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筋板类LY12铝合金零件蠕变时效成形有限元分析 被引量:7

FE analysis on creep age forming of Al alloy LY12 ribbed-plate parts
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摘要 蠕变时效成形技术对于航空航天器件中大型复杂整体壁板类零件的制造具有独特优势,被认为是大型飞机特别重要的金属成形工艺之一。文章利用自行设计的工装,经试验确定了LY12铝合金的最佳蠕变时效成形温度;通过蠕变拉伸试验,得出LY12铝合金材料在最佳温度下的蠕变本构方程中的材料常数,并应用有限元软件ABAQUS分析了筋板类LY12铝合金零件的弯曲蠕变过程及回弹效应。 Creep age forming have unique advantage in manufacture of large and complex integral ribbed-plate parts for aerospace component and is considered to be one of the most important metallic forming process for large airplane. The best creep age forming temperature for A1 alloy LY12 was determined through experiment by using self-designed technical equipment. Then the material parameters of A1 alloy LY12 in the creep constitutive is obtained by creep tensile test under optimum forming temperature. Furthermore, the creep process and springback effect of ribbed-plate A1 alloy LY12 parts are analyzed by using FE software ABAQUS.
出处 《塑性工程学报》 CAS CSCD 北大核心 2010年第2期24-27,共4页 Journal of Plasticity Engineering
基金 航空基金资助项目(BA200700171) 江西省教育厅资助项目(GJJ08207)
关键词 LY12铝合金 蠕变时效成形 蠕变试验 本构方程 有限元分析 al alloy LY12 creep age forming creep test constitutive equation FE analysis
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参考文献10

  • 1Mitchell C Holman, Autoclave Age Forming Large Aluminum Aircraft Panels [ J]. Journal of Mechanical Working Technology, 1989. (20) : 477-488.
  • 2曾元松,黄遐,黄硕.蠕变时效成形技术研究现状与发展趋势[J].塑性工程学报,2008,15(3):1-8. 被引量:74
  • 3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
  • 4Denise M Hambrick. Age Forming Technology Expanded in an Aotoclave [C], SAE Transaction, 1985 : 94.
  • 5H Brewer. Age Forming Integrally Stiffened Aluminum Aerospace Structures in an Autoclave[C], AIAA89- 2087.
  • 6Kate Watchan. Airbus A380 takes creep age-forming to new heights[J]. Materials World. 2004. (2): 10-11.
  • 7《中国航空材料手册》编辑委员会.中国航空材料手册(铝合金.镁合金)[S].北京:中国标准出版社,2001.第3卷.
  • 8黎俊初,陈佳,熊洪淼,谭险峰,常春.LY12MO铝合金板时效成形回弹率研究[J].南昌航空大学学报(自然科学版),2008,22(4):68-70. 被引量:5
  • 9全国量和单位标准化技术委员会.GB/T2039-1997金属拉伸蠕变及持久试验方法[S].北京:中国标准出版社,1997.
  • 10黄霖,万敏,黄硕,迟彩楼,季秀升.7B04铝合金厚板蠕变时效成形有限元分析[J].航空制造技术,2007,0(z1):484-487. 被引量:12

二级参考文献46

  • 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[1]Takafumi Adachi,ShirouK.imura.Age Forming Technology for Aircraft Wing Skin[J].Materials Forum Volume.2004,(28):202-207.
  • 4[3]M.J.Jackson,J.Peddieson,S.Foroudastan.Age-forming of beam structures analysis of springback using a unified viscoplastic model[J].Proc.ImechE Vol.219 Part Ⅰ:Journal of Materials Design and Applicalions,2005,17-24.
  • 5Starink M J,Sinclair I,Gao N,et al.Development of new damage tolerant alloys for age-forming[J].Mater Sci Forum,2002,396-402:601
  • 6Kamp N,Starink M J,Sinclair I,et al.Development of AlCu-Mg-Li(Mn,Zr,Sc) alloys for age forming[A].In:proceedings of the 9th international conference on aluminium alloys.Brisbane,Australia,2004.369
  • 7Timeothy Warner,Philippe Lassince,Plilippe Lequev.Aircraft structure element made of Al-Cu-Mg alloy[P].US Pat,2001006082.2001
  • 8AeroMat.http://asm.confex.com/asm/aero05/techprogram/paper_ 7238.html
  • 9Zhu A M,Stark Jr E A.Stress aging of Al-XCu alloys:experiments[J].Acta Mater,2001,49:2285
  • 10Zhu A W,Stark Jr E A.Precipitation strengthening of stress-aged Al-XCu alloys[J].Acta Mater,2000,48:2239

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