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INFLUENCE OF MICROSTRUCTURE OF ALLOY 718 ON HIGH STRAIN RATE DEFORMATION

机译:合金718微观结构对高应变速率变形的影响

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There are a number of situations where alloys for aero engines undergo deformation with high strain rates, e.g. during metal cutting. To understand, model and predict the behaviour we need knowledge of high strain rate behaviour, but also understand the influence of the microstructures. The material investigated is Alloy 718, a precipitate heat treatable nickel base alloy, heat treated to generate four microstructures; small and large grain size, aged and solution treated condition. Split Hopkinson was used for high strain rate compression testing; the strain rates tested in tensile and compression ranges 0.001-3000 s~(-1). To describe the deformation, the Johnson Cook material model was optimized for each microstructure. Present microstructure is influencing the stress response more than the strain rate and the different microstructures deform in slightly different manner where small grains tend to deform in primary glide and large grains deform in both primary and secondary glide systems.
机译:有许多情况,适用于Aero发动机的合金经历高应变率的变形,例如,在金属切割期间。要了解,模型和预测我们需要了解高应变率行为的行为,还可以理解微观结构的影响。研究的材料是合金718,沉淀热处理镍基合金,热处理以产生四种微观结构;小而大的粒度,老化和溶液处理条件。 Split Hopkinson用于高应变速率压缩测试;在拉伸和压缩中测试的应变速率范围为0.001-3000S〜(-1)。为了描述变形,为每个微观结构进行了优化了Johnson Cook材料模型。目前的微观结构是影响压力响应大于应变速率,并且不同的微观结构变形,略微不同的方式,其中小晶粒在初级滑动和大晶粒中变形,在初级滑动系统和次级滑行系统中变形。

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