L 型碳纤维增强复合材料连接件承载力的渐进损伤分析

doi:10.12066/j.issn.1007-2861.2126

上海大学学报(自然科学版) ›› 2021, Vol. 27 ›› Issue (2): 325-335.doi: 10.12066/j.issn.1007-2861.2126

L 型碳纤维增强复合材料连接件承载力的渐进损伤分析

都亚鹏¹, 胡晓郁², 楚海建¹^,²()

1.上海大学上海市应用数学和力学研究所, 上海 200072
2.上海大学力学与工程科学学院, 上海 200444

收稿日期:2019-03-04 出版日期:2021-04-30 发布日期:2021-04-27
通讯作者: 楚海建 E-mail:hjchu@shu.edu.cn
作者简介:楚海建(1972—), 男, 教授, 博士生导师, 博士, 研究方向为固体力学. E-mail:hjchu@shu.edu.cn
基金资助:
国家自然科学基金资助项目(11872237);上海市自然科学基金资助项目(18ZR1414600)

Progressive damage analysis of the bearing capacity of L-type carbon fibre reinforced composite connectors

DU Yapeng¹, HU Xiaoyu², CHU Haijian¹^,²()

1. Shanghai Institute of Applied Mathematics and Mechanics, Shanghai University,Shanghai 200072, China
2. School of Mechanics and Engineering Science, Shanghai University, Shanghai 200444, China

Received:2019-03-04 Online:2021-04-30 Published:2021-04-27
Contact: CHU Haijian E-mail:hjchu@shu.edu.cn

摘要/Abstract

摘要：

从试验与计算两个方面, 对比研究了 L 型碳纤维增强复合材料连接件(carbon fiber reinforced composite connector, CFRCC)的失效形式和极限承载力. 结果表明: ① 在拉伸载荷工况下, 复合材料 L 型 CFRCC 失效形式主要为圆角处的分层和开孔周边基体破坏; ② 对比两种失效准则和两种退化准则的不同组合, 发现在有限元分析中采用混合失效准则和 Camanho-Matthews 刚度退化准则的渐近失效分析方案可以较好地模拟实验现象; ③ 将有限元分析模型及其模拟获得的参数应用于预测不同辅层顺序和圆角半径的 L 型 CFRCC 性能, 与试验结果吻合良好, 极限承载力误差为 9.4%. 建立的"设计-试验-模拟-预测-验证"分析方法及其获得的结果可为复合材料 L 型构件的强度设计提供借鉴.

关键词: 碳纤维增强复合材料, L 型连接件, 失效准则, 渐进失效分析, 有限元分析

Abstract:

The failure modes and bearing capacities of L-type carbon fibre reinforced composite connectors (CFRCC) were studied through experimental testing and computational simulation. The results demonstrated the following. ① Delamination at the corner and matrix damage around bolt holes were the dominant failure modes of L-type CFRCC under tensile loading. ② Comparing the different combinations of two strength failure criteria and two material degradation criteria revealed that the combination of mixed strength failure criteria and the Camanho-Mathews stiffness degradation criteria was more suitable for analysing the progressive damage to the connectors. ③ The predictions from the finite element simulation were in good agreement with the experimental results, and the relative error of the bearing capacity was 9.4%. The strategy of "design-test-simulation-prediction-validation" and the results obtained in this study may provide reliable guidance for the design of L-type CFRCC.

Key words: carbon fibre reinforced composite (CFRC), L-type connector, failure criteria, progressive failure analysis, finite element analysis

中图分类号:

TB332

都亚鹏, 胡晓郁, 楚海建. L 型碳纤维增强复合材料连接件承载力的渐进损伤分析[J]. 上海大学学报(自然科学版), 2021, 27(2): 325-335.

DU Yapeng, HU Xiaoyu, CHU Haijian. Progressive damage analysis of the bearing capacity of L-type carbon fibre reinforced composite connectors[J]. Journal of Shanghai University（Natural Science Edition）, 2021, 27(2): 325-335.

