Volume 40 Issue 3
Mar.  2025
Turn off MathJax
Article Contents
LIU Xiaogang, WEI Hao, ZHANG Sheng, et al. Fatigue life prediction method of tensile and shear load of welded joints[J]. Journal of Aerospace Power, 2025, 40(3):20230441 doi: 10.13224/j.cnki.jasp.20230441
Citation: LIU Xiaogang, WEI Hao, ZHANG Sheng, et al. Fatigue life prediction method of tensile and shear load of welded joints[J]. Journal of Aerospace Power, 2025, 40(3):20230441 doi: 10.13224/j.cnki.jasp.20230441

Fatigue life prediction method of tensile and shear load of welded joints

doi: 10.13224/j.cnki.jasp.20230441
  • Received Date: 2023-07-07
    Available Online: 2024-05-20
  • In order to establish a life prediction method for welded joints under multiaxial tensile and shear stress conditions, a butterfly shaped test piece of GH4169 electron beam welded joints was designed and fatigue tests were conducted at different loading angles (0°, 15 °, 30°, and 45°) to obtain F-N curves respectively. The influences of different shear/tensile stress ratios γ on the fatigue performance of welded joints were explored. The critical distance method was applied to determine the characteristic size of the notch root of the welded pieces, and the effective stress parameters on the weld plane were obtained. Furthermore, relevant correction coefficients $ k(\gamma ) $ were introduced to modify the material parameters in the Findley model, and a unified multiaxial fatigue life prediction model suitable for different loading angles was established. By comparing with test results, it was verified that the proposed model had high prediction accuracy, with an error within ±2 times dispersion band.

     

  • loading
  • [1]
    LI Ming,ZHU Zheng. Features and application of electron beam welding technology[J]. Advanced Materials Research,2015,1120/1121: 1308-1312. doi: 10.4028/www.scientific.net/AMR.1120-1121.1308
    [2]
    康文军,梁养民. 电子束焊接在航空发动机制造中的应用[J]. 航空制造技术,2008,51(21): 54-56. KANG Wenjun,LIANG Yangmin. Application of electron beam welding in aeroengine manufacturing[J]. Aeronautical Manufacturing Technology,2008,51(21): 54-56. (in Chinese

    KANG Wenjun, LIANG Yangmin. Application of electron beam welding in aeroengine manufacturing[J]. Aeronautical Manufacturing Technology, 2008, 51(21): 54-56. (in Chinese)
    [3]
    陈国庆,张秉刚,冯吉才,等. 电子束焊接在航空航天工业中的应用[J]. 航空制造技术,2011,54(11): 42-45. CHEN Guoqing,ZHANG Binggang,FENG Jicai,et al. Application of electron beam welding technology in aerospace industry[J]. Aeronautical Manufacturing Technology,2011,54(11): 42-45. (in Chinese

