期刊文献+

Tensile and high-cycle fatigue properties of spray formed Al10.8Zn2.9Mg1.9Cu alloys after two-stage aging treatment 被引量:4

Tensile and high-cycle fatigue properties of spray formed Al10.8Zn2.9Mg1.9Cu alloys after two-stage aging treatment
下载PDF
导出
摘要 Based on the investigation of the tensile properties of spray formed ultra-high strength Al10.8Zn2.9Mg1.9Cu alloys, the high-cycle fatigue properties under different theoretical stress concentration factors were investigated, the fatigue fracture surfaces and microstructures were observed, and the fatigue mechanism was discussed. The results indicate that the ultimate tensile strength of spray formed Al10.8Zn2.9Mg1.9Cu alloys can reach up to 730?740 MPa, and the elongation is about 8%?10% under the condition of two-stage aging treatment. For the stress ratio is 0.1, the maximum stress for 107 cycles is over 400 MPa and 120 MPa, when the theoretical stress concentration factor is 1 and 3, respectively. Based on the investigation of the tensile properties of spray formed ultra-high strength Al10.8Zn2.9Mg1.9Cu alloys, the high-cycle fatigue properties under different theoretical stress concentration factors were investigated, the fatigue fracture surfaces and microstructures were observed, and the fatigue mechanism was discussed. The results indicate that the ultimate tensile strength of spray formed Al10.8Zn2.9Mg1.9Cu alloys can reach up to 730-740 MPa, and the elongation is about 8%-10% under the condition of two-stage aging treatment. For the stress ratio is 0.1, the maximum stress for 107 cycles is over 400 MPa and 120 MPa, when the theoretical stress concentration factor is 1 and 3, respectively.
出处 《中国有色金属学会会刊:英文版》 CSCD 2006年第4期808-812,共5页 Transactions of Nonferrous Metals Society of China
基金 Project(2001AA332030) supported by the National High-Tech Research and Development Program of China
关键词 Al10.8Zn2.9Mg 1.9Cu 铝合金 喷镀成形 高循环疲劳性能 时效处理 Al10.8Zn2.9Mg 1.9Cu alloy spray forming ultra-high strength aluminum alloy high-cycle fatigue properties
  • 相关文献

参考文献3

二级参考文献22

  • 1Lukasak D A, Hart R M. Strong aluminum alloy shave airframe weight[J]. Advanced Materials and Processes, 1991, 10: 46.
  • 2Fridlyander I N.Russian aluminum alloys for Aeroepace and transport applications[J]. Materials Sci. Forum, 2000, 331-337 : 921.
  • 3Schaffer G B, Huo S H. On development d sintered 7XXX series aluminum alloys[J]. Powder Metallurgy, 1999, 42(3) : 219.
  • 4Srivatsan T S, Vasudevan V K. Temperature and the ductility,deformation, and fracture of A1 7055[J]. JOM, 1999, 1 : 42.
  • 5Leatham A G.Spray forming: alloys, products, and markets[ A ]. Fourth Intemation Conference on Spray forming[ C ]. Baltimore, USA, 1999.
  • 6Lengsfeld P, Juarez J A, Lavemia E J, et al. Microstructure and mechanical behavior of spray deposited Zn modified 7XXX Al alloys[J]. Inter. J. Rap. Sol., 1995, 8: 237.
  • 7Wei Qiang, Xiong Baiqing, Zhang Yongan. Production of high strength ALZnMgCu alloys by spray forming process[ J ]. Trans.Nonferrous Met. Soc. China, 2001, 11(2): 258.
  • 8团体著者,1979年
  • 9宋仁国,Acta Metall Mater,1996年,44卷,3241页
  • 10宋仁国,矿冶工程,1996年,16卷,68页

共引文献35

同被引文献76

引证文献4

二级引证文献1

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