[1] 徐灏. 疲劳强度[M]. 北京:机械工业出版社, 1981:3-7. XU H. Fatigue strength[M]. Beijing:China Machine Press, 1981:3-7(in Chinese).[2] LIU J, YUE Z F, LIU Y S. Surface finish of open holes on fatigue life[J]. Theoretical and Applied Fracture Mechanics, 2007, 47(1):35-45.[3] 孙暄, 王珉. 孔的开缝衬套冷挤压强化技术[J]. 制造工艺, 1998(1):22-24. SUN X, WANG M. Split sleeve hole cold expansion technique[J]. Manufacture Process, 1998(1):22-24(in Chinese).[4] 王珉. 抗疲劳制造原理与技术[M]. 南京:江苏科学技术出版社, 1999:297-303. WANG M. Anti-fatigue manufacture principle and technology[M]. Nanjing:Jiangsu Science & Technology Press, 1999:297-303(in Chinese).[5] 张波. 内孔高频淬火工艺研究[J]. 热加工工艺, 2010, 39(14):181-182. ZHANG B. Study on high frequency quenching of inter-bore[J]. Hot Working Technology, 2010, 39(14):181-182(in Chinese).[6] 姜杰凤, 董辉跃, 毕运波. 高锁螺栓干涉配合安装工艺参数对凸瘤的影响分析[J]. 航空学报, 2013, 34(4):936-945. JIANG J F, DONG H Y, BI Y B. Analysis of process parameters influencing protuberance during interference fit installation of hi-lock bolts[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(4):936-945(in Chinese).[7] LIU J, XU H L, ZHAI H B, et al. Effect of detail design on fatigue performance of fastener hole[J]. Materials & Design, 2010, 31(2):976-980.[8] 王海荣, 张兴权, 张标, 等. 深小孔强化技术的研究[J]. 机械设计与制造, 2012(8):118-120. WANG H R, ZHANG X Q, ZHANG B, et al. Research of strengthening technologies on deep hole[J]. Machinery Design & Manufacture, 2012(8):118-120(in Chinese).[9] 毕凤琴, 张春成, 李红翠, 等. 激光冲击强化技术的发展及应用[J]. 兵器材料科学与工程, 2010, 33(1):101-104. BI F Q, ZHANG C C, LI H C, et al. Development and application of laser shock processing[J]. Ordnance Material Science and Engineering, 2010, 33(1):101-104(in Chinese).[10] 李伟, 李应红, 何卫锋, 等. 激光冲击强化技术的发展和应用[J]. 激光与光学电子学进展, 2008, 45(12):15-19. LI W, LI Y H, HE W F, et al. Development and application of laser shock processing[J]. Laser & Optoelect ronics Process, 2008, 45(12):15-19(in Chinese).[11] ZHANG X Q, CHEN L S, YU X L, et al. Effect of laser shock processing on fatigue life of fastener hole[J]. Transactions of Nonferrous Metals Society of China, 2014, 24(4):969-974.[12] 张宏, 余承业, 吴鸿兴, 等. 小孔激光冲击表面强化技术研究[J]. 兵工学报, 2001, 22(3):330-333. ZHANG H, YU C Y, WU H X, et al. Laser shock processing of small hole[J]. Acta Armamentarii, 2001, 22(3):330-333(in Chinese).[13] 姜银方, 李娟, 潘禹, 等. 双面激光冲击次序对小孔件强化效果影响研究[J]. 激光技术, 2016, 40(1):82-85. JANG Y F, LI J, PAN Y, et al. Investigation of effect of two-side laser shock order on small hole specimen strengthening[J]. Laser Technology, 2016, 40(1):82-85(in Chinese).[14] MONTROSS C S, WEI T, YE L, et al. Laser shock processing and its effect on microstructure and properties of metal alloy:A review[J]. International Journal of Fatigue, 2002, 24(10):1021-1036.[15] IVETIC G, MENEGHIN E, TROIANI E, et al. Characterization of fatigue and crack propagation in laser shock peened open hole 7075-T3 aluminium specimens[C]//ICAF 2011 Structural Integrity:Influence of Efficiency and Green Imperatives:Proceedings of the 26th Symposium of the International Committee on Aeronautical Fatigue. Montreal:International Committee on Aeronautical Fatigue, 2011:855-866.[16] IVETIC G, MENEGHIN E, TROIANI E, et al. Fatigue in laser shock peened open hole thin aluminium specimens[J]. Materials Science and Engineering:A, 2012, 534:573-579.[17] 张永康. 激光冲击强化产业化关键问题和应用前景[J]. 激光与光学电子学进展, 2007, 44(3):74-77. ZHANG Y K. Key problems and application prospect of industrialization of laser shock processing[J]. Laser & Optoelectronics Process, 2007, 44(3):74-77(in Chinese).