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首页> 外文期刊>Journal of Materials Science >Fatigue crack propagation and in-situ observations in three tool steel alloys manufactured using a rapid solidification technique
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Fatigue crack propagation and in-situ observations in three tool steel alloys manufactured using a rapid solidification technique

机译:使用快速凝固技术制造的三种工具钢合金的疲劳裂纹扩展和原位观察

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摘要

By utilizing special manufacturing conditions, e.g., using only pure elements and applying a rapid cooling rate, tool materials with high quasi-static fracture toughness can be produced. However, tool materials are often subjected to cyclic loading and, hence, their lifetime is dominated by fatigue failure. This study is focused on fracture mechanics and in-situ experiments to characterize the fatigue crack propagation behavior of three newly developed tool steels at a stress ratio R of 0.05. Microstructural examinations revealed that the materials consist of the phases α′-martensite, retained austenite, and complex carbides in different amounts. Results of preliminary tests are presented, in which it was attempted to grow the crack in a plane parallel to the plane of the starter notch. The determined a??K threshold values ranged between 4 and 5 MPa√m with Paris-Erdogan exponents of 3.3-4.6. In-situ observations were performed to understand the inherent damage mechanisms and microstructural effects during fatigue loading. These observations showed that fatigue crack growth is mainly dominated by the ductility of the martensitic-austenitic matrix. Only in cases in which the primary carbides are oriented favorably (with respect to the direction of crack propagation) does the crack follow the coherent carbide network to a certain extent. Furthermore, for the first time, a phase transformation from retained austenite to α′-martensite was detected at the crack tip during fatigue crack propagation for the material group of tool steels.
机译:通过利用特殊的制造条件,例如仅使用纯元素并施加快速的冷却速率,可以生产具有高准静态断裂韧性的工具材料。但是,工具材料经常承受循环载荷,因此,其寿命主要取决于疲劳失效。这项研究集中于断裂力学和原位实验,以表征三种新开发的工具钢在应力比R为0.05时的疲劳裂纹扩展行为。显微组织检查表明,材料由不同数量的α'-马氏体相,残余奥氏体和复杂的碳化物组成。给出了初步测试的结果,其中试图在平行于起动器缺口平面的平面上扩展裂纹。所确定的ΔεK阈值范围为4至5MPa√m,巴黎-埃尔多安指数为3.3-4.6。进行了现场观察,以了解疲劳载荷过程中的固有损伤机理和微观结构效应。这些观察表明,疲劳裂纹扩展主要由马氏体-奥氏体基体的延展性决定。只有在一次碳化物的取向良好(相对于裂纹扩展的方向)的情况下,裂纹才在一定程度上遵循相干碳化物网络。此外,工具钢材料组在疲劳裂纹扩展过程中,首次在裂纹尖端检测到从残余奥氏体到α'马氏体的相变。

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