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Z-pin增强树脂基复合材料单搭接接头抗冲击性能

许爱华 李勇 还大军 褚奇奕 周煦洁

许爱华, 李勇, 还大军, 褚奇奕, 周煦洁. Z-pin增强树脂基复合材料单搭接接头抗冲击性能[J]. 航空动力学报, 2018, 33(3): 671-682. doi: 10.13224/j.cnki.jasp.2018.03.021
引用本文: 许爱华, 李勇, 还大军, 褚奇奕, 周煦洁. Z-pin增强树脂基复合材料单搭接接头抗冲击性能[J]. 航空动力学报, 2018, 33(3): 671-682. doi: 10.13224/j.cnki.jasp.2018.03.021
Impact resistance performances of resin matrix composite single lap joints reinforced by Z-pin[J]. Journal of Aerospace Power, 2018, 33(3): 671-682. doi: 10.13224/j.cnki.jasp.2018.03.021
Citation: Impact resistance performances of resin matrix composite single lap joints reinforced by Z-pin[J]. Journal of Aerospace Power, 2018, 33(3): 671-682. doi: 10.13224/j.cnki.jasp.2018.03.021

Z-pin增强树脂基复合材料单搭接接头抗冲击性能

doi: 10.13224/j.cnki.jasp.2018.03.021
基金项目: 航空科学基金(2015ZE52049);江苏高校优势学科建设工程资助项目

Impact resistance performances of resin matrix composite single lap joints reinforced by Z-pin

  • 摘要: 为了研究Z-pin增强树脂基复合材料接头的抗冲击性能,制备了Z-pin增强单搭接接头冲击试样。对比不同树脂体系Z-pin/层合板界面裂纹扩展,分别通过Z-pin拔脱试验和接头剪切试验研究Z-pin冲击后拔脱强度和单搭接接头冲击后剪切强度;结合有限元模拟和超声C扫描研究搭接面分层损伤情况。结果表明,相同冲击能量下,环氧Z-pin/环氧层合板界面抗冲击性更强,冲击能量越大,裂纹扩展越显著;Z-pin增强树脂基复合材料显著减小分层损伤面积,提高冲击后剪切强度,体积分数为1.5%、直径为0.5mm的Z-pin增强层合板分层损伤面积仅为40%,冲击后剪切强度的下降率仅为24.89%。随着Z-pin体积分数增加,搭接面损伤面积逐渐减小,冲击后剪切强度先增加后降低;随着Z-pin直径增加,层间损伤面积增加,冲击后剪切强度逐渐降低。Z-pin增强接头分层损伤模型模拟结果与试验结果基本吻合。

     

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出版历程
  • 收稿日期:  2016-09-14
  • 刊出日期:  2018-03-28

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