[18] REID L. Attaining fatigue and damage tolerance life goals in helicopter bushed assemblies[C]//Annual Forum Proceedings-American Helicopter Society. American Helicopter Society, INC, 2000, 56(2):1015-1020.[19] RANSOM J, RESTIS J, WEISS M. F-16 fighting falcon upper fuselage skin fatigue life enhancement[C]//Proceedings of USAF ASIP Conference. 1999:1-8.[20] CHAKHERLOU T N, VOGWELL J. The effect of cold expansion on improving the fatigue life of fastener holes[J]. Engineering Failure Analysis, 2003, 10(1):13-24.[21] 钱晓明, 姜银方, 管海兵, 等. 飞机结构件紧锢孔强化技术综述[J]. 机械强度, 2011, 33(5):749-753. QIAN X M, JIANG Y F, GUAN H B, et al. Research and application of strengthening technology for fastening holes of aircraft structures[J]. Journal of Mechanical Strength, 2011, 33(5):749-753(in Chinese).[22] 龚澎, 郑林斌, 张坤, 等. 7B50-T7451铝合金板材孔挤压工艺性能研究[J]. 航空材料学报, 2011, 31(4):45-50. GONG P, ZHENG L B, ZHANG K, et al. Effects of hole cold-expansion on microstructure and fatigue property of 7B50-T7451 aluminum alloy plate[J]. Journal of Aeronautical Materials, 2011, 31(4):45-50(in Chinese).[23] SU M, AMROUCHE A, MESMACQUE G, et al. Numerical study of double cold expansion of the hole at crack tip and the influence on the residual stresses field[J]. Computer Material Science, 2008, 41(3):350-355.[24] AMROUCHE A, MESMACQUE G, GARCIA S, et al. Cold expansion effect on the initiation and the propagation of the fatigue crack[J]. International Journal of Fatigue, 2003, 25(9):949-954.[25] CATHEY W H, GRANDT A F. Fracture mechanics consideration of residual stresses introduced by cold working fastener holes[J]. Journal of Engineering Materials and Technology, 1980, 102(1):85-91.[26] GIZIN M H, KHAFRI M A. Cold work simulation of hole expansion process and its effect on crack closure[J]. Iranian Journal of Materials Forming, 2014, 1(1):11-23.[27] BALL D L, LOWRY D R. Experimental investigation on the effect of cold expansion of fastener holes[J]. Fatigue & Fracture of Engineering Materials & Structure, 1998, 21(1):17-35.[28] WANG Y L, ZHU Y L, HOU S, et al. Investigation on fatigue performance of cold expansion holes of 6061-T6 aluminum alloy[J]. International Journal of Fatigue, 2017, 95:216-228.[29] PAPANIKOS P, MEGUID S A. Elasto-plastic finite element analysis of the cold expansion of adjacent fastener holes[J]. Journal of Materials Processing Technology, 1999, 92:424-428.[30] ÖDEMIR A T, HERMANN R. Effect of expansion technique and plate thickness on near hole residual stresses and fatigue life of cold expanded holes[J]. Journal of Material Science, 1999, 34(6):1243-1252.[31] ÖDEMIR A T, EDWARDS L. Through thickness residual stress distribution after the cold expansion of fastener holes and its effect on fracturing[J]. ASME Journal of Engineering Materials Technology, 2004, 126(1):129-135.[32] 薛巍. 带开缝衬套的冷扩孔挤压工艺[J]. 中国高新技术企业, 2011(34):85-88. XUE W. Split sleeve hole cold expansion process[J]. China High-Tech Enterprises, 2011(34):85-88(in Chinese).[33] PRIEST M, POUSSARD C G, PAVIER M J, et al. An assessment of residual stress measurements around cold worked holes[J]. Experimental Mechanics, 1995, 35(4):361-366.[34] STEFANESCU D, SANTISTEBAN J R, EDWARDS L, et al. Residual stress measurement and fatigue crack growth prediction after cold expansion of cracked fastener holes[J]. Journal of Aerospace Engineering, 2004, 17(3):91-97.[35] BERNARD M, BUI Q T, BURLAT M. Effect of re-cold working on fatigue life enhancement of a fastener hole[J]. Fatigue & Fracture of Engineering Materials & Structures, 1995, 18(7):765-775.[36] STEFANESCU D. Experimental study of double cold expansion of holes[J]. The Journal of Strain Analysis for Engineering Design, 2003, 38(4):339-347.