首页> 外文期刊>The International Journal of Advanced Manufacturing Technology >A complete study on satellite thruster structure (STS) manufactured by a hybrid manufacturing (HM) process with integration of additive and subtractive manufacture
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A complete study on satellite thruster structure (STS) manufactured by a hybrid manufacturing (HM) process with integration of additive and subtractive manufacture

机译:一种完整的卫星推进器结构(STS)采用杂交制造(HM)工艺制造,添加剂和减法制造

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摘要

Recently, the fact that hybrid manufacturing (HM) combines different manufacturing processes mechanism of additive and subtractive processes has gained significant attentions. This work attempts to study a process of HM in order to overcome the disadvantages of each manufacturing process. Selective laser melting (SLM) of ANSI 316L stainless and machining are used as the additive and subtractive manufacturing process, respectively, in this work. Firstly, the mechanical properties and the standard samples manufactured by HM are analyzed. The results show that the finished surface roughness has no apparent influence on the tensile strength. The tensile strength of HM is reduced in comparison with the substrate materials. The yield strength of HM is higher than the substrate material. And the heat treatment is beneficial for the mechanical properties improvement. Further, the geometrical feature structure manufacture complexity indices (GFS-MCIs) are defined and calculated from the computer-aided design (CAD) model. In reference to GFS-MCIs, a satellite thruster structure (STS) is analyzed and decomposed into two geometrical feature structures. Based on the result of GFS-MCIs, STS is manufactured by HM approach as a complete component.
机译:最近,混合动力制造(HM)结合了不同制造方法的添加剂和减法过程的事实已经取得了显着的关注。这项工作试图研究HM的过程,以克服每个制造过程的缺点。在这项工作中,ANSI 316L不锈钢和加工的选择性激光熔融(SLM)用作添加剂和减法制造过程。首先,分析由HM制造的机械性能和标准样品。结果表明,成品表面粗糙度对拉伸强度没有明显影响。与基材材料相比,HM的拉伸强度降低。 HM的屈服强度高于基材材料。热处理有利于机械性能改善。此外,从计算机辅助设计(CAD)模型定义和计算了几何特征结构制造复杂性指数(GFS-MCIS)。参考GFS-MCI,分析卫星推进器结构(STS)并分解成两个几何特征结构。基于GFS-MCI的结果,STS是通过HM方法作为完整组成的。

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