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方舟, 马保吉, 曹岩, 姚慧. 复合纤维缠绕模型的缺陷仿真设计[J]. 计算机辅助设计与图形学学报, 2014, 26(10): 1894-1899,1908.
引用本文: 方舟, 马保吉, 曹岩, 姚慧. 复合纤维缠绕模型的缺陷仿真设计[J]. 计算机辅助设计与图形学学报, 2014, 26(10): 1894-1899,1908.
Fang Zhou, Ma Baoji, Cao Yan, Yao Hui. Defect Simulation Design of Composite Filament Winding Model[J]. Journal of Computer-Aided Design & Computer Graphics, 2014, 26(10): 1894-1899,1908.
Citation: Fang Zhou, Ma Baoji, Cao Yan, Yao Hui. Defect Simulation Design of Composite Filament Winding Model[J]. Journal of Computer-Aided Design & Computer Graphics, 2014, 26(10): 1894-1899,1908.

复合纤维缠绕模型的缺陷仿真设计

Defect Simulation Design of Composite Filament Winding Model

  • 摘要: 为解决复合纤维缠绕制品三维设计仿真、应力和变形分析问题,以复杂三维模型构造方法为研究对象,提出基于三维模型数据重构的程序驱动方法创建三维大型缠绕纤维模型.首先以网格化的数据结构作为三维模型中心线上控制点坐标信息的组织形式;然后以圆柱形螺旋方程为基础,结合几何图形变换的方法生成全部控制点坐标;再根据用户输入的缺陷参数,由缠绕于芯轴上的第1层纤维起逐层向外查找缺陷产生的位置并依次修正控制点的坐标参数,生成有缺陷的纤维缠绕模型.该方法将较为复杂的圆锥螺旋线缺陷计算问题转变为对三维圆柱螺旋线上点坐标计算和几何图形变换问题,简化了中心线上控制点的定位坐标计算和逻辑关系判定.实验结果表明,文中方法可以创建任意长度纤维缠绕时具有多个缠绕缺陷,且单层轴向累计误差小于等于1.5倍纤维直径的复合缠绕缺陷模型.

     

    Abstract: In order to achieve the three-dimensional (3D) simulation of composite fibre winding, a program-driven method of constructing 3D large fibre winding models based on 3D model data reconstruction is put forward.First, agrid data structure is used to organize the coordinate data of control points on the centerline of a 3D model.Then, based on the cylindrical helix equation and geometric transformation, the coordinates of all the control points are generated.After that, according to the defective parameters input by the user, from the first fibre layer on the core, the locations of defects are determined layer by layer from the inside to the outside.Finally, the coordinates of the control points are modified in turn to generate a fibre winding model with defects.The method converts the complex defect computation on a conical helix into the coordinate computation on a cylindrical helix and geometric transformation.It simplifies the coordinate computation of the control points on the centerline and logical relation determination.The experimental results show that the method can be applied to the generation of the fibre winding defect model of any length with multiple defects where the accumulative axial error of one layer is no more than 1.5 times of the fibre diameter.

     

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