期刊文献+

蠕变时效对7050铝合金板材组织与性能的影响 被引量:11

Microstructures and Properties of 7050 Aluminum Alloy Sheet During Creep Aging
在线阅读 下载PDF
导出
摘要 通过金相显微、透射电子显微、电子拉伸和剥落腐蚀实验研究了7050铝合金板材蠕变时效与人工时效的微结构及性能。结果表明:蠕变时效过程中施加的应力使板材不断产生变形,为η′析出相提供了大量形核点,析出相尺寸更加细小,特别是晶界无沉淀带较人工时效明显变窄,晶界析出相不连续。与人工时效相比,蠕变时效试样的抗拉强度和抗剥落腐蚀性能略有提高。 Microstructures and properties of 7050 aluminum alloy sheet after creep aging and artificial aging were studied by optical microscopy(OM),transmission electron microscopy(TEM),electronic tensile test and exfoliation corrosion test respectively.The results show that the loaded stress during creep aging generates continuously deformation,which provides a large amount of nucleation points for the precipitation of the η′ particles.The size of the η′ particles is smaller than that of the artificial aging.Especially,the precipitation free zone is narrower than that of the artificial aging,and grain boundary precipitates are discontinuous.The tensile strength and the resistance to exfoliation corrosion of the creep aging samples are better than those of the artificial aging.
出处 《材料工程》 EI CAS CSCD 北大核心 2012年第1期71-76,共6页 Journal of Materials Engineering
基金 国家重点基础研究发展计划(973)项目(2010CB731700)
关键词 7050铝合金 蠕变时效 微结构 力学性能 剥落腐蚀 7050 Al alloy creep aging microstructure mechanical property exfoliation corrosion
  • 相关文献

参考文献17

  • 1HOLMAN M C.Autoclave age forming large aluminum aircraft panels[J].Mechanical Working and Technology,1989,20 (9):477-488.
  • 2ZHU A W,STARKE Jr E A.Materials aspects of age-forming of Al-xCu alloys[J].Journal of Materials Processing Technology,2001,117(3):354-358.
  • 3ZHU A W,STARKE JR E A.Stress ageing of Al-xCu alloys:experiments[J].Acta Materialia,2011,49(12):2285-2295.
  • 4LI C,WAN M,WU X D,et al.Constitutive equations in creep of 7B04 aluminum alloys[J].Materials Science and Engineering A,2010,527(16-17):3623-3629.
  • 5ZHAN L H,LIN J G,DEAN T A.A review of the development of creep age forming:experimentation,modeling and applications[J].International Journal of Machine Tools and Manufacture,2011,51(1):1-17.
  • 6周亮,邓运来,晋坤,张新明.预处理对2124铝合金板材蠕变时效微结构与力学性能的影响[J].材料工程,2010,38(2):81-85. 被引量:20
  • 7ADACHI T,KIMURA S,NAGAYAMA T,et al.Age forming technology for aircraft wing skin[J].Materials Forum,2004,28:202-207.
  • 8EBERL F,GARDINER S,CAMPANILE G,et al.Agefomable panels for commercial aircraft[J].Proceeding of the Institution of Mechanical Engineers,Part G:Aerospace Engineering,2008,222(6):873-886.
  • 9LEQUEU PH,LASSINCE PH,WARNER T.Alcan aluminum development for the airbus A380-part2[J].Advanced Materials & Processes,2007,165(7):41-44.
  • 10BAKAVOS D,PRANGNELL P B,BES B,et al.Microstructural interactions during stress aging a 7475 aerospace alloy[J].Materials Science Forum,2006,519-521(7):333-338.

二级参考文献38

  • 1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
  • 2李志辉,熊柏青,张永安,朱宝宏,王锋,刘红伟.7B04铝合金的时效沉淀析出及强化行为[J].中国有色金属学报,2007,17(2):248-253. 被引量:24
  • 3HEINZ A, HASZLER A ,KEIDEL C,et al. Recent development in aluminium alloys for aerospace applications [ J ]. Mater Sci Eng A, 2000, A280:102 - 107.
  • 4DESCHAMPS A, BRECHET Y. Influence of quench and heating rates on the ageing response of an Al-Zn-Mg-(Zr) alloy[J]. Mater SciEng A, 1998, A251:200-207.
  • 5PRIME M B, HILL M R. Residual stress relief and inhomogeneity in aluminium plate [ J]. Scripta Materialia,2002,46 (1) :77 -82.
  • 6DUMONT D,DESCHAMPS A, BRECHETY. On the relationship between microstructure, strength and toughness in AAT050 aluminum alloy [ J ]. Mater Sci Eng A, 2003, A356,326 -336.
  • 7MUKHOPADHYAY A K, REDDY G M, PRASAD K S, et al. Microstructure property relationships in a high strength Al-Zn-Mg-Cu-Zr alloy[A]. Nie J F, Morton A J, Muddle B C. Proceedings of the 9th International Conference on Atuminium Alloys [ C ]. Australia : Institute of Materials Engineering Australasia Ltd, 2004:883 - 888.
  • 8ZHU Bao-hong, ZHANG Yong-an, XIONG Bai-qing, et al. Effect of artificial aging temper on the microstructure and properties of 7B04 pre-stretched thick plate[ J]. Materials Science Forum, 2006, 519-521:901 -906.
  • 9MITCHELL C Holman. Autoclave age forming large aluminum aircraft panels [ J ]. Journal of Mechanical Working Technology, 1989, 20:477-488
  • 10Airbus A380 takes creep age-forming to new heights[ R ]. Airbus Materials World, 2004.

共引文献51

同被引文献98

引证文献11

二级引证文献37

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