期刊文献+

Effect of large cold deformation on characteristics of age-strengthening of 2024 aluminum alloys 被引量:10

Effect of large cold deformation on characteristics of age-strengthening of 2024 aluminum alloys
在线阅读 下载PDF
导出
摘要 Effect of large cold deformation on the age-hardening characteristics of 2024 aluminum alloys was investigated. The results reveal: 1) the aging response is accelerated after large cold deformation, and the peak strength is attained after aging for 40 min; 2) double aging peaks can be found in the age-hardening curves, and the first peak appears when aged for 40 min. The corresponding peak tensile strength (sb) and elongation are up to 580 MPa and 9.2% respectively, the second peak appears when aged for 120 min, but the peak tensile strength(520 MPa) is lower than the first one; 3) in early stage of aging (<40 min), elongation slightly increases from 8% with prolonging aging time of the alloy. Elongation markedly decreases to 2% after aging for 60 min, and shows a plateau with the prolonging of aging time on the age-elongation curve. It is indicated that the high density of dislocation introduced by large deformation accelerates the precipitation of GP zones and the aging response of the alloy. The first aging peak is due to the formation of GP zones and the deformation strengthening caused by the high density of dislocation. And the second peak present in the aging curve is attributed to the nucleation and growth of S’ phase. The offset between dislocation density decreases and precipitation S’-phase finally results in the phenomenon of double aging peaks when aged at 190 ℃. Moreover, it is suggested that the formation of PFZ and coarse equilibrium phase accompanied by the precipitation of S’ phase decrease the elongation. Effect of large cold deformation on the age-hardening characteristics of 2024 aluminum alloys was investigated. The results reveal: 1) the aging response is accelerated after large cold deformation, and the peak strength is attained after aging for 40 rain; 2) double aging peaks can be found in the age-hardening curves, and the first peak appears when aged for 40 min. The corresponding peak tensile strength (σb) and elongation are up to 580 MPa and 9.2% respectively, the second peak appears when aged for 120 min, but the peak tensile strength (520 MPa) is lower than the first one; 3) in early stage of aging (〈40 min), elongation slightly increases from 8% with prolonging aging time of the alloy. Elongation markedly decreases to 2% after aging for 60 rain, and shows a plateau with the prolonging of aging time on the age-elongation curve. It is indicated that the high density of dislocation introduced by large deformation accelerates the precipitation of GP zones and the aging response of the alloy. The first aging peak is due to the formation of GP zones and the deformation strengthening caused by the high density of dislocation. And the second peak present in the aging curve is attributed to the nucleation and growth of S' phase. The offset between dislocation density decreases and precipitation S'-phase finally results in the phenomenon of double aging peaks when aged at 190 ℃ Moreover, it is suggested that the formation of PFZ and coarse equilibrium phase accompanied by the precipitation of S' phase decrease the elongation.
出处 《中国有色金属学会会刊:英文版》 EI CSCD 2006年第5期1121-1128,共8页 Transactions of Nonferrous Metals Society of China
基金 Project(50571069) supported by the National Natural Science Foundation of China Project(05A061) supported by the Department of Education of Hunan Province, China
关键词 铝合金 冷变形 时效强化 机械性能 aluminum alloy cold deformation aging strengthening mechanical properties
  • 相关文献

参考文献24

  • 1DUCKWORTH W E. Thermomechanical treatment of metals [J].JOM, 1966, 1: 915-922.
  • 2MCEVILY A J, CLARK J B, BOND A P. Effect of thermal-mechanical processing on the fatigue and stress-corrosion properties of an Al-Zn-Mg alloy [J]. ASM Trans, 1967, 60: 661-671.
  • 3RUSSO E D I, CONSERVA M, GATTO F, MARKUS H.Thermomechenical treatments on high strength Al-Zn-Mg(-Cu)alloys [J]. Metall Trans, 1973, 4(4): 1133-1144.
  • 4OSTERMANN F. Improved fatigue resistance of Al-Zn-Mg-Cu(7075) alloys through thermomechanical processing [J]. Metall Trans, 1971,2(10): 2897-2902.
  • 5RUSSO E D I, CONSERVA M, BURATTI M, GATTO F. A new thermomechanical procedure for improving the ductility and toughness of Al-Zn-Mg-Cu alloys in the transverse directions [J].Mater Sci Eng, 1974, 14: 23-36.
  • 6RACK H J. The influence of prior strain upon precipitation in a high-purity 6061 aluminum alloy [J]. Mater Sci Eng, 1977, 29:179-188.
  • 7CHIA E H, STRARKE E A. Application of subgrain control to aluminum wire products [J]. Metall Trans, 1977, 8A(6): 825-832.
  • 8JAHN M T, LUO J. Tensile and fatigue properties of a thermomechanically treated 7475 aluminum alloy [J]. J Mater Sci,1988, 23: 4115-4120.
  • 9WANHILL R J H, GESTEL G F J A V. Thermomechaaical treatment of aluminum alloy [J]. Aluminum, 1978(9): 573-580.
  • 10NOURBAKHSH S, NUTTING J. The high strain deformation of an aluminum -4% copper alloy in the supersatured and aged conditions[J]. Acta Metall, 1979, 28: 357-365.

同被引文献97

引证文献10

二级引证文献47

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