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| Naji, M. |
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| Motta, Antonella |
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| Aletan, Dirar |
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| Mohamed, Tarek |
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| Ertürk, Emre |
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| Taccardi, Nicola |
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| Kononenko, Denys |
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| Petrov, R. H. | Madrid |
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| Alshaaer, Mazen | Brussels |
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| Bih, L. |
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| Casati, R. |
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| Muller, Hermance |
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| Kočí, Jan | Prague |
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| Šuljagić, Marija |
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| Kalteremidou, Kalliopi-Artemi | Brussels |
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| Azam, Siraj |
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| Ospanova, Alyiya |
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| Blanpain, Bart |
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| Ali, M. A. |
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| Popa, V. |
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| Rančić, M. |
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| Ollier, Nadège |
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| Azevedo, Nuno Monteiro |
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| Landes, Michael |
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| Rignanese, Gian-Marco |
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Hümbert, Simon
German Aerospace Center
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (8/8 displayed)
- 2024Modelling of Bond Formation during Overprinting of PEEK Laminatescitations
- 2023Bonding of Low-Melting Polyaryletherketone onto Polyamide 6: A Concept for Molds for Automated Fiber Placementcitations
- 2023COMBINING FUSED GRANULAR FABRICATION AND AUTOMATED FIBRE PLACEMENT FOR THE RAPID PRODUCTION OF COMPLEX SANDWICH-STRUCTURES
- 2022Entwicklung eines lokalen Heizkonzeptes für das in-situ Fügen FFF gedruckter Strukturen auf thermoplastische Laminate (Studienarbeit)
- 2021The effect of a superhydrophobic coating on moisture absorption and tensile strength of 3D-printed carbon-fibre/polyamidecitations
- 2021Additive manufacturing of radiation shielding for small satellites
- 2019Topology Optimization of a Star Tracker Camera Bracket
- 2016Influence of the Screw Configuration on the LFT-D Processing of Glass Fiber Reinforced PA6
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document
Topology Optimization of a Star Tracker Camera Bracket
Abstract
Topology optimization is a powerful tool in lightweight design and has become increasingly popular with recent advances in additive manufacturing (AM). In the space industry, optimized and 3D-printed structures have the potential to meet the increasing demand for cost-efficient, flexible design and manufacturing strategies driven by large satellite constellations. In this paper a case study for re-designing a satellite structure is presented, identifying and exploring challenges and opportunities throughout the entire process chain. The reference part for this study is a star tracker camera bracket from the academic satellite Flying Laptop from the University of Stuttgart, currently operating in orbit. The original part was manufactured using standard machining processes and is used for functional as well as the cost reference of the AM optimization and manufacturing approach. The first step of the investigation is a characterization of AlSi10Mg manufactured by Laser Powder Bed Fusion (LPBF), focusing on the demands for topology optimization and associated cost-intensive post processing. Mechanical and metallographic properties for different sample geometries, orientations and heat treatments have been analyzed. This data provides the input for the material model in the optimization process as well as the optimization constraints. Following this step, the mesh-based optimization result is converted to a CAD geometry to assess manufacturability. For validation and cost assessment, the bracket is printed three times in one build-job using a Trumpf TruPrint 3000. Printed brackets are assessed for their natural frequency, the dominant design constraint, as well as the geometrical distortion and compared to the analysis results. Finally, design and manufacturing costs of the single part and of a small series of 99 parts is calculated to evaluate economic potential of the optimized and printed design. For the reference part presented in this study, the optimized design is 30 % lighter than the original and exhibits a 43 % higher first natural frequency. Additionally, a considerable scaling effect on the manufacturing costs is shown, keeping additive manufacturing competitive compared to small series machining production.