张明达,曹京霞,周毅,邓瑞刚,史栋钢,黄旭. Ti6242合金微观组织差异及其演变对拉伸和疲劳性能影响[J]. 航空制造技术, 2021, 64(1/2): 14-20. ZHANG Mingda,CAO Jingxia,ZHOU Yi,DENG Ruigang,SHI Donggang,HUANG Xu. Effects of Microstructure Difference and Evolution on Tensile and Fatigue Properties of Ti6242 Alloy. Aeronautical Manufacturing Technology, 2021, 64(1/2): 14-20.
ZHANG Mingda, CAO Jingxia, ZHOU Yi, et al. Effects of Microstructure Difference and Evolution on Tensile and Fatigue Properties of Ti6242 Alloy[J]. Aeronautical Manufacturing Technology, 2021, 64(1/2).
张明达,曹京霞,周毅,邓瑞刚,史栋钢,黄旭. Ti6242合金微观组织差异及其演变对拉伸和疲劳性能影响[J]. 航空制造技术, 2021, 64(1/2): 14-20. ZHANG Mingda,CAO Jingxia,ZHOU Yi,DENG Ruigang,SHI Donggang,HUANG Xu. Effects of Microstructure Difference and Evolution on Tensile and Fatigue Properties of Ti6242 Alloy. Aeronautical Manufacturing Technology, 2021, 64(1/2): 14-20. DOI: 10.16080/j.issn1671-833x.2021.01/02.014.
ZHANG Mingda, CAO Jingxia, ZHOU Yi, et al. Effects of Microstructure Difference and Evolution on Tensile and Fatigue Properties of Ti6242 Alloy[J]. Aeronautical Manufacturing Technology, 2021, 64(1/2). DOI: 10.16080/j.issn1671-833x.2021.01/02.014.
Effects of Microstructure Difference and Evolution on Tensile and Fatigue Properties of Ti6242 Alloy
The mechanical properties of the near-alpha titanium alloys Ti6242 alloy disc forgings usually have close relationship with the original microstructure of bars. In this study
three kinds of Ti6242 alloy bars with different original microstructure were selected to quantitatively analyze the difference and evolution of different microstructure characteristics
including the forged state
the solid solution state and the solid solution and aging state. The effects of the microstructure difference and evolution on the mechanical properties were also compared. The results showed that the differences of primary α phase volume fraction reduced after similar solid solution and aging treatment process
while the sectional area distribution and shape distribution of primary α phase still retained some differences. Room temperature tensile mechanical properties showed no significant difference
while the low fatigue property and dwell fatigue property exhibited significant difference. According to the microstructure difference analysis and mechanical property results
the original microstructure of bar with fine
non-equiaxed and no obvious orientation primary alpha phase contributed to good fatigue properties.
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Related Institution
School of Aeronautics, Northwestern Polytechnical University
National Key Laboratory of Aircraft Configuration Design, Northwestern Polytechnical University