期刊文献+

利用分段G^2插值方法构造铺丝路径 被引量:1

Constructing Fiber Placement Paths With Piecewise G^2 Interpolation
下载PDF
导出
摘要 提出了复合材料铺丝路径的规划方法,其中铺丝基准路线是通过对给定数据点的切方向及曲率向量或测地曲率值,G2连续地插值曲面上点列的方法得到。利用正则参数曲面上一点的切空间与其参数平面对应点的切空间同构原理。将曲面上曲线的插值问题转化为其参数平面上类似的曲线插值问题。该方法能够用显式方程来表示曲面上的G2连续插值曲线。由于引入了若干控制参数,可对曲线进行局部或整体的交互修改。利用该方法进行铺丝路径规划可以反映芯模面的曲率信息,改变纤维的局部走向,使其最终的结果更好地满足丝束铺放要求和构件几何性能的要求。实验证明该方法简单可行,还可用于计算机辅助设计、计算机图形学等领域。 This paper presents a method for path planning of robotic fiber placement,where the initial path is created with curvature continuous(G2) interpolation of data points on surface with specified tangent direction and curvature vector at every point.Making use of some conclusions deduced from the isomorphic relations between tangent spaces of both surface and its parametric domain at corresponding points,we convert the problem of curve interpolation on a parametric surface to a similar one on its parametric plane.The method enables us to express G2 interpolation curve of an arbitrary sequence of points on a parametric surface explicitly in parametric form.For introducing several free parameters into the method,we can modify the curve's shape locally or globally.Moreover,the resulted placement path can reflect the curvature of the mould surface and change the fiber's direction locally so as to satisfy better the demand of both fiber placement and surface geometry.Experiments demonstrate the method is simple,feasible and also applicable to computer aided design and computer graphics,etc.
出处 《宇航材料工艺》 CAS CSCD 北大核心 2010年第3期18-22,共5页 Aerospace Materials & Technology
基金 国家自然科学基金(Nos.60673026&50475041)
关键词 HERMITE插值 连续 参数曲面 铺丝路径 Hermite interpolation G2 continuity Parametric surface Fiber placement path
  • 相关文献

参考文献10

二级参考文献28

  • 1林福建.自动铺丝束成型的关键技术[J].组合机床与自动化加工技术,2005(3):25-26. 被引量:6
  • 2安鲁陵,许斌.复合材料纤维铺放自动编程技术研究[J].工程设计学报,2005,12(2):80-84. 被引量:11
  • 3陈亚莉.复合材料在飞机上的新应用[J].航空维修与工程,2005(3):31-32. 被引量:10
  • 4邵冠军,游有鹏,熊慧.自由曲面构件的纤维铺放路径规划[J].南京航空航天大学学报,2005,37(B11):144-148. 被引量:30
  • 5金通光,科技报告,1988年
  • 6Tosh M W, Kelly D W. Fiber steering for a composite C-beam[J]. Composite Structures, 2001, 53:133~141.
  • 7Gliesche K, Hubner T, Orawetz H. Application of the tailored fibre placement (TFP) process for a local reinforcement on an "open-hole" tension plate from carbon/epoxy laminates [J]. Composites Science and Technology, 2003,63: 81~88.
  • 8Li R, Kelly D, Crosky A. Strength improvement by fibre steering around a pin loaded hole[J]. Composite Structures, 2002, 57:377~383.
  • 9熊慧.[D].南京:南京航空航天大学,2004.
  • 10Foong C W,Shirinzadeh B,Cassidy G,et al.Force-based trajectory generation for robotic fibre placement on large complex surfaces[C]//Proceedings of 7th International Conference on Manufacturing.Thailand:[s.n.],2002.

共引文献80

同被引文献23

引证文献1

二级引证文献28

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部