[37] CHAKHERLOU T N, VOGWELL J. A novel method of cold expansion which s near-uniform compressive tangential residual stress around a fastener hole[J]. Fatigue & Fracture of Engineering Materials & Structures, 2004, 27(5):343-351.[38] CHAKHERLOU T N, AGHDAM A B. An experimental investigation on the effect of short time exposure to elevated temperature on fatigue life of cold expanded fastener holes[J]. Materials & Design, 2008, 29(8):1504-1511.[39] JANG J S, KIM D, CHO M R. The effect of cold expansion on the fatigue life of the chamfered holes[J]. Journal of Engineering Materials and Technology, 2008, 130(3):031014.[40] KARABIN M E, BARLAT F, SCHULTZ R W. Numerical and experimental study of the cold expansion process in 7085 plate using a modified split sleeve[J]. Journal of Materials Processing Technology, 2007, 189(1):45-57.[41] GIGLIO M, LODI M. Optimization of a cold working process for increasing fatigue life[J]. International Journal of Fatigue, 2009, 31(11):1978-1995.[42] MAXIMOV J T, DUNCHEVA G V, AMUDJEV I M. A novel method and tool which enhance the fatigue life of structural components with fastener holes[J]. Engineering Failure Analysis, 2013, 31:132-143.[43] 张坤, 龚鹏, 宋德玉, 等. 孔挤压强化对超高强7055-T7751厚板组织性能的影响[J]. 航空材料学报, 2010, 30(5):44-48. ZHANG K, GONG P, SONG D Y, et al. Effects of cold hole-expansion on microstructure and fatigue property of 7055-T7751 aluminum alloy plate[J]. Journal of Aeronautical Materials, 2010, 30(5):44-48(in Chinese).[44] 华文君, 赵振业, 丁传富. 300M钢孔挤压强化疲劳断口扫描电镜观察与分析[J]. 材料工程, 1994(1):31-34. HUA W J, ZHAO Z Y, DING C F. SEM study on fatigue fracture of 300M steel after holes coining strengthening[J]. Journal of Materials Engineering, 1994(1):31-34(in Chinese).[45] 丁传富, 赵振业, 宋德玉. 孔挤压强化对两种超高强度钢疲劳裂纹起始与扩展寿命的影响[J]. 航空学报, 1994, 15(8):960-967. DING C F, ZHAO Z Y, SONG D Y. Effect of cold worked holes on the initiation life and propagation life of fatigue cracks in two ultra-high strength steels[J]. Acta Aeronautica et Astronautica Sinica, 1994, 15(8):960-967(in Chinese).[46] 杨洪源, 刘文珽. 孔挤压强化疲劳增寿效益的试验研究[J]. 机械强度, 2010, 32(3):446-450. YANG H Y, LIU W T. Test research on fatigue life enhancing effect of cold expanding hole[J]. Journal of Mechanical Strength, 2010, 32(3):446-450(in Chinese).[47] 王强, 陈雪梅, 张文光, 等. A-100钢开缝衬套孔挤压强化残余应力场[J]. 中国表面工程, 2011, 24(5):64-67. WANG Q, CHEN X M, ZHANG W G, et al. Residual stress induced by cold expansion with sleeve process of A-100 steel[J]. China Surface Engineering, 2011, 24(5):64-67(in Chinese).[48] 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):290-296.[49] FU Y C, GE E D, SU H H, et al. Cold expansion technology of connection holes in aircraft structures:A review and prospect[J]. Chinese Journal of Aeronautics, 2015, 28(4):961-973.[50] 朱有利, 侯帅, 王燕礼, 等. 芯棒锥面结构对孔冷挤压强化残余应力场的影响[J]. 材料科学与工艺, 2015, 23(4):87-92. ZHU Y L, HOU S, WANG Y L, et al. Effects of cone surface profile of mandrel on residual stress distribution of cold expansion strengthening of hole[J]. Materials Science and Technology, 2015, 23(4):87-92(in Chinese).[51] 侯帅, 朱有利, 王燕礼, 等. 孔边倒角对直接芯棒孔冷挤压残余应力场的影响[J]. 兵器材料科学与工程, 2015, 38(3):89-92. HOU S, ZHU Y L, WANG Y L, et al. Effect of chamfering on residual stress distribution of directly cold expanded mandrel hole[J]. Ordnance Material Science and Engineering, 2015, 38(3):89-92(in Chinese).[52] FARHANGDOOST K. The effect of mandrel speed upon the residual stress distribution around cold expanded hole[J]. Procedia Engineering, 2011, 10:2184-2189.[53] 张飞, 何宇廷, 张腾, 等. 