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

Abstract

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

CLC Number:

TB332

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.

References

[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.