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中间退火及轧制工艺对Al-Mg-Li合金塑性开裂及晶粒细化的影响 被引量:5

Effects of intermediate annealing and rolling on plastic failure and grain refinement of Al-Mg-Li alloy
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摘要 采用机械热处理法制备Al-Mg-Li合金细晶板材,研究预热温度、中间退火温度及转向轧制对板材塑性开裂及晶粒细化的影响。结果表明:板材在低温(≤300℃)轧制时往往开裂,将轧制温度提高到400℃,可获得无开裂的板材,但经再结晶退火后的晶粒组织粗大,约为16μm;降低中间退火温度虽然可以明显提高晶粒细化程度,但退火后采用单向轧制,当形变量较大时,板材会出现开裂问题;中间退火后采用转向轧制,不但大形变量下板材轧制不开裂,而且细化晶粒及减小板材厚度方向层状分布的程度,再结晶后2个表面层的晶粒细小等轴,平均晶粒粒径为9.26μm;中心层晶粒组织相对粗大略成扁平状,平均晶粒粒径为12.73μm,约占板材总厚度的1/5。 Fine grained Al-Mg-Li alloy sheets were produced by thermo-mechanical processing. The effects of preheating temperatures, intermediate annealing temperatures and cross-rolling on failure and grain refinement of an Al-Mg-Li alloy plate were investigated. The results show that low temperature rolling (≤300℃) usually leads to failure of the plate. Non-fractured sheets can be obtained by rolling at the enhancing temperature of 400℃, which results in a coarse grain structure with grain size of about 16 μm after recrystallization. Intermediate annealing at lower temperatures gives rise to finer grains, but if a unidirectional rolling is applied after annealing, cracks occur when the rolling reduction is too large. However, direction-changing rolling after annealing not only eliminates the cracks during deformation but also enhances grain refinement and decreases layer grain structure through the thickness. The surface layer contains fine equiaxed grains of about 9.26μm whereas central layer contains coarse elongated grains of about 12.73μm which accounts for about 1/5 of the whole thickness.
出处 《中南大学学报(自然科学版)》 EI CAS CSCD 北大核心 2009年第1期88-93,共6页 Journal of Central South University:Science and Technology
基金 国际科技合作重点资助项目(2006DFA53250) 国家重大基础研究资助项目(2005CB623706)
关键词 Al-Mg-Li合金 转向轧制 中间退火 晶粒细化 机械热处理 粒子激发形核 Al-Mg-Li alloy cross-rolling intermediate annealing grain refinement thermo-mechanical processing particle stimulated nucleation (PSN)
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参考文献16

  • 1Fridlyander I N. Aluminum alloys in aircraft in the periods of 1970-2000 and 2001-2015[J]. Metal Science and Heat Treatment, 2001, 43(1): 6-10.
  • 2Kaibyshev O A. Superplsticity of alloys, intermetallides, and ceramics[M]. Berbin: Springer Verlag Press, 1992.
  • 3Kaibyshev R, Shipilova K, Musin F, et al. Achieving high strain rate superplasticity in an Al-Li-Mg alloy through equal channel angular extrusion[J]. Materials Science and Technology, 2005, 21(4): 408-418.
  • 4Wang Z C, Prangnell P B. Microstructure refinement and mechanical properties of severely deformed A1-Mg-Li alloys[J]. Materials Science and Engineering A, 2002, A328(1): 87-97.
  • 5Furukawa M, Berbon P B, Horita Z, et al. Ageing hardening and the potential for superplasticity in a fine-grained Al-Mg-Li-Zr alloy[J]. Metallurgical and Materials Transactions A, 1998, 29A(1): 169-177.
  • 6Kaibyshev R, Shipilova K, Musin F, et al. Continuous dynamic recrystallization in an Al-Li-Mg-Sc alloy during equal-channel angular extrusion[J]. Materials Science and Engineering A, 2005, A396(2): 341-351.
  • 7Mazilkin A A, Myshlyaev M M. Microstructure and thermal stability of superplastic aluminium-lithium alloy after severe plastic deformation[J]. Journal of Materials Science, 2006, 41(12): 3767-3772.
  • 8杜予晅,张新明.强变形制备超细晶金属材料的方法[J].材料导报,2006,20(F11):241-244. 被引量:11
  • 9李献民,崔建忠,胡忠式,徐祝萍,周清燕.01420合金的超塑变形行为[J].材料研究学报,2000,14(3):318-320. 被引量:6
  • 10王淑云,张晓博,崔建忠,张彩培.两种Al-Mg合金超塑性能的对比研究[J].热加工工艺,1997,26(1):20-22. 被引量:5

二级参考文献67

  • 1张新明,肖蓉,杜予晅,唐建国.1420铝锂合金的温压变形及动态再结晶行为[J].中南大学学报(自然科学版),2006,37(4):629-634. 被引量:10
  • 2王淑云,张晓博,崔建忠,张彩培.两种Al-Mg合金超塑性能的对比研究[J].热加工工艺,1997,26(1):20-22. 被引量:5
  • 3胡俊.Al-Mg-Li合金组织性能的研究:硕士论文[M].东北大学,1989..
  • 4王淑云.高Mg铝合金超塑性的研究:硕士论文[M].东北大学,1996..
  • 5蒋兴钢.高强铝合金超塑性的研究:博士论文[M].东北大学,1990..
  • 6吴诗淳.金属超塑性变形理论[M].北京:国防工业出版社,1997.115.
  • 7林兆荣.金属超塑性的成型原理及应用[M].北京:航空工业出版社,1980.150.
  • 8王淑云,张晓博,崔建忠,张彩培.Al-Mg-Li-Zr合金超塑性能的研究[J].轻金属,1997(5):50-52. 被引量:6
  • 9吴诗淳,金属超塑性变形理论,1997年,115页
  • 10王淑云,硕士学位论文,1996年

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