| Citation: | CHEN Di, LI Yu, ZHANG Yibo, et al. Cycle-by-cycle accumulation algorithm for predicting fatigue lives of double-lap and double-lug joints[J]. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(6): 1175-1184. doi: 10.13700/j.bh.1001-5965.2018.0603(in Chinese)
|
This paper aims to investigate the failure mechanics of complex joints and evaluate the crack initiate and growth lifetimes of complex joints. Fatigue tests were respectively carried out on double-lap and double-lug joints, failure modes and mechanisms were investigated through scanning electron microscope (SEM) analysis, and fatigue lifetime for crack initiation and growth was determined from fractographic quantitatively interpreted data by using reverse inference method. From the stress severity factor method, fatigue
| [1] |
ESMAEILI F, CHAKHERLOU T N, ZEHSAZ M.Investigation of bolt clamping force on the fatigue life of double lap simple bolted and hybrid (bolted/bonded) joints via experimental and numerical analysis[J].Engineering Failure Analysis, 2014, 45(8):406-420. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=079eeb92922c4440104e72ab705930d7
|
| [2] |
ESMAEILI F, CHAKHERLOU T N.Investigation on the effect of tigthening torque on the stress distribution in double lap simple bolted and hybrid (bolted-bonded) joints[J].Journal of Solid Mechanics, 2015, 7(3):268-280.
|
| [3] |
JIMÉNEZ-PEÑA C, TALEMI R H, ROSSI B, et al.Investigations on the fretting fatigue failure mechanism of bolted joints in high strength steel subjected to different levels of pre-tension[J].Tribology International, 2016, 108(4):128-140. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=54b59d0f11731d596fe587a3487326ef
|
| [4] |
ABAZADEH B, CHAKHERLOU T N, ALDERLIESTEN R C.Effect of interference fitting and/or bolt clamping on the fatigue behavior of Al alloy 2024-T3 double shear lap joints in different cyclic load ranges[J].International Journal of Mechanical Sciences, 2013, 72(7):2-12. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=b4d12a350c6b0881f92ff6f48ef9f52c
|
| [5] |
CHAKHERLOU T N, MIRZAJANZADEH M, ABAZADEH B, et al.An investigation about interference fit effect on improving fatigue life of a holed single plate in joints[J].European Journal of Mechanics A/Solids, 2010, 29(4):675-682. doi: 10.1016/j.euromechsol.2009.12.009
|
| [6] |
CHAKHERLOU T N, MIRZAJANZADEH M, VOGWELL J.Experimental and numerical investigations into the effect of an interference fit on fatigue life of double shear lap joints[J].Engineering Failure Analysis, 2009, 16(7):2066-2080. doi: 10.1016/j.engfailanal.2009.01.009
|
| [7] |
CHAKHERLOU T N, TAGHIZADEH H, AGHDAM A B.Experimental and numerical comparison of cold expansion and interference fit methods in improving fatigue life of holed plate in double shear lap joints[J].Aerospace Science and Technology, 2013, 29(1):351-362. doi: 10.1016/j.ast.2013.04.006
|
| [8] |
GOPALAKRISHNA H D, MURTHY H N N, KRISHNA M, et al.Cold expansion of holes and resulting fatigue life enhancement and residual stresses in Al 2024 T3 alloy-An experimental study[J].Engineering Failure Analysis, 2010, 17(2):361-368. doi: 10.1016/j.engfailanal.2009.08.002
|
| [9] |
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. doi: 10.1016/S1350-6307(02)00028-6
|
| [10] |
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(7):1319-1327. doi: 10.1016/j.ijfatigue.2006.10.016
|
| [11] |
MUCHA J, WITKOWSKI W.The experimental analysis of the double joint type change effect on the joint destruction process in uniaxial shearing test[J].Thin-Walled Structures, 2013, 66(5):39-49. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=c838331ff1e113cbca3abe28877551f9
