制造缺陷对蒸压成型层压板疲劳性能的影响

IF 1.8 Q3 ENGINEERING, MANUFACTURING
L. Maragoni, P. Carraro, M. Quaresimin
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引用次数: 4

摘要

摘要本文采用高压灭菌成型技术制备了交叉层合板和多向层合板。工艺参数的变化导致纤维体积分数、整体孔隙含量和孔隙大小等微观结构特征的不同。疲劳试验表明,微观结构对层合板的长期性能有很强的影响,包括裂纹萌生、裂纹扩展、裂纹密度演变和相关刚度下降的寿命。作者最近提出的一个标准,用于预测第一次疲劳裂纹的形成,考虑到实际的材料微观结构,包括空隙,然后在新的实验数据上进行了验证。结果表明,为了更高效、更安全地设计复合材料零件,需要适当地考虑制造引起的缺陷,并指出有必要开发将制造工艺参数、微尺度形貌和机械性能联系起来的模型,以实现性能/成本比最大化的成本效益生产。图形抽象
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Influence of manufacturing-induced defects on the fatigue performances of autoclave moulded laminates
Abstract In the present work, cross-ply and multidirectional laminates were produced by autoclave moulding. Changes in the process parameters led to different microstructural features in terms of fibre volume fraction, global void content, and void size. Fatigue tests revealed a strong influence of the microstructure on the long-term performances of the laminates, in terms of life to crack initiation, crack propagation, crack density evolution and associated stiffness drop. A criterion recently proposed by the authors to predict the formation of the first fatigue cracks accounting for the actual material microstructure, including voids, was then validated on the new experimental data. The results show the need to properly account for the manufacturing induced defects for a more efficient and safer design of composite parts, and remark the necessity of developing models that link manufacturing process parameters, micro-scale morphology, and mechanical performances to enable a cost-effective production that maximizes the performance/cost ratio. Graphical Abstract
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来源期刊
CiteScore
4.00
自引率
0.00%
发文量
11
审稿时长
16 weeks
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