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Crystal plasticity assessment of crystallographic Stage Ⅰ crack propagation in a Ni-based single crystal superalloy

机译:基于Ni基单晶超合金中晶体阶段Ⅰ裂纹繁殖的晶体塑性评估

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摘要

Stage I fatigue crack propagation along crystallographic slip planes was experimentally and analytically investigated in a single crystal Ni-base superalloy, NKH-304. Fatigue crack propagation tests at room temperature were conducted using four types compact specimens with different combinations of primary and secondary orientations. It was revealed in the experiment that the fatigue crack propagated along crystallographic slip planes in a mixed mode with Mode I, II and III components. The mixture ratio and fatigue crack propagation rate were strongly influenced by the primary and secondary crystal orientations. To interpret the effect of crystal orientations on the Stage I cracking behavior, a crystal plasticity finite element analysis was conducted considering the actual geometry of the crystallographic crack planes. The slip activities of the individual octahedral slip systems were evaluated, and then a damage parameter was proposed based on the critical plane approach. As a result, a reasonable explanation was obtained for the effect of crystal orientations on the cracking path and propagation rate of the crystallographic Stage I cracking.
机译:实验和分析在单晶Ni碱超合金,NKH-304中研究了沿着晶体滑架的舞台裂纹裂缝繁殖。使用具有不同组合的初级和次级取向的不同组合进行室温在室温下疲劳裂纹繁殖试验。在实验中揭示了沿着混合模式的疲劳裂纹在具有模式I,II和III组分的混合模式中传播的疲劳裂纹。混合比和疲劳裂纹繁殖速率受到初级和二级晶体取向的强烈影响。为了解释晶体取向对阶段I开裂行为的影响,考虑到晶体裂纹平面的实际几何形状进行晶体塑性有限元分析。评估各个八面体滑动系统的滑移活性,然后基于临界平面方法提出损伤参数。结果,获得了合理的解释,用于晶体取向对晶体阶段I开裂的裂缝路径和传播速率的影响。

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