碳纤维增强聚合物(CFRP)复合材料加工诱导分层和毛刺最小化的纤维取向驱动缺陷概率映射

IF 7 Q2 MATERIALS SCIENCE, COMPOSITES
Norbert Geier
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引用次数: 0

摘要

加工引起的毛刺和分层损害了切割碳束增强聚合物复合材料组件的完整性。因此,开发了一种基于图像的优化算法,可以在预成形余量范围内定位理想的孔中心,以最大限度地降低缺陷风险。在多种光照条件下捕获的高分辨率图像经过处理,生成毛刺和分层形成的概率图。然后,递归卷积得到一个矩阵,其最小值确定最优孔位置。首先,进行了边缘修剪实验,确定了算法的参数(临界纤维切割角及其范围)。经证实,上铣削优于下铣削,毛刺高度更小,缺陷临界纤维切削角度范围更窄。然后,基于边缘修剪结果,对孔进行圆铣,并证明优化的“最佳情况”中心将平均轮廓高度降低了64.99%,轮廓深度降低了86.51%,而毛刺和分层面积指标分别提高了84.90%和77.07%,表明了所提方法的效率和重要性。该方法在TRL 4上使用标准CNC设备和开源Python脚本实现,为将毛刺和分层最小化集成到CFRP组件设计和制造过程规划中提供了实用框架。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Fibre-orientation-driven defect probability mapping for machining-induced delamination and burr minimisation in carbon fibre-reinforced polymer (CFRP) composites
Machining-induced burrs and delamination compromise the integrity of polymer composite components reinforced by chopped carbon tows. An image-based optimisation algorithm was therefore developed that locates the ideal hole centre within the preform allowance to minimise defect risk. High-resolution images, captured under multiple lighting conditions, are processed to generate a probability map of burr and delamination formation. Then, recursive convolution yielded a matrix whose minima identified the optimal hole position. First, edge trimming experiments were conducted to determine the arguments (critical fibre cutting angle and its range) of the developed algorithm. Up-milling was confirmed to outperform down-milling, yielding an order-of-magnitude smaller burr heights and a narrower defect-critical fibre cutting angle range. Then, based on the edge trimming results, holes were circular-milled, and demonstrated that the optimised “best-case” centre reduced average contour height by 64.99 % and contour-depth by 86.51 %, while burr- and delamination-area metrics improved by 84.90 % and 77.07 %, respectively, underlying the efficiency and importance of the proposed method. Implemented at TRL 4 with standard CNC equipment and open-source Python scripts, the method offers a practical framework for integrating burr- and delamination minimisation into CFRP component design and manufacturing process planning.
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来源期刊
Composites Part C Open Access
Composites Part C Open Access Engineering-Mechanical Engineering
CiteScore
8.60
自引率
2.40%
发文量
96
审稿时长
55 days
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