复合材料层合板双面贴补结构渐进损伤分析

摘要/Abstract

摘要：

提出了一种分析和预测在拉伸载荷作用下复合材料层合板双面贴补结构的极限承载能力的方法，建立了分析复合材料双面贴补结构渐进损伤的三维有限元模型.胶层用各向同性模型描述，提出了基于3个方向剪切应变描述的二次剪切失效判据来预测胶层的损伤起始，定义了与材料应力应变相关的刚度折减函数来模拟损伤后胶层刚度的连续退化.层合板用正交各向异性三维模型描述，采用基于应变描述的三维Hashin准则和Ye分层准则来预测其损伤起始，引入损伤变量来考虑层合板的损伤扩展.计算结果与试验数据吻合较好,说明该方法和模型可以有效地预测复合材料双面贴补结构的拉伸极限强度.

关键词: 复合材料, 双面贴补, 渐进损伤, 拉伸强度

Abstract:

A method for predicting and analyzing the ultimate load of the double-sided repaired structures of composite laminates subjected to tensile load was proposed. A three dimensional FEA model was established to analyze the damage process. The adhesive layer was modeled with the isotropic constitutive. A square criterion based on three direction shear strains to predict the occurrence of the damage of the adhesive layer, and a degradation function associated with the stress and strain was defined to degenerate the stiffness of the damaged material. The composite laminates was modeled with the orthotropic constitutive, and the occurrence of damage was predicted by 3D Hashin’s initiation criterion and Ye criterion. Damage variables was introduced to characterize the damage extension. The ultimate load obtained from the numerical prediction agreed well with the experimental results. It is verified that the method and model can predict the tensile ultimate strength of the double-sided repaired composite laminate structures effectively.

Key words: composite material, double-sided repair, progressive damage, tensile strength

中图分类号:

TB 332

李振凯，余音，汪海. 复合材料层合板双面贴补结构渐进损伤分析[J]. 上海交通大学学报（自然版）, 2014, 48(06): 877-882.

LI Zhenkai,YU Yin,WANG Hai. Progressive Damage Analysis of Double-Sided Adhesively Bonding Repaired Structures of Composite Laminates[J]. Journal of Shanghai Jiaotong University, 2014, 48(06): 877-882.

参考文献

［1］Yang C, Sun W, Tomblin J S, et al. A semianalytical method for determining the strain energy release rate of cracks in adhesivelybonded singlelap composite joints ［J］. Journal of Composite Materials, 2007, 41(13): 15791602.

［2］Turon A, Camanho P P, Costa J. Accurate simulation of delamination growth under mixedmode loading using co hesive elements: Definition of interlaminar strengths and elastic stiffness ［J］. Composite Structures, 2010, 92(8): 18571864.

［3］Camanho P P. Mixedmode decohesion finite elements for the simulation of delamination in composite materials ［R］. US: NASA, 2002.

［4］王跃全, 童明波, 朱书华. 复合材料层合板胶接贴补修理渐进损伤分析［J］. 复合材料学报, 2011, 28(3): 197202.

WANG Yuequan, TONG Mingbo, ZHU Shuhua. Progressive damage analysis on adhesively bonding patch repair of composite laminates ［J］. Acta Materiae Compositae Sinica, 2011, 28(3): 197202.

［5］朱书华, 王跃全, 童明波. 复合材料层合板阶梯形挖补胶接修理渐进损伤分析［J］. 复合材料学报, 2012, 29(6): 164169.

ZHU Shuhua, WANG Yuequan, TONG Mingbo. Progressive damage analysis on composite laminates steppedpatch adhesively bonding repair ［J］. Acta Materiae Compositae Sinica, 2012, 29(6): 164169.

［6］Pinho S T, Dàvila C G, Camanho P P, et al. Failure models and criteria for FRP under inplane or threedimensional stress states including shear nonlinearity［R］. US: NASA, 2005.

［7］刘遂，关志东，郭霞，等. 复合材料蜂窝夹层板挖补修理后的侧压性能［J］. 科技导报, 2013, 31(7): 2832.

LIU Sui, GUAN Zhidong, GUO Xia, et al. Lateral compressive behavior of scarf repaired honeycomb sandwich panels［J］. Science & Technology Review, 2013, 31(7): 2832.

