Volume 39 Issue 12
Dec.  2013
Turn off MathJax
Article Contents
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)
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)

Fatigue life estimation of riveted joints subjected to asymmetrical loading

  • Received Date: 09 Jan 2013
  • Publish Date: 30 Dec 2013
  • Based on the identity assumption of transfer loads of the rivets, novel simplified formulas were derived to predict transfer and bypass stresses of riveted joints subjected to complicated asymmetrical stresses, and the formula was then deduced to calculate stress severity factor (SSF) of rivet holes. Finally, new SSF formulas were applied to predict fatigue life of riveted joints subjected to a given asymmetrical stress spectrum and the calculated results were compared with those by using the detail fatigue rating (DFR) method, demonstrating the practical and effective use of the proposed simplified approach. It is shown that good correlation is achieved between the results predicted by resorting to novel simplified approach presented and in accordance with the DFR method, but the calculated result from simplified approach is more conservative than that of the DFR method.

     

  • loading
  • [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
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views(1315) PDF downloads(506) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return