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Microstructure of CrMnNi Cast Steel After Explosive-Driven Flyer-Plate Impact at Room Temperature and Below

机译:室温及以下爆炸驱动飞板撞击后CrMnNi铸钢的组织

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摘要

A low-carbon metastable austenitic CrMnNi cast steel was investigated under shock conditions in a flyer-plate impact test. The samples were impacted by aluminum flyer-plates with impact velocities of 620 +/- A 30 m/s. Depending on deformation temperature and strain rate, the material exhibited different deformation mechanisms (dislocation glide, martensitic transformation, and mechanical twinning), which determined the microstructural evolution and mechanical behavior. Flyer-plate impact tests were carried out at 213 K and 293 K (-60 A degrees C and +20 A degrees C). A soft recovered sample revealed microstructural changes directly after impact. The subsequent microstructural investigations via light-optical microscopy and scanning electron microscopy revealed that transformation-induced plasticity (TRIP effect) was the primary deformation mechanism. Moreover, it was possible to quantify the martensite volume fraction by different methods and to identify the hcp epsilon-martensite phase as an intermediate transformation stage. A decrease in temperature also increased the driving force for the martensitic transformation.
机译:在飞板冲击试验中,在冲击条件下研究了低碳亚稳态奥氏体CrMnNi铸钢。样品被铝制飞行器板撞击,撞击速度为620 +/- A 30 m / s。取决于变形温度和应变速率,材料表现出不同的变形机理(位错滑移,马氏体转变和机械孪晶),这决定了微观组织的演变和力学行为。飞板冲击试验在213 K和293 K(-60 A摄氏度和+20 A摄氏度)下进行。回收的软样品在冲击后立即显示出微结构变化。随后通过光学显微镜和扫描电子显微镜进行的显微结构研究表明,转变诱导的可塑性(TRIP效应)是主要的变形机制。此外,有可能通过不同的方法对马氏体体积分数进行定量,并将hcpε-马氏体相鉴定为中间转化阶段。温度的降低也增加了马氏体相变的驱动力。

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