复合材料科学与工程 ›› 2021, Vol. 0 ›› Issue (8): 50-59.DOI: 10.19936/j.cnki.2096-8000.20210828.008

• 应用研究 • 上一篇    下一篇

起圈织物泡沫夹芯复合材料低速冲击性能研究

崔为运, 陈广思, 熊信发, 彭锦峰, 蔡登安, 周光明*   

  1. 南京航空航天大学 机械结构力学及控制国家重点实验室,南京210016
  • 收稿日期:2020-11-30 出版日期:2021-08-28 发布日期:2021-09-09
  • 通讯作者: 周光明(1966-),男,博士,教授,主要研究方向为先进复合材料结构设计及工程问题的计算机建模,zhougm@nuaa.edu.cn。
  • 作者简介:崔为运(1995-),男,硕士研究生,主要研究方向为先进复合材料的力学行为。
  • 基金资助:
    中央高校基本科研业务费专项资金资助项目(NS2019001);江苏省基础研究计划(自然科学基金)资助项目(BK20190394);南京市2019年度留学人员科技创新项目;江苏高校优势学科建设工程资助项目

Low velocity impact properties of foam core sandwich composites with looped fabric

CUI Wei-yun, CHEN Guang-si, XIONG Xin-fa, PENG Jin-feng, CAI Deng-an, ZHOU Guang-ming*   

  1. State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
  • Received:2020-11-30 Online:2021-08-28 Published:2021-09-09

摘要: 根据ASTM试验标准D7136,采用落锤冲击试验对起圈织物泡沫夹芯复合材料(U-cor)进行低速冲击试验研究。采用聚氨酯发泡工艺制备了四种夹芯密度、两种夹芯厚度、三种面板铺层的试验件,分别在5 J、10 J、15 J能量下进行冲击试验。试验结果表明:在较低能量冲击下,当夹芯密度较高时,接触力时间历程曲线接近于一条沿顶点对称的二次曲线;当冲击能量增加到一定程度后,含起圈织物夹芯板相比较同型号传统平纹织物夹芯板,最大接触载荷增加;由于起圈织物泡沫夹芯复合材料特殊的成型工艺,当夹芯的平均密度相同时,夹芯厚度的增加会带来冲击面附近局部刚度的增加,进而导致不同厚度夹芯板冲击响应存在较大差异以及抗冲击性能增加。

关键词: U-cor, 起圈织物, 泡沫夹芯, 低速冲击响应, 抗冲击性能, 复合材料

Abstract: According to the ASTM test standard D7136, the impact test of low impact impact on the wound fabric foam sandwich composite (U-cor) was carried out by drop hammer impact test. Four kinds of sandwich density, two kinds of sandwich thickness and three kinds of panel layers were prepared by polyurethane foaming process. The impact tests were carried out under the energy of 5 J, 10 J and 15 J, respectively. The experimental results show that under low energy impact, when the density of sandwich is pretty high, the contact force-time history curve is close to a quadratic curve symmetrical along the vertex. When the impact energy increases to a certain extent, the maximum contact load of loop starting fabric sandwich panel is higher than that of the same type of plain weave fabric sandwich panel. Due to the special forming process of the foam core sandwich composite with loop fabric, the increase of the core thickness will increase the local stiffness near the impact surface when the average density of the sandwich is the same, which will lead to a larger difference in impact response and an increase in impact resistance of sandwich panels with different thickness.

Key words: U-cor, loop fabric, foam core, low velocity impact response, impact resistance, composites

中图分类号: