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Effects of heat treatment on the nanoscale precipitation behavior of 7055 aluminum alloy under dynamic shock

机译:热处理对动态冲击下7055铝合金纳米级沉淀行为的影响

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This study is intended to examine the effects of heat treatment on the microstructural evolution of 7055 aluminum, an area rarely reached by previous studies. Considering that 7055 aluminum alloy belongs to the aging hardening type, the difference of heat treatment process will lead to a large difference in mechanical properties and microstructure of the materials. Dynamic shock test is conducted on the alloy after treated by T6 and T6I4 processes. The result demonstrates that before dynamic shock, the precipitates on the grain boundary of T4-state alloy are fine, straight and continuously, and the precipitation-free zones (PFZs) around the grain boundary are quite narrow; the precipitates on the grain boundary of T6I4-state alloy are spheroidized and discontinuous, and the PFZs around the grain boundary are quite broad. Under room temperature, the dispersed grains of T4-state alloy are large in size while those of T-6I4-state alloy are finer with concentrated, very dense dislocations around the dispersed grains. The dislocation density displays an obvious positive correlation to the strain rate: The larger the strain rate, the higher the dislocation density. After dynamic shock at 6000s-1, the dislocations are tangled into dislocation walls and the dislocation cells shrink in size. More dislocation cells form in T6I4-state alloy than in T4-state alloy. Under high temperatures, the dislocation density displays an obvious negative correlation to the dynamic shock temperature: As the dynamic shock temperature increases, the dislocation density in the alloy decreases significantly. Under 120 degrees C, the dislocation density in T4-state specimen increases. A lot of the dislocations are tangled into dislocation walls. Dislocation walls as well as cellular substructures occur in T6I4-state alloy. Under 320 degrees C, a lot of irregular dislocation networks appear in T6-state alloy, and these dislocations are obstructed by coarsening precipitates; the precipitates in the
机译:本研究旨在检测热处理对7055铝的微观结构演进的影响,这是先前研究很少达到的区域。考虑到7055铝合金属于老化硬化型,热处理过程的差异将导致材料的机械性能和微观结构差异。在T6和T6I4处理处理后,在合金中对动态冲击试验进行动态冲击试验。结果表明,在动态冲击之前,T4-态合金的晶界面上的沉淀物是细,直线和连续的,并且晶界周围的沉淀区域(PFZ)非常窄; T6i4-状态合金的晶界面上的沉淀物是球化和不连续的,并且晶界周围的PFZ非常宽。在室温下,T4-态合金的分散晶粒的尺寸大,而T-6i4-状态合金的浓缩粒子较好,在分散的晶粒周围浓缩,非常致密的脱位。位错密度显示出与应变速率明显的正相关:应变率越大,位错密度越高。在6000s-1处动态冲击后,脱位缠结成位错壁,位错细胞尺寸缩小。在T6I4 - 状态合金中形成更多位错细胞,而不是T4-状态合金。在高温下,位错密度显示出与动态冲击温度明显的负相关:随着动态冲击温度的增加,合金中的位错密度显着降低。在120摄氏度下,T4状态样本中的位错密度增加。很多脱臼都纠结成位错墙。位错壁以及蜂窝子结构发生在T6I4 - 状态合金中。在320℃下,在T6状态合金中出现大量不规则的位错网络,并且这些脱位通过粗化沉淀物阻碍;沉淀物中的沉淀物

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