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巨型压机C型机架的疲劳寿命预测研究
英文标题:Study on fatigue life prediction for C-type frame of huge pressure machine
作者:黄宁 杨建湘 李素云 
单位:贺州学院 
关键词:疲劳寿命 模拟缩比模型 缺口试样尺寸系数 疲劳综合修正系数 名义应力法 C型板 
分类号:O346
出版年,卷(期):页码:2016,41(5):136-141
摘要:
针对循环拉伸载荷下光滑件的尺寸效应不显著和大型零件难于进行原型疲劳试验,给出了利用小试样试验去预测大型零件疲劳寿命的分析方法。首先,基于疲劳模拟试验建立模拟缩比模型,引入缺口试样尺寸系数。其次,引入表征尺寸变化对疲劳性能影响的特征参量,利用两种材料(45钢, Q235)的几何相似试样(Kt=2, Kt=3)疲劳寿命试验结果,获得缺口试样尺寸系数经验公式。同时兼顾尺寸、应力集中和表面状况之间的相互影响,建立了拉伸载荷下的疲劳综合修正系数模型,并用一算例验证了其有效性。最后,在名义应力法的基础上,应用该模型对大型C型板材料的S-N曲线进行修正,成功地预测出C型板的疲劳寿命。该方法符合实际情况,使疲劳寿命估算更合理,可用于评估拉伸作用下的大型零件疲劳评估。
For insignificant size effect of smooth specimen under cyclic tensile load and difficulty in the fatigue test for large-scale component, fatigue life prediction method for large-scale component was presented by experiments of small samples. Firstly, simulate-scale model was created based on fatigue simulation test, and size coefficient of notched-sample was introduced. Secondly, characteristic parameter that represents the influences of size change condition on fatigue properties was introduced, and an empirical size coefficient formula was obtained by utilizing the tested fatigue life results of geometrically similar specimens (Kt=2, Kt=3) made in two kinds of materials (Steel 45, Q235). Simultaneously considering interaction of size, stress concentration and surface quality, a fatigue comprehensive correction factor model was proposed, and its validity was proved. Finally, on the basis of the nominal stress method, fatigue life of large-scaled C-type plate was successfully predicted after modifying S-N curve of plate material through fatigue comprehensive correction factor model. This method was in well accordance with the practical situation, and fatigue life prediction was more reasonably. Furthermore, this method provided a new way for fatigue assessment of large-scale component under tension.
基金项目:
贺州学院博士基金启动项目(HZUBS201303);贺州市科技开发项目(贺科能1408013);广西高校科研项目(KY2015ZD128)
作者简介:
黄宁(1974-),男,博士,讲师
参考文献:


[1]Zheng J Y,Wu L L, Shi J F. Extreme pressure equipments[J]. Chinese Journal of Mechanical Engineering, 2011, 24(2): 202-206.
[2]奚蔚,姚卫星. 一种考虑尺寸效应的缺口件疲劳寿命预测方法[J]. 南京航空航天大学学报,2013,45(4): 497-502.Xi W, Yao W X. Method for fatigue life prediction of notched specimen considering size effect [J]. Journal of Nanjing University of Aeronautics & Astronautics, 2013, 45(4): 497-502.
[3]吴志荣,胡绪腾,宋迎东.多轴载荷下缺口件的疲劳寿命估算方法[J]. 工程力学,2014,31(4): 215-221.Wu Z R, Hu X T, Song Y D. Estimation method for fatigue life of notched specimen under multi-axial loading [J]. Engineering Mechanics, 2014,31(4): 215-221.
[4]张小丽,陈雪峰,李兵,等. 机械重大装备寿命预测综述[J]. 机械工程学报, 2011, 47(11): 100-116.Zhang X L, Chen X F, Li B, et al. Review of life prediction for mechanical major equipment [J]. Chinese Journal of Mechanical Engineering, 2011, 47(11): 100-116.
[5]黄宁. 大型结构件的疲劳寿命预测方法研究[D]. 长沙: 中南大学, 2012.Huang N. Research on Fatigue Life Prediction Methods for Large-Scale Components [D]. Changsha: Central South University, 2012.
[6]Wilfrled Eichlseder. Fatigue analysis by local stress concept based on finite element results [J]. Computers and Structures, 2002, 80:2109-2113.
[7]Bruder T, Strzel K, Baumgartner J, et al. Evaluation of nominal and local stress based approaches for the fatigue assessment of seam welds[J]. International Journal of Fatigue, 2012, 34: 86-102.
[8]Zhao S C, Xie J J, Wu X L. Numerical simulation of fatigue initiation life for notched specimens with gradient surface layer[J]. Sci. Sin.-Phys. Mech. Astron., 2013,43: 737-745.
[9]Yves Vverrman, Nathalie Limodin. Fatigue notch factor and short crack propagation[J]. Engineering Fracture Mechanics, 2008,75: 1320-1335.
[10]Stamoulis K, Giannakopoulos A E. Size effects on strength, toughness and fatigue crack growth of gradient elastic solids[J]. International Journal of Solids and Structures, 2008, 45: 4921-4935.
[11]Adib-Ramezani H, Jeong J. Advanced volumetric method for fatigue life prediction using stress gradient effects at notch roots[J]. Computational Materials Science, 2007, 39: 649-663.
[12]Norberg S, Olsson M. The effect of loaded volume and stress gradient on the fatigue limit[J]. International Journal of Fatigue, 2007, 29(12): 2259-2272.
[13]黄宁, 黄明辉, 湛利华. 新的缺口试样尺寸系数经验公式[J]. 华南理工大学学报:自然科学版, 2012, 40(12): 35-40.Huang N, Huang M H, Zhan L H. New empirical formula of size coefficient of notched samples [J]. Journal of South China University of Technology: Natural Science Edition, 2012, 40(12): 35-40.
[14]姚卫星. 结构疲劳寿命分析[M]. 北京: 国防工业出版社, 2003.Yao W X. Fatigue Life Prediction of Structures [M]. Beijing: National Defense Industry Press, 2003.
[15]陈耀明. 评价及估算切口疲劳强度的新方法[M]. 北京:航空工业出版社,2006.Chen Y M. A New Method of Evaluating and Estimating Notch Fatigue Strength[M]. Beijing: Aviation Industry Press, 2006. 

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