期刊文献+

回归时间对7050铝合金晶间腐蚀性能的影响 被引量:29

Effect of retrogression time on intergranular corrosion of 7050 aluminum alloy
在线阅读 下载PDF
导出
摘要 采用硬度、电导率测试、金相及透射电镜观察等手段,研究了回归时间对7050铝合金力学和晶间腐蚀性能的影响。结果表明:合金经190℃/60min回归和再时效处理,屈服强度最高,抗晶间腐蚀能力最好,具有最佳的综合性能;但合金在接近回归硬度曲线的谷值时,经190℃/4min回归处理,抗晶间腐蚀性能最差。透射电镜观察表明,190℃回归4min时,晶界析出相粗大,基本连续分布,没有明显无沉淀析出带,4min后,随回归时间的延长,晶界无沉淀析出带略宽,同时晶界析出相逐渐粗大且不连续分布,进而提高了合金的抗晶间腐蚀性能。 The effects of retrogression time on the mechanical properties and intergranular corrosion (IGC) resistance of 7050 aluminum alloy were investigated by means of hardness and electrical conductivity test, optical microscopy (OM) and transmission electron microcopy (TEM). The results show that the highest yield strength and IGC resistance are obtained by 190 ℃/60 rain retrogression and reaging. But when the alloy is treated near the lowest value of hardness curve of retrogression, the lowest IGC resistance is gotten by 190 ℃/4 min retrogression treatment. The TEM observation shows that the grain boundary precipitates are continuous and coarse by 190 ℃/4 min retrogression treatment, and no obvious precipitate free zone (PFZ) is observed. With retrogression time increasing, more spaced and coarser grain boundary precipitates are observed, and the PFZ becomes wider, which can attribute to improve IGC resistance of 7050 aluminum alloy.
出处 《中国有色金属学报》 EI CAS CSCD 北大核心 2008年第10期1795-1801,共7页 The Chinese Journal of Nonferrous Metals
基金 国家重点基础研究发展计划资助项目(2005CB623700)
关键词 7050铝合金 回归时间 力学性能 晶间腐蚀 7050 aluminum alloy retrogression time mechanical properties intergranular corrosion
  • 相关文献

参考文献16

  • 1CLARK 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.
  • 2杨守杰,戴圣龙.航空铝合金的发展回顾与展望[J].材料导报,2005,19(2):76-80. 被引量:206
  • 3苏景新,张昭,曹发和,张鉴清,曹楚南.铝合金的晶间腐蚀与剥蚀[J].中国腐蚀与防护学报,2005,25(3):187-192. 被引量:103
  • 4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:54
  • 5C1NA B M. Reducing the susceptibility of alloys, particularly aluminum alloys, to stess corrosion cracking, US 3856584[P]. 1974.
  • 6OLIVEIRA A F JR, DE BARROS M C, CARDOSO K R, TRAVESSA D N. The effect of RRA on the strength and SCC resistance on AA7050 and AA7150 aluminium alloys[J]. Mater Sci EngA, 2004, 379: 321-326.
  • 7KOMISAROV V, TALIANKER M, CINA B. Effect of retrogression and reaging on the precipitates in an 8090 AI-Li alloy[J]. Mater Sci Eng A, 1998, 242: 39-49.
  • 8ARAN A. Optimization of the strength and intergranular corrosion properties of the 7075 A1 alloy by retrogression and reaging[J]. Z Metallkde, 1989, 3:170-178.
  • 9URAL K. Study of optimization of heat-treatment conditions in retrogression and reaging treatment of 7075-T6 aluminum alloy[J]. Journal of Materials Science Letter, 1994, 13(5): 383-340.
  • 10GB7998-87.铝合金晶间腐蚀测定方法[S].1987.

二级参考文献113

共引文献412

同被引文献318

引证文献29

二级引证文献380

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