| [1] 徐灏.疲劳强度[M].北京,机械工业出版社,1981.XU H. Fatigue strength[M].Beijing,China Machine Press,1981. (in Chinese).[2] LIU J, YUE Z F, LIU Y S. Surface finish of open holes on fatigue life[J]. Theor Appl Fract Mech, 2007, 47: 35-45.[3] 孙暄,王珉,许洪昌等.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, XU H C, et al. Split sleeve hole cold expansion technique [J]. Manufacture Process, 1998, (1): 22-24. (in Chinese).[4] 王眠.抗疲劳制造原理与技术[M].南京,江苏科学技术出版社,1999年第1版, 297-303.WANG M. Anti-fatigue manufacture principle and technology[M]. Nanjing, Jiangsu Science & Technology Press, 1st, 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] 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).[7] 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).[8] 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 Aeronaut Astronaut Sin, 2013, 34(4): 936-45.[9] LIU J, XU H L. Effect of detail design on fatigue performance of fastener hole [J]. Materials and Design, 2010, (31): 976-980.[10] 钱晓明,姜银方,管海兵等.飞机结构件禁锢孔强化技术综述[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).[11] 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).[12] 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.[13] 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): 949-954.[14] 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.[15] 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): 11-23.[16] 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.[17] 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.[18] 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, (92–93): 424–428.[19] ?DEMIR 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): 1243-1252.[20] ?DEMIR 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): 129-135.[21] 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,(11):85-88.XUE W. Split sleeve hole cold expansion process[J]. China High-Tech Enterprises, 2011, (11): 85-88. (in Chinese).[22] 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.[23] 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(7): 91-97.[24] BERNARD M, BUI Q T, BURLAT M. Effect of re-cold working on fatigue life enhancement of a fastener hole[J]. Engineering Fracture Mechanics, 1995(18): 765-775.[25] STEFANESCU D. Experimental study of double cold expansion of holes[J]. Journal of Strain Analysis, 2003(38): 339-347.[26] ChAKHERLOU T N, VOGWELL J. A novel method of cold expansion which creates near-uniform compressive tangential residual stress around a fastener hole[J]. Fatigue Fracture Engineering & Material Structure, 2004(27): 343-351.[27] 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): 1504-1511.[28] JANG J S, KIM D, ChO M R. The effect of cold expansion on the fatigue life of the chamfered holes[J]. ASME Journal of Engineering Material and Technology, 2008(130): 10141-10147.[29] 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):45-57.[30] GIGLIO M, LODI M. Optimization of a cold working process for increasing fatigue life[J]. International Journal of Fatigue, 2009(31):1978-1995.[31] 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.[32] 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).[33] 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).[34] 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 iniation 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).[35] 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).[36] 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).[37] 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): 290-296.[38] 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.[39] 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).[40] 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).[41] FARHANGDOOST K. The effect of mandrel speed upon the residual stress distribution around cold expanded hole[J]. Procedia Engineering, 2011(10): 2184-2189.[42] 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).[43] West Coast Industries. Engineering Handout WCI-EH-9201-4.1 Split Sleeve Coldworking Holes (Aluminum, Steel & Titanium) [M]. Whitman Ave. Seattle, Washington, 2012.[44] 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).[45] KIM C, KIMB 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(153–154): 986–991.[46] 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).[47] 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): 189-203.[48] 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).[49] 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]. Australian Government Department of Defence, Defence Sicence and Technology Organisation, 2008.[50] 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): 997-1004.[51] 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): 800-810.[52] 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).[53] 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]. In 1992 USAF Aircraft Structural Integrity Program Conference, San Antonio, Texas, 1~3 December 1992.[54] BEMARD M, BAI Q T, BURLAT M. Effect of re-coldworking on fatigue life enhancement of a fastener hole[J]. Fatigue Fract. Engng. Mater. Struct., 1995,1897/80:765-775.[55] LEN R. Split sleeve cold expansion as a rework process for previously cold expanded holes[C]. ICAF 93, International Committee on Aeronautical Fatigue, Stockholm, Sweden, June, 1993.[56] PELL R A, BEAVER F W, MANN J Y, et al. Fatigue of thick section cold expanded holes with and without cracks[J]. Fatigue Fract. Engng. Mater. Struct., 1989,12:553-567.[57] REID L. Airframe life extension through cold expansion techniques[C]. International Conference on Aircraft Damage Assessment and Repair, Melboume 26-28, August, 1991. |
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