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Analysis and optimization of temperature distribution in carbon fiber reinforced composite materials during microwave curing process

机译:碳纤维增强复合材料微波固化过程中温度分布的分析与优化

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摘要

Vacuum assisted microwave curing technologies and modified optical sensing systems have been employed to investigate the influence of ply orientation and thickness on through-thickness temperature distribution of carbon fiber reinforced composite laminates. Two different types of epoxy systems have been studied. The results demonstrated that the ply orientation did not affect the temperature distribution of composite materials. However, the thickness was an important influencing factor. Nearly 10 ◦C temperature difference was found in 22.5 mm thick laminates. Through analyzing the physical mechanismsudduring microwave curing, the temperature difference decreased when the heat-loss in surface laminates was reduced and the absorption of microwave energy in the center laminates was improved. The maximum temperature difference of the samples formed using the modified microwave curing technologies in this research could be reduced by 79% to 2.1 ◦C. Compared with the 5.29 ◦C temperature difference of laminates using thermal heating process, the maximum temperature difference in laminates using modified microwave curing technologies was reduced by 60%, and the curing time was cut down by 25%.
机译:真空辅助微波固化技术和改进的光学传感系统已用于研究层取向和厚度对碳纤维增强复合材料层压板的贯穿厚度温度分布的影响。已经研究了两种不同类型的环氧体系。结果表明,层取向不影响复合材料的温度分布。但是,厚度是重要的影响因素。在22.5 mm厚的层压板中发现了近10℃的温差。通过分析微波固化过程中的物理机理,当降低表面层合板的热损失时,温差减小,中心层合板的微波能量吸收得到改善。这项研究中使用改进的微波固化技术形成的样品的最大温差可降低79%至2.1℃。与采用热加热工艺的层压板的5.29℃温差相比,采用改进的微波固化技术的层压板的最大温差降低了60%,固化时间减少了25%。

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