开孔对热塑性复合材料层合板抗反复冲击性能影响的研究

复合材料科学与工程 ›› 2019, Vol. 0 ›› Issue (11): 100-104.

开孔对热塑性复合材料层合板抗反复冲击性能影响的研究

彭丕, 王继辉^*, 陈宏达, 骆传龙

武汉理工大学材料科学与工程学院,武汉 430070

收稿日期:2019-01-14 出版日期:2019-11-28 发布日期:2019-11-28
通讯作者: 王继辉(1962-),男,博士,教授/博导,主要从事复合材料结构方面的研究,jhwang@whut.edu.cn。
作者简介:彭丕(1993-),男,硕士研究生,主要从事热塑性复合材料方面的研究。

STUDY ON THE EFFECT OF OPENING HOLE ON THE RECIPROCATING IMPACT RESISTANCE OF THERMOPLASTIC COMPOSITE LAMINATES

PENG Pi, WANG Ji-hui^*, CHEN Hong-da, LUO Chuan-long

School of Material Science and Engineering, Wuhan University of Technology, Wuhan 430070, China

Received:2019-01-14 Online:2019-11-28 Published:2019-11-28

摘要/Abstract

摘要： 研究了孔与冲击点的距离对玻璃纤维增强聚丙烯复合材料层合板抗反复冲击性能的影响。采用热压成型工艺制备了连续玻璃纤维增强聚丙烯层合板,通过落锤冲击试验机对层合板进行反复冲击,直至其发生完全穿透,获得冲击响应的相关数据。结果表明:孔与冲击点的距离d对玻纤增强聚丙烯层合板抗反复冲击性能的影响显著,就一次冲击而言,距离d越大,最大接触力越大,位移和吸收能量反而越小。相比于无孔层合板,d为5 mm、10 mm、15 mm、20 mm的开孔板抗反复冲击的次数分别降低了88.1%、57.6%、20.3%、3.3%。反复冲击过程中,d=5 mm和d=10 mm开孔板的最大接触力存在峰值点,开孔促进了层合板吸收冲击能量,每次冲击的吸收能量随着冲击次数的增加而缓慢增加。

关键词: 复合材料, 开孔, 抗反复冲击

Abstract: In this paper, the effect of the distance between the hole and the impact point on the repeated impact resistance of the glass fiber reinforced polypropylene composite (GFRPP) laminate is studied. GFRPP laminates were prepared by hot press forming. Repeated impact on laminates were performed by drop hammer impact tester. Until it is completely penetrated, the relevant data of the impact response is obtained. The results show that the distance d between the hole and the impact point has a significant effect on the repeated impact resistance of the GFRPP laminate. For a single impact, the larger the distance is, the larger the maximum contact force of the impact response, and the smaller the displacement and the absorption energy. Compared with non-hole laminates, the number of times of d=5 mm, 10 mm, 15 mm, 20 mm perforated plates against repeated impacts decreased by 88.1%, 57.6%, 20.3%, and 3.3%, respectively. During the repeated impact process, the maximum contact force of the d=5 mm and d=10 mm aperture plates has a peak point, which promotes the absorption energy of the laminate, and the absorption energy of each impact increases slowly with the increase of the number of impacts.

Key words: composite material, holes, anti-repetitive impact

中图分类号:

TB332

彭丕, 王继辉, 陈宏达, 骆传龙. 开孔对热塑性复合材料层合板抗反复冲击性能影响的研究[J]. 复合材料科学与工程, 2019, 0(11): 100-104.

PENG Pi, WANG Ji-hui, CHEN Hong-da, LUO Chuan-long. STUDY ON THE EFFECT OF OPENING HOLE ON THE RECIPROCATING IMPACT RESISTANCE OF THERMOPLASTIC COMPOSITE LAMINATES[J]. Composites Science and Engineering, 2019, 0(11): 100-104.

参考文献

[1] 林雨佳. 长玻璃纤维增强聚丙烯复合材料在汽车中的应用[J]. 国外塑料, 2015, 33(4): 42-45.
[2] 范子杰, 桂良进, 苏瑞意. 汽车轻量化技术的研究与进展[J]. 汽车安全与节能学报, 2014, 5(1): 1-16.
[3] 鲍宏琛, 刘广彦. 准各向同性纤维增强复合材料层合板的开孔拉伸破坏模拟[J]. 复合材料学报, 2016, 33(5): 1026-1032.
[4] Dai S, Cunningham P R, Marshall S, et al. Open hole quasi-static and fatigue characterisation of 3D woven composites[J]. Composite Structures, 2015, 131: 765-774.
[5] Erin G H, Camanho P P, Xavier J, et al. Size effects on the tensile and compressive failure of notched composite laminates[J]. Composite Structures, 2013, 96: 736-744.
[6] Chang F K, Chang K Y. A progressive damage model for laminated composites containing stress concentrations[J]. Journal of Composite Materials, 1987, 21(9): 834-855.
[7] 王丹勇, 温卫东, 崔海涛. 含孔复合材料层合板静拉伸三维逐渐损伤分析[J]. 力学学报, 2005(6): 118-125.
[8] 关志东, 黎增山, 刘德博, 等. 复合材料层板开孔压缩损伤分析[J]. 复合材料学报, 2012, 29(3): 167-172.
[9] 李明, 马力, 吴林志, 等. 含孔复合材料层合板拉伸强度研究[J]. 哈尔滨工业大学学报, 2011, 43(s1): 1-5.
[10] Goyal V K, Jaunky N R, Johnson E R, et al. Intralaminar and interlaminar progressive failure analyses of composite panels with circular cutouts[J]. Composite Structures, 2004, 64(1): 91-105.
[11] Amaro A M, Reis P N B, de Moura M F S F, et al. Influence of open holes on composites delamination induced by low velocity impact loads[J]. Composite Structures, 2013, 97: 239-244.
[12] 杜江涛. 复合材料层合板低速冲击损伤表征与开孔分析[D]. 郑州: 郑州大学, 2017.
[13] Green E R, Morrison C J, Luo R K. Simulation and experimental investigation of impact damage in composite plates with holes[J]. Journal of Composite Materials, 2016, 34(6): 502-521.
[14] Moure M M, Otero F, García-Castillo S K, et al. Damage evolution in open-hole laminated composite plates subjected to in-plane loads[J]. Composite Structures, 2015, 133: 1048-1057.
[15] Arikan V, Sayman O. Comparative study on repeated impact response of E-glass fiber reinforced polypropylene & epoxy matrix composites[J]. Composites Part B: Engineering, 2015, 83: 1-6.
[16] Luo R K. The evaluation of impact damage in a composite plate with a hole[J]. Composites Science and Technology, 2000, 60(1): 49-58.