TC4ELI钛合金二次退火后的疲劳对比试验

The Fatigue Contrast Test on TC4ELI Titanium Alloy Secondary Annealed

  • 摘要: 对两种状态的TC4ELI钛合金进行疲劳对比试验,分析二次退火对疲劳性能的影响。结果表明,当最大疲劳应力为0.8Rp0.2及以上时,二次退火工艺可以提高TC4ELI钛合金的疲劳寿命,小于0.8Rp0.2时,对其疲劳寿命没有明显影响;当最大疲劳应力在0.8Rp0.2及以上时,位错容易产生滑移,经过二次退火之后,TC4ELI钛合金的等轴α组织增加、β转变组织的含量减少、α/β两相界面减小,位错滑移程增加,从而延迟裂纹的萌生;当最大疲劳应力低于0.8Rp0.2时,二次退火降低了抵抗位错运动的晶格强度,在晶格强度与位错滑移程的共同影响下,裂纹在萌生阶段的寿命没有明显变化。

     

    Abstract: Effects of secondary annealing on fatigue performances of two groups of TC4ELI titanium alloys (annealed and secondary annealed) were studied.The results showed that secondary annealing could prolong the fatigue life of TC4ELI titanium alloy when the maximum fatigue stress was 0.8Rp0.2 or above, while the fatigue life changed little when the maximum fatigue stress was less than 0.8Rp0.2; that when the maximum fatigue stress was no lower than 0.8Rp0.2, the dislocation was prone to slip, and after the secondary annealing, the equiaxed α-structure of TC4ELI titanium alloy increasesd, β-transformed structure and the interface between the α/β phases decreased, and the dislocation slip path increasesd, which delayed the initiating of cracks; that when the maximum fatigue stress was lower than 0.8Rp0.2, secondary annealing reduced the lattice strength which resisted the movement of dislocation, and under the effects of lattice strength and dislocatial slip path, the fatigue life of crack at initiation stage didn't change significantly.

     

/

返回文章
返回