单向碳纤维增强塑料多纤维模型复合材料纵向压缩破坏研究

T. Jeong, M. Ueda
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引用次数: 4

摘要

采用多纤维模型复合材料对单向碳纤维增强塑料(CFRP)纵向压缩破坏进行了研究。排列整齐的碳纤维被嵌在环氧树脂基体中,并置于矩形梁上。通过矩形梁的四点弯曲试验,对模型复合材料进行了压缩试验。将碳纤维的数量从1根增加到数千根,研究了碳纤维对压缩破坏模式的影响。单纤维模型复合材料的压缩破坏是纤维粉碎。纤维的破碎应变远高于单向碳纤维增强塑料的压缩破坏应变。而多纤维模型复合材料的压缩破坏表现为扭结带。随着纤维数量的增加,纵向压缩破坏机制由纤维压碎向扭结带转变。扭结带参数,即扭结带角和扭结带宽度取决于紧密排列的碳纤维的数量。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Longitudinal Compressive Failure of Multiple-Fiber Model Composites for a Unidirectional Carbon Fiber Reinforced Plastic
The longitudinal compressive failure of a unidirectional carbon fiber reinforced plastic (CFRP) was studied using multiple-fiber model composites. Aligned carbon fibers were embedded in an epoxy matrix and put on a rectangular beam. A compression test of the model composite was performed by means of a four point bending test of the rectangular beam. The number of carbon fibers was changed from one to several thousands, by which the effect on compressive failure modes was investigated. A compressive failure of a single-fiber model composite was fiber crush. The fiber crush strain was much higher than the compressive failure strain of the unidirectional carbon fiber reinforced plastic. By contrast, a compressive failure of a multiple-fiber model composite was kink-band. The longitudinal compressive failure mechanism shifted from fiber crush to kink-band due to an increasing number of fibers. Kink-band parameters i.e. kink-band angle and kink-band width were dependent on the number of closely-aligned carbon fibers.
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