[1] 孙暄,王珉,许洪昌,等. 孔的开缝衬套冷挤压强化技术[J]. 机械制造,1998(1):22-24. SUN Xuan,WANG Min,XU Hongchang,et al. Split sleeve hole cold expansion technique[J]. Machinery,1998(1):22-24. [2] PUCILLO G P. The effects of the cold expansion degree on the fatigue crack growth rate in rail steel[J]. International Journal of Fatigue,2022,164:107130. [3] 王燕礼,朱有利,曹强,等. 孔挤压强化技术研究进展与展望[J]. 航空学报,2018,39(2):6-22. WANG Yanli,ZHU Youli,CAO Qiang,et al. Progress and prospect of research on hole cold expansion technique[J]. Acta Aeronautica et Astronautica Sinica,2018,39(2):6-22. [4] 曹增强,胡朝阳,甘学东,等. 小边距孔的压合衬套强化工艺研究[J]. 机械强度,2016,38(5):1093-1098. Cao Zengqiang,HU Zhaoyang,GAN Xuedong,et al. The research of bushing strengthening process on short edge-margin hole[J]. Journal of Mechanical Strength,2016,38(5):1093-1098. [5] ABDELKADER D,ABDELGHANI B,MOSTEFA L,et al. Numerical analysis of plate thickness effect on residual stress distribution around a cold expanded hole[J]. Transactions of Famena,2023,47(3):47-59. [6] 唐伟,林忠亮,吴保全,等. 孔结构压合衬套冷挤压强化的疲劳寿命试验研究[J]. 航空精密制造技术,2022,58(4):11-15,41. TANG Wei,LIN Zhongliang,WU Baoquan,et al. Test study on fatigue life of cold extrusion strengthening bushings for hole structure[J]. Aviation Precision Manufacturing Technology,2022,58(4):11-15,41. [7] LIU Jun,WU Henggui,YANG Jinjie,et al. Effect of edge distance ratio on residual stresses induced by cold expansion and fatigue life of TC4 plates[J]. Engineering Fracture Mechanics,2013,109130-109137. [8] 董卫萍,高飞,邢欣,等. 开缝衬套冷挤压强化工艺对7050铝合金孔连接结构疲劳寿命的影响[J]. 工具技术,2021,55(12):68-72. DONG Weiping,GAO Fei,XING Xin,et al. Effect of cold extrusion strengthening technology of split-sleeve bushing on fatigue life of 7050 Al alloy hole connection structure[J]. Tool Engineering,2021,55(12):68-72. [9] GOPALAKRISHNA H,MURTHY N H,KRISHNA M. Cold expansion of holes and resulting fatigue life enhancement and residual stresses in Al 2024 T3 alloy- An experimental study[J]. Engineering Failure Analysis,2010,17(2):361-368. [10] 鲁世红,高越,李大川. 开缝衬套冷挤压强化技术研究进展[J]. 锻压技术,2021,46(1):1-9. LU Shihong,GAO Yue,LI Dachuan. Research progress of split sleeve cold expansion strengthening technology[J]. Forging & Stamping Technology,2021,46(1):1-9. [11] 刘莉,何庆芝,瞿履和. 螺接接头最优干涉配合问题的研究[J]. 航空学报,1989(12):640-644. LIU Li,HE Qingzhi,QU Lühe. Studies on the optimization of the interference fit of a bolt joint[J]. Acta Aeronautica et Astronautica Sinica,1989(12):640-644. [12] 计欣华,邓宗白,鲁阳,等. 工程试验力学[M]. 北京:机械工业出版社,2007. JI Xinhua,DENG Zongbai,LU Yang,et al. Engineering experimental mechanics[M]. Beijing:China Machine Press,2007. [13] HAKIM A B,HACÈNE T,KHALED B. Analytical solution of aluminum alloy plates with holes subjected to cold expansion with reverse yielding[J]. J. Pressure Vessel Technol,2021,143(4):041302-041312. [14] Feng Feng,ZHAO Zirui,WANG Zibiao,et al. A calculation method for residual stress of cold expanded hole based on measured springback[J]. Measurement,2023,218:113162. [15] 闫五柱. 压合衬套的安装方法及结构件:中国,CN112077564B[P]. 2022-07-29. YAN Wuzhu. Installation method and structural parts of bushing:China,CN112077564A[P]. 2022-07-29. [16] 王耀伟,闫五柱,梁淑静. 一种新型压合衬套冷挤压工艺研究[J]. 航空制造技术,2024,67(10):107-114. WANG Yaowei,YAN Wuzhu,LIANG Shujing. A novel cold expansion technology with forcemate bushing[J]. Aeronautical Manufacturing Technology,2024,67(10):107-114. [17] 黄宏,赵庆云,刘风雷,等. 孔强化对7050-T7451铝合金疲劳寿命的影响[C]//2015年全国失效分析学术会议论文集. 北京:中航工业北京航空制造工程研究所,2015:486-489. HUANG Hong,ZHAO Qingyun,LIU Fenglei,et al. Effect of strengthened hole on the fatigue life of 7050 T7451 aluminum alloy[C]//Proceedings of the 2015 National Conference on Failure Analysis. Beijing:Beijing Avic Aviation Manufacturing Engineering Research Institute,2015:486-489. [18] 卢浩,魏永合,江晓宇,等. 孔的开缝衬套冷挤压强化工艺研究[J]. 航空制造技术,2024,67(21):98-105. LU Hao,WEI Yonghe,JIANG Xiaoyu,et al. Study on cold extrusion strengthening technology of split sleeve[J]. Aeronautical Manufacturing Technology,2024,67(21):98-105. [19] 王强,赵勇,倪孟龙. 高干涉量压合衬套强化铝合金孔结构的疲劳性能[J]. 机械工程材料,2020,44(7):46-50. WANG Qiang,ZHAO Yong,NI Menglong. Fatigue properties of aluminum alloy hole structure strengthened by high interference fit bushing technique[J]. Materials for Mechanical Engineering,2020,44(7):46-50. [20] SHARIFFUDIN A K,KARUPPANAN S,PATIL S S. Finite element analysis of residual stress in cold expanded plate with different thickness and expansion ratio[J]. IOP Conference Series:Materials Science and Engineering,2017,257(1):12-17. [21] DEY M K,KIM D,TAN H. Finite element parametric study of the split sleeve cold expansion on residual stresses and pulling force[J]. Proceedings of the Institution of Mechanical Engineers,Part C:Journal of Mechanical Engineering Science,2022,236(5):2447-2461. |