干涉配合弹性强化机理分析

doi:10.7527/S1000-6893.2017.21687

材料工程与机械制造

本期目录 | 过刊浏览 | 高级检索

前一篇 |

干涉配合弹性强化机理分析

张岐良¹, 曹增强², 李红梅¹, 向聪¹, 刘平¹

1. 中国工程物理研究院总体工程研究所, 绵阳 621900;
2. 西北工业大学机电学院, 西安 710072

收稿日期:2017-08-22 修回日期:2017-12-07 出版日期:2018-04-15 发布日期:2017-12-07
通讯作者: 张岐良,E-mail:tyrone1225@hotmail.com E-mail:tyrone1225@hotmail.com
基金资助:
国家自然科学基金（51505447，11602255）

Elastic fatigue enhancement mechanism of interference fit

ZHANG Qiliang¹, CAO Zengqiang², LI Hongmei¹, XIANG Cong¹, LIU Ping¹

1. Institute of Systems Engineering, China Academy of Engineering Physics, Mianyang 621900, China;
2. School of Mechanical Engineering, Northwestern Polytechnical University, Xi'an 710072, China

Received:2017-08-22 Revised:2017-12-07 Online:2018-04-15 Published:2017-12-07
Supported by:
National Natural Science Foundation of China (51505447, 11602255)

摘要/Abstract

摘要： 鉴于基于支撑效应（SE）的干涉配合疲劳强化理论具有内在的局限性，通过引入弹簧模型（SM）研究了干涉配合的强化机理，以期获得更全面的认识并促进干涉配合技术的应用。首先，分析了支撑效应理论的不足之处，提出了经典理论难以解释的多个问题；然后，介绍了弹簧模型的基本思想及其求解结果，从弹性变形的角度对以上疑难问题作出了解释；最后，借助弹簧模型给出了干涉量的优化方法，并得到了最佳干涉量的解析表达式。弹簧模型的计算结果表明：干涉配合存在一种动态的弹性强化机制，在交变外载作用下结构组件的弹性变形及接触的自动调节作用，是被连接件传载幅值得以降低的原因；干涉量的选取不仅要考虑结构尺寸和材料，同时还应结合实际的载荷条件。

关键词: 干涉配合, 弹簧模型, 强化机理, 疲劳, 应力幅

Abstract: In view of the limitations of the traditional interference theory based on the supporting effect (SE), the spring model (SM) is introduced here to study the fatigue enhancing mechanism of interference, in the hope of obtaining a more comprehensive understanding of the interference strengthening technology and promoting its applications. The inadequacies of the SE theory are firstly analyzed, and a range of insoluble problems are discussed. Then, an introduction of the basic concepts and the analytical results of the SM are given. The mentioned problems are explained in terms of elastic deformation, and the analytical solution for the optimum amount of interference is derived. An analysis of the SM indicates that there exists an elasticity reinforcement mechanism in an interference-fitted joint, and the elastic deformation of member components subjected to alternating external applied load and the automatic regulating effect of contact are the reason for the reduction of the amplitude of load transferred by the connected members. It is also concluded that the sizes and materials of components, as well as actual loading conditions, should be taken into consideration in determining the optimum interference.

Key words: interference fit, spring model, enhancing mechanism, fatigue, stress amplitude

中图分类号:

V260.1

张岐良, 曹增强, 李红梅, 向聪, 刘平. 干涉配合弹性强化机理分析[J]. 航空学报, 2018, 39(4): 421687-421687.

ZHANG Qiliang, CAO Zengqiang, LI Hongmei, XIANG Cong, LIU Ping. Elastic fatigue enhancement mechanism of interference fit[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(4): 421687-421687.

