复合材料带填充钉孔层压板拉伸载荷下损伤特性分析

doi:10.19936/j.cnki.2096-8000.20230328.013

复合材料科学与工程 ›› 2023, Vol. 0 ›› Issue (3): 89-94.DOI: 10.19936/j.cnki.2096-8000.20230328.013

复合材料带填充钉孔层压板拉伸载荷下损伤特性分析

张幻实, 张发, 高丽敏, 贾银磊

中国商飞北京民用飞机技术研究中心民用飞机结构与复合材料北京市重点实验室,北京 102211

收稿日期:2022-09-07 出版日期:2023-03-28 发布日期:2023-04-28
作者简介:张幻实(1992—),男,硕士,工程师,主要从事飞行器结构强度设计分析等方面的研究。

Damage characteristics analysis of composite laminates with filled nail holes under tensile load

ZHANG Huanshi, ZHANG Fa, GAO Limin, JIA Yinlei

Beijing Key Laboratory of Commercial Aircraft Structures and Composite Materials, COMAC Beijing Aircraft Technology Research Institute, Beijing 102211, China

Received:2022-09-07 Online:2023-03-28 Published:2023-04-28

摘要/Abstract

摘要： 复合材料填充钉孔层压板常用于机械连接设计中,考虑了开孔处的螺栓约束和层压板钉孔周边区域挤压变形的旁路失效问题,主要用于飞机复合材料结构的强度许用值设计,在航空航天等领域受到日益广泛的应用。为比较依据不同失效准则开展的复合材料带填充钉孔层压板拉伸损伤扩展失效特性,利用ABAQUS有限元软件,建立了二维和三维有限元模型,建模中考虑了材料非线性行为和失效判断等基本问题,基于Hashin准则和LaRC05准则对相应铺层顺序的含填充钉孔复合材料层压板进行了静态拉伸数值模拟,根据ASTM D6742进行了填充钉孔层压板单轴拉伸试验,将数值模拟结果与试验结果进行对比,数值模拟结果较好地模拟了含填充钉孔复合材料层压板的拉伸渐进失效模式,具有良好的工程应用意义。

关键词: 复合材料层压板, 扩展有限元法, LaRC05准则, Hashin准则, 拉伸破坏, 损伤特性

Abstract: Composite laminates filled with pin holes are often used in mechanical connection design. Considering the bolt constraint at the opening and the bypass failure of extrusion deformation in the area around the pin hole of the laminate, they are mainly used for the design of strength allowable values of aircraft composite structures, and are increasingly widely used in aerospace and other fields. In order to compare the tensile damage propagation failure characteristics of composite laminates with filled pin holes based on different failure criteria, two-dimensional and three-dimensional finite element models were established using ABAQUS finite element software. The nonlinear behavior of materials and failure judgment were considered in the modeling. Based on Hashin criterion and LaRC05 criterion, the static tensile numerical simulation of composite laminates with filled pin holes in the corresponding stacking sequence was carried out. According to ASTM D6742, uniaxial tensile test of composite laminates with filled pin holes was carried out. The numerical simulation results were compared with the test results. The numerical simulation results simulated the tensile progressive failure mode of composite laminates with filled pin holes, which has good engineering application significance.

Key words: composite laminates, extended finite element method, LaRC05 criterion, Hashin criterion, tensile failure, damage characteristics

中图分类号:

TB332

张幻实, 张发, 高丽敏, 贾银磊. 复合材料带填充钉孔层压板拉伸载荷下损伤特性分析[J]. 复合材料科学与工程, 2023, 0(3): 89-94.

ZHANG Huanshi, ZHANG Fa, GAO Limin, JIA Yinlei. Damage characteristics analysis of composite laminates with filled nail holes under tensile load[J]. COMPOSITES SCIENCE AND ENGINEERING, 2023, 0(3): 89-94.

参考文献

[1] PETIT P H,WADDOUPS M E. A method of predicting the nonlinear behavior of laminated composites[J]. Journal of Composite Materials, 1969, 3(1): 2-19.
[2] CHANG K Y, LIU S, CHANG F K. Damage tolerance of laminated composites containing an open hole and subjected to tensile loadings[J]. Journal of Composite Materials, 1991, 25(3): 274-301.
[3] TAN S C, PEREZ J. Progressive failure of laminated composites with a hole under compressive loading[J]. Jourmal of Reinforced Plastics and Composites, 1993, 12: 1043-1057.
[4] TOLSON S, ZABARAS N. Finite element analysis of progressive failure in laminated composite plates[J]. Computer and Structure,1991, 38(3): 361-376.
[5] REDDY Y S, REDDY J N. Three-dimensional finite element progressive failure analysis of composite laminates under axial extension[J]. Journal of Composites Technology and Research, 1993, 15(2): 73-87.
[6] CHEN W H, LEE S S, YEH J T. Three-dimensional contact stress analysis of a composite laminate with bolted joint[J]. Composite Structures, 1995, 30: 287-297.
[7] 卢子兴, 徐强, 王伯平, 等. 含缺陷平纹机织复合材料拉伸力学行为数值模拟[J]. 复合材料学报, 2011, 28(6): 200-207.
[8] 张超, 许希武, 毛春见. 三维编织复合材料渐进损伤模拟及强度预测[J]. 复合材料学报, 2011, 28(2): 222-230.
[9] CHANG F K, LESSARD L B. Damage tolerance of laminated composites containing an open hole and subjected to tensile loadings: Part Ⅰ-analysis[J]. Journal of Composite Materials, 1991, 25: 2-43.
[10] 姚辽军, 赵美英, 周银华. 不同孔径复合材料层合板应变集中及失效强度分析[J]. 机械科学与技术, 2011, 30(5): 95-102.
[11] ZHANG D, ZHENG X T, WU T C. Damage characteristics of open-hole laminated composites subjected to longitudinal loads[J]. Composite Structures, 2019, 230: 111474.
[12] MA Z Y, CHEN J L, YANG Q D, et al. Progressive fracture analysis of the open-hole composite laminates: Experiment and simulation[J]. Composite Structures, 2021, 262: 113628.
[13] LIU H B, BRIAN G F, LI S P, et al. Compressive failure of woven fabric reinforced thermoplastic composites with an open-hole:An experimental and numerical study[J]. Composite Structures, 2019, 213: 108-117.
[14] FAN H T, WANG H. Predicting the open-hole tensile strength of composite plates based on probabilistic neural network[J]. Applied Composite Materials, 2014, 21: 827-840.
[15] WANG X, JIA P R,WANG B. Progressive failure model of high strength glass fiber composite structure in hygrothermal environment[J]. Composite Structures, 2022, 280: 114932.

复合材料带填充钉孔层压板拉伸载荷下损伤特性分析

Damage characteristics analysis of composite laminates with filled nail holes under tensile load

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