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在热模拟试验机上进行高温压缩实验,研究了含β相的Ti-42Al-9V-0.3Y合金的高温变形行为,分析了其不连续屈服行为的产生机理.研究表明,含β相的Ti-42Al-9V-0.3Y合金的主要热变形软化机制为β相的动态回复和γ相的动态再结晶,高温变形过程的不连续屈服行为与β相的动态回复和γ相中超位错(Burgers矢量b=1/2〈112〉)的增殖相关.基于Orowan方程建立的位错动力学模型可合理解释该合金不连续屈服的产生原因,证实可动位错密度的快速增加和低的位错速度应力敏感系数m*容易诱发TiAl合金的不连续屈服.合金在较低温度(1100-1150℃)和较高应变速率(1 s-1)下产生波动屈服归因于位错滑移和孪晶交互作用.

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