Citation: | Tian Benjian, Xiong Junjiang. Fatigue life estimation of riveted joints subjected to asymmetrical loading[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(12): 1649-1653. (in Chinese) |
[1] |
Urban M R.Analysis of the fatigue life of riveted sheet metal helicopter airframe joints[J].International Journal of Fatigue, 2003(25):1013-1026
|
[2] |
Lehonff T F, Bunyard B A.Effect of bolt threads on the stiffness of bolted joints[J].Journal of Pressure Bessel Technology, 1998(381):141-146
|
[3] |
Lehonff T F, Bunyard B A.Effect of bolt threads on the stiffness of bolted joints[J].Journal of Pressure Bessel Technology, 1998(381):141-146
|
[4] |
蒋持平, 张行.多钉连接件钉传载荷计算的一个解析方法[J].航空学报, 1994, 15(3):310-317 Jiang Chiping, Zhang Xing.An analytical method of pin load computations for joints with multi-fasteners[J].Acta Aeronautica et Astronautica Sinica, 1994, 15(3):310-317 (in Chinese)
|
[5] |
Kelly B, Costello C.FEA modeling of setting and mechanical testing of aluminum blind rivets[J].Materials Processing Technology, 2004(153/154):74-79
|
[6] |
Oskouei R H, Keikhosravy M, Soutis C.Estimating clamping pressure distribution and stiffness in aircraft bolted joints by finite-element analysis[J].Proceeding of the Institution of Mechanical Engineers Part G-Journal of Aerospace Engineering, 2009(223):863-871
|
[7] |
Oskouei R H.A finite element stress analysis of aircraft bolted joints loaded in tension[J].Aeronautical Journal, 2010(114):315-320
|
[8] |
Blanchot V, Daidie A.Riveted assembly modeling:study and numerical characterization of a riveting Process[J].Materials Proeessing Teehnology, 2006(180):201-209
|
[9] |
谢卫东, 吴富民, 肖寿庭.干涉配合连接件应力应变分析及疲劳寿命估算[J].航空学报, 1988(9):58-64 Xie Weidong, Wu Fumin, Xiao Shouting.Stress-strain analysis and fatigue life prediction of interference joints[J].Acta Aeronautica et Astronautica Sinica, 1988(9):58-64 (in Chinese)
|
[10] |
刘道新, 何家文.微动疲劳影响因素及钛合金微动疲劳行为[J].航空学报, 2001, 21(2):454-457 Liu Daoxin, He Jiawen.Review of factors that influence fretting fatigue (FF) and investigation on FF behavior of Ti-alloy[J].Acta Aeronautica et Astronautica Sinica, 2001, 21(2):454-457 (in Chinese)
|
[11] |
Ralph W C, Johnson W S, Makeev A, et al.Fatigue performance of production quality aircraft fastener holes[J].International Journal of Fatigue, 2007(29):1319-1327
|
[12] |
陈福玉, 朱如鹏, 蒋红宇, 等.孔径对铆接连接件疲劳寿命影响的试验[J].机械设计与研究, 2011(2):98-101 Chen Fuyu, Zhu Rupeng, Jiang Hongyu, et al.Test study of hole diameter on fatigue life of riveting[J].Machine Design and Research, 2011(2):98-101 (in Chinese)
|
[13] |
Finney J M, Evans R L.Extending the fatigue life of multi-layer metal joints[J].Fatigue and Fracture of Engineering Materials and Structures, 1995, 18(11):1231-1247
|
[14] |
Park C Y, Grandt Jr A F.A proposed fatigue test proto-col for generic mechanical joints[J].Engineering Failure Analysis, 2006(13):136-154
|
[15] |
Park C Y, Grandt Jr A F.Effect of load transfer on the cracking behavior at a countersunk fastener hole[J].International Journal of Fatigue, 2007(29):146-157
|
[16] |
Liu Y S, He X D, Shao X J, et al.Analytical and experimental investigation of fatigue and fracture behaviors for anti-double dog-bone riveted joints[J].Engineering Failure Analysis, 2010(17):1447-1456
|
[17] |
Lanciotti A, Lazzeri L.Fatigue resistance and residual strength of riveted joints in FML[J].Fatigue and Fracture of Engineering Materials and Structures, 2009, 32(10):837-846
|
[18] |
熊峻江.飞行器结构疲劳与寿命设计[M].北京:北京航空航天大学出版社, 2004:93-96 Xiong Junjiang.Fatigue life design for aircraft structure[M].Beijing:Beijing University of Aeronautics and Astronautics Press, 2004:93-96 (in Chinese)
|
[19] |
Federal Aviation Administration.Metallic materials properties development and standardization[M].Washington DC:Hughes Technical Center, 2006
|
[20] |
飞机结构强度研究所.航空结构连接件疲劳分析手册[M].西安:飞机结构强度所, 1985:51-52 Aircraft Structure Strength Research Institute.Aviation structural joints fatigue analysis manual[M].Xian:Aircraft Structure Strength Research Institute, 1985:51-52 (in Chinese)
|
[21] |
李令芳.民机结构耐久性与损伤容限设计手册(上册)[M].北京:航空工业出版社, 2003 Li Lingfang.Civil aircraft structure durability and damage tolerance design manual(Volume 1)[M].Beijing:Aviation Industry Press, 2003
|