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首页> 外文期刊>Composite Structures >Unfolding the effects of tuft density on compression after impact properties in unidirectional carbon/epoxy composite laminates
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Unfolding the effects of tuft density on compression after impact properties in unidirectional carbon/epoxy composite laminates

机译:展开簇绒密度对单向碳/环氧复合层压材料冲击性能后压缩的影响

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摘要

Post impact compressive residual strength of epoxy-based composite laminates is studied in the presence of through-thickness reinforcement (TTR). The tufting technique is used to introduce TTR in compact carbon unidirectional (UD) composites. Composite laminates are tufted using Kevlar thread with different tuft density by varying tuft pitch and spacing. The specimens are impacted with low-velocity impact to achieve barely visible impact damage (BVID). The damaged area is quantified using the ultrasonic C-scan method. Tufted specimens exhibited a significant reduction in the damaged area. The reduction in damage area is about 26% to 51% depending upon the tuft density. Residual strength post impact is determined by compression after impact (CAI) test. Upon increasing the tuft density up to 0.56%, the damaged area decreases by 51%, and CAI strength increases by 43%. Above this tuft density, damage area slightly decreases and CM strength remains almost the same. The improvement in CAI strength is due to an increase in apparent interlaminar strength attributed to the enhancement in bridging effect due to TTR. Different failure modes such as delamination, fiber crushing, kink-band formation, etc. are observed in both the untufted and tufted specimens.
机译:在通过厚度增强(TTR)的存在下,研究了环氧基复合层压板的后撞击压缩残余强度。簇绒技术用于引入紧凑型碳单向(UD)复合材料中的TTR。复合层压板采用Kevlar螺纹簇绒,通过不同的簇绒间距和间距,具有不同的簇绒密度。标本受到低速冲击的影响,以实现几乎可见的影响损伤(BVID)。使用超声波C扫描方法量化受损区域。簇绒标本表现出受损区域的显着减少。根据簇绒密度,损伤区域的减少约为26%至51%。残留的强度后撞击是通过冲击后的压缩(CAI)测试而确定的。在将簇绒密度增加至0.56%时,受损区域减少51%,CAI强度增加43%。高于该簇绒密度,损伤区域略微降低,CM强度几乎保持相同。 CAI强度的提高是由于由于TTR引起的桥接效应增强增加了表观层间强度。在无限和簇绒的标本中观察到不同的失效模式,例如分层,光纤破碎,扭结带等。

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