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7075高强度铝合金多级时效处理及微观组织分析 被引量:4

Analysis on Multistage Aging Treatment and Microstructure of 7075 High Strength Al Alloy
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摘要 以7075系高强度铝合金挤压材为研究对象,对比合金的力学性能(强度、韧性、断裂韧性)、微观组织,并重点研究了其固溶处理后的双级时效热处理工艺。结果表明,7075挤压材采用适宜的双级时效热处理工艺后具有良好的综合性能,其抗剥落腐蚀性能优于T6单级人工时效状态的性能,在保证强度满足设计要求的前提下,提高了7075型材的抗应力腐蚀性能。 7075 series high strength aluminum alloy was taken as the research object, and the mechanical properties (strength, ductility and fracture ductility) and microstructure were compared. The heat-treatment technics of double-grade aging after solution treatment was researched. The results show that after double-grade aging heat-treatment, 7075 extrusion has good mechanical properties, whose exfoliation-corrosion-resistance property is better than those after T6 single-grade artifical aging, and stress-corrosion-resistance property of the 7075 extrusion is improved when the strength meets the design requirement.
出处 《热加工工艺》 CSCD 北大核心 2013年第12期190-191,196,共3页 Hot Working Technology
基金 河南省第八批重点学科"机械制造及其自动化"资助项目(2012SJGLX289)
关键词 高强度铝合金 微观组织 固溶处理 双级时效 high strength aluminum alloy microstructure solution treatment double-grade aging
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  • 1吴一雷,李永伟,强俊,李春玉.超高强度铝合金的发展与应用[J].航空材料学报,1994,14(1):49-55. 被引量:90
  • 2库德良绍夫ВГ 高云震等(译).铝合金断裂韧性[M].北京:冶金工业出版社,1980..
  • 3Tanguy D, Bayle B, Dif R, et al. Hydrogen effects during SCC propagation of Al-5Mg in 30g/l NaCl solution [ A]. Mater Sci Forum [ C ]. Swizerland:2000 Trans Tech Publications, 2000. 1479 ~ 1488.
  • 4Albrecht J, Thompson A W, Beenstein I M. The role of microstructure in hydrogen-assisted fracture of 7075 aluminum [J]. Metall Trans A, 1979, 10A(11): 1759~ 1766.
  • 5John Liu, Michael Kulak. A new paradigm in the design of aluminum alloys for aerospace applications [ A ]. Mater Sci Forum [ C ]. Swizerland: 2000 Trans Tech Publications, 2000. 127 ~ 140.
  • 6Uguz A, Martin J W. The effect of retrogression and reageing on the ductile fracture toughness of Al-Zn-Mg alloys containing different dispersoid phases [J].J Mater Sci, 1995, 30:5923 ~ 5926.
  • 7Tsai T C, Chang J C, Chuang T H. Stress corrosion cracking of superplastically formed 7475 aluminum alloy [J]. Metall Mater Trans A, 1996, 28A(10):2113 ~ 2121.
  • 8Fleck P, Calleros D, Madsen M, et al. Retrogression and reaging of 7075 T6 aluminum alloy [ A ]. Mater. Sci. Forum [ C ]. Swizerland: 2000 Trans Tech Publications, 2000. 649~ 654.
  • 9Cina B. US Patent 3856584, 1974.
  • 10TaliankerM, Cina B. Retrogression and reageing and the role of dislocations in the stress corrosion of 7000-type aluminum alloy[J]. Metall Trans A, 1989,20A(10): 2087 ~ 2092.

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