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J Chin Soc Corr Pro  2010, Vol. 30 Issue (4): 313-316    DOI:
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EXPERIMENTAL RESEARCH ON FATIGUE PROPERTY OF WELDED JOINTS OF BT20 TITANIUM ALLOY IN CORROSION ENVIRONMENT
BAO Juncheng, ZHAO Jie, WANG Zhiqi, MA Xu
School of Materials Science and Engineering, Tianjin University of Technology, Tianjin 300384
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Abstract  

The axial loading fatigue testing results show that the fatigue life of welded joints of BT20 titanium alloy decreased under the condition of salt fog, SO2 and salt fog at different stress radio and stress concentration factor K t=1. The loss of fatigue life was obvious in acidic of SO2 and salt fog. As stress ratio R changsed from 0.5 to 0.06 at fatigue life N=105, wet air made fatigue strength decreases 18%,salt fog made fatigue strength decreases 16%, SO2 and salt fog made fatigue strength decreases 7%.

Key words:  BT20 titanium alloy, welding joint      corrosion environment      fatigue strength      fatigue life     
Received:  03 March 2009     
ZTFLH: 

TG405

 
Corresponding Authors:  BAO Juncheng     E-mail:  old_bao@sina.com

Cite this article: 

BAO Juncheng, ZHAO Jie, WANG Zhiqi, MA Xu.
EXPERIMENTAL RESEARCH ON FATIGUE PROPERTY OF WELDED JOINTS OF BT20 TITANIUM ALLOY IN CORROSION ENVIRONMENT. J Chin Soc Corr Pro, 2010, 30(4): 313-316.

URL: 

https://www.jcscp.org/EN/     OR     https://www.jcscp.org/EN/Y2010/V30/I4/313

[1] Zhang Q L, Li X W.Effect of structure on fatigue properties and fracture toughness for TA15 titanium alloy [J] Mater. Eng., 2007, (7): 3-5
    (张庆玲,李兴无.TA15钛合金两类组织对疲劳性能和断裂韧度的影响 [J], 材料工程, 2007, (7): 3-5)
[2] Jin L, Su B. Research on low cycle fatigue properties of TA15 titanium alloy [J]. J.Aeronaut. Mater., 2005, 25(2): 16-19
    (金磊, 苏彬. TA15合金低周疲劳性能研究 [J]. 航空材料学报, 2005,25(2):16-19)
[3] Wu C Z, Li X W, Huang X, et al. Relationship of fatigue crack propagation and microstructure for TA15 alloy [J]. Rare Met. Mater. Eng., 2007, 36(12): 2128-2131
    (吴崇周,李兴无,黄旭等. TA15钛合金疲劳裂纹扩展与显微组织的关系 [J]. 稀有金属材料与工程, 2007. 36(12): 2128-2131)
[4] Lee H K. Fracture resistance of a steel weld joint under fatigue loading [J]. Eng. Fract. Mech., 2000, 66: 403-419
[5] Gao Z T. Fatigue Statistics [M]. Beijing.National Defense Industry Press. 1980: 1
    (高镇同.疲劳统计学 [M].北京: 国防工业出版社,1980: 1)
[6] Speidel M O, Blackburn M J. Beck T R, et al. Corrosion fatigue and stress corrosion crack growth in high strength aluminum alloys,magnesium alloys and titanium alloys exposed to aqueous solutions [A]. In: Devereux O, McEvily A J, Staehle R W, eds., Corrosion Fatigue: Chemistry,Mechanics and Microstructure [M]. NACE, 1972, 324-345
[7] Shimojo M, Higo Y, Nunomura S.Relation between the amount of fresh bare surface at the crack tip and the  fatigue crack propagation rate [J]. ISIJ lnt., 1991, 31:870-874
[8] Meyn D A.An analysis of frequency and amplitude effects on corrosion fatigue crack propagation in Ti-8Al-1Mo-1V [J]. Metall. Trans., 1971, 2:853-865
[9] Peters M, Gysler A, Tjering G L. Influence of texture on fatigue properties of Ti-6Al-4V [J]. Metall. Trans., 1984, 15A:1597-1605
[10] Nakasa K, Satoh H. The effect of hydrogen charging on the fatigue crack propagation behavior of β-titanium alloys [J]. Corros. Sci., 1996,38:457-468
[11] Venkataraman G, Goolsby A D.Hydrogen embrittlement in titanium alloys from cathodic polarization in offshore environments, and its mitigation [A]. Corrosion/96 [C]. NACE, 1996, 554
[12] Shipilov S A. Mechanisms for corrosion fatigue crack propagation [J]. J. Chin. Soc. Corros. Prot., 2004, 24(6): 321-331
     (Shipilov S A. 腐蚀疲劳裂纹扩展的机理 [J]. 中国腐蚀与防护学报, 2004, 24(6): 321-331)

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