期刊文献+

Al-6.2Zn-2.3Mg-2.3Cu铝合金厚板的双级时效工艺

Double aging of Al-6.2Zn-2.3Mg-2.3Cu aluminum alloy plate
在线阅读 下载PDF
导出
摘要 采用力学性能和电导率测定、透射电镜组织观察等方法,研究了Al-6.2Zn-2.3Mg-2.3Cu超高强铝合金厚板双级时效过程第一级时效条件及第二级时效温度和时间对合金性能的影响。结果表明,影响该合金厚板性能最重要的因素是第二级时效温度,其次是第二级时效时间,第一级时效条件对合金性能的影响不大;当第二级时效温度为165℃或175℃时,温度低、长时间(165℃8 h)时效或温度高、短时间(175℃4 h)时效可使板材获得相似的性能;该合金厚板合适的双级时效处理制度为120℃4 h+165℃(8~12)h。 In this paper,using the mechanical properties,the measurement of the electrical conductivity and transmission electron microscopy to study the first class of the two stage aging process and the temperature and time of the two aging of the Al-6.2Zn-2.3Mg-2.3Cu ultra high strength aluminum alloy plate effect on properties of alloys.The results show that the most important factor effect on the performance of alloy plate is the aging temperature of the second stage,followed by a second-class aging time.The first-class aging conditions will not significantly affect the performance of the alloy.When the temperature of the seeondclass aging was 165℃ or 175℃ ,similar performance was obtained no matter low temperature and long time or high temperature and short time.The suitable system of two-stage aging treatment of this alloy plate was 120℃ 4 h+ 165℃ (8-12) h.
出处 《轻合金加工技术》 CAS 北大核心 2010年第1期45-48,58,共5页 Light Alloy Fabrication Technology
基金 国家科技支撑计划资助项目(2007BAE38806)
关键词 超高强铝合金 厚板 双级时效 super-high strength aluminum thick plate double aging
  • 相关文献

参考文献11

  • 1田福泉,崔建忠.双级时效对7050铝合金组织和性能的影响[J].中国有色金属学报,2006,16(6):958-963. 被引量:55
  • 2张录泉.7×××合金的双级时效.轻合金加工技术,1986,(1):16-21.
  • 3FRIDLYANDERJ N, SENATOR.OVA O G. Development and application ofhigh-strengthAl- Zn-Mg- Cu alloys [J ] .Mater Science Forum, 1996,217-222:1813-1818.
  • 4DAVID A L, RAY M H. Aluminum alloy development efforts for compression structure of aircraft [J ].Light Metal Age, 1991,2(9): 11 - 15.
  • 5HEINZ A, HASZLER A, KEIDEL C,et al. Recent development in aluminum alloys for aerospace apphcations[J].Materials Science and Engineering A, 2000,280(1):102-107.
  • 6MAGNUSEN P E. Analysis and prediction of microstructural effects on long-term fatigue performance of an aluminum aerospace alloy [ J ]. International Journal of Fatigue, 1997,119 ( 1 ) :275 - 283.
  • 7KIM J H, LEE S B. Behavior of plasticity-induced crack closure and roughness-induced crack closure in aluminum alloy[ J]. International Journal of Fatigue, 2001,23:247 -251.
  • 8CLARK D A,JOHNSON W S. Temperature effects on fatigue performance of cold expanded holes in 7050 - T7451 aluminum alloy[ J]. International Journal of Fatigue,2003,25 : 159 - 165.
  • 9KEVIN R, COOPER, KELLYR G. Crack tip chemistry and electrochemistry of environmental crack in AA7050 [ J], Corrosion Science ,2007,49:2636 - 2662.
  • 10LIN J C. Effect of heat treatments on the tensile strength and SCC resistance of AA7050 in an alkaline solution [ J ]. Corrosion Science,2006,48 : 3139 - 3156.

二级参考文献18

  • 1陆海庆,张思平.7050-T7651铝合金预拉伸厚板生产工艺研究[J].铝加工,2004,27(4):48-51. 被引量:12
  • 2郭俊锋,李平,赵刚,刘春明.7055合金挤压带板纵横向的组织与性能[J].材料与冶金学报,2004,3(3):219-223. 被引量:3
  • 3宋仁国,曾梅光,张宝金,刘军,金真弘.7050铝合金晶界偏析与应力腐蚀、腐蚀疲劳行为的研究[J].中国腐蚀与防护学报,1996,16(1):1-8. 被引量:37
  • 4Clark D A,Johnson W S.Temperature effects on fatigue performance of cold expanded holes in 7050 -T7451 aluminum alloy[J].International Journal of Fatigue,2003,25:159-165.
  • 5Magnusen P E,Buci R J,Hinkle A J,et al.Analysis and prediction of microstructural effect on long-term fatigue performance of an aluminum aerospace alloy[J].International Journal of Fatigue,1997,19 (1):275-283.
  • 6Lin C K,Yang S T.Corrosion fatigue behavior of7050 aluminum alloys in different tempers[J].Engineering Fracture Mechanics,1998,59(6):779-795.
  • 7Gang S,Alfred C.Early-stage precipitation in Al-ZnMg-Cu alloy(7050)[J].Acta Materialia,2004,52(4):503-4516.
  • 8Robson J D.Microstructural evolution in aluminium alloy 7050 during processing[J].Materials Science and Engineering A,2004,382:112-121.
  • 9Adler P N,Deilsi R.Calorimetric studies of 7000 series aluminum alloys:Ⅱ.Comparison of 7075,7050and RX720 alloys[J].Metallurgical Transactions A,1977,8(7):1185-1190.
  • 10Staley J T.Aging kinetics of aluminum alloy 7050[J].Metallurgical Transactions,1974,5:929-932.

共引文献54

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