期刊文献+

循环温度场作用下空冷态TC4合金的拉伸性能和显微组织的变化 被引量:4

TENSILE PROPERTIES AND CHANGE IN MICROSTRUCTURE OF AIR COOLED TC4 ALLOY SUBJECTED TO CYCLIC TEMPERATURE FIELD
下载PDF
导出
摘要 对1020、950和900℃空冷的TC4合金在-196~350℃间进行了热循环试验,测定了热循环前后的拉伸性能。结果表明:经1000次热循环后强度上升,塑性下降,合金中的位错密度增大,形变孪晶的数量增多,其中950℃空冷合金的强度上升幅度最大。 The thermal cycling tests between -196 and 350 ℃ were performed on the TC4 alloy air cooled from 1 020, 950 and 900 ℃. The tensile properties before and after thermal cycling were evaluated. Experimental results show that after 1 000 thermal cycles, the strength increases, the ductility decreases and the dislocation density or amount of deformation twins increase, among which the specimens air cooled from 950 ℃ have the largest increase in strength and have the largest residual ductility.
出处 《中国有色金属学报》 EI CAS CSCD 北大核心 1997年第2期90-93,103,共5页 The Chinese Journal of Nonferrous Metals
关键词 钛合金 循环热处理 拉伸性能 显微组织 titanium alloy thermal cycling tensile property microstructure
  • 相关文献

参考文献6

  • 1盛磊,宇航材料工艺,1992年,4卷,27页
  • 2吴运学,宇航材料工艺,1992年,4卷,62页
  • 3李承受,宇航学报,1992年,1卷,1页
  • 4何世禹,Acta Metall Sin,1991年,4卷,A55页
  • 5金峰,宇航材料工艺,1991年,4卷,24页
  • 6邱惠中,宇航材料工艺,1991年,4卷,1页

同被引文献15

  • 1宋志坤,谢基龙,张励忠,李纯华,马小全.铸钢轮材料在700℃~20℃热循环下断裂机制分析[J].铁道学报,2007,29(2):141-144. 被引量:3
  • 2Peng X,Pan W P,Riley J T.A degradation mode of a carbon steel during thermal cycling under a simulated combustion environment[J].MaterialsScience and Engineering A,2002,332(1-2):270-275.
  • 3Horvath W,Prantl W,Werner E,et al.Influence of thermal cycling on the microstructure of a Ferritic-Austeniticduplex stainless steel[J].MaterialsCharacterization,1995,34(4):277-285.
  • 4Song J M,Lui T S,Kao I H,et al.Effect of microstructural refinement on tensile behavior of the AC9A aluminum alloy suffering thermal shock fatigue[J].Scripta Materialia,2004,51(12):1159-1163.
  • 5MEI Hui,CHENG Lai-fei,ZHANG Li-tong.Damage mechanisms of C/SiC composites subjected to constant load and thermal cycling in oxidizingatmosphere[J].Scripta Materialia,2006,54(2):163-168.
  • 6Sharmilee Pal,Bhanuprasad V V,Mitra R.Damage evaluation in discontinuously reinforced aluminum matrix composites subjected to thermal cycling[J].Materials Science and Engineering A,2008,489(1-2):11-20.
  • 7Jiang H,Rong T S,Hu D,et al.Thermal cycling of Ti46Al8Nb1B[J].Intermetallics,2006,14(12):1433-1447.
  • 8徐文娟,操光辉,吴申庆.金属基复合材料的热循环行为[J].材料科学与工程,1999,17(1):39-42. 被引量:5
  • 9刘锋,金恂叔.论航天器的热试验[J].中国空间科学技术,1999,19(6):39-39. 被引量:9
  • 10姜传海,吴建生,王德尊,张榴凤.热循环对20%SiC_w/6061Al复合材料尺寸稳定性的影响[J].金属热处理,2001,26(6):9-11. 被引量:3

引证文献4

二级引证文献11

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