期刊文献+

均匀化处理对7150铝合金冲击性能影响 被引量:2

Study of homogenization treatment on 7150 aluminum alloy impact properties
下载PDF
导出
摘要 采用光学显微镜、SEM和冲击试验机研究了均匀化处理后的7150铝合金圆铸锭的冲击性能。7150铝合金圆铸锭晶界存在大量的网状非平衡析出相,在晶粒内部同时也存在部分颗粒状析出相。经过均匀化处理后,晶界与晶粒内部的析出相均出现了回溶现象。铸态晶界处析出相为MgZn2和Al2Cu,经过高温长时间均匀化已大部分回溶,同时仍残留有部分Al6(FeCu)析出相,该相是由不稳定的FeAl6化合物转变而来,均匀化处理对Al6(FeCu)相的形貌及成分未产生影响。经过均匀化热处理后,改变了析出相数量和分布,增加了材料的塑性,试样的抗冲击性能得到提高,更有利于适应恶劣的服役环境。 The impact properties of homogenized 7150 aluminum alloy bar were studied by optical microscope,SEM and impact testing machine.There are a lot of network non-equilibrium precipitates in the grain boundary of 7150 aluminum alloy bar,and some granular precipitates also exist in the grains.After homogenization,the precipitates the grains boundary and in the grain are redissolved.MgZn2 and Al2Cu precipitates at the grain boundary as cast are mostly redissolved after homogenization at high temperature for a long time,while some Al6(FeCu) precipitates remain.This phase is transformed from unstable FeAl6 compound.Homogenization treatment has no effect on the morphology and composition of Al6(FeCu) phase.After homogenization heat treatment,the amount and distribution of precipitates are changed,the plasticity of the material is increased,and the impact resistance of the sample is improved,which is more conducive to adapt to the harsh service environment.
作者 张建宇 王征 王进录 柯伟 陆起高 ZHANG Jian-yu;WANG Zheng;WANG Jin_lu;KE Wei;LU Qi-gao(Yunnan Aluminum Zexin Co.,Ltd.,Qujing 655500,China)
出处 《轻合金加工技术》 CAS 北大核心 2020年第10期14-16,共3页 Light Alloy Fabrication Technology
基金 云南省重大科技专项计划(项目编号:2018ZE005)。
关键词 7150铝合金 均匀化处理 析出相 冲击性能 7150 aluminum alloy homogenization treatment precipitated phase impactproperties
  • 相关文献

参考文献6

二级参考文献53

  • 1杨守杰,戴圣龙.航空铝合金的发展回顾与展望[J].材料导报,2005,19(2):76-80. 被引量:205
  • 2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
  • 3张君尧.航空结构用高纯高韧性铝合金的进度[J].轻金属,1994(6):54-57. 被引量:8
  • 4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:40
  • 5蒙多尔福.铝合金的组织与性能[M].北京:冶金工业出版社,1988..
  • 6Heinz A, Haszler A, Keidel C, et al. Recent development in aluminium alloys for aerospace applications [ J]. Materials Science and Engineering A, 2000, 280:102 - 107.
  • 7William Q E, Michael H V. Method of producing an aluminum alloy product: U S, 4305763 [ PI. 1981 - 12 - 15.
  • 8Brown Melvin H. Producing combined high strength and high corrosion resistance in A1-Zn-Mg-Cu alloys:U S, 4832758 [ P]. 1989 -5 -23.
  • 9Srivatsan T S, Guruprasad G, Vijay K Vasudevan. The quasi static deformation and fracture behavior of aluminum alloy 7150 [ Jl. Materials and Design,2008, 29 : 742 -751.
  • 10Srivatsan T S. The low-cycle fatigue and cyclic fracture behaviour of 7150 aluminium alloy [ J ]. International Journal of Fatigue, 1991, 13 (6) :313 -321.

共引文献39

同被引文献31

引证文献2

二级引证文献6

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