选择性激光熔化
多孔性
航空航天
过程(计算)
3D打印
热等静压
材料科学
工艺工程
火箭(武器)
选择性激光烧结
机械工程
制造工程
计算机科学
复合材料
航空航天工程
烧结
工程类
微观结构
操作系统
作者
Joshua Herrick,Andrew Younglove,Chris Sharp
标识
DOI:10.1115/detc2022-92015
摘要
Abstract This paper looks to explore how variances in printing process parameters affect the density, porosity, and mechanical properties of additively manufactured GRCop-42, ultimately providing additional testing for this novel material. Since increased porosity can be correlated to decreased part performance, it is imperative that additive manufacturing companies understand what combination of printing parameters in the Selective Laser Melting process result in near fully dense parts. GRCop-42 presents an opportunity for the aerospace industry to make significant advancement in liquid rocket engine design. Currently there have been few studies published concerning additively manufactured GRCop-42 outside of NASA, making additional testing on vendor specific processes paramount. The GRCop-42 specimens tested in this paper were provided by i3D-MFG, a metal additive manufacturing company based in Redmond Oregon. As to not compromise their specific testing parameter sets the specimens have been codified. From the testing conducted on additive manufactured GRCop-42 for this paper, it was shown that variances in printing process parameters had significant effects on the porosity, and consequently the mechanical properties. With the addition of post processes such as Hot Isostatic Pressing, near fully dense parts were achieved. The intention of this publication is to provide an initial understanding of this new material in an effort to support its broader use in academia and industry.
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