Acoustic emission study on bending failure mechanisms of GLARE laminates with different stacking structures

doi:10.19936/j.cnki.2096-8000.20240328.002

Abstract

Abstract: Glass fiber reinforced aluminum(GLARE) laminates are hybrid composite materials widely used in the aerospace industry. In this study, the three-point bending test method is used to carry out the bending loading, and the Acoustics Emission (AE) technique is used to monitor the real-time damage behavior of the laminates during the bending process, based on the multi-AE parameters and K-means clustering method, the bending performance and failure mechanism of GLARE laminate with different ply structures were investigated. The results show that the location of aluminum alloy layer has a significant effect on the bending properties of GLARE laminates, and the deformation coordination of the outermost aluminum alloy layer and the composite layer can effectively delay the initiation and evolution of the damage. The damage modes and corresponding peak frequencies of GLARE laminate during bending failure include 0~50 kHz for aluminum alloy damage, 80~210 kHz for matrix cracking, 210~320 kHz for fiber peeling and interface delamination, and 320~400 kHz for fiber breakage.

Key words: glass fiber reinforced aluminum laminates, acoustic emission technology, three-point bending experiment, K-means clustering method, failure mechanism

CLC Number:

TB332

ZHANG Mai, ZHENG Yingxiao, HU Kejun, HAN Wenqin, DUAN Liuyang, SHI Qinghe. Acoustic emission study on bending failure mechanisms of GLARE laminates with different stacking structures[J]. COMPOSITES SCIENCE AND ENGINEERING, 2024, 0(3): 13-19.

References

[1] 华小歌. GLARE层板Ⅰ型层间断裂韧性的试验方法研究[D]. 南京: 南京航空航天大学, 2019.
[2] 武多多, 郑会龙, 康振亚, 等. 金属-机织复合材料混合结构的三点弯曲力学性能及失效机理[J]. 材料工程, 2022, 50(12): 79-88.
[3] 白鑫, 王云英, 王雅娜, 等. 跨厚比对高强玻璃纤维增强复合材料单向板弯曲性能的影响[J]. 航空材料学报, 2022, 42(2): 57-63.
[4] 赵宗, 郑兴伟, 钱仁飞, 等. 纤维稀土镁合金超混杂层板弯曲性能及其失效机理[J]. 航空材料学报, 2021, 41(4): 157-166.
[5] ZHOU C Y, LI Y H, ZHU G H, et al. Tensile and flexural behavior of metal/CFRP hybrid laminated plates[J]. Polymer Composites, 2021, 42(6): 2882-2897.
[6] BOSBACH B, OHLE C, FIEDLER B, et al. Structural health monitoring of fibre metal laminates under mode Ⅰ and Ⅱ loading[J]. Composites Part A: Applied Science and Manufacturing, 2018, 107: 471-478.
[7] KUMAR M H, MATHIVANAN N R, KUMAR S, et al. Experiment investigations of effect of laminate thickness on flexural properties of GLARE and GFRP laminates[J]. Materials Research Express, 2018, 6(2): 025313.
[8] SOLYAEV Y, LURIE S, PROKUDIN O, et al. Elastoplastic behavior and failure of thick GLARE laminates under bending loading[J]. Composites Part B: Engineering, 2020, 200: 108302.
[9] 赵文政, 李敏, 张燕南, 等. 复合材料损伤过程声发射信号聚类分析与压缩变形测量[J]. 玻璃钢/复合材料, 2018(6): 5-10.
[10] 龙宪海, 王汉功, 阳能军. 碳/环氧复合材料三点弯曲过程声发射特性研究[C]//中国振动工程学会故障诊断专业委员会. 2008年全国振动工程及应用学术会议暨第十一届全国设备故障诊断学术会议论文集. 上海: 2008: 50-52.
[11] 张亚楠. 基于声发射信号处理的风力机叶片损伤演化研究[D]. 沈阳: 沈阳工业大学, 2020.
[12] 张鹏飞, 商雅静, 周伟, 等. 碳纤维编织复合材料弯曲损伤破坏声发射监测[J]. 中国测试, 2019, 45(5): 47-53.
[13] 俞方艾, 周勃, 张雪岩, 等. 含分层缺陷的叶片复合材料层合板损伤识别方法的研究[J]. 机械强度, 2022, 44(6): 1327-133.
[14] 沈书乾, 李伟, 龙飞飞, 等. 复合材料层合板损伤声发射信号特征提取方法[J]. 压力容器, 2022, 39(9): 72-76.
[15] 徐栋. 基于声发射多特征统计分析的纤维增强复合材料损伤分类与性能预测[D]. 杭州: 浙江大学, 2022.
[16] 徐翌伟. GLARE层板弯曲性能及失效机制的研究[D]. 南京: 南京航空航天大学, 2017.
[17] 秦礽, 李小童, 商雅静, 等. 含分层损伤复合材料弯曲变形与破坏实验研究[J]. 玻璃钢/复合材料, 2019(6): 30-36.
[18] 孟超, 彭卫东, 宁小波, 等. 玻璃纤维复合材料损伤过程的声发射特性研究[J]. 玻璃钢/复合材料, 2016(12): 23-27.
[19] 张鹏林, 李梅, 王汝姣, 等. 风电叶片复合材料在三点弯曲过程中的声发射研究[J]. 工程塑料应用, 2016, 44(4): 21-26.