FENG Pingfa, LIU Jiahui, WANG Zibiao, FENG Feng, ZHANG Xiangyu, SHEN Yue, ZHANG Jianfu, WANG Jianjian, WU Zhijun, YU Dingwen. Experimental Study on Residual Stress and Fatigue Life of TB6 Titanium Alloy Connection Hole After Cold Expansion[J]. Aeronautical Manufacturing Technology, 2023, 66(11): 14-21.
FENG Pingfa, LIU Jiahui, WANG Zibiao, FENG Feng, ZHANG Xiangyu, SHEN Yue, ZHANG Jianfu, WANG Jianjian, WU Zhijun, YU Dingwen. Experimental Study on Residual Stress and Fatigue Life of TB6 Titanium Alloy Connection Hole After Cold Expansion[J]. Aeronautical Manufacturing Technology, 2023, 66(11): 14-21. DOI: 10.16080/j.issn1671-833x.2023.11.014.
Experimental Study on Residual Stress and Fatigue Life of TB6 Titanium Alloy Connection Hole After Cold Expansion
Aiming at the connection hole of TB6 titanium alloy
the strengthening effect of cold expansion parameters on titanium alloy lug samples was studied. Plastic deformation
residual stress and surface roughness of the hole expanded with different ratios and times were characterized. The tension-tension fatigue life of lug samples before and after cold expansion was tested. Morphology characteristics of fatigue fracture and the reasons for the improvement of fatigue life were analyzed. The results show that cold expansion can hardly improve the surface quality of the hole
but can cause severe plastic deformation of the hole wall and introduce compressive residual stress. With the increase of expansion ratio
the plastic deformation
the peak value and depth of compressive residual stress increase significantly and the attenuation rate decreases
while expansion times has less impact. The fatigue life of lug samples after cold expansion is significantly improved
and the fatigue limit of cold expansion with 3% expansion ratio is increased by at least 38%.