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Simulation and experiments of abrasive assisted electrochemical jet machining of SiC reinforced aluminum matrix composites

机译:SiC增强铝基基复合材料磨料辅助电化学喷射加工的仿真与实验

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Silicon carbide reinforced aluminum matrix composites (SiCp/Al) exhibit excellent properties and performance in fields of aerospace, electronic packaging, precision instrumentation and automotive industry. The SiC_p/Al composites are hard-to-machine materials due to different physical properties between reinforcement material and matrix material. This study investigated the removal mechanism of the reinforcement in abrasive assisted electrochemical jet machining (AECJM) of SiCp/Al composites through simulation and experiments. The results show that the lifetime of the bonding interface between SiC and matrix significantly decreases with lowering of the bonding area. For a given bonding area, the lifetime of that is proportional to the SiC size. Therefore, the material removal rate is markedly influenced by the SiC particle size. The SiC reinforcement can be extracted out when the bonding area drops off to a low level. This results in many micro pits left at the machined surface. The roughness of the surface is highly related to the number and size of these micro pits. Larger size of or higher volume fraction of the reinforcement will result in rougher machined surfaces.
机译:碳化硅增强铝基复合材料(SICP / AL)在航空航天,电子包装,精密仪表和汽车行业领域表现出优异的性能和性能。由于增强材料和基质材料之间的不同物质,SiC_P / Al复合材料是难以加入的材料。本研究通过模拟和实验研究了SICP / Al复合材料的磨料辅助电化学喷射加工(AECJM)中加固的去除机理。结果表明,在粘接区域降低的情况下,SiC和基质之间的粘合界面的寿命显着降低。对于给定的粘合区域,这的寿命与SiC尺寸成比例。因此,材料去除率明显受到SiC粒径的影响。当粘合区域掉落到低电平时,可以提取SiC加强件。这导致许多微坑在加工表面处留下。表面的粗糙度与这些微坑的数量和尺寸高度相关。较大尺寸或更高体积的加强件将导致粗糙的机加工表面。

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