Research progress on energy absorption mechanism and damage mode of fiber reinforced resin based bulletproof composites
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摘要: 本文对纤维增强树脂基复合材料在抗冲击领域的吸能机制及损伤模式进行了综述。首先,介绍了纤维增强复合材料在弹道防护、航空航天等领域的应用,对比了超高分子量聚乙烯(UHMWPE)纤维、芳纶纤维、碳纤维等高性能纤维的优缺点;其次,以各种纤维增强树脂基复合材料的弹道实验及理论模拟为基础,分析了防弹复合材料的吸能机制和损伤模式,发现拉伸变形是复合材料的主要吸能方式,分层破坏是其主要损伤模式;最后,总结了纤维编织结构的分类、特点及其对复合材料防弹性能的影响并对纤维增强树脂基复合材料的发展前景进行了展望。
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关键词:
- 纤维增强树脂基复合材料 /
- 弹道响应 /
- 吸能机制 /
- 损伤模式 /
- 编织结构
Abstract: This article reviews the energy absorption mechanism and damage modes of fiber reinforced resin matrix composites in the field of impact resistance. Firstly, the applications of fiber reinforced composites in the fields of ballistic protection and aerospace are introduced. In addition, the advantages and disadvantages of high-performance fibers such as ultra-high molecular weight polyethylene fiber (UHMWPE), aramid fibers and carbon fibers are compared. Secondly, based on ballistic experiments and theoretical simulations of various fiber reinforced resin matrix composites, the energy absorption mechanism and damage mode of bulletproof composites are analyzed. It is found that tensile deformation is the main energy absorption mode of composites, and delamination is its main damage mode. Finally, the classification and characteristics of fabric structures and their influence on the ballistic performance of composites are summarized and the development prospect of fiber reinforced resin matrix composites is prospected. -
图 1 弹道极限实验纤维断裂形貌(12.7 mm FSP以1346 m/s的速度撞击35 mm厚的靶板): (a)正面; (b)距正面9 mm; (c)距正面18 mm;(d)背面[34]
Figure 1. Fiber fracture morphology from ballistic limit tests (35 mm thick target impacted by 12.7 mm FSP at 1346 m/s). Images taken: (a) at the front face; (b) 9 mm from the front face; (c) 18 mm from the front face; and (d) at the back face [34]
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