期刊文献+

等温自由锻温度对7085铝合金组织与性能的影响 被引量:7

Effects of isothermal free forging temperature on microstructure and properties of 7085 aluminum alloy
在线阅读 下载PDF
导出
摘要 通过金相组织观察、扫描电镜分析和室温拉伸力学性能及剥落腐蚀实验,分析探讨等温自由锻温度对7085铝合金显微组织、力学性能和剥落腐蚀的影响。研究结果表明:在370℃和400℃等温自由锻时,合金发生严重再结晶,强度较低,伸长率稍高,剥蚀抗力较差;在420℃锻造时,合金出现大量细小且分布均匀的亚晶粒,抗拉强度、屈服强度、伸长率和剥蚀抗力均较好,分别达到533.2MPa,495MPa,13.3%和EA。在450℃锻造时,该合金的晶粒开始长大,强度下降,伸长率稍有升高,剥蚀抗力较差。综合考虑显微组织、强度、塑性和剥落腐蚀等因素,确定420℃为合金等温自由锻最佳锻造温度。 The microstructure, mechanical and corrosion property of 7085 aluminum alloy deformed at different isothermal free forging temperatures were analyzed using optical microscope (OM), scanning electron microscope (SEM), mechanical tensile test and exfoliation corrosion. The experimental results show that serious recrystallization occurs at 370 ℃ or 400 ℃, resulting in the strength severely decreases, the elongation increases slightly and exfoliation corrosion gets worse. At 420 ℃, the alloy exhibits small and uniform sub-grain structure, leading to better strength, elongation and exfoliation resistance. The ultimate strength, yield strength and elongation achieve 533.2 MPa, 495 MPa and 13.3%, respectively. Exfoliation corrosion grade reaches EA. While the deformation temperature rises 450 ℃, the grains begin to grow up. The strength and exfoliation resistance decrease, but the elongation increases slightly. Considering the factors of microstructure, strength, plastic and exfoliation resistance, 420 ℃ is determined to be the best isothermal free forging temperature.
出处 《中南大学学报(自然科学版)》 EI CAS CSCD 北大核心 2012年第3期900-905,共6页 Journal of Central South University:Science and Technology
基金 国家重点基础研究发展计划("973"计划)项目(2012CB619502 2010CB731701) 国家自然科学基金委员会创新研究群体科学基金资助项目(51021063)
关键词 7085铝合金 等温自由锻 再结晶 显微组织 力学性能 剥蚀抗力 7085 aluminum alloy isothermal free forging recrystallization microstructure mechanical properties exfoliation resistance
  • 相关文献

参考文献16

  • 1王祝堂 田荣璋.铝合金及其加工手册[M].长沙:中南工业大学出版社,1996..
  • 2邱惠中,吴志红.航天用高性能金属材料的新进展[J].宇航材料工艺,1996,26(2):18-23. 被引量:30
  • 3Warner T. Recently-developed aluminum solutions for aerospace applications[J]. Mater Sci Forum, 2006, 519/520/521(2): 1271-1278.
  • 4Miller W S, Zhuang L, Bottema J, et al. Recent development in aluminium alloys for the automotive industry[J]. Mater Sci Eng A, 2000, 280(3): 37-49.
  • 5Starke E A, Staley J T. Application of modem aluminum alloys to aircraft[J]. Progress in Aerospace Science, 1996, 32(2/3): 131.
  • 6Chakrabarti D J, Liu J, Sawtell R R, et al. New generation highstrength high damage tolerance 7085 thick alloy product with low quench sensitivity[C]//Proceedings of ICAA9. Melbourne: Institute of Materials Engineering Australasia Ltd, 2004: 969-974.
  • 7陈文.先进铝合金在A380上的应用[J].航空维修与工程,2005(2):40-41. 被引量:43
  • 8John L. Advanced aluminum and hybrid aerostructure for future aircraft[J]. Mater Sci Forum, 2006, 519: 1271-1278.
  • 9刘鸣,郭鸿镇,梁业,姚泽坤,阙基蓉,方清万.等温锻造温度对2B70铝合金组织性能的影响[J].热加工工艺,2008,37(5):9-11. 被引量:8
  • 10Robson J D, Prangnell P B. Predicting the recrystallized volume fraction in AA7050 hot rolled plate[J]. Materials Science and Technology, 2002, 18(6): 607-619.

二级参考文献39

共引文献159

同被引文献95

引证文献7

二级引证文献29

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