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铝含量和退火温度对锆铝合金相组成和力学性能的影响 被引量:3

Effect of Al Content and Annealing Temperature on Phase Compositions and Mechanical Properties of ZrAl Alloys
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摘要 利用非自耗电弧炉熔炼了Al含量为6.0%,7.0%,8.0%(质量分数)的锆铝二元合金,通过退火过程中的包析反应得到了不同相组成的Zr3Al基合金,借助光学显微镜、XRD分析研究了合金的金相组织和相组成,进行了显微硬度测定和拉伸试验。结果表明:铸态的锆铝合金显微硬度随着铝含量的增加而增大;退火可得到组织均匀的Zr3Al基合金,其显微硬度和抗拉强度主要与相组成和基体晶粒大小有关,而与第二相的形态无关;合金的显微硬度、抗拉强度随着Zr3Al相的增多而增大,延伸率随着Zr3Al相的增多而减小;合金的显微硬度、抗拉强度和延伸率随着Zr3Al晶粒的细化而不同程度地增大。 ZrAl alloys with three different Al contents (6.0, 7.0, 8.0, wt%) were melted by the non-consumable electric-arc furnace. Zr3Al-based alloys with different phase compositions were obtained by peritectoid reaction during the annealing process. Microstructures and phase compositions of alloys was studied by optical microscope and XRD, and then its microhardnesses and tensile properties were tested. The results show that the microhardness of as-cast ZrAl alloys increases with the increase of Al content. Homogeneous microstructure of Zr3Al-based alloys can be obtained by annealing. Its microhardness and tensile strength are relative to matrix grain size and phase composition, but independent of the form and distribution of the second phases. Microhardness and tensile strength of the annealed alloy increase with the increase of Zr3Al content, while the elongation decreases. In addition, microhardness, tensile strength and elongation of the annealed alloys increase with Zr3Al grain refinement. Key words: Zr3Al-based alloys; annealing; phase composition; mechanical properties
出处 《稀有金属材料与工程》 SCIE EI CAS CSCD 北大核心 2014年第9期2227-2231,共5页 Rare Metal Materials and Engineering
基金 国家重点基础研究发展规划('973'计划)(2010CB731600) 河北省博士后科研项目择优资助
关键词 Zr3Al基合金 退火 相组成 力学性能 Zr3Al-based alloys annealing phase composition mechanical properties
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  • 1ZhangYonggang(张永刚),HanYafang(韩雅芳),ChenGuoliang(陈国良).lntermetallics Structural Materials(金属间化合物结构材料)[M].Beijing: National Defense Industry Press, 2001:619.
  • 2HuangBoyun(黄伯云).lntermetallics of Titanium Aluminides(钛铝基金属间化合物)[M].Changsha:Central South University Press,1999:22.
  • 3Tribble A. The Space Environment-lmplications for Spacecraft Design[M]. Princeton: Princeton University Press, 1995:25.
  • 4Yang C, Wang W K, Liu R Pet al. Journal of Spacecraft and Rockets[J], 2006, 43:565.
  • 5张喜燕,朱玉涛,叶林凤,刘庆,李聪,邱绍宇,李中奎.Zr-4合金表面变形纳米结构TEM研究[J].稀有金属材料与工程,2009,38(3):506-509. 被引量:7
  • 6杨志南,刘峰超,闫志刚,张福成.退火对热轧和冷轧Zr705组织及硬度影响(英文)[J].稀有金属材料与工程,2013,42(2):254-258. 被引量:6
  • 7Sorensen B R, Kimsey K D, Love B M. International Journal of lmpact Engineering[J], 2008, 35:1808.
  • 8LiuJianzhang(刘建章).Nuclear Structure Materials(核结构材料)[M].Beijing:Chemical Industry Press,2007:27.
  • 9LuanBaifeng(栾佰峰),YuHongbing(余泓冰),HuangTianlin(黄天林)et al.稀有金属材料与工程[J],2012,41(2):357.
  • 10刘文庆,钟柳明,彭剑超,刘仁多,姚美意,周邦新.锆合金中第二相的研究[J].稀有金属材料与工程,2011,40(7):1216-1219. 被引量:13

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