A Design Procedure for Textile Composite Materials

Y. Gowayed, L. Barowski
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引用次数: 5

Abstract

A design procedure for textile composite materials that is able to satisfy a set of target mechanical and thermal properties is presented. First the search space, within which a feasible solution may exist, is divided into discrete sections. These sections are sufficiently small so that material properties show little variation. In each section, the composite is defined as a set of yarn segments that possess certain relative volume fractions, initial elliptical cross-section shape, and spatial direction cosines. A unique solution is calculated using a stiffness averaging routine. Solutions are then compared and ranked based on a chosen selection criterion. The nature of the textile forming process is considered in the design approach. Proposed textile preforms are graphically constructed in 3-D space. The feasibility of changing the elliptical cross-section shape of yarns at different locations to fit within a high fiber-volume-fraction composite is investigated. A distortion factor is introduced to characterize the departure of the yarn cross-section from an initial elliptical shape. Two shapes for yarns cross-section, race track and boat-shape, are parametrically defined and used in the model.
纺织复合材料的设计程序
提出了一种纺织复合材料的设计方法,使其能满足一定的力学和热性能要求。首先,将可能存在可行解的搜索空间划分为离散的部分。这些截面足够小,因此材料性质变化不大。在每个截面中,复合材料被定义为一组具有一定相对体积分数、初始椭圆截面形状和空间方向余弦的纱线段。利用刚度平均程序计算出唯一解。然后根据选定的选择标准对解决方案进行比较和排序。在设计方法中考虑了纺织品成型过程的性质。所提出的纺织预制品在三维空间中以图形方式构造。研究了改变不同部位纱线的椭圆截面形状以适应高纤维体积分数复合材料的可行性。引入畸变因子来表征纱线横截面偏离初始椭圆形状的情况。在模型中参数化定义了纱线横截面的两种形状,赛道形状和船型形状。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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