|
| [12] |
SKORUPA M, MACHNIEWICZ T, SKORUPA A, et al.Fatigue life predictions for riveted lap joints[J].International Journal of Fatigue, 2017, 94(1):41-57. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=6036f5b560aaa90c10a906dc08f35ad6
|
| [13] |
LIU J H, ZHANG R L, WEI Y B, et al.A new method for estimating fatigue life of notched specimen[J].Theoretical and Applied Fracture Mechanics, 2018, 93(1):137-143. https://www.sciencedirect.com/science/article/pii/S0167844217301155
|
| [14] |
田本鉴, 熊峻江.非对称疲劳载荷作用铆钉连接件疲劳寿命估算[J].北京航空航天大学学报, 2013, 39(12):1649-1653. http://bhxb.buaa.edu.cn/CN/abstract/abstract12806.shtml
TIAN B J, XIONG J J.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). http://bhxb.buaa.edu.cn/CN/abstract/abstract12806.shtml
|
| [15] |
张天宇, 何宇廷, 陈涛, 等.一种多钉铆接连接件的疲劳寿命分析方法[J].北京航空航天大学学报, 2018, 44(9):1933-1940. http://bhxb.buaa.edu.cn/CN/abstract/abstract14590.shtml
ZHANG T Y, HE Y T, CHEN T, et al.A fatigue life analysis method for multiple riveted joint[J].Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(9):1933-1940(in Chinese). http://bhxb.buaa.edu.cn/CN/abstract/abstract14590.shtml
|
| [16] |
HUANG W, WANG T J, GARBATOV Y, et al.DFR based fatigue reliability assessment of riveted lap joint accounting for correlations[J].International Journal of Fatigue, 2013, 47(2):106-114. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=636554b3c9834951c9441068f8443e2b
|
| [17] |
TIAN B J, XIONG J J, LIU J Z.A new approach for evaluating fatigue lives of multi-fastener mechanical joints based on a nominal stress concept and minimal datasets[J].International Journal of Fatigue, 2015, 80(11):257-265. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=0827e1f3d1da9fa10c12834d72b0db4d
|
| [18] |
DE JESUS A M P, DA SILVA A L L, CORREIA J A F O.Fatigue of riveted and bolted joints made of puddle iron-A numerical approach[J].Journal of Constructional Steel Research, 2014, 102(1):164-177. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=4ef7b4f762249493f176430d1dd757cf
|
| [19] |
SANCHES R F, DE JESUS A M P, CORREIA J A F O, et al.A probabilistic fatigue approach for riveted joints using Monte Carlo simulation[J].Journal of Constructional Steel Research, 2015, 110(7):149-162. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=fa57fbfa6fe1d9dd21ba0710585c4849
|
| [20] |
MIKKOLA E, MURAKAMI Y, MARQUIS G.Equivalent crack approach for fatigue life assessment of welded joints[J].Engineering Fracture Mechanics, 2015, 149:144-155. doi: 10.1016/j.engfracmech.2015.10.022
|
| [21] |
CORREIA J A F O, BLASÓN S, DE JESUS A M P, et al.Fatigue life prediction based on an equivalent initial flaw size approach and a new normalized fatigue crack growth model[J].Engineering Failure Analysis, 2016, 69(11):15-28. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=6d25668300cbb189ed7704c77517c230
|
| [22] |
MIKKOLA E, MURAKAMI Y, MARQUIS G.Fatigue life assessment of welded joints by the equivalent crack length method[J].Procedia Materials Science, 2014, 3:1822-1827. doi: 10.1016/j.mspro.2014.06.294
|
| [23] |
WU Y Z, XU Y W, GUO X, et al.Fatigue life prediction based on equivalent initial flaw size for Al-Li 2297 under spectrum loading[J].International Journal of Fatigue, 2017, 103(14):39-47. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=862693c62498cbd172801c0977ed80aa
|
| [24] |
张丽娜, 吴学仁, 刘建中.疲劳裂纹扩展中单峰过载引起的残余应力强度因子计算[J].机械强度, 2011, 33(3):432-437. http://d.old.wanfangdata.com.cn/Periodical/jxqd201103022