参考文献

[1] CHAKHERLOU T N, RAZAVI M J, AGHDAM A B, et al. An experimental investigation of the bolt clamping force and friction effect on the fatigue behavior of aluminum alloy 2024-T3 double shear lap joint[J]. Materials & Design, 2011, 32(8):4641-4649.
[2] WU T, ZHANG K F, CHENG H, et al. Analytical modeling for stress distribution around interference fit holes on pinned composite plates under tensile load[J]. Composites Part B:Engineering, 2016,100(1):176-185.
[3] MOHAMMADPOUR A, CHAKHERLOU T N. Numerical and experimental study of an interference fitted joint using a large deformation Chaboche type combined isotropic-Kinematic hardening law and mortar contact method[J]. International Journal of Mechanical Sciences, 2016, 106:297-318.
[4] MIRZAJANZADEH M, CHAKHERLOU T N, VOGWELL J. The effect of interference-fit on fretting fatigue crack initiation and ΔK of a single pinned plate in 7075 Al-alloy[J]. Engineering Fracture Mechanics, 2011, 78(6):1233-1246.
[5] 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.
[6] LIU J, WU H, YANG J, et al. Effect of edge distance ratio on residual stresses induced by cold expansion and fatigue life of TC4 plates[J]. Engineering Fracture Mechanics, 2013,109(3):130-137.
[7] 左杨杰, 曹增强, 杨柳,等. 基于对称加载的均匀干涉配合铆接方法[J]. 航空学报, 2016, 37(3):1049-1059. ZUO Y J, CAO Z Q, YANG L, et al. Interference-fit evenness riveting method based on symmetrical loading[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(3):1049-1059(in Chinese).
[8] 姜杰凤, 董辉跃, 柯映林. 高锁螺栓干涉连接中极限干涉量[J]. 机械工程学报, 2013, 49(3):145-152. JIANG J F, DONG H Y, KE Y L. Maximum interference fit size of hi-lock bolted joints[J]. Chinese Journal of Mechanical Engineering, 2013, 49(3):145-152(in Chinese).
[9] CHAKHERLOU T N, ABAZADEH B. Investigating clamping force variations in Al2024-T3 interference fitted bolted joints under static and cyclic loading[J]. Materials & Design, 2012, 37:128-136.
[10] ABAZADEH B, CHAKHERLOU T N, ALDERLIESTEN R C. Effect of interference fitting and/or bolt clamping on the fatigue behavior of Al alloy 2024-T3 double shear lap joints in different cyclic load ranges[J]. International Journal of Mechanical Sciences, 2013, 72(7):2-12.
[11] TIMOSHENKO S P. Strength of materials part Ⅱ:Advanced theory and problems[M].3rd ed. 1956:205-213.
[12] HSU Y C, FORMAN R G. Elastic-plastic analysis of an infinite sheet having a circular hole under pressure[J]. Journal of Applied Mechanics, 1975, 42(2):347-352.
[13] GUO W L. Elastic-plastic analysis of a finite sheet with a cold-worked hole[J]. Engineering fracture mechanics, 1993, 46(3):465-472.
[14] 郭兰中, 朱琪, 邢文珍. 过盈压入强化预应力及其变化规律的研究[J]. 应用力学学报, 2002, 19(1):27-31. GUO L Z, ZHU Q, XING W Z. Prestressing of force-fit and its characters under load[J]. Chinese Journal of Applied Mechanics, 2002, 19(1):27-31(in Chinese).
[15] KIM S Y, HE B, SHIM C S, et al. An experimental and numerical study on the interference-fit pin installation process for cross-ply glass fiber reinforced plastics (GFRP)[J]. Composites Part B:Engineering, 2013, 54:153-162.
[16] LANCIOTTI A, POLESE C. The effect of interference-Fit fasteners on the fatigue life of central hole specimens[J]. Fatigue & Fracture of Engineering Materials & Structures, 2005, 28(7):587-597.
[17] HAO D, WANG D. Finite-element modeling of the failure of interference-fit planet carrier and shaft assembly[J]. Engineering Failure Analysis, 2013, 33(7):184-196.
[18] 张岐良, 曹增强, 甘学东, 等. 拉伸板中心孔干涉配合对载荷幅值的影响[J]. 航空学报, 2014, 35(6):1643-1650. ZHANG Q L, CAO Z Q, GAN X D, et al. Effect of interference-fit on load amplitude of a single central holed tensile plate[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(6):1643-1650(in Chinese).
[19] ZHANG Q L, CAO Z Q, WEI FY, et al. Mechanical analysis of a pin interference-fitted sheet under tensile loading[J]. Journal of Aerospace Engineering, 2016, 29(4):04015085.
[20] 中国航空科学技术研究院. 飞机结构抗疲劳断裂强化设计手册[M]. 北京:航空工业出版社, 1993. Chinese Academy of Aviation Science and Technology. Handbook of aircraft structure anti-fatigue and anti-fracture strengthen technology[M]. Beijing:Aviation Industry Press, 1993(in Chinese).
[21] BROWN M A, EVANS J L. Fatigue life variability due to variations in interference fit of steel bushings in 7075-T651 aluminum lugs[J]. International Journal of Fatigue, 2012, 44(9):177-187.
[22] CHAKHERLOU T N, MIRZAJANZADEH M, VOGWELL J. Experimental and numerical investigations into the effect of an interference fit on the fatigue life of double shear lap joints[J]. Engineering Failure Analysis, 2009, 16(7):2066-2080.
[23] CROCCOLO D, DE A M, CESCHINI L, et al. Interference fit effect on improving fatigue life of a holed single plate[J]. Fatigue & Fracture of Engineering Materials & Structures, 2013, 36(7):689-698.
[24] 郝小忠, 王珉, 陈文亮. 自动钻铆最佳干涉量试验研究[J]. 航空制造技术, 2012(12):77-79. HAO X Z, WANG M, CHEN W L. Experimental research of best interference fit level on automatic drilling and riveting[J]. Aeronautical Manufacturing Technology, 2012(12):77-79(in Chinese).

