Abstract
AbstractMetal-filled polymers can serve as the starting material to produce complex metal structures using the cost-effective additive manufacturing process Fused Filament Fabrication (FFF). In this process, the filaments consisting of polymer binders (e.g., polylactic acid (PLA)) and micropowder of highly conductive metals (e.g., copper) are extruded through a nozzle to build up the desired geometry layer by layer. The manufacturability of a complex copper coil for use in satellite actuators with two commercially available filaments (Electrifi and Filamet Copper) using FFF was investigated and the electrical conductivity of the printed material was determined. A design of experiment with variation of extruder temperature and printing speed was used to evaluate different parameter sets. The selected parameter set was then used to produce cuboids to determine the electrical conductivity and an exemplary coil geometry. While the coil could be printed in two sizes (original and enlarged by a factor of two) with one of the investigated filaments, this was not possible with the other filament because the printed material was not dimensionally stable with the selected process parameter set. For the Electrifi filament, that is electrically conductive without post processing, the material achieved a maximum electrical conductivity of $$5.59 \cdot 10^{ - 3} {\text{\% IACS }}\left( {0.033{ }\Omega {\text{cm}}} \right)$$
5.59
·
10
-
3
\% IACS
0.033
Ω
cm
. This was in alignment with other published results for this filament. The other filament Filamet Copper is not conductive in the as-built state. After debinding and sintering, the material achieved a maximum electrical conductivity of $$45.84{\text{\% IACS}} \left( {3.77 \cdot 10^{ - 6} { }\Omega {\text{cm}}} \right)$$
45.84
\% IACS
3.77
·
10
-
6
Ω
cm
.
Publisher
Springer Science and Business Media LLC
Subject
Space and Planetary Science,Aerospace Engineering
Reference40 articles.
1. Gradl, P. R. et al.: “Progress in Additively Manufactured Copper-Alloy GRCop-84, GRCop-42, and Bimetallic Combustion Chambers for Liquid Rocket Engines,” in 70th International Astronautical Congress (IAC), pp. 1-14. Washington D.C., USA (2019)
2. Gradl, P. R. et al.: “Development and Hot-fire Testing of Additively Manufactured Copper Combustion Chambers for Liquid Rocket Engine Applications,” in 53rd AIAA/SAE/ASEE Joint Propulsion Conference 2017. Atlanta GA, USA (2017)
3. Gradl, P. R. et al.: “GRCop-42 Development and Hot-fire Testing Using Additive Manufacturing Powder Bed Fusion for Channel-cooled Combustion Chambers,” in 55th AIAA/SAE/ASEE Joint Propulsion Conference 2019. Indianapolis IN, USA (2019)
4. Gradl, P. R. et al.: “Additive Manufacturing and Hot-fire Testing of Bimetallic GRCop-84 and C-18150 Channel Cooled Combustion Chambers Using Powder Bed Fusion and Inconel 625 Hybrid Directed Energy Deposition,” in 55th AIAA/SAE/ASEE Joint Propulsion Conference 2019. Indianapolis IN, USA (2019)
5. Seltzman, H., Wukitch, S. J.: “Nuclear response of additive manufactured GRCop-84 copper for use in Lower hybrid launchers in a fusion environment,” Fusion Engineering and Design 159, 111726 (2020)
Cited by
6 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献