期刊文献+

TC17合金焊接接头显微组织与疲劳裂纹扩展特性 被引量:5

Microstructure and Fatigue Crack Growth Characteristics of Welded Joints of TC17 Titanium Alloy
下载PDF
导出
摘要 研究了TC17钛合金惯性摩擦焊焊接接头的疲劳裂纹扩展规律,并利用光学显微镜、扫描电镜对材料的显微组织和断口形貌进行分析。结果表明:TC17钛合金母材为α+β网篮状组织,晶粒较大;焊缝区和热影响区内可以看到明显的原β相晶界,焊缝区的原β晶粒较细小,热影响区的原β晶粒较粗大,晶粒内部存在细小的α相。在室温下,当ΔK≤15 MPa.m1/2时,焊缝区疲劳裂纹扩展速率较小,而当ΔK≥15 MPa.m1/2时,焊缝区的扩展速率最大,其次是热影响区,母材的裂纹扩展速率最小;在高温下,焊接接头各部位的裂纹扩展速率相差不大,均小于室温。 The fatigue crack growth rate of inertia friction welded joints of TC17 titanium alloy was studied.The microstructure and the fracture surface were analyzed by means of optical microscopy and scanning electron microscopy.The results show that the microstructure of TC17 titanium alloy is α+β phase with bigger grain.The microstructure of weld zone and heat affected zone is tiny α phase and clear β phase grain boundary,the original β grain of weld zone is smaller,the original β grain of heat affected zone is bigger.At room temperature;when ΔK≤15 MPa·m1/2,the fatigue crack growth rate of weld zone is smaller;when ΔK≥15 MPa·m1/2,the fatigue crack growth rate of weld zone is the largest.The next is heat affected zone,the growth rate of parent metal is the smallest.At high temperature,the fatigue crack growth rate of different parts of welded joints shows little difference,but all lower than those tested at room temperature.
出处 《宇航材料工艺》 CAS CSCD 北大核心 2010年第6期81-85,共5页 Aerospace Materials & Technology
  • 相关文献

参考文献8

  • 1吴冰,李晋炜,巩水利,张建勋.TC17钛合金电子束焊接接头的疲劳裂纹扩展规律及疲劳剩余寿命[J].稀有金属材料与工程,2009,38(A03):170-174. 被引量:12
  • 2何胜春,张田仓.TC17钛合金惯性摩擦焊接头组织特征分析[J].焊接,2008(4):61-63. 被引量:3
  • 3GB/T 6398-2000.金属材料疲劳裂纹扩展速率试验方法[S],2000.
  • 4陶春虎等.航空发动机转动部件的失效与预防[M]国防工业出版社,2000.
  • 5Material Properties Handbood:Titanium Alloy. . 1994
  • 6Nakajima K,,Terao K,Miyata T.The effect of micro-structure on fatigue crack propagation ofα+βtitanium. Mate-rials Science and Engineering . 1998
  • 7Wu A P,Zou G S,Ren J L,et al.Microstructure and mechanical properties of Ti-24Al-17Nb ( at. %) laser beam welding joints. Intermetallics . 2002
  • 8Filip R,Kubiak K,Ziaja W,et al.The effect of microstructure on the mechanical properties of two-phase titanium alloys. Journal of Materials . 2003

二级参考文献9

  • 1宋西平,孟为如,邵潭华,王士元,刘效方.TC4钛合金惯性摩擦焊焊缝微观组织形成的研究[J].材料工程,1996,24(2):24-26. 被引量:5
  • 2Wood Favor. Titanium Handbook(钛合金手册)[M].Chongqing: Chongqing Science Technology Press, 1983.
  • 3E A. Titanium Alloy Metallography(钛合金金相学)[M].Beijing: National Defense Industry Press, 1986.
  • 4China Aeronautical Materials Handbook's edit committee( 《中国航空材料手册》编辑委员会).China Aeronautical Materials Handbook, The Forth Book(中国航空材料手册)[M].Beijing:National Standard Press, 2002:179.
  • 5Wu Bing, Li Jinwei. Engineering Structural Integrity: Research, Development and Application, Proceeding of Ninth International Conference on Engineering Structural Integrity Assessment[C], Beijing: China Machine Press, 2007:673.
  • 6Liu Changfu(刘长福).The Constitution of Aeroengine(航空发动机构造)[M].Beijing:National Defence Industry Press,1989.97.
  • 7《中国航空材料手册》编辑委员会.中国航空材料手册(第4卷).钛合金[M].北京:中国标准出版社,2001.
  • 8莱茵斯 C,皮特尔斯 M.陈振华译.钛与钛合金[M].化学工业出版社.2005.81-120.
  • 9姚泽坤,郭鸿镇,刘建超,苏祖武,姜明,应志毅,刘建宇,崔健.双性能钛合金压气机盘的成形机理[J].中国有色金属学报,2000,10(3):378-382. 被引量:19

共引文献13

同被引文献40

引证文献5

二级引证文献16

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