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Effect of Aging Treatment on the Initiation and Propagation of Fatigue Cracks in the Ti-15V-3Al-3Sn-3Cr Metastable β Titanium Alloy

机译:时效处理对Ti-15V-3Al-3Sn-3Cr亚稳β钛合金疲劳裂纹萌生和扩展的影响

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The scope of this study is the investigation of the effect of microstructure on fatigue behavior of Ti-15V-3Al-3Sn-3Cr (Ti 15–3) metastable beta titanium alloy. Aging treatment was applied to Ti 15–3 alloy at low and high aging temperatures. The fatigue crack initiation and propagation behavior of the alloy was determined by applying fatigue crack propagation tests under constant amplitude loading. Fatigue crack propagation in the solution treated sample showed a propagation due to grain boundaries, while the aging treated samples were affected by the homogeneous distribution and size of the $a$ phases. The fatigue crack propagation rate decreased with increasing aging time due to the formation of $a$ phases at low temperatures for long periods. At high aging temperatures, the increase in the aging time caused the $a$ phases to grow and the $a$ platelets amount to decrease. This situation created an inhomogeneous distribution of $a$ phases in the microstructure and adversely affected the fatigue behavior of the sample. The highest rate of fatigue crack propagation was observed in 450°C 10 hour sample, while the lowest rate of fatigue crack propagation was obtained in 300°C 10 hours sample.
机译:本研究的范围是研究微观结构对Ti-15V-3Al-3Sn-3Cr(Ti 15-3)亚稳β钛合金疲劳行为的影响。在较低和较高的时效温度下对Ti 15-3合金进行时效处理。通过在恒定振幅载荷下进行疲劳裂纹扩展测试来确定合金的疲劳裂纹萌生和扩展行为。在固溶处理后的样品中,疲劳裂纹扩展表现为晶界扩展,而时效处理后的样品则受均匀分布和尺寸的影响。 $ a $ 阶段。疲劳裂纹扩展速率随着时效时间的增加而降低,这是由于形成了 $ a $ 相长期处于低温状态。在较高的老化温度下,老化时间的增加导致了 $ a $ 成长的阶段 $ a $ 血小板数量减少。这种情况造成了 $ a $ 微观结构中的相变对样品的疲劳行为有不利影响。在450°C 10小时样品中观察到最高的疲劳裂纹扩展速率,而在300°C 10小时样品中观察到了最低的疲劳裂纹扩展速率。

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