期刊文献+

成分微调对中强钛合金组织与力学性能的影响 被引量:4

Effect of Composition Minor Modification on Microstructure and Mechanical Properties of Middle-Strength Titanium Alloy
下载PDF
导出
摘要 通过成分微调在Ti-6Al-4V合金基础上发展了一种基于Ti-Al-V-Si四元系TC4S两相钛合金。研究表明,添加少量合金元素Si,并对Al,V元素含量进行微调,使新合金的主要力学性能得到提高,强度、塑性和断裂韧性得到良好匹配,从而满足了设计要求。TC4S合金可以在不明显降低塑性和韧性的前提下,比Ti-6Al-4VELI合金的强度提高80MPa^100MPa。 A new alloy belonging to Ti-AI-V-Si system has been developed on the base of Ti-6Al-4V, designated as TC4S. Experimental test results show that mechanical properties of TC4S have been improved evidently by proper adjusting the contents of Al and V, adding small amount of Si when compared with conventional Ti-6Al-4V alloy. The satisfied match among the strength, the ductility and the fracture toughness of the alloy has been reached, and meets the requirements of the design. The strength of TC4S alloy can be increased by 60 MPa-100 MPa on the condition of the slight damaging its plasticity and toughness, compared with Ti-6Al-4V ELI.
出处 《稀有金属材料与工程》 SCIE EI CAS CSCD 北大核心 2007年第3期480-483,共4页 Rare Metal Materials and Engineering
基金 国家重大自然科学基金项目(50434030) "863"高技术项目(2002AA305107)资助
关键词 钛合金 TI-6AL-4V TC4S 显微组织 力学性能 titanium alloy Ti-6Al-4V TC4S microstructure mechanical properties
  • 相关文献

参考文献10

  • 1Martin Patrick Lyle. Titanium Alloy Having Enhanced Notch Toughness and Method of Producing Same[P]. American Invention Patent, USP6190473, 2001.
  • 2张永强 陶海林 冯永琦.稀有金属材料与工程,2005,34(3):498-498.
  • 3朱知寿,马少俊,王新南,童路,吴学仁,赵永庆,曲恒磊.TC4-DT损伤容限型钛合金疲劳裂纹扩展特性的研究[J].钛工业进展,2005,22(6):10-13. 被引量:50
  • 4李辉,曲恒磊,赵永庆,冯亮,郭红超,周伟.Ti-6Al-4V ELI合金板材的显微组织与力学性能研究[J].钛工业进展,2005,22(6):24-27. 被引量:6
  • 5张延生,胡洋海,马英,徐祝萍.热处理对Ti-6Al-4V棒材固溶时效性能的影响[J].钛工业进展,2005,22(6):18-23. 被引量:8
  • 6ATI Allegheny Technology. Technical Data Sheet TI-040-Allvac Titanium 6Al-4V Alloy [M]. Monroe, NC 28110-5030, USA: ATI Properties Inc, 2004:1.
  • 7ATI Allegheny Technology. Technical Data Sheet TI-020-Allvac Titanium 6Al-4V ELI Alloy [M]. Monroe, NC 28110-5030, USA: ATI Properties Inc, 2004:1.
  • 8曲恒磊,赵永庆,朱知寿..一种低成本损伤容限钛合金及其制备方法[P]....CNP200510001210.3..2005..
  • 9郭萍 赵永庆 吴玮璐.稀有金属材料与工程,2005,34(3):526-526.
  • 10曲恒磊 赵永庆 周廉.稀有金属材料与工程,2006,35(1):181-181.

二级参考文献13

  • 1曹春晓.选材判据的变化与高损伤容限钛合金的发展[J].金属学报,2002,38(z1):4-11. 被引量:104
  • 2吴学仁.飞机结构金属材料力学性能手册[M].北京:航空工业出版社,1996..
  • 3Rodney Boyer,Gerhard Welsch,Coilings E W.Material Properties Handbook:Titanium Alloy[M].PA:ASM International Materials Information Society,1994:256.
  • 4BK亚力山大etal (宁兴龙译).钛合金半成品加工[M].西安:稀有金属杂志社,1984.203.
  • 5Wanhill R J H.Damage Tolerance Engineering Property Evaluations of Aerospace Aluminium Alloys with Emphais on Fatigue Crack Growth[M].New York:NLR Technical Publication,1990.
  • 6中国航空材料手册编辑委员会.中国航空材料手册(第二版)[M].北京:中国标准出版社,2002..
  • 7CampbellJE UnderwoodJH GerberichWW (汪一麟 邵本逑译).断裂力学在选材方面的应用[M].北京:冶金工业出版社,1992..
  • 8Atsushi Sugeta,Yoshihiko Uematsu,Masahiro Joho.Fatigue Crack Growth Behavior on Ti-6Al-4V Alloys under Variable Amplitude Load Sequences[C].In:Blom A F.Fatigue 2002,Proceedings of the Eighth International Fatigue Congress.Stockholm:EMAS,2002:2911.
  • 9SureshS(王中光译).材料的疲劳[M].北京:国防工业出版社,1993..
  • 10Yuen.Correlations between Fracture Surface Appearance and Fracture Mechanics Parameters for Stage-Ⅱ Fatigue Crack-Propagation in Ti-6Al-4V[J].Metallurgical Transactions,1996,5(8):1833.

共引文献57

同被引文献34

引证文献4

二级引证文献14

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