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Enhancing hygrothermal resistance of aeronautical carbon fabric/epoxy composites via air plasma processing

机译:通过空气等离子体处理提高航空碳纤维织物/环氧树脂复合材料的耐湿热性

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摘要

Air plasma processing is introduced as a surface modification technique for carbon fibers to enhance the hygrothermal resistance of carbon fabric/epoxy composites. On carbon fiber surface subjected to 4-min plasma processing, there are 37.6 of carbon species present as -C-O-C groups and 9.3 of carbon species as -COOH groups. The moisture adsorption behavior of composites can be described by Fick's law. Increase in temperature accelerates the initial moisture adsorption rate and results in a higher diffusion coefficient. The decreasing interlaminar shear strength (ILSS) of composites is mainly ascribed to the loss of adhesion at the fiber/matrix interface. A lower equilibrium moisture content of composites is caused by air plasma processing, which leads to the improved interfacial bonding strength and the higher retention rate of ILSS of carbon fabric/epoxy composites. The interface sensitivity and temperature dependence of moisture adsorption for carbon fabric/epoxy composites are discussed. The results presented herein demonstrate an effective strategy for enhancing hygrothermal resistance of carbon fiber-reinforced composites.
机译:空气等离子体处理作为碳纤维的表面改性技术被引入,以提高碳纤维/环氧树脂复合材料的吸湿热性。在经过4 min等离子体处理的碳纤维表面上,有37.6%的碳物种以-C-O-C基团形式存在,9.3%的碳物种以-COOH基团存在。复合材料的吸湿行为可以用菲克定律来描述。温度升高会加速初始水分吸附速率,并导致更高的扩散系数。复合材料层间剪切强度(ILSS)的降低主要归因于纤维/基体界面的附着力丧失。空气等离子体处理导致复合材料的平衡含水率降低,导致碳织物/环氧树脂复合材料的界面粘结强度提高,ILSS的保留率更高。讨论了碳织物/环氧树脂复合材料吸湿的界面敏感性和温度依赖性。本文提出的结果证明了提高碳纤维增强复合材料的耐湿热性的有效策略。

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