复合材料沉头衬套螺栓干涉连接渐进损伤数值模拟分析方法

doi:10.3901/JME.2025.07.156

机械工程学报 ›› 2025, Vol. 61 ›› Issue (7): 156-166.doi: 10.3901/JME.2025.07.156

• 特邀专栏：先进纤维增强复合材料加工 • 上一篇下一篇

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复合材料沉头衬套螺栓干涉连接渐进损伤数值模拟分析方法

王岚, 樊宇航, 程晖

西北工业大学机电学院西安 710072

收稿日期:2024-07-05 修回日期:2024-10-29 出版日期:2025-04-05 发布日期:2025-05-12
作者简介:王岚，女，1998年出生，博士研究生。主要研究方向为复合材料衬套螺栓干涉连接损伤机理及强度。E-mail：wangwl@mail.nwpu.edu.cn
程晖(通信作者)，男，1984年出生，博士，教授，博士研究生导师。主要研究方向为复合材料结构装配损伤机理与工艺控制方法、功能结构一体化组装理论与装备。E-mail：chenghui@nwpu.edu.cn
基金资助:
国家自然科学基金资助项目(51975472)。

Numerical Simulation Analysis Method of Progressive Damage for Composite Interference-fit Joint with Countersunk Sleeved Bolt

WANG Lan, FAN Yuhang, CHENG Hui

School of Mechanical Engineering, Northwestern Polytechnical University, Xi'an 710072

Received:2024-07-05 Revised:2024-10-29 Online:2025-04-05 Published:2025-05-12

摘要/Abstract

摘要： 强度增益的衬套式干涉连接技术已成为碳纤维增强复合材料结构的先进连接技术之一，然而在复杂轴、径向安装载荷下，衬套容易发生非均匀塑性变形，从而导致不均匀的损伤分布，降低连接质量。对CFRP沉头衬套螺栓干涉安装进行了试验研究，提出基于应变3D-Hashin准则和连续刚度退化理论的渐进损伤模型，用于模拟CFRP干涉安装层内损伤行为，并采用内聚力模型揭示CFRP分层损伤起始与扩展。结果表明：有限元模型与试验结果拟合度较好，沉头衬套材料在安装过程中向出口处流动堆积，孔壁径向位移沿安装方向逐渐增大；孔壁出口处损伤最为严重，基体压缩损伤面积最大，其与孔壁径向位移分布趋势相似；衬套螺栓的设计干涉量为3%时，能在降低制孔精度的要求下有效控制干涉安装损伤。

关键词: 衬套式干涉连接, 非均匀塑性变形, CFRP, 渐进损伤模型, 干涉量

Abstract: The strength-enhancing interference-fit sleeved bolt joint has evolved into a advanced joint design for carbon fiber reinforced polymer(CFRP) structures. However, under complex axial and radial installation loads, the sleeve is prone to non-uniform plastic deformation, leading to uneven damage distribution and reduced joint quality. An experimental study is conducted to investigate the installation behavior of CFRP interference-fit joint with sleeved bolt. A progressive damage model based on the strain-based 3D-Hashin criterion and continuous stiffness degradation theory is proposed to simulate the intra-laminar damage behavior of CFRP during interference-fit installation. Additionally, a cohesive zone model is employed to reveal the initiation and propagation of delamination. The results indicated that the finite element model showed good agreement with the experimental results. During installation, the countersunk sleeve material is flowed and accumulated towards the exit, with the radial displacement of the hole wall gradually increasing along the installation direction. The damage is most severe at the hole wall exit, with the largest area of matrix compression damage, which follows a distribution trend similar to the radial displacement of the hole wall. When the interference-fit size of the sleeved bolt is designed to be 3%, it can effectively control interference installation damage while reducing the hole-making precision requirements.

Key words: interference-fit joint with sleeved bolt, non-uniform plastic deformation, CFRP, progressive damage model, interference-fit size

中图分类号:

TB330

王岚, 樊宇航, 程晖. 复合材料沉头衬套螺栓干涉连接渐进损伤数值模拟分析方法[J]. 机械工程学报, 2025, 61(7): 156-166.

WANG Lan, FAN Yuhang, CHENG Hui. Numerical Simulation Analysis Method of Progressive Damage for Composite Interference-fit Joint with Countersunk Sleeved Bolt[J]. Journal of Mechanical Engineering, 2025, 61(7): 156-166.

