工艺设计问题,提出了一种基于非正交干涉矩阵的飞机部件装配序列规划方法.通过分析被装配零件的结构特点,增加非正交的装配坐标方向,构建了非正交干涉矩阵;给出了装配可行性的推导方法,实现了装配序列的自动生成.并以装配时间为目标函数,采用遗传算法对装配序列进行了优化.基于MATLAB仿真平台,对某型号飞机舱门装配过程进行了模拟.仿真结果表明,该方法简单易行.与传统的基于正交干涉矩阵的方法相比,对于可装配性和装配效率都有显著提高.

     

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出版历程
  • 收稿日期:  2013-01-23
  • 修回日期:  2013-04-16
  • 网络出版日期:  2013-05-31

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