期刊文献+

基于最弱环理论的缺口件概率疲劳寿命预测方法 被引量:5

Probabilistic Fatigue Life Prediction Method for Notched Specimens Based on the Weakest-link theory
下载PDF
导出
摘要 基于最弱环理论和光滑试样疲劳寿命的Weibull分布,建立了一种缺口件概率疲劳寿命预测方法。该方法首先基于最弱环理论和光滑试样的疲劳强度分布,通过定义缺口件的Weibull有效应力,建立了缺口件在给定循环载荷下的疲劳失效概率计算公式。基于Weibull有效应力和光滑试样的疲劳应力-特征寿命方程,可计算得到给定循环载荷时缺口件的特征疲劳寿命,进一步根据光滑试样的Weibull疲劳寿命分布可最终获得缺口件在给定循环载荷下的疲劳寿命分布。采用上述方法对TC4缺口试样进行了概率疲劳寿命预测,并与局部应力应变法预测结果进行了对比。结果表明:局部应力应变法预测结果过于保守,本文方法预测精度较高,50%失效概率时的疲劳寿命预测结果与缺口试样试验均值寿命吻合很好,10%和90%失效概率时的疲劳寿命预测结果基本分布在试验均值寿命的两倍分散带之内。 A probabilistic fatigue life prediction method for notched specimens was established based on the wea- kest-link theory and Weibull fatigue life distribution of smooth specimen. A Weibull equivalent stress was derived and fatigue failure probability for notched specimen was formulated based on the weakest-link theory and fatigue strength distribution of smooth specimen. According to the relationship between the Walker equivalent stress and the characteristic fatigue life, the characteristic life of notched specimen can be calculated based on the Weibull e- quivalent stress. Finally the life distribution of notched specimens can be obtained based on the fatigue life distribu- tion of smooth specimen. This method was evaluated by the probabilistic fatigue life prediction of TC4 alloy notched specimens and the prediction result was compared with the local stress-strain method. The result shows that the lo- cal stress-strain method was very conservative, the method presented in this paper can predict more accurately. The predicted life with 50% failure rate agrees well with the test mean tested life of TC4 alloy notched specimens. The predicted life with 10% and 90% failure rate are mostly within the scatter band of 2 compared to the test mean life.
出处 《机械科学与技术》 CSCD 北大核心 2013年第2期164-169,共6页 Mechanical Science and Technology for Aerospace Engineering
基金 航空科学基金项目(2010ZB52014) 国家自然科学基金青年基金项目(51105198) 国防基础科研项目资助
关键词 材料疲劳 裂纹起始 概率 WEIBULL分布 应力集中 fatigue of materials crack initiation probability Weibull distribution stress concentration
  • 相关文献

参考文献12

  • 1Taylor D.The theory of critical distance.Engineering FractureMechanics[J] ,2008,75(7):1695-1890.
  • 2Susmel L,Taylor D.An elasto-plastic reformulation of the theoryof critical distances to estimate lifetime of notched componentsfailing in the low/medium-cycle fatigue regime[J].Journal ofEngineering Materials and Technology,2010,132(2).
  • 3Yamashita Y,Ueda Y,Kuroki H,et al.Fatigue life predictionof small notched Ti-6Al-4V specimens using critical distance[J].Engineering Fracture Mechanics,2010,77(9):1439-1453.
  • 4Yang X G,Wang J K,Liu J L.High temperature LCF life pre-diction of notched DS Ni-based superalloy using critical distanceconcept[J].International Journal of Fatigue,2011,33(11):1470-1476.
  • 5辛朋朋,胡绪腾,宋迎东.基于临界距离理论的TC4合金缺口试样低循环疲劳寿命预测[J].航空动力学报,2012,27(5):1105-1112. 被引量:10
  • 6Schweiger G,Heckel K.Size effect in randomly loaded speci-mens[J].International Journal of Fatigue,1986,8(4):231-234.
  • 7Lanning D B,Nicholas T,Palazotto A.HCF notch predictionsbased on weakest-link failure models[J].International Journalof Fatigue,2003,25(3):835-841.
  • 8Slavik D,Kurath P.Fatigue crack initiation modeling in Ti-6Al-4V for smooth and notched specimens under complex stress states[A].Fifth National Turbine Engine HCF Conference[C] ,Chandler AZ,2000.
  • 9Weibull W.A statistical distributions function of wide applicabil-ity[J].Journal of Applied Mechanics,1951,9:293-297.
  • 10Walker K.The Effects of Stress Ratio During Crack Propa-gation and Fatigue for 2024-T3 and 7075-T6 Aluminum:Effect of Environment and Complex Load History on FatigueLife[R].West Conshohocken:American Society Testing andMaterials,STP 462,1970.

二级参考文献14

  • 1Neuber H. Theory of notch stresses:principles for exact calculation of strength with reference to structural form and material[M].Beilin:Springer-Verlag,1958.
  • 2Peterson R E. Notch sensitivity[M].Metal Fatigue,New York:McGraw Hill,1959.293-306.
  • 3Taylor D. The theory of critical distances:a new perspec-tive in fracture mechanics[M].Oxford:Elsevier,2007.
  • 4Taylor D. Geometrical effects in fatigue:a unifying theo-retical model[J].International Journal of Fatigue,1999,(05):413-420.doi:10.1016/S0142-1123(99)00007-9.
  • 5Susmel L. The theory of critical distances:a review of its applications in fatigue[J].Engineering Fracture Mechanics,2008,(07):1706-1724.doi:10.1016/j.engfracmech.2006.12.004.
  • 6Taylor D,Bologna P,Knani K B. Prediction of fatigue fail ure location on a component using a critical distance meth od[J].International Journal of Fatigue,2000,(09):735-742.
  • 7Susmel L,Taylor D. A novel formulation of the theory of critical distances to estimate lifetime of notched compo-nents in the medium-cycle fatigue regime[J].Fatigue Fracture of Engineering Materials& Structures,2007,(07):567-581.
  • 8Susmel L,Taylor D. An elasto plastic reformulation of the theory of critical distances to estimate lifetime of notched components failing in the low/medium-cycle fatigue regime[J].ASME Journal of Engineering Materials and Technology,2010,(02):021002,(8).
  • 9Yamashita Y,Ueda Y,Kuroki H. Fatigue life predic-tion of small notched Ti-6AI-4V specimens using critical distance[J].Engineering Fracture Mechanics,2010,(09):1439-1453.
  • 10YANG Xiaoguang,WANG j'ingke,LIU Jinlong. High tem-perature LCF life prediction of notched DS Ni-hased super-alloy using critical distance concept[J].International Jour-nal of Fatigue,2011,(11):1470-1476.

共引文献18

同被引文献60

引证文献5

二级引证文献18

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部