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参考文献

[1] ARTEIRO A，FURTADO C，CATALANOTTI G，et al. Thin-ply polymer composite materials：A review[J]. Composites Part A: Applied Science and Manufacturing，2020，132：105777.
[2] OZKAN D，GOK M S，KARAOGLANLI A C. Carbon fiber reinforced polymer (CFRP) composite materials，their characteristic properties，industrial application areas and their machinability[J]. Engineering Design Applications III：Structures，Materials and Processes，2020：235-253.
[3] ZHAI Y N，LI D S，LI X Q，et al. An experimental study on the effect of bolt-hole clearance and bolt torque on single-lap，countersunk composite joints[J]. Composite structures，2015，127：411-419.
[4] WANG A Y，WANG Z Q，ZHAO M L，et al. Effects of ply thickness and interference-fit on the bearing strength of single-lap countersunk composite joints[J]. Thin- Walled Structures，2023，189：110878.
[5] 程晖，樊新田，徐冠华，等. 航空复合材料结构精密干涉连接技术综述[J]. 航空学报，2021，42(10)：55-73. CHENG Hui，FAN Xintian，XU Guanhua，et al. State of the art of precise interference-fit technology for composite structures in aircraft[J]. Chinese Journal of Aeronautics，2021，42(10)：55-73.
[6] CHAKHERLOU T N，TAGHIZADEH H，AGHDAM A B. Experimental and numerical comparison of cold expansion and interference fit methods in improving fatigue life of holed plate in double shear lap joints[J]. Aerospace Science and Technology，2013，29(1)：351-362.
[7] SONG D L，ZHANG K F，LI Y，et al. Effect of interference percentage on damage mechanism of carbon fiber reinforced plastics laminate during interference-fit bolt installation[J]. Journal of Composite Materials，2017，51(8)：1031-1043.
[8] WEI J C，JIAO G Q，JIA P R，et al. The effect of interference fit size on the fatigue life of bolted joints in composite laminates[J]. Composites Part B：Engineering，2013，53：62-68.
[9] ZUO Y J，YUE TING，JIANG R S，et al. Bolt insertion damage and mechanical behaviors investigation of CFRP/ CFRP interference fit bolted joints[J]. Chinese Journal of Aeronautics，2022，35(9)：354-365.
[10] ZOU P，LI Y，ZHANG K F，et al. Mode I delamination mechanism analysis on CFRP interference-fit during the installation process[J]. Materials & Design，2017，116：268-277.
[11] 刘华东，赵庆云. 长寿命机械连接技术研究应用进展[J]. 航空制造技术，2016，59(19)：64-69，79. LIU Huadong，ZHAO Qingyun. Development of long-life mechanical joining technology[J]. Aeronautical Manufacturing Technology，2016，59(19)：64-69，79.
[12] RAJU K P，BODJONA K，LIM G H，et al. Improving load sharing in hybrid bonded/bolted composite joints using an interference-fit bolt[J]. Composite Structures，2016，149：329-338.
[13] 陈坤，舒茂盛，胡仁伟，等. 带衬套沉头螺栓复合材料/金属接头拉伸性能[J]. 北京航空航天大学学报，2019，45(3)：633-640. CHEN Kun，SHU Maosheng，HU Renwei，et al. Tensile performance of countersunk bolted composite/metal joints with sleeve[J]. Journal of Beijing University of Aeronautics and Astronautics，201945(3)：633-640.
[14] 邹鹏，屈凡. 复合材料衬套螺栓干涉连接安装过程损伤机制[J]. 复合材料学报，2022，39(5)：2449-2459. ZOU Peng，QU Fan. Damage mechanism of composite sleeve-type bolt interference fit structure during the installation process[J]. Acta Materiae Compositae Sinica，2022，39(5)：2449-2459.
[15] 赵庆云，孙昂，黄宏，等. 内锥衬套高锁螺栓性能及接头疲劳寿命研究[J]. 航空制造技术，2023，66(16)：104-110+123. ZHAO Qingyun，SUN Ang，HUANG Hong，et al. Research on properties and joint fatigue life of sleeve taper-hi-bolt[J]. Aeronautical Manufacturing Technology，2023，66(16)：104-110，123.
[16] XU G H，ZHANG K F，CHENG H，et al. An efficient physically-based damage model for interface damage of composites sleeved interference joint and influence analysis of its interface friction[J]. Composite Structures，2021，275：114425.
[17] ASTM D5961/D5961M-13. Standard test method for bearing response of polymer-matrix composite laminates[S]. ASTM Standard，2013.
[18] LIU Y，ZHUANG W M，LUO Y F，et al. Joining mechanism and damage of self-piercing riveted joints in carbon fibre reinforced polymer composites and aluminium alloy[J]. Thin-Walled Structures，2023，182：110233.
[19] HU C X，XU Z H，QIU J Z，et al. A unified modeling strategy of the stability and progressive damage behavior of CFRP double-blade composite stiffened structures (DCSS) under uniaxial compression[J]. Thin-Walled Structures，2023，189：110896.
[20] FAGGIANI A，FALZON B G. Predicting low-velocity impact damage on a stiffened composite panel[J]. Composites Part A：Applied Science and Manufacturing，2010，41(6)：737-749.
[21] CAMANHO P P，DAVILA C G，DE MOURA M F. Numerical simulation of mixed-mode progressive delamination in composite materials[J]. Journal of Composite Materials，2003，37(16)：1415-1438.
[22] BENZEGGAGH M L，KENANE M. Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus[J]. Composites Science and Technology，1996，56(4)：439-449.
[23] ZHOU J W，ZHAO Z B，JIA L Y，et al. A new integrated modeling method for predicting low-velocity impact behavior and residual tensile failure of Z-pinned T- joints[J]. Composites Science and Technology，2024，245：110316.
[24] ASTM E8/E8M-22. Standard test method for tension testing of metallic materials[S]. ASTM Standard，2022.

复合材料沉头衬套螺栓干涉连接渐进损伤数值模拟分析方法

Numerical Simulation Analysis Method of Progressive Damage for Composite Interference-fit Joint with Countersunk Sleeved Bolt

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