    CHEN Guoqing, ZHANG Binggang, FENG Jicai, et al. Application of electron beam welding technology in aerospace industry[J]. Aeronautical Manufacturing Technology, 2011, 54(11): 42-45. (in Chinese)
    [4]
    LAKSHMINARAYANAN A K,BALASUBRAMANIAN V,MADHUSUDHAN REDDY G. On the fatigue behaviour of electron beam and gas tungsten arc weldments of 409M grade ferritic stainless steel[J]. Materials & Design,2012,35: 760-769.
    [5]
    AGILAN M,KRISHNA S C,MANWATKAR S K,et al. Effect of welding processes (GTAW & EBW) and solutionizing temperature on microfissuring tendency in inconel 718 welds[J]. Materials Science Forum,2012,710: 603-607. doi: 10.4028/www.scientific.net/MSF.710.603
    [6]
    LONG Jian,ZHANG Linjie,ZHANG Liangliang,et al. Analysis of heterogeneity of fatigue properties of double-sided electron beam welded 140 mm thick TC4 titanium alloy joints[J]. International Journal of Fatigue,2021,142: 105942. doi: 10.1016/j.ijfatigue.2020.105942
    [7]
    ABECASSIS M,KÖSTER A,ESIN V A,et al. Crack growth behavior in dissimilar welded Ti based alloys under biaxial fatigue loading[J]. International Journal of Fatigue,2019,118: 209-224. doi: 10.1016/j.ijfatigue.2018.09.013
    [8]
    BANVILLET A. Fatigue life under non-Gaussian random loading from various models[J]. International Journal of Fatigue,2004,26(4): 349-363. doi: 10.1016/j.ijfatigue.2003.08.017
    [9]
    YU Zhengyong,ZHU Shunpeng,LIU Qiang,et al. A new energy-critical plane damage parameter for multiaxial fatigue life prediction of turbine blades[J]. Materials,2017,10(5): 513. doi: 10.3390/ma10050513
    [10]
    朱阳阳. 基于循环滞回能的电子束焊接头疲劳裂纹萌生数值模拟[D]. 南京: 南京航空航天大学,2022. ZHU Yangyang. Numerical simulation of fatigue crack initiation of electron beam welded joint based on cyclic hysteresis energy[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2022. (in Chinese

    ZHU Yangyang. Numerical simulation of fatigue crack initiation of electron beam welded joint based on cyclic hysteresis energy[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2022. (in Chinese)
    [11]
    刘俭辉,吕鑫,韦尧兵,等. 考虑附加强化效应及平均应变的多轴疲劳寿命预估[J]. 中国机械工程,2020,31(3): 314-320. LIU Jianhui,LYU Xin,WEI Yaobing,et al. Multiaxial fatigue life prediction considering additional hardening effects and mean stains[J]. China Mechanical Engineering,2020,31(3): 314-320. (in Chinese

    LIU Jianhui, LYU Xin, WEI Yaobing, et al. Multiaxial fatigue life prediction considering additional hardening effects and mean stains[J]. China Mechanical Engineering, 2020, 31(3): 314-320. (in Chinese)
    [12]
    FINDLEY W N. A theory for the effect of mean stress on fatigue of metals under combined torsion and axial load or bending[J]. Journal of Engineering for Industry,1959,81(4): 301-305. doi: 10.1115/1.4008327
    [13]
    MATAKE T. An explanation on fatigue limit under combined stress[J]. Bulletin of JSME,1977,20(141): 257-263. doi: 10.1299/jsme1958.20.257
    [14]
    MCDIARMID D L. Cumulative damage effects in high cycle multiaxial fatigue[M]//TEOH LEE S H,EOH LEE K H. Fracture of Engineering Materials and Structures. Dordrecht: Springer,1991: 537-542.
    [15]
    KAROLCZUK A,KLUGER K,ŁAGODA T. A correction in the algorithm of fatigue life calculation based on the critical plane approach[J]. International Journal of Fatigue,2016,83: 174-183. doi: 10.1016/j.ijfatigue.2015.10.011
    [16]
    BÄCKSTRÖM M. Multiaxial fatigue life assessment of welds based on nominal and hot spot stresses[J]. VTT Publications,2003(502): 3-97.
    [17]
    BÄCKSTRÖM M,MARQUIS G. A review of multiaxial fatigue of weldments: experimental results,design code and critical plane approaches[J]. Fatigue & Fracture of Engineering Materials & Structures,2001,24(5): 279-291.
    [18]
    刘天奇,时新红,张建宇,等. 平均应力对30CrMnSiA钢多轴疲劳失效的影响[J]. 航空动力学报,2018,33(12): 2972-2980. LIU Tianqi,SHI Xinhong,ZHANG Jianyu,et al. Effect of mean stress on multiaxial fatigue failure of 30CrMnSiA steel[J]. Journal of Aerospace Power,2018,33(12): 2972-2980. (in Chinese

