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AA2050合金蠕变时效本构方程的改进

Improvement on the Constitutive Equations for Creep Age Behaviour of AA2050 Alloy
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摘要 有限元法预测铝合金蠕变成形工件回弹量的关键是蠕变时效本构方程的构建,为更精确模拟铝合金蠕变时效成形过程,本文改进了文献[18]提出的AA2050合金蠕变时效本构方程,提出本构方程中微观组织相关参数的新算法。基于改进后的本构方程,模拟计算了Al-Cu-Li合金AA2050-T34试样受拉应力作用下的蠕变时效行为,计算结果与实验结果吻合良好。改进后的本构方程可用于模拟预测AA2050合金蠕变时效成形行为。 The constitutive model is one of the key technologies in predicting the spring back during creep age forming of the aluminum alloys.To calculate the creep age forming of alloys precisely,the constitutive equations is presented by Li nwere modified.A new numerical algorithm of microstructure-dependant creep variables are presented.The tension creep behaviour of Al-Cu-Li alloy AA2050-T34 is simulated by using of the modified constitutive equations.A good agreement has been achieved between the experimental results,predicted results of Li and the present numerical calculation.The modified constitutive equationscan can be applied to research on the creep age forming of AA2050 aluminium alloys.
作者 张显飞 赵忠兴 ZHANG Xianfei;ZHAO Zhongxing(Shenyang Ligong University,Shenyang 110159,China)
出处 《沈阳理工大学学报》 CAS 2019年第5期12-16,共5页 Journal of Shenyang Ligong University
关键词 蠕变时效 本构方程 模拟 AA2050合金 creep age forming constitutive equations simulation AA2050 alloy
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  • 1陈大钦,郑子樵,李世晨,陈志国,刘祖耀.外加应力对Al-Cu及Al-Cu-Mg-Ag合金析出相生长的影响[J].金属学报,2004,40(8):799-804. 被引量:35
  • 2李劲风,郑子樵,李世晨,任文达,陈文敬.铝合金时效成形及时效成形铝合金[J].材料导报,2006,20(5):101-103. 被引量:34
  • 3航空制造工程手册-飞机钣金工艺[M].北京:航空工业出版社,1992:397-400
  • 4Holman, M C. Autoclave age forming large aluminium aircraft panels[J]. J. Mech. Work. Technol. , 1989. 20: 477-488
  • 5Denise M. Hambrick. Age Forming Technology Expanded in an Aotoclave[C]. SAETransaction, 1985. 94
  • 6H Brewer. Age Forming Integrally Stiffened[C]. Aluminum Aerospace Structures in an Autoclave, AIAA89- 2087
  • 7Brewer,Jr. et al. Method of Tool Development[P]. U. S. Patent, 5,168,169
  • 8Airbus A380 takes creep age-forming to new heights[J]. Materials World, 2004. (2): 10-11
  • 9J Munroe, K Wilkins, M Gruber. Integral Airframe Structures (IAS)-Validated Feasibility Study of Integrally Stiffened Metallic Fuselage Panels for Reducing Manufacturing Costs. NASA/CR-2000-209337
  • 10Erhard Krempl. Viscop[asticity Based on Total Strain. The Modeling of Creep Special Considerations of Initial Strain and Aging[J]. Journal of Enfineering Materials and Technology, 1979. 101 (10) : 380-386

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