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撞击物对复合材料层合板冲击损伤特性的影响
引用本文:梁嘉瑞,黄金红,杭宇,张欣玥,侯兵,李玉龙.撞击物对复合材料层合板冲击损伤特性的影响[J].北京理工大学学报,2022,42(6):629-633.
作者姓名:梁嘉瑞  黄金红  杭宇  张欣玥  侯兵  李玉龙
作者单位:1.西北工业大学 航空学院,陕西,西安 710072
基金项目:国家自然科学基金资助项目(11972310);
摘    要:针对一种采用预浸料成型工艺制备的复合材料层合板,开展不同撞击物作用下复合材料层合板低能量冲击损伤特性研究. 通过对比相同冲击能量(60 J)下,钢球、铝球和聚合物球撞击复合材料层合板的落锤/气炮冲击试验结果和冲击后含损伤结构的压缩试验结果,研究了不同撞击因素对复合材料低能量冲击损伤面积和剩余压缩强度的影响. 结果表明,相同冲击能量下,同种材质撞击物(不同质量)以不同速度冲击复合材料层合板的损伤特性相似;而不同材质撞击物(不同弹性模量和泊松比)得到的结果差异显著. 结合赫兹接触理论,初步解释了撞击物弹性性能影响接触刚度和冲击损伤程度的规律. 

关 键 词:复合材料层合板    低能量冲击    冲击损伤    剩余强度
收稿时间:2021-08-31

Influences of Impactor Parameters on the Impact Damage Response of Composite Laminate
LIANG Jiarui,HUANG Jinhong,HANG Yu,ZHANG Xinyue,HOU Bing,LI Yulong.Influences of Impactor Parameters on the Impact Damage Response of Composite Laminate[J].Journal of Beijing Institute of Technology(Natural Science Edition),2022,42(6):629-633.
Authors:LIANG Jiarui  HUANG Jinhong  HANG Yu  ZHANG Xinyue  HOU Bing  LI Yulong
Institution:1.School of Aeronautics, Northwestern Polytechnical University, Xi’an, Shaanxi 710072, China2.Shaanxi Key Laboratory of Impact Dynamics and Engineering Application, Xi’an, Shaanxi 710072, China3.Aviation Key Laboratory of Science and Technology on Structures Impact Dynamics, Xi’an, Shaanxi 710065, China
Abstract:The low-energy impact damage responses of a composite laminate prepared by prepreg forming process were studied under the impacts with various impactors. Firstly, the impactors made of steel, aluminum and polymer were applied to impact the laminates at the same energy (60 J) by using drop weight/air gun facilities. Then, the damaged structures after impact were compressed to obtain the residual strength/residual stiffness of composites under low-energy impact. From these experimental results, one can see that with the same impact energy, the damage responses of composite laminate impacted by the same material (with different mass and velocity) are almost the same, however, the results of impactors with different materials are significantly different. The Hertzian contact theory is employed to illustrate the influence of elastic parameters of impactors on the contact stiffness as well as the damage responses of composite laminate. 
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