［8］Linde P, Pleitner J, de Boer H, et al. Modelling and simulation of fibre metal laminates［C］//2004 ABAQUS Users’ Conference. Boston Massachusetts: ABAQU Inc, 2004: 421439.

［9］胡祎乐，余音，汪海，等. 纤维增强复合材料机翼长桁压缩破坏预测方法［J］. 上海交通大学学报, 2012, 46 (9): 14711475.

HU Yile, YU Yin, WANG Hai, et al. A failure prediction method of fiberreinforced composite wing stringer subjected to compressive loading［J］. Journal of Shanghai Jiaotong University, 2012,46 (9): 14711475.

［10］Tong L, Kuruppu M, Kelly D. Analysis of adhesively bonded composite double lap joints［J］. Journal of Thermoplastic Composite Materials, 1997, 10(1): 6175.

[1]	刘庆升, 薛鸿祥, 袁昱超, 唐文勇. 含复合材料结构的非黏结柔性立管弯曲特性[J]. 上海交通大学学报, 2022, 56(9): 1247-1255.
[2]	杨玲玉, 董顺, 洪长青. 新型低密度树脂裂解碳改性碳纤维复合材料的制备与性能研究[J]. 空天防御, 2022, 5(4): 1-9.
[3]	贾米芝, 徐澧明, 林楠, 南博华, 王坤, 蔡登安, 周光明. 具有回弹复位功能易裂盖的结构设计及力学性能研究[J]. 空天防御, 2022, 5(2): 8-16.
[4]	王烨成, 李洋, 张迪, 杨越, 罗震. 碳纤维增强热塑性复合材料与高强钢的电阻单元焊[J]. 上海交通大学学报, 2022, 56(10): 1349-1358.
[5]	王卓鑫, 赵海涛, 谢月涵, 任翰韬, 袁明清, 张博明, 陈吉安. 反向传播神经网络联合遗传算法对复合材料模量的预测[J]. 上海交通大学学报, 2022, 56(10): 1341-1348.
[6]	陶威, 刘钊, 许灿, 朱平. 三维正交机织复合材料翼子板多尺度可靠性优化设计[J]. 上海交通大学学报, 2021, 55(5): 615-623.
[7]	安庆升, 孙立东, 武秋生. 碳纤维增强复合材料发射筒设计研究[J]. 空天防御, 2021, 4(2): 13-.
[8]	管清宇, 夏品奇, 郑晓玲, 吴光辉. 复合材料层压板冲击后压缩强度拟合模型[J]. 上海交通大学学报, 2021, 55(11): 1459-1466.
[9]	胡济珠, 周俊, 李云云. 基于有机/无机复合材料的航天环境下高效热电转换技术研究 [J]. 空天防御, 2020, 3(2): 72-75.
[10]	栾建泽，那景新，慕文龙，谭伟，陈宏利. 低速加载对铝合金-玄武岩纤维增强树脂复合材料粘接接头失效的影响[J]. 上海交通大学学报, 2020, 54(11): 1200-1208.
[11]	刘海龙，张大旭，祁荷音，伍海辉，郭洪宝，洪智亮，陈超，张毅. 基于X射线CT原位试验的平纹SiC/SiC复合材料拉伸损伤演化[J]. 上海交通大学学报, 2020, 54(10): 1074-1083.
[12]	刘晓东，吴磊，孔谅，王敏，陈一东. 空气等离子处理对碳纤维增强复合材料表面特性及胶接性能的影响[J]. 上海交通大学学报, 2019, 53(8): 971-977.
[13]	李昱霖, 安庆升, 杨坤好, 唐晓峰, 刘龙涛. 防热承载一体化复合材料电缆罩分析及验证[J]. 空天防御, 2019, 2(3): 1-7.
[14]	杜思琦，王继崇，彭雄奇，顾海麟. 可生物降解的黄麻纤维/聚乳酸复合材料的制备和力学性能[J]. 上海交通大学学报, 2019, 53(11): 1335-1341.
[15]	杨万友，王家序，黄彦彦，周青华，杨勇. 热载荷作用下颗粒增强复合材料温升分布数值模拟[J]. 上海交通大学学报, 2019, 53(11): 1342-1351.