铝锂合金薄板自动钻铆残余应力特性

上海交通大学学报（自然版） ›› 2016, Vol. 50 ›› Issue (04): 595-600.

铝锂合金薄板自动钻铆残余应力特性

郑斌1，余海东1，林忠钦1，邹成2

(1. 上海交通大学上海市复杂薄板结构数字化制造重点实验室，上海 200240； 2. 上海飞机制造有限公司航空制造技术研究所，上海 200436)

收稿日期:2015-04-06 出版日期:2016-04-28 发布日期:2016-04-28
基金资助:
国家自然科学基金(51275292),国家商飞制造工程技术研究中心创新基金(SAMC13JS15026)资助

Residual Stresses of AlLi Alloy Sheets in Automatic Drilling Riveting Process

ZHENG Bin1,YU Haidong1，LIN Zhongqin1,ZOU Cheng2

(1. Shanghai Key Laboratory of Digital Manufacture for ThinWalled Structure Technology, Shanghai Jiaotong University, Shanghai 200240, China; 2. Institute of Aeronautical Manufacturing Technology, Shanghai Aircraft Manufacturing Co. Ltd., Shanghai 200436, China)

Received:2015-04-06 Online:2016-04-28 Published:2016-04-28

摘要/Abstract

摘要： 摘要：利用主应力法推导了铆接壁板所受压力的力学公式，将壁板等效为厚壁圆筒，根据空间轴对称问题求解方法，得出铆接孔孔壁处径向和周向残余应力的表达式，理论分析结果可以合理解释镦头高度和钉孔直径对孔壁处残余应力的影响规律：随着镦头高度和钉孔直径的变化，孔壁各处径向残余应力的变化并不明显，而周向残余应力的变化十分显著；镦头高度和孔径尺寸的增加使周向残余压应力的绝对值下降，甚至出现残余压应力转变为残余拉应力的情况.对于孔壁处残余应力沿板厚方向的分布，采用有限元方法进行分析.结果表明，上、下壁板间应力存在突变，下壁板孔壁处残余应力呈“C”型分布.得出铝锂合金材料在自动钻铆过程中相关工艺参数的合理取值.

关键词: 铝锂合金, 镦头高度, 钉孔直径, 残余应力

Abstract: Abstract： Residual stress induced by riveting process is critical to the fatigue life of riveted structures. In this paper, the principal stress method was employed to calculate the pressure on the surface of rivet hole and the stress between upset head and sheet. The radial and circumferential residual stresses were solved by using the spatial axisymmetric elastoplasticity theory, where the sheets were equivalent to a thickwalled cylinder. The change of residual stresses caused by various process parameters was explained by the analytical results reasonably. The results show that the circumferential residual stress decreases with the increase of the upset head height and the rivet hole diameter. However, the radial residual stress is approximately independent of the two parameters. The distribution of residual stress on the surface of rivet hole along the thickness direction was investigated by using the finite element method. The results indicate that the residual stress on the faying surface is discontinuous. A Cshaped distribution of residual stress was introduced into the surface of rivet hole in the lower sheet. Reasonable process parameters were given for the Al-Li alloy sheets in the automatic drilling riveting process.

Key words: Key words： Al-Li alloy, upset head height, rivet hole diameter, residual stress

中图分类号:

V 261

郑斌1，余海东1，林忠钦1，邹成2. 铝锂合金薄板自动钻铆残余应力特性[J]. 上海交通大学学报（自然版）, 2016, 50(04): 595-600.

ZHENG Bin1,YU Haidong1，LIN Zhongqin1,ZOU Cheng2. Residual Stresses of AlLi Alloy Sheets in Automatic Drilling Riveting Process[J]. Journal of Shanghai Jiaotong University, 2016, 50(04): 595-600.

参考文献

［1］袁立. 航空制造工程手册: 飞机装配［M］. 2版. 北京：航空工业出版社, 2010. ［2］PARK J H, ATLURI S N. Fatigue growth of multicracks near a row of fastenerholes in a fuselage lapjoint ［J］. Computational Mechanics, 1993, 13(3): 189203. ［3］SHISHKIN S S. Computation of the contact load in a rivet bond ［J］. Journal of Machinery Manufacture and Reliability, 2010, 39(1): 4346. ［4］邓将华, 李春峰, 于海平，等. 电磁铆接钉杆长度对连接的影响［J］. 福州大学学报(自然科学版)，2010， 38(6): 866870. DENG Jianghua, LI Chunfeng, YU Haiping, et al. Effect of rivet shaft length on joining in electromagnetic riveting ［J］. Journal of Fuzhou University (Natural Science), 2010, 38(6): 866870. ［5］李奕寰, 曹增强, 张岐良，等.铆模倾角对铆接质量的影响研究［J］. 航空学报, 2013, 34(2): 426433. LI Yihuan, CAO Zengqiang, ZHANG Qiliang, et al. Study on the effect of riveting quality with different angles of the forming cup of riveting die ［J］. Acta Aeronoutica et Astronautica Sinica, 2013, 34(2): 426433. ［6］于海平, 邓将华, 李春峰，等. 电磁铆接加载速率对TA1铆钉变形影响研究［J］. 哈尔滨工程大学学报, 2011， 32(3): 378383. YU Haiping, DENG Jianghua, LI Chunfeng, et al. Effects of loading rate on TA1 rivet deformation in electromagnetic riveting［J］. Journal of Harbin Engineering University, 2011, 32(3): 378383. ［7］曹增强, 佘公藩, 夏力农，等. 不同加载速率下铆钉材料变形研究［J］. 西北工业大学学报， 2000, 18(1): 2730. CAO Zengqiang, SHE Gongfan, XIA Linong, et al. The deformation of rivet materials under different loading rate［J］. Journal of Northwestern Polytechnical University, 2000, 18(1): 2730. ［8］SZOLWINSKI M P, FARRIS T N. Linking riveting process parameters to the fatigue performance of riveted aircraft structures ［J］. Journal of Aircraft, 2000, 37(1): 130137. ［9］LI G, SHI G, BELLINGER N C. Studies of residual stress in singlerow countersunk riveted lap joints ［J］. Journal of Aircraft， 2006， 43(3)： 592599. ［10］LI G, SHI G, BELLINGER N C. Study of the residual strain in lap joints ［J］. Journal of Aircraft, 2006, 43(4): 11451151. ［11］RANS C D, STRAZNICKY P V, ALDERLIESTEN R C. Riveting process induced residual stresses around solid rivets in mechanical joints ［J］. Journal of Aircraft, 2007, 44(1): 323329. ［12］罗子健. 金属塑性加工理论与工艺［M］. 西安：西北工业大学出版社，1994. ［13］梁亚平, 王惠珍, 任兴民. 两端均布轴向线性分布压力作用下厚壁圆筒空间轴对称问题的解析解［J］. 中国科学(G辑: 物理学力学天文学), 2007, 37(5): 684688. LIANG Yaping, WANG Huizhen, REN Xingmin. Analytical solution for spatial axisymmetric problem of a thickwall cylinder subjected to both ends average pressure and axially linear distribution pressure ［J］. Science in China (Series G: Physics, Mechanics & Astronomy), 2007, 37(5): 684688. ［14］MANES A, GIGLIO M, VIGANò F. Effect of riveting process parameters on the local stress field of a Tjoint ［J］. International Journal of Mechanical Sciences, 2011, 53(12): 10391049.

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