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Author:

Fang, Wei-Ping (Fang, Wei-Ping.) | Chen, Lun (Chen, Lun.) | Shi, Yao-Wu (Shi, Yao-Wu.) | Yu, Wen-Jun (Yu, Wen-Jun.) | Mao, Zhi-Yong (Mao, Zhi-Yong.) | Tang, Zhen-Yun (Tang, Zhen-Yun.)

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EI Scopus PKU CSCD

Abstract:

The damage tolerance titanium alloys, such as Ti-6Al-4V ELI, TC4-DT, TC21 and TA15 ELI alloys, were summarized. The development process and the new study of damage tolerance titanium alloy were introduced. It pointed out that Ti-6Al-4V ELI alloy was successfully used in the airplane manufacture industry in foreign countries. However, TC4-DT, TC21 and TA15 ELI alloys were still under research in our country. The fracture toughness and fatigue crack propagation rate properties of TC4-DT, TC21 and TA15 ELI alloys were importantly discussed in detail. The lamellar microstructure was beneficial to improve the damage tolerance properties of titanium alloys.

Keyword:

Aluminum alloys Titanium alloys Fracture toughness Fatigue crack propagation Damage tolerance Research Applications

Author Community:

  • [ 1 ] [Fang, Wei-Ping]College of Materials Science and Engineering, Beijing University of Technology, Beijing 100124, China
  • [ 2 ] [Fang, Wei-Ping]Key Laboratory of High Energy Density Beam Processing Technology, Beijing Aeronautical Manufacturing Technology Research Institute, Beijing 100024, China
  • [ 3 ] [Chen, Lun]Representative Office of Naval, Chengdu Aircraft Industrial Group Co., Ltd., Chengdu 610092, China
  • [ 4 ] [Shi, Yao-Wu]College of Materials Science and Engineering, Beijing University of Technology, Beijing 100124, China
  • [ 5 ] [Yu, Wen-Jun]Chengdu Aircraft Industrial Group Co., Ltd., Chengdu 610092, China
  • [ 6 ] [Mao, Zhi-Yong]Key Laboratory of High Energy Density Beam Processing Technology, Beijing Aeronautical Manufacturing Technology Research Institute, Beijing 100024, China
  • [ 7 ] [Tang, Zhen-Yun]Key Laboratory of High Energy Density Beam Processing Technology, Beijing Aeronautical Manufacturing Technology Research Institute, Beijing 100024, China

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Source :

Journal of Materials Engineering

ISSN: 1001-4381

Year: 2010

Issue: 9

Page: 95-98

Cited Count:

WoS CC Cited Count: 0

SCOPUS Cited Count:

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count:

Chinese Cited Count:

30 Days PV: 7

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