ZHANG L N, WU X R, LIU J Z.Computation of residual stress intensity factors induced by single overload during fatigue crack growth[J].Journal of Mechanical Strength, 2011, 33(3):432-437(in Chinese). http://d.old.wanfangdata.com.cn/Periodical/jxqd201103022
|
| [25] |
王延忠, 田志敏, 侯良威, 等.航空重载面齿轮三维裂纹分析与疲劳裂纹扩展寿命预测[J].北京航空航天大学学报, 2014, 40(2):148-153. http://bhxb.buaa.edu.cn/CN/abstract/abstract12839.shtml
WANG Y Z, TIAN Z M, HOU L W, et al.Three-dimensional crack analysis and fatigue life prediction of aero heavy-load face gear[J].Journal of Beijing University of Aeronautics and Astronautics, 2014, 40(2):148-153(in Chinese). http://bhxb.buaa.edu.cn/CN/abstract/abstract12839.shtml
|
| [26] |
KUMAR S A, BHATTACHARYA A, BABU N C M.Fatigue crack growth life prediction around cold expanded hole using finite element method[J].Procedia Materials Science, 2014, 5:316-325. doi: 10.1016/j.mspro.2014.07.273
|
| [27] |
BERGARA A, DORADO J I, MEIZOSO A M, et al.Fatigue crack propagation in complex stress fields:Experimental and numerical simulations using the extended finite element method (XFEM)[J].International Journal of Fatigue, 2017, 103(14):112-121. https://www.sciencedirect.com/science/article/pii/S0142112317302396
|
| [28] |
NASRI K, ZENASNI M.Fatigue crack growth simulation in coated materials using X-FEM[J].Comptes Rendus Mecanique, 2017, 345(4):271-280. doi: 10.1016/j.crme.2017.02.005
|
| [29] |
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.
XIONG J J.Fatigue life design for aircraft structure[M].Beijing:Beihang University Press, 2004.
|
| [30] |
赵少汴.抗疲劳设计手册[M].北京:机械工业出版社, 2015.
ZHAO S B.Fatigue design manual[M].Beijing:China Machine Press, 2015.
|
| [31] |
FU Y, XIONG J J, SHENOI R A.Practical models for characterizing corrosion fatigue behaviours of metallic materials and for evaluating calendar lives of aircraft structural components[J].Proceedings of Institution of Mechanical Engineers Part C-Journal of Mechanical Engineering Science, 2017, 231:207-222. doi: 10.1177/0954406216637633
|
| [32] |
HERTZBERG R W.Deformation and fracture mechanics of engineering materials[M].Hoboken:Wiley Jones and Sons, 1996.
|
| [33] |
CHANG J, XU J Q, MUTOH Y.A general mixed-mode brittle fracture criterion for cracked materials[J].Engineering Fracture Mechanics, 2006, 73(9):1249-1263. doi: 10.1016/j.engfracmech.2005.12.011
|
| [34] |
AYGVL M, AL-EMRANI M, BARSOUM Z, et al.An investigation of distortion-induced fatigue cracking under variable amplitude loading using 3D crack propagation analysis[J].Engineering Failure Analysis, 2014, 45(10):151-163. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=e15305d471171c34b8c6e07b1523e0ac
|
| [35] |
Federal Aviation Administration.Metallic materials properties development and standardization[M].Columbia:U.S.Department of Transportation, 2006:3-94.
|
| [36] |
ASTM.Standard practice for: Presentation of constant amplitude fatigue test results for metallic materials: ASTM E468-90[S].West Conshohocken: ASTM International, 2004: 1-6.
|
| [37] |
刘新灵, 张铮, 陶春虎.疲劳断口定量分析[M].北京: 国防工业出版社, 2010.
LIU X L, ZHANG Z, TAO C H.Fatigue fractography quantitative analysis[J].Beijing: National Defense Industry Press, 2010(in Chinese).
|
| [38] |
郑晓玲, 刘文珽, 李令芳, 等.民机结构耐久性与损伤容限设计手册[M].北京:航空工业出版社, 2003.
ZHENG X L, LIU W T, LI L F, et al.Design manual for durability and damage tolerance of civil aircraft structures[M].Beijing:Aviation Industry Press, 2003(in Chinese).
|
Figures(10) / Tables(4)
Copyright © Journal of Beijing University of Aeronautics and Astronautics
Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn
Supported by:
Beijing Renhe Information Technology Co., Ltd.
DownLoad:
