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2E12铝合金中心孔板材疲劳寿命分析 被引量:2

Fatigue Life Analysis of Aluminum Alloy 2E12 Plates with Center Holes
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摘要 以2E12铝合金光滑疲劳实验为基础,结合有限元软件ABAQUS和疲劳分析软件MSC.Fatigue,详细地介绍了疲劳寿命预测的流程和实现过程。进行疲劳寿命分析,分析结果表明孔径与板长之比D/L对板材疲劳寿命有显著的影响,D/L与对数寿命呈幂函数关系。数值模拟结果与理论计算结果基本相吻合,进行疲劳寿命分析,分析结果表明孔径与板长之比D/L对板材疲劳寿命有显著的影响,D/L与对数寿命呈幂函数关系。 On the basic of the fatigue tension test of aluminum alloy 2E12, the process and realization process of fatigue life prediction is deeply introduced by using FEM software ABAQUS and fatigue analysis software MSC. Fatigue. Numerical simulation results are consistent with the theoretical calculation results and the reliability of numerical simulation to analyze the fatigue life of products is verified. Then aluminum alloy 2E12 plates models with different aperture to analyze fatigue life are created. The results show that the ratio of aperture and the length has a marked impact on fatigue life and D/L has power function relation with logarithmic life.
出处 《材料工程》 EI CAS CSCD 北大核心 2009年第7期58-61,66,共5页 Journal of Materials Engineering
基金 国家重点基础研究发展计划973计划(2005CB623705)
关键词 疲劳实验 数值模拟 疲劳寿命分析 MSC.Fatigue fatigue test numerical simulation fatigue life analysis MSC. Fatigue
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参考文献7

  • 1杨胜,易丹青,杨守杰,钟利.腐蚀环境下2E12航空铝合金疲劳裂纹扩展行为研究[J].材料工程,2007,35(12):26-29. 被引量:11
  • 2丁文江,王渠东,刘满平.轻合金技术新进展[R].中国科学院高技术发展报告,2002.
  • 3吴富民.结构疲劳强度[M].西安:西北工业大学出版社,1985.141-148.
  • 4杨守杰,戴圣龙.航空铝合金的发展回顾与展望[J].材料导报,2005,19(2):76-80. 被引量:203
  • 5LIU J,YUE Z F,LIU Y S.Surface finish of open holes on fatigue life[J].Theoretical and Applied Fracture Mechanics.2007(47):35-45.
  • 6DAMIR A N,ELKHATIB A,NASSEF G.Prediction of fatigue life using modal analysis for grey and ductile cast iron[J].International Journal of Fatigue,2007,29:499-507.
  • 7BUCAR T,NAGODE M,FAJDIGA M.An improved neural computing method for describing the scatter of S-N curves[J].International Journal of Fatigue,2007,29:2125-2137.

二级参考文献35

  • 1Heinz A,et al. Recent development in aluminum alloys for aerospace applications. Mater Sci Eng, 2000,A280: 102.
  • 2Staley James T, Liu John,Hunt Warren H Jr. Aluminum alloys for aerostructures. Adv Mater Proc, 1997,10: 17.
  • 3Filatov Y A,et al. New Al-Mg-Sc alloys. Mater Sci Eng,2000,A280:97.
  • 4Wu Y L, Li C G,et al. Microalloying of Sc,Ni and Ce in an advanced Al-Zn-Mg-Cu alloy. Metall Trans, 1999, 30A (4):1017.
  • 5Liu J,Kulak M. A New paradigm in the design of aluminum alloys for aerospace applications. Mater Sci Forum,2000,331-337:127.
  • 6Rogacki J R. Materials for air and space. Adv Mater Proc,2000, (9) :63.
  • 7Bucci R J, Warren C J,et al. Need for new materials in aging aircraft structures. J Aircraft, 2000,37(1) : 122.
  • 8Matsuoka H, Hiros Y, Kishi Y,et al. Experimental study on strengthening mechanism of Al-Zn-Mg-Cu system alloy.J Soc Mat Sci Japan,1997,46(6):655.
  • 9Waterloo G, Hansen V, Gjonnes J, Skjervold S R. Effect of predeformation and presaging at room temperature in Al-Zn-Mg- (Cu,Zr) alloys. Mat Sci Eng, 2001 ,A303: 226.
  • 10Senatorova O G,Frindlyander I N. Influence of machining on residual stresses and properties of superhigh strength B96ц thin elements. Mater Sci Forum, 2002,396-402:1597.

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