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Shock-Induced Mechanical Response and Substructural Evolution of Ti-6Al-4V Alloy

机译:Ti-6Al-4V合金的冲击诱导的机械响应和副结构演化

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The effects of shock stress amplitude on the post-shock mechanical response and substructural evolution of Ti-6Al-4V alloy are investigated within the impact stress range of 6-10 GPa. The reload yield behavior of post-shock Ti-6Al-4V does not exhibit enhanced shock-induced strengthening at an effective strain level even if the shock stress achieves 10 GPa. The residual substructures of post-shock Ti-6Al-4V are examined by transmission electron microscopy. Results reveal that planar slip is the dominant deformation mechanism of this alloy during shock loading pulse. Dislocations tangle and form developed dislocation clusters (planar slip bands) with increased impact stress. The lack of dislocation cells or cell-like structures, high-density twins and additional strengthening phases limits the shock-induced strengthening effect in post-shock materials. However, dislocation multiplication and tangles lead to increased yield strength and strain hardening rate of reloaded materials.
机译:在6-10GPa的冲击应力范围内研究了冲击应力振幅对Ti-6Al-4V合金后冲击机械响应和副结构演化的影响。即使冲击应力达到10GPa,休克后Ti-6AL-4V的重载产量行为也没有表现出在有效应变水平上提高的冲击引起的强化。通过透射电子显微镜检查后冲击后Ti-6Al-4V的残留副结构。结果表明,平面滑移是震动加载脉冲期间该合金的主导变形机制。脱位缠绕并形成具有增加的冲击压力的脱位簇(平面滑动带)。缺少位错细胞或细胞样结构,高密度双胞胎和额外的强化阶段限制了休克后物质中的冲击诱导的强化效果。然而,位错倍增和缠结导致屈服强度和重新装载材料的应变硬化速率增加。

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