支撑板孔径对7A04-T6铝合金板冷挤压后孔周环向残余应力分布的影响[J]. 机械工程材料, 2015, 39(9):89-93. ZHANG F, HE Y T, ZHANG T, et al. Effect of backing plate hole diameter on residual stress distribution around 7A04-T6 aluminum alloy hole after cold expansion[J]. Materials for Mechanical Engineering, 2015, 39(9):89-93(in Chinese).[54] West Coast Industries. Engineering handout WCI-EH-9201-4.1 split sleeve coldworking holes (aluminum, steel & titanium)[M]. 2012:8-9.[55] 杜洪增, 田秀云. 飞机结构修理部位的可检测性与耐久性[J]. 中国民航学院学报, 1997, 15(6):1-8. DU H Z, TIAN X Y. The detectability & durability of the repaired aircraft structures[J]. Journal of Civil Aviation University of China, 1997, 15(6):1-8(in Chinese).[56] KIM C, KIM D J, SEOK C S, et al. Finite element analysis of the residual stress by cold expansion method under the influence of adjacent holes[J]. Journal of Materials Processing Technology, 2004, 153:986-991.[57] 丁传富, 李谦. 腐蚀环境和孔挤压强化对300M超高强度钢疲劳性能的影响[J]. 材料工程, 1997(5):15-19. DING C F, LI Q. Influence of corrosion environment and cold worked holes on fatigue properties of 300M ultra-high strength steel[J]. Journal of Material Engineering, 1997(5):15-19(in Chinese).[58] LACARAC V D, SMITH D J, PAVIER M J. Fatigue crack growth from plain and cold expanded holes in aluminum alloys[J]. International Journal of Fatigue, 2000, 22(3):189-203.[59] 刘一兵, 邢文珍. 循环应力作用下紧固孔冷胀强化残余应力的衰减响应分析[J]. 航空学报, 1997, 18(3):272-276. LIU Y B, XING W Z. Analysis of attenuation response for the residual stress of cold expanded strengthening of tight hole under applied cyclic stress[J]. Acta Aeronautica et Astronautica Sinica, 1997, 18(3):272-276(in Chinese).[60] CLARK D A, JOHNSON WS. Temperature effects on fatigue performance of cold expanded holes in 7050-T7451 aluminum alloy[J]. International Journal of Fatigue, 2003,25(2):159-165.[61] LIU Q, BABURAMANI P, LOADER C. Effect of high temperature exposure on the mechanical properties of cold expanded open holes in 7050-T7451 aluminum alloy[R]. Sydney:Australian Government Department of Defence, Defence Science and Technology Organisation, 2008.[62] MÍNGUEZ J M, VOGWELL J. Fatigue life of an aerospace aluminum alloy subjected to cold expansion and a cyclic temperature regime[J]. Engineering Failure Analysis, 2006, 13(6):997-1004.[63] CHAKHERLOU T N, TABRIZI Y A, KIANI A. On the fatigue behavior of cold expanded fastener holes subjected to bolt tightening[J]. International Journal of Fatigue, 2011, 33(6):800-810.[64] 王智, 李京珊. 影响冷挤压强化效果的因素[J]. 机械强度, 2002, 24(2):302-304. WANG Z, LI J S. Factors of influencing the beneficial effect of cold expansion[J]. Journal of Mechanical Strength, 2002, 24(2):302-304(in Chinese).[65] WANGER R V, REID L, EASTERBROOK E T, et al. Beneficial effects of split sleeve cold expansion on the fatigue lives of pre-cycled cold expanded structure[C]//USAF Aircraft Structural Integrity Program Conference, 1992.[66] BEMARD M, BAI Q T, BURLAT M. Effect of re-coldworking on fatigue life enhancement of a fastener hole[J]. Fatigue & Fracture of Engineering Materials & Structures, 1995, 18(7):765-775.[67] LEN R. Split sleeve cold expansion as a rework process for previously cold expanded holes[C]//International Committee on Aeronautical Fatigue, 1993.[68] PELL R A, BEAVER F W, MANN J Y, et al. Fatigue of thick section cold expanded holes with and without cracks[J]. Fatigue & Fracture of Engineering Materials & Structures, 1989, 12(6):553-567.[69] REID L. Airframe life extension through cold expansion techniques[C]//International Conference on Aircraft Damage Assessment and Repair. Barton, ACT:Institution of Engineers, 1991:109-114.
CJA