E-mail：hkxb@buaa.edu.cn

关于我们

期刊社服务

专业学科

封面文章

友情链接

主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

干涉配合弹性强化机理分析

Elastic fatigue enhancement mechanism of interference fit

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	范永升, 杨晓光, 石多奇, 谭龙, 黄渭清. 服役涡轮叶片筏化判废：定量表征及阈值确定[J]. 航空学报, 2022, 43(9): 625100-625100.
[2]	徐家进, 高镇同. 疲劳统计学智能化的进一步研究[J]. 航空学报, 2022, 43(8): 225138-225138.
[3]	李晓阳, 陶昭, 张慰. 基于不确定微分方程的疲劳可靠性建模[J]. 航空学报, 2022, 43(8): 225820-225820.
[4]	毛森鑫, 时寒阳, 李开响, 张晓, 朱云涛, 杜娟, 邹康庄, 熊峻江. 振动疲劳载荷谱编制与试验验证[J]. 航空学报, 2022, 43(7): 426585-426585.
[5]	郭琼, 刘玮, 裴连杰, 郭俊豪. 全尺寸复合材料机身筒段静力/疲劳试验技术[J]. 航空学报, 2022, 43(6): 525816-525816.
[6]	王秋懿, 吴彦增, 鲍蕊. 疲劳裂纹扩展过程中的CTOD相关参量分析[J]. 航空学报, 2022, 43(6): 526632-526632.
[7]	杨宇, 王彬文, 祁小凤. 面向全尺寸民机结构疲劳试验的声发射监测技术[J]. 航空学报, 2022, 43(6): 527044-527044.
[8]	吕帅帅, 杨宇, 王彬文, 殷晨飞. 基于改进FaceNet的飞行器结构裂纹识别方法[J]. 航空学报, 2022, 43(6): 525463-525463.
[9]	苏少普, 常文魁, 陈先民. 飞机典型壁板结构剪切屈曲疲劳试验与分析方法[J]. 航空学报, 2022, 43(5): 225219-225219.
[10]	王育鹏, 田文朋, 宋鹏飞, 夏峰, 冯建民. 民机全机疲劳试验综合加速技术研究与验证[J]. 航空学报, 2022, 43(5): 224919-224919.
[11]	陈克明, 田若洲, 郭素娟, 王润梓, 张成成, 陈浩峰, 张显程, 涂善东. 循环热机载荷作用下航空涡轮盘蠕变疲劳寿命预测[J]. 航空学报, 2022, 43(5): 225290-225290.
[12]	刘欣, 杨景超, 李恒, 张艳红, 杨智伟, 谷箐菲, 李光俊, 黄丹. 管路构件塑性变形连接技术研究进展及挑战[J]. 航空学报, 2022, 43(4): 525258-525258.
[13]	王天帅, 贺小帆, 王金宇, 李玉海. 基于双峰对数正态分布模型的DED-TA15钛合金DFR值估计方法[J]. 航空学报, 2022, 43(3): 225013-225013.
[14]	贺小帆, 朱俊贤. 军用飞机结构耐久性严重谱编制与应用研究进展[J]. 航空学报, 2022, 43(12): 25070-025070.
[15]	张亦波, 陈迪, 成正强, 沈培良, 熊峻江. 铝合金薄板冲击后疲劳试验与谱载寿命[J]. 航空学报, 2022, 43(1): 224811-224811.