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Stress-strain characteristics of linear friction welding of TC11 and TC17 alloys 被引量:1
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作者 赵鹏康 傅莉 +2 位作者 张田仓 钟德超 王佩艳 《China Welding》 EI CAS 2015年第1期13-17,共5页
Abstract Transient stress and strain fields of dissimilar titanium alloys (TCll and TC17 ) joint during linear friction welding ( LFW) were investigated by a two-dimensional model with ABAQUS/Explicit. The results... Abstract Transient stress and strain fields of dissimilar titanium alloys (TCll and TC17 ) joint during linear friction welding ( LFW) were investigated by a two-dimensional model with ABAQUS/Explicit. The results showed that in the X-axis, the maximum compressive stress of 850 MPa occurred in the center zone of friction interface , and the maximum tensile stress of 190 MPa distributed at the flash; in the Y-axis, the maximum compressive stress of 1 261 MPa located at the junction region between the welding fixture and edge of the specimen, and the maximum tensile stress of 320 MPa distributed in the connecting portion between the flash and edge of the specimen. In addition, areas of plastic strain increased gradually during welding process. In the X-axis, tensile strain mainly existed at the heads of the specimens; in the Y-axis, compressive strain mainly occurred at the heads of the specimens. 展开更多
关键词 linear friction welding TC11/tc17 titanium alloys joint stress and strain fields
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High-temperature failure mechanism and defect sensitivity of TC17 titanium alloy in high cycle fatigue 被引量:2
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作者 Gen Li Chengqi Sun 《Journal of Materials Science & Technology》 SCIE EI CAS CSCD 2022年第27期128-140,共13页
Crack initiation is an essential stage of fatigue process due to its direct effect on fatigue failure.However,for titanium alloys in high-temperature high cycle fatigue(HCF),the crack initiation mechanisms remain uncl... Crack initiation is an essential stage of fatigue process due to its direct effect on fatigue failure.However,for titanium alloys in high-temperature high cycle fatigue(HCF),the crack initiation mechanisms remain unclear and the understanding for the defect sensitivity is also lacking.In this study,a series of fatigue tests and multi-scale microstructure characterizations were conducted to explore the high-temperature failure mechanism,and the coupled effect of temperature and defect on TC17 titanium alloy in HCF.It was found that an oxygen-rich layer(ORL)was produced at specimen surface at elevated temperatures,and brittle fracture of ORL at surface played a critical role for surface crack initiation in HCF.Besides,internal crack initiation with nanograins at high temperatures was a novel finding for the titanium alloy.Based on energy dispersive spectroscopy,electron backscatter diffraction and transmission electron microscope characterizations,the competition between surface and internal crack initiations at high temperatures was related to ORL at surface and dislocation resistance in inner microstructure.The fatigue strengths of smooth specimens decreased at elevated temperatures due to the lower dislocation resistance.While the fatigue strengths of the specimens with defect were not very sensitive to the temperatures.Finally,a fatigue strength model considering the coupled effect of temperature and defect was proposed for TC17titanium alloy. 展开更多
关键词 tc17 titanium alloy High temperature DEFECT High cycle fatigue Oxygen-rich layer Rough area
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