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时效温度对TB15钛合金微观组织和力学性能影响

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采用扫描电镜、电子背散射衍射仪、X射线衍射仪和万能材料试验机等研究了不同时效温度对固溶态的TB15钛合金组织和力学性能的影响.结果表明:合金在单相区固溶后,组织主要由等轴β晶粒组成,在较低温度时效后,基体析出了针状α相和等温ω相,在β晶界附近出现无析出区(PFZ),随着时效温度的升高,PFZ和ω相消失,α相由针状向片状形貌转变,在晶界附近出现了晶界魏氏体α相(αWGB).随时效温度的增加,合金硬度降低,抗拉强度先升高后下降,伸长率则相反.在500℃时效后合金抗拉强度达到峰值1431.73 MPa,但伸长率仅为3.82%;在530℃时效时合金获得较好的综合力学性能,此时的抗拉强度为1155 MPa,伸长率为7.21%.
Effects of Aging Temperature on Microstructure and Mechanical Properties of TB15 Titanium Alloy
The effects of different aging temperatures on the microstructure and mechanical properties of TB15 titanium alloy in solid solution were investigated by scanning electron microscopy, electron backscatter scatter diffraction, X-ray diffraction and universal material testing machine. The results show that, the alloy is mainly composed of equiaxed β grains after solution in the single phase zone. After aging at lower temperature, needle-like α phase and isothermal ω phase precipitate in the matrix, and a precipitation-free zone (PFZ) appears near the β grain boundary. With the increase at aging temperature, the PFZ and ω phases disappear, α phase changes from needle-like morphology to lamellar morphology, and α phase of grain boundary Widmanstätten (αWGB) appears near the grain boundary. With the increase of aging temperature, the hardness of the alloy decreases, the tensile strength increases first and then decreases, while the elongation is on the contrary. After aging at 500℃, the tensile strength of the alloy reaches the peak of 1431.73 MPa, but the elongation is only 3.82%. When the alloy is agedat530℃,the comprehensive mechanical properties are better,the tensile strength is 1155 MPa and the elongation is 7.21%.

TB15 titanium alloyaging temperaturemicrostructuremechanical properties

况云华、辛周媛、徐勇、朱琳、陈乐平

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航空工业江西洪都航空工业集团有限责任公司, 江西 南昌 330063

南昌航空大学 航空制造工程学院, 江西南昌 330063

TB15钛合金 时效温度 微观组织 力学性能

航空科学基金江西省重点研发计划

2020Z04705600320202BBEL53012

2024

热加工工艺
中国船舶重工集团公司热加工工艺研究所 中国造船工程学会船舶材料学术委员会

热加工工艺

CSTPCD北大核心
影响因子:0.55
ISSN:1001-3814
年,卷(期):2024.53(4)
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