[1] HB/Z 170-2005. 航空金属零件孔挤压强化工艺[S]. 北京:中国航空综合技术研究所, 2005. HB/Z 170-2005. Cold expansion process for hole of aircraft metal part[S]. Beijing:China Aero-poly technology Establishment, 2005.
[2] WU H. On the prediction of initiation life for fatigue crack emanating from small cold expanded holes[J]. Journal of Materials Processing Technology, 2012, 212(9):1819-1824.
[3] LARUE J E, DANIEWICZ S R. Predicting the effect of residual stress on fatigue crack growth[J]. International Journal of Fatigue, 2007, 29(3):508-515.
[4] CHAKHERLOU T N, VOGWELL J. The effect of cold expansion on improving the fatigue life of fastener hole[J]. Engineering Failure Analysis, 2003, 10(1):13-24.
[5] NIGRELLI V, PASTA S. Finite-element simulation of residual stress induced by split-sleeve cold-expansion process of holes[J]. Journal of Materials Processing Technology, 2008, 205(1/3):290-296.
[6] HOUGHTON S J, CAMPBELL S K. Identifying the residual stress field developed by hole cold expansion using finite element analysis[J]. Fatigue & Fracture of Engineering Materials & Structures,2012, 35(1):74-83.
[7] 何志明,张晓晶,刘天琦,等.300M钢耳片孔挤压强化全过程有限元模拟[J].浙江大学学报:工学版,2016,50(4):783-791. HE Zhi-ming,ZHANG Xiao-jing,LIU Tian-qi,et al. Numerical simulation of the whole process of cold expansion in 300M steel lug[J]. Journal of Zhejiang University:Engineering Science, 2016, 50(4):783-791.
[8] 刘晓龙,高玉魁,刘蕴韬,等.孔挤压强化残余应力场的三维有限元模拟和试验研究[J].航空材料学报,2011,31(2):24-27. LIU Xiao-long, GAO Yu-kui, LIU Yun-tao, et al. 3D finite element simulation and experimental test on residual stress field by hole cold expansion[J]. Journal of Aeronautical Materials, 2011,31(2):24-27.
[9] 赵艳丽,高玉魁,仲政.30CrMnSiNi2A超高强度钢孔挤压强化残余应力场的模拟[J].力学季刊,2014(2):243-252. ZHAO Yan-li,GAO Yu-kui,ZHONG Zheng. Finite element simulation of the residual stress fields of 30CRMNSINI2A ultrahigh strength steel by hole cold expansion[J].Chinese Quarterly of Mechanics,2014(2):243-252.
[10] 葛恩德,苏宏华,程远庆,等.TC4板孔冷挤压强化残余应力分布与疲劳寿命[J].中国机械工程,2015,26(7):971-976. GUO En-de,SU Hong-hua,CHEN Yuan-qing, et al. Residual stress fields and fatigue life of cold expansion hole in Titanium alloy TC4[J].China Mechanical Engineering,2015,26(7):971-976.
[11] 卢国鑫,王强,宋颖刚,等.芯棒规格对孔挤压强化效果的影响[J].制造业自动化,2014(17):34-38+48. LU Guo-xin, WANG Qiang, SONG Yi-gang, et al. Hole extrusion strengthening effect caused by mandrel specifications[J]. Journal of Manufacturing Automation,2014(17):34-38+48.
[12] MAHENDRA BABU N C, JAGADISH T, RAMACHANDRA K, et al. A simplified 3-D finite element simulation of cold expansion of a circular hole to capture through thickness variation of residual stresses[J]. Engineering Failure Analysis, 2008, 15(4):339-348.
[13] LIU Y S, SHAO X J, LIU J, et al. Finite element method and experimental investigation on the residual stress fields and fatigue performance of cold expansion hole[J]. Materials and Design, 2010, 31(3):1208-1215.
[14] 欧阳小穗,张晓晶,杨树勋.孔挤压强化有限元分析及疲劳寿命估算[J].科学技术与工程,2011,11(12):2787-2790. OUYANG Xiao-sui, ZHANG Xiao-jing, YANG Shu-xun. Finite element analysis and fatigue life prediction of cold expansion[J]. Science Technology and Engineering, 2011, 11(12):2787-2790.
[15] ISMONOV S, DANIEWICZ S R, NEWMAN J C, et al. Three dimensional finite element analysis of a split-sleeve cold expansion process. Journal of Engineering Materials and Technology, 2009,131(3):031007-1-031007-8.
[16] CHAKHERLOU T N, VOGWELL J. The effect of cold expansion on improving the fatigue life of fastener holes. Engineering failure analysis. 2003, 10(1):13-24.
[17] 张成成,姚卫星.典型缺口件疲劳寿命分析方法[J].航空动力学报,2013,28(6):1223-1230. ZHANG Cheng-cheng,YAO Wei-xing.Typical fatigue life analysis approaches for notched components[J].Journal of Aerospace Power, 2013,28(6):1223-1230.
[18] TAYLOR D. Geometrical effects in fatigue:a unifying theoretical model[J].International Journal of Fatigue,1999,21(5):413-420. |