Volume 44 Issue 6
Jun.  2018
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LIU Xiaoxiao, WANG Yibing, ZHANG Zhenget al. A novel method for determining fatigue damage parameters[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(6): 1253-1257. doi: 10.13700/j.bh.1001-5965.2017.0448(in Chinese)
Citation: LIU Xiaoxiao, WANG Yibing, ZHANG Zhenget al. A novel method for determining fatigue damage parameters[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(6): 1253-1257. doi: 10.13700/j.bh.1001-5965.2017.0448(in Chinese)

A novel method for determining fatigue damage parameters

doi: 10.13700/j.bh.1001-5965.2017.0448
Funds:

National High-tech Research and Development Program of China 2015AA034401

More Information
  • Corresponding author: ZHANG Zheng, E-mail:jordanzzhang@buaa.edu.cn
  • Received Date: 05 Jul 2017
  • Accepted Date: 20 Oct 2017
  • Publish Date: 20 Jun 2018
  • Fatigue fracture of metal materials is a common failure mode in engineering structures. Damage mechanics regards crack initiation as a progressive damage process, describing and conducting life estimates through the damage evolution equation. However, the parameters in the damage evolution equation need to be fitted according to the standard experimental data. This process usually requires multi-parameter fitting, which involves complicated operation, large computational amount and vague physical meaning. To avoid these problems, based on the theoretical basis of damage mechanics, a new method to determine the parameters of damage evolution equation was proposed. According to the properties of damage evolution equation and the characteristics of S-N curves, a single parameter method, which employs single parameter to determine the damage evolution equation, was proposed using mathematical method. The proposed method avoids the disadvantage of multi-parameter fitting at the same time and improves the calculation accuracy and speed, which provides an alternative for engineering analysis. Finally, a concrete example is given to demonstrate the effect of the proposed method.

     

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  • [1]
    ARGENTE DOS SANTOS H A, AURICCHIO F, CONTI M.Fatigue life assessment of cardiovascular balloon expandable stents:A two-scale plasticity-damage model approach[J].Journal of the Mechanical Behavior of Biomedical Materials, 2012, 15:78-92. doi: 10.1016/j.jmbbm.2012.06.011
    [2]
    张建宇, 费斌军.疲劳裂纹扩展随机过程相关参数的估计[J].北京航空航天大学学报, 1998, 24(3):308-310. http://bhxb.buaa.edu.cn/CN/abstract/abstract11654.shtml

    ZHANG J Y, FEI B J.Estimation of related parameters for stochastic process of fatigue crack propagation[J].Journal of Beijing University of Aeronautics and Astronautics, 1998, 24(3):308-310(in Chinese). http://bhxb.buaa.edu.cn/CN/abstract/abstract11654.shtml
    [3]
    ZHANG L, LIU X S, WANG L S, et al.A model of continuum damage mechanics for high cycle fatigue of metallic materials[J].Transactions of Nonferrous Metals Society of China, 2012, 22(11):2777-2782. doi: 10.1016/S1003-6326(11)61532-X
    [4]
    曾春华, 邹实践.疲劳分析方法及应用[M].北京:国防工业出版社, 1991.

    ZENG C H, ZOU S J.Fatigue analysis method and appliction[M].Beijing:National Defense Industry Press, 1991(in Chinese).
    [5]
    张明, 王珉, 左敦稳.TC4钛合金微动疲劳特性的研究[J].机械设计与制造, 2002(1):12-13. http://www.cqvip.com/qk/91722X/200201/6142455.html

    ZHANG M, WANG M, ZUO D W.Study on the fretting fatigue properties of TC4 titanium alloy[J].Journal of Mechanics, 2002(1):12-13(in Chinese). http://www.cqvip.com/qk/91722X/200201/6142455.html
    [6]
    杨锋平, 孙秦, 罗金恒, 等.一个高周疲劳损伤演化修正模型[J].力学学报, 2012, 44(1):140-147. http://www.oalib.com/paper/4291031

    YANG F P, SUN Q, LUO J H, et al.A corrected damage law for high cycle fatigue[J].Acta Mechanica Sinica, 2012, 44(1):140-147(in Chinese). http://www.oalib.com/paper/4291031
    [7]
    SHANG D G, SUN G Q, DENG J, et al.Nonlinear cumulative damage model for multi-axial fatigue[J].International Journal of Fatigue, 2006, 1(3):265-269. doi: 10.1007/s11465-006-0035-x
    [8]
    张行, 崔德渝, 孟庆春, 等.断裂与损伤力学(第二版)[M].北京:北京航空航天大学出版社, 2009:318-348.

    ZHANG X, CUI D Y, MENG Q C, et al.Fracture and damage mechanics(2nd Edition)[M].Beijing:Beihang University Press, 2009:318-348(in Chinese).
    [9]
    彭艳, 李浩然.考虑附加强化效应的多轴高周疲劳损伤演化模型[J].机械工程学报, 2015, 51(16):135-142. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=jxgcxb201516015

    PENG Y, LI H R.Multiaxial high cycle fatigue damage evolution model including additional hardening effect[J].Journal of Mechanical Engineering, 2015, 51(16):135-142(in Chinese). http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=jxgcxb201516015
    [10]
    LI D L, CHOW C L.A damage mechanics approach to fatigue assessment in offshore structures[J].International Journal of Damage Mechanics, 1993, 1(2):385-405. http://deepblue.lib.umich.edu/handle/2027.42/67255
    [11]
    徐小兵.表面有横向裂纹的抽油杆寿命估算[J].石油机械, 1993, 21(5):29-33. http://www.cqvip.com/QK/94770X/199305/1161678.html

    XU X B.Life estimation of sucker rod with transverse cracks on the surface[J].Journal of Petroleum Machinery:1993, 21(5):29-33(in Chinese). http://www.cqvip.com/QK/94770X/199305/1161678.html
    [12]
    袁熙, 李舜酩.疲劳寿命预测方法的研究现状与发展[J].航空制造技术, 2005(12):80-84. doi: 10.3969/j.issn.1671-833X.2005.12.016

    YUAN X, LI S M.Research status and development of forecast method of fatigue life[J].Aeronautical Manufacturing Technology, 2005(12):80-84(in Chinese). doi: 10.3969/j.issn.1671-833X.2005.12.016
    [13]
    詹志新, 佟阳, 李彬恺, 等.考虑冲击缺陷的钛合金板的疲劳寿命预估[J].航空学报, 2016, 37(7):2200-2207. http://mall.cnki.net/magazine/Article/WHZC201402031.htm

    ZHAN Z X, TONG Y, LI B K, et al.Fatigue life prediction for titanium plate considering impact defect[J].Acta Aeronautica et Astronautica Sinica, 2016, 37(7):2200-2207(in Chinese). http://mall.cnki.net/magazine/Article/WHZC201402031.htm
    [14]
    WAN H L, WANG Q Z, ZHANG Z.Anisotropic elastoplastic damage mechanics method to predict fatigue life of the structure[J].Advances in Materials Science and Engineering, 2016, 2016:7128347.
    [15]
    吴学仁.飞机结构金属材料力学性能手册[M].北京:航空工业出版社, 1996:55-100.

    WU X R.Manual of metal material mechanics performance in plane structure[M].Beijing:Aviation Industry Press, 1996:55-100(in Chinese).
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