图/表 14

图1

表1

图2

图3

图4

表2

图5

表3

图6

图7

图8

图9

表4

图10

参考文献 21

[1]	沈真. 复合材料结构设计手册 [M]. 北京: 航空工业出版社, 2001: 145-146.
	Shen Z. Composite structure design handbook [M]. Beijing: Aviation Industry Press, 2001: 145-146.
[2]	薛克兴, 周瑾. 复合材料结构连接件设计与强度 [M]. 北京: 航空工业出版社, 1988: 50-75.
	Xue K X, Zhou J. Design of compsite structural connector and strength [M]. Beijing: Aviation Industry Press, 1988: 50-75.
[3]	中国航空航天工业部. 复合材料手册 [M]. 北京: 航空工业出版社, 1992: 134-189.
	Ministry of Aerospace Industry of China. Composite material handbook [M]. Beijing: Aviation Industry Press, 1992: 134-189.
[4]	Lee J D. Three dimensional finite elelment analysis damage accumulation in composite laminate[J]. Fracture of Composite Materials, 1982,15:335-350.
[5]	张爽, 王栋, 郦正能, 等. 复合材料层合板多钉连接结构累积损伤过程可视化仿真模拟[J]. 复合材料学报, 2006,23(3):135-140.
	Zhang S, Wang D, Li Z N, et al. Visual simulation of damage accumulation for composite multiple bolted joints[J]. Acta Materiae Compositae Sinica, 2006,23(3):135-140.
[6]	Pandey A K, Reddy J N. A post first-ply analysis of composite laminates[C]// Proceeding soft the AIAA/ASME/ASCE/AHS/ASC 28th Structures. Strucural Dynamics and Materials Conference. 1987: 788-797.
[7]	Hühne C, Zerbst A K, Kuhlmann G, et al. Progressive damage analysis of composite bolted joints with liquid shim layers using constant and continuous degradation models[J]. Composite Structures, 2010,92(2):189-200.
[8]	Dano M L, Gendron G, Picard A. Stress and failure analysis of mechanically fastened joints in composite laminates[J]. Composite Structures, 2000,50(3):287-296.
[9]	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, 2005,37(6):788-795.
	Wang D Y, Wen W D, Gui H T. Theree dimensional progressive damage analysis of composite laminates containing a hole subjected to tensile loading[J]. Chinese Journal of Theoretical and Applied Mechanics, 2005,37(16):788-795.
[10]	陈业标, 汪海, 陈秀华. 飞机复合材料结构强度分析 [M]. 上海: 上海交通大学出版社, 2011: 188-189.
	Chen Y B, Wang H, Chen X H. Strength analysis of composite aircraft structures [M]. Shanghai: Shanghai Jiao Tong University Press, 2011: 188-189.
[11]	Herrington P D, Sabbaghian M. Factors affecting the friction coefficients between metallic washers and composite surfaces[J]. Composites, 1991,22(6):418-424.
[12]	王娟, 施建伟, 张书亭, 等. 复合材料螺栓连接接头渐进损伤分析研究进展[J]. 航空制造技术, 2016,59(3):85-89.
	Wang J, Shi J W, Zhang S T, et al. Research progress of progressive damage analysis of composite bolted joint[J]. Aeronautical Manufacturing Technology, 2016,59(3):85-89.
[13]	Hashin Z. Fatigue failure criteria for unidirectional fiber composites[J]. Journal of Applied Mechanics, 1981,48(4):846.
[14]	Tserpes K I, Labeas G, Papanikos P, et al. Strength prediction of bolted joints in graphite/epoxy composite laminates[J]. Composites Part B (Engineering), 2002,33(7):521-529.
[15]	Olmedo Á, Santiuste C. On the prediction of bolted single-lap composite joints[J]. Composite Structures, 2012,94(6):2110-2117.
[16]	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.
[17]	McCarthy C T, McCarthy M A, Lawlor V P. Progressive damage analysis of multi-bolt composite joints with variable bolt-hole clearances[J]. Composites Part B (Engineering), 2005,36(4):290-305.
[18]	Xiao Y, Ishikawa T. Bearing strength and failure behavior of bolted composite joints (part I: experimental investigation)[J]. Composites Science and Technology, 2005,65(7/8):1022-1031.
[19]	Valenza A, Fiore V, Borsellino C, et al. Failure map of composite laminate mechanical joint[J]. Journal of Composite Materials, 2007,41(8):951-964.
[20]	Camanho P P, Matthews F L. A progressive damage model for mechanically fastened joints in composite laminates[J]. Journal of Composite Materials, 1999,33(24):2248-2280.
[21]	Tan S C. A progressive failure model for composite laminates containing openings[J]. Journal of Composite Materials, 1991,25(5):556-577.

L 型碳纤维增强复合材料连接件承载力的渐进损伤分析

Progressive damage analysis of the bearing capacity of L-type carbon fibre reinforced composite connectors

RichHTML

PDF

可视化

摘要/Abstract

引用本文

使用本文

图/表 14

参考文献 21

相关文章 7

编辑推荐

Metrics

本文评价

[1]	杨凯, 裴宁, 王琦鑫, 蔡兰兰. 一种新型磁性生物贴片的性质[J]. 上海大学学报(自然科学版), 2019, 25(5): 767-775.
[2]	唐旭辉, 张顺琦, 应申舜, 陈敏. 复合材料螺栓连接结构的失效行为[J]. 上海大学学报(自然科学版), 2019, 25(4): 502-515.
[3]	陈玥, 李凯, 彭雨晴, 李爱军, 张东升. 离子推进C/C栅极的设计与力学分析[J]. 上海大学学报(自然科学版), 2019, 25(2): 235-244.
[4]	张智梅, 张振波, 黄海涛, 张振凯, 熊浩. 表层嵌贴CFRP 板加固RC 梁的抗弯性能[J]. 上海大学学报(自然科学版), 2017, 23(2): 298-307.
[5]	陆舒逸, 李冬梅, 杨伟光, 黄璐, 金晶, 王晨, 陈阳, 史伟民. HgI₂探测器的共面栅电极设计及有限元模拟优化[J]. 上海大学学报(自然科学版), 2015, 21(5): 657-662.
[6]	张智梅, 李贺林, 张晏戌. CFRP 布约束混凝土矩形短柱轴压性能的非线性有限元分析[J]. 上海大学学报(自然科学版), 2013, 19(2): 203-207.
[7]	欧阳煜,李游. CFRP布加固圆形木梁抗弯性能的试验[J]. 上海大学学报(自然科学版), 2012, 18(5): 545-550.