| 162 | 0 | 9 |
| 下载次数 | 被引频次 | 阅读次数 |
聚焦于干涉量这一核心工艺参数,系统探究了其对CFRP单搭螺栓连接静力与疲劳性能的双重影响规律。通过开展涵盖4种干涉水平的准静态拉伸与拉-拉疲劳试验,量化分析了干涉量对连接结构屈服载荷、失效模式及疲劳寿命的调控作用。试验结果表明,结构的静强度随干涉量增加呈单调递增趋势,疲劳寿命则呈现先增后降的非线性响应规律,并在0.6%的干涉量下达到峰值。此外,构建了考虑干涉装配效应的三维渐进损伤有限元模型,该模型耦合了三维Hashin失效准则、剩余刚度/强度退化模型及等寿命方程。仿真结果与试验数据高度吻合,精确预测了全工况下的疲劳寿命,最大误差小于3.6%,成功复现了孔周基体损伤等关键失效形貌。
Abstract:Focusing on interference amount as the core process parameter, its dual influence on both the static and fatigue performance of CFRP single-lap bolted joints was systematically explored. Through conducting quasi-static tension and tension-tension fatigue tests across four interference levels, the regulatory effects of interference amount on the yield load, failure mode and fatigue life of the joint structures were quantitatively analyzed. Test results indicate that the static strength increases monotonically with the increase of interference amount,while the fatigue life exhibits nonlinear response laws of increasing first and then decreasing, and reaches peak value with interference amount of 0. 6%. Furthermore, a three-dimensional progressive damage finite element model incorporating the interference assembly effect was developed. This model couples 3D Hashin failure criterion with residual stiffness/strength degradation models and constant life equation. The simulation results align well with test data, the fatigue life across all working conditions is accurately predicted, with the maximum error below 3. 6%, and the key failure morphologies such as matrix damage around the hole are successfully replicated.
[1]曹增强,张铭豪,谭学才,等.航空复合材料结构铆接技术综述[J].航空制造技术, 2023, 66(Z1):26-37.CAO Zengqiang, ZHANG Minghao, TAN Xuecai, et al. Review of riveting technology for aviation composite structures[J]. Aeronautical Manufacturing Technology, 2023, 66(Z1):26-37.
[2] VAN DER SYPT P, CHéRIF M, BOIS C. Analysis of the fatigue behaviour of laminated composite holes subjected to pin-bearing loads[J]. International Journal of Fatigue, 2017, 103:86-98.
[3] KIM S Y, HE B, KIM D, et al. Bearing strength of interference-fit pin joined glass fiber reinforced plastic composites[J]. Journal of Composite Materials, 2020, 54(12):1579-1591.
[4]杨柳,岳婷,左杨杰,等.复合材料结构用干涉配合高锁螺栓技术[J].航空精密制造技术, 2022, 58(3):27-30.YANG Liu, YUE Ting, ZUO Yangjie, et al. Technology of interference-fit Hi-lock bolts for composite structures[J]. Aviation Precision Manufacturing Technology, 2022, 58(3):27-30.
[5]魏景超,柴亚南,刘风雷,等.单面螺纹抽钉干涉配合复合材料连接结构的疲劳性能研究[J].航空制造技术, 2017,(22):50-55.WEI Jingchao, CHAI Yanan, LIU Fenglei, et al. Study on fatigue performance of interference-fit composite joint structure with singleside threaded blind rivets[J]. Aeronautical Manufacturing Technology, 2017,(22):50-55.
[6] WEI J, JIAO G, JIA P, 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.
[7] WANG A, WANG Z, ZHAO M, 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.
[8]程小全,杜晓渊.纤维增强复合材料疲劳寿命预测及损伤分析模型研究进展[J].北京航空航天大学学报, 2021, 47(7):1311-1322.CHENG Xiaoquan, DU Xiaoyuan. Research progress on fatigue life prediction and damage analysis models of fiber-reinforced composites[J]. Journal of Beijing University of Aeronautics and Astronautics, 2021, 47(7):1311-1322.
[9] GERENDT C, DEAN A, MAHRHOLZ T, et al. On the progressive fatigue failure of mechanical composite joints:Numerical simulation and experimental validation[J]. Composite Structures,2020, 248. DOI:10. 1016/j. compostruct. 2020. 112488.
[10] ZHOU S, LI Y, FU K, et al. Progressive fatigue damage modelling of fibre-reinforced composite based on fatigue master curves[J]. Thin-Walled Structures, 2021, 158.
[11] ASTM D5961—2013, Standard test method for bearing response of polymer matrix composite laminates[S].
[12] ASTM D6873—2013, Standard practice for bearing fatigue response of polymer matrix composite laminates[S].
[13] WANG A, WANG Z, ZHAO Y, et al. Fatigue behaviour and failure mechanism of the thin/thick-ply hybrid laminated composite bolted joints[J]. Composite Structures, 2022, 295:115636.
[14] KAPID?IC'Z, GRANADOS D Lá, ARIAS J A M, et al. Bolt fatigue in CFRP joints[J]. International Journal of Fatigue, 2022,164.
[15]徐颖.层合板接头损伤失效与疲劳寿命研究[J].南京:南京航空航天大学, 2007.XU Ying. Study on impact damage and post-impact fatigue life of composite laminates[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2007.
[16] SHOKRIEH M M, LESSARD L B. Progressive fatigue damage modeling of composite materials, Part I:Modeling[J]. Journal of composite materials, 2000, 34(13):1056-1080.
[17] BEHESHTY M, HARRIS B, ADAM T. An empirical fatigue-life model for high-performance fibre composites with and without impact damage[J]. Composites Part A:Applied Science and Manufacturing, 1999, 30(8):971-987.
[18] GATHERCOLE N, REITER H, ADAM T, et al. Life prediction for fatigue of T800/5245 carbon-fibre composites:I. Constant-amplitude loading[J]. International Journal of Fatigue, 1994, 16(8):523-532.
[19] ZUO Y, YUE T, JIANG R, 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.
基本信息:
中图分类号:V215;TH131.3
引用信息:
[1]张金煜,王盟圣,杨永泰.干涉量对CFRP螺栓连接力学性能的影响分析与数值仿真[J].塑性工程学报().
基金信息:
福建省科技计划-STS院省合作项目(2024T3052)
2025-12-31
2025-12-31
2025-12-31