田宁, 宋晓云, 叶文君, 惠松骁. SP700钛合金热变形行为及组织演变[J]. 工程科学学报, 2024, 46(4): 676-683. DOI: 10.13374/j.issn2095-9389.2023.03.09.004
引用本文: 田宁, 宋晓云, 叶文君, 惠松骁. SP700钛合金热变形行为及组织演变[J]. 工程科学学报, 2024, 46(4): 676-683. DOI: 10.13374/j.issn2095-9389.2023.03.09.004
TIAN Ning, SONG Xiaoyun, YE Wenjun, HUI Songxiao. Hot deformation behavior and microstructure evolution of SP700 titanium alloy[J]. Chinese Journal of Engineering, 2024, 46(4): 676-683. DOI: 10.13374/j.issn2095-9389.2023.03.09.004
Citation: TIAN Ning, SONG Xiaoyun, YE Wenjun, HUI Songxiao. Hot deformation behavior and microstructure evolution of SP700 titanium alloy[J]. Chinese Journal of Engineering, 2024, 46(4): 676-683. DOI: 10.13374/j.issn2095-9389.2023.03.09.004

SP700钛合金热变形行为及组织演变

Hot deformation behavior and microstructure evolution of SP700 titanium alloy

  • 摘要: 采用Gleeble3800热模拟试验机对SP700钛合金进行热压缩试验,研究合金在变形温度为800~880 ℃、应变速率为1~10 s–1、压缩变形量为30%和50%条件下的流变行为及显微组织演变. 结果表明,随着变形温度升高和应变速率降低,SP700钛合金热压缩变形的峰值流变应力降低. 合金在800 ℃压缩变形时,流变应力曲线呈明显的动态软化,其显微组织中α片层逐渐破碎球化,部分α片层发生动态再结晶. 随变形温度升高,合金压缩真应力–应变曲线呈稳态流变状态. 在相同变形温度下,随应变速率和压缩变形量增加,α片层球化程度增加. 热变形过程中,平行于压缩轴的α片层在压应力作用下弯曲扭折,片层内取向差不连续存在,并于不连续处存在新α/α界面. 垂直于压缩轴的α片层在压应力作用下界面发生起伏,片层内部存在累积取向差. 在界面起伏处β相楔入α片层,最终导致α片层的破碎球化.

     

    Abstract: The hot compression test of SP700 titanium alloy was performed using a Gleeble3800 thermal simulation test machine, and the thermal deformation behavior and microstructure evolution were examined in the temperature range of 800–880 °C, strain rate range of 1–10 s−1, and compression deformation of 30%–50%. The findings reveal that the peak flow stress of the SP700 titanium alloy decreases with increasing deformation temperature but increases with increasing strain rate. At a deformation temperature of 800 ℃, the flow stress curves demonstrate evident dynamic softening features with a rapid decrease in flow stress after the peak stress. By metallographic and scanning electron microstructure observations of the deformed microstructure, the α lamellar is gradually broken and spheroidized, and dynamic recrystallization occurs. With increasing deformation temperature, the induced phase transformation occurs, which leads to the dissolution of the α phase and an increase in the volume fraction of the β phase. The degree of recrystallization of the β phase increases with several β recrystallization grains at the grain boundaries, whereas the degree of globularization of the α lamellae decreases with increasing temperature. As the deformation temperature increases to 880 ℃, the flow stress curves exhibit steady flow. Recrystallization behavior preferentially occurs in the β grains, while the α lamellar remains flat without globularization behavior. That is, recrystallization of the β phase occurs under the test deformation conditions. For the α lamellae, when the deformation temperature is constant, the degree of spheroidization of the α lamellae increases with strain rate and compression deformation. During the hot deformation process, the α lamellae parallel to the compression axis kink, and the cumulative misorientation is discontinuous inside the α lamellae. At the discontinuous points, the new α/α interface boundary is produced, which causes the formation of unstable dihedral angles. To lower the surface tension energy, the β phase wedges into the α lamellae, which eventually results in the break of the α lamellae. For the α lamellae perpendicular to the compression axis, the interface fluctuates, resulting in continuous cumulative misorientation inside the α lamellae. When the rotation axis of the lamellae changes, a new α/α interface boundary is produced. At the interface fluctuation or the new α/α interface, the β phase easily wedges into the α lamellae by element diffusion, which finally causes fragmentation and spheroidization. Moreover, some of the α lamellae experience a shear deformation, leading to fragmentation under compression.

     

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