    LIU Tianqi, SHI Xinhong, ZHANG Jianyu, et al. Effect of mean stress on multiaxial fatigue failure of 30CrMnSiA steel[J]. Journal of Aerospace Power, 2018, 33(12): 2972-2980. (in Chinese)
    [19]
    魏大盛,冯俊淇,马梦弟,等. 航空发动机轮盘中心孔模拟试验件设计方法及试验验证[J]. 航空动力学报,2022,37(10): 2157-2166. WEI Dasheng,FENG Junqi,MA Mengdi,et al. Design method and test verification of simulated specimen of aeroengine disc center hole[J]. Journal of Aerospace Power,2022,37(10): 2157-2166. (in Chinese

    WEI Dasheng, FENG Junqi, MA Mengdi, et al. Design method and test verification of simulated specimen of aeroengine disc center hole[J]. Journal of Aerospace Power, 2022, 37(10): 2157-2166. (in Chinese)
    [20]
    王霄翔. TC17钛合金电子束焊接接头多轴疲劳寿命研究[D]. 南京: 南京航空航天大学,2012. WANG Xiaoxiang. Multiaxial fatigue life evaluation of TC17Titanium alloy electron beam welded joints[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2012. (in Chinese

    WANG Xiaoxiang. Multiaxial fatigue life evaluation of TC17Titanium alloy electron beam welded joints[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2012. (in Chinese)
    [21]
    EL-HAJJAR R,HAJ-ALI R. In-plane shear testing of thick-section pultruded FRP composites using a modified Arcan fixture[J]. Composites Part B: Engineering,2004,35(5): 421-428. doi: 10.1016/j.compositesb.2003.12.004
    [22]
    刘艳磊. 铝合金焊接接头拉剪性能试验研究及有限元分析[D]. 大连: 大连海事大学,2016. LIU Yanlei. Experimental study on tensile-shear behavior of aluminum alloy welded joints and finite element analysis[D]. Dalian: Dalian Maritime University,2016. (in Chinese

    LIU Yanlei. Experimental study on tensile-shear behavior of aluminum alloy welded joints and finite element analysis[D]. Dalian: Dalian Maritime University, 2016. (in Chinese)
    [23]
    许磊. GH4169电子束焊接头拉剪复合应力下疲劳寿命预测模型研究[D]. 南京: 南京航空航天大学,2021. XU Lei. Study on fatigue life prediction model of gh4169 electron beam welding joint under tensile and shear composite stress[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2021. (in Chinese

    XU Lei. Study on fatigue life prediction model of gh4169 electron beam welding joint under tensile and shear composite stress[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2021. (in Chinese)
    [24]
    AL ZAMZAMI I,RAZAVI N,BERTO F,et al. The critical distance method to estimate the fatigue strength of notched additively manufactured titanium alloys[J]. Procedia Structural Integrity,2020,28: 994-1001. doi: 10.1016/j.prostr.2020.11.114
    [25]
    刘小刚,于盛吉,许磊. 高温合金电子束焊接头缺口疲劳寿命预测[J]. 航空动力学报,2023,38(5): 1210-1216. LIU Xiaogang,YU Shengji,XU Lei. Fatigue life prediction of electron beam welding joint of superalloy[J]. Journal of Aerospace Power,2023,38(5): 1210-1216. (in Chinese

    LIU Xiaogang, YU Shengji, XU Lei. Fatigue life prediction of electron beam welding joint of superalloy[J]. Journal of Aerospace Power, 2023, 38(5): 1210-1216. (in Chinese)
    [26]
    WANG Rongqiao,LI Da,HU Dianyin,et al. A combined critical distance and highly-stressed-volume model to evaluate the statistical size effect of the stress concentrator on low cycle fatigue of TA19 plate[J]. International Journal of Fatigue,2017,95: 8-17. doi: 10.1016/j.ijfatigue.2016.10.003
  • 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 (917) PDF downloads(41) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return