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Mechanical and Thermal Properties of Carbonized PAN Nanofibers Cohesively Attached to Surface of Carbon Fiber Reinforced Composites

机译:碳化锅纳面纤维的机械和热性能含有碳纤维增强复合材料表面

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Unidirecitonal pre-preg carbon fibers of ten peel plies were laid up at 0-, 45-,-45-, and 45-degree stacking sequences on a flat and smooth aluminum (Al) plate, and then carbonized electrospun polyacrylonitrile (PAN) nanofibers were placed on top of the last ply prior to vacuum curing in a vacuum oven. The PAN electrospun fibers were oxidized at 280° C in an ambient condition for 1 hr and then carbonized at 850° C for 1 hr in an argon (Ar) gas atmosphere. The resultant composite panels were cut into small pieces and subjected to a number of different characterization techniques. Thermal mechanical analysis (TMA) measurements clearly showed that significant reinforcement was achieved for the pre-preg/ carbonized PAN fiber composites because of the enhanced interfacial bonding between the PAN nanofibers and the matrix. Dynamic mechanical analysis (DMA) tests exhibited a shift of the glass transition temperature of the carbonized PAN nanofiber/composite, which may be helpful for high-temperature applications of the present composites. A Raman spectroscopy peak around 897 cm~(-1) indicated formation of the g-phase of the carbonized PAN fibers. The highest stretching peak of the CH2 group was recognized within the range of 2,500-2,800 cm~(-1) for the carbonized fibers. The vibration peak of the C≡N group also appeared at 1,452 cm~(-1) spectrum. TMA determined the coefficient of thermal expansion (CTE), indicating an improvement in stability of the composite material, which can be useful for structural health monitoring (SHM) as well as lightning strikes and electromagnetic interference shielding applications of new carbon fiber composites.
机译:在平坦和光滑的铝(Al)板上的0-,45 - -45-和45度堆叠序列中,铺设了十个剥离层的非思考前PREG碳纤维,然后碳化电纺 - 聚丙烯腈(锅)纳米纤维在真空烘箱中真空固化之前将最后一层的顶部放在最后。将PAN电纺纤维在280℃下在环境条件下氧化1小时,然后在850℃下碳化1小时,在氩(AR)气体气氛中。将所得复合板切成小块并进行多种不同的表征技术。热机械分析(TMA)测量清楚地表明,由于PAN纳米纤维和基质之间的界面粘合增强了PREG /碳化盘纤维复合材料,实现了显着的增强。动态力学分析(DMA)测试表现出碳化锅纳纤维/复合材料的玻璃化转变温度的偏移,这可能有助于本复合材料的高温应用。拉曼光谱峰值约为897cm〜(-1)表示形成碳化盘纤维的G相。 CH2基团的最高拉伸峰被碳化纤维的2,500-2,800cm〜(-1)范围内识别。 C 1n组的振动峰也出现在1,452cm〜(-1)谱。 TMA确定了热膨胀系数(CTE),表明复合材料的稳定性的改善,这可用于结构健康监测(SHM)以及新的碳纤维复合材料的雷击和电磁干扰屏蔽应用。

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