Study of microwave responses on layered woven CFRP composites

Ruslee Sutthaweekul, A. M. J. Marindra, G. Tian
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引用次数: 4

Abstract

Woven carbon fibre reinforced polymer (CFRP) have been widely used in the airline industry. The main challenge of microwave inspection on woven CFRPs is the complex electromagnetic responses related to their layered-woven structures and associated defect (e.g., impact damage). This work focuses on the simulation study of microwave responses for woven CFRPs based on microwave open-ended waveguide (OEW) system in K-band. Simulation studies of woven composites with different weaving structures are carried out through structural parameters including width, gap between fibres, ply thickness and number of plies. The simulation results suggest that gap and ply thickness significantly affect frequency shift in the response, whereas woven texture and number of plies are related to occurrences of multiple resonances/ripples. In the experiment, we examine microwave responses of a 12-layers, 5HS woven composite in areas of with and without impact damage. The initial experimental results show good agreement with the simulation. The understanding of microwave responses related to woven CFRP structures is the foundation for future development of defect characterisation technique and inverse problem solving on woven composites.
层织CFRP复合材料微波响应研究
编织碳纤维增强聚合物(CFRP)在航空工业中得到了广泛的应用。微波检测编织cfrp的主要挑战是其层状编织结构和相关缺陷(如冲击损伤)的复杂电磁响应。本文主要研究了基于微波开放式波导(OEW)系统的编织cfrp在k波段的微波响应仿真。通过织物宽度、纤维间隙、层厚、层数等结构参数,对不同编织结构的机织复合材料进行了仿真研究。仿真结果表明,间隙和厚度显著影响响应中的频移,而织构和层数与多重共振/波纹的发生有关。在实验中,我们研究了12层5HS编织复合材料在有和没有冲击损伤区域的微波响应。初步实验结果与仿真结果吻合较好。对CFRP编织结构微波响应的理解是未来发展CFRP编织结构缺陷表征技术和反问题求解的基础。
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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