Development of a topology optimization method for the design of composite lattice ring structures
DOI:
https://doi.org/10.15587/1729-4061.2021.238266Keywords:
сomposite lattice ring structures, topology optimization, winding trajectory, robotic filament windingAbstract
Composite lattice ring structures are known for their lightweight and high efficiency, which have a strong attraction in the aeronautical and aerospace industries. The general manufacturing process for such structures is to use wet filament winding technology. Due to the anisotropic properties of continuous fibers, the filament winding trajectory determines the mechanical properties of the composite lattice ring structures. In this work, a topology optimization method is proposed to generate the efficient filament winding trajectory, which follows the load transfer path of the composite part and can offer higher mechanical strengths. To satisfy the periodicity requirement of the structure, the design space is divided into a prescribed number of identical substructures during the topology optimization process. In order to verify the effectiveness and capability of the proposed approach, the topological design of ring structures with the different number of substructures, the ratio of outer to inner radius and the loading case is investigated. The results reflect that the optimal topology shape strongly depends on the substructure numbers, radius ratio and loading case. Moreover, the compliance of the optimized structures increases with the total number of substructures, while the structural efficiency of the optimized structures decreases with the radius ratio. Finally, taking the specified topological structure as the object, the conceptual design of a robotic filament winding system for manufacturing the composite lattice ring structure is presented. In particular, the forming tooling, integrated deposition system, winding trajectory and manufacturing process are carefully defined, which can provide valuable references for practical production in the future
References
- Xu, Y., Zhu, J., Wu, Z., Cao, Y., Zhao, Y., Zhang, W. (2018). A review on the design of laminated composite structures: constant and variable stiffness design and topology optimization. Advanced Composites and Hybrid Materials, 1 (3), 460–477. doi: https://doi.org/10.1007/s42114-018-0032-7
- Totaro, G., De Nicola, F. (2012). Recent advance on design and manufacturing of composite anisogrid structures for space launchers. Acta Astronautica, 81 (2), 570–577. doi: https://doi.org/10.1016/j.actaastro.2012.07.012
- Mack, J., McGregor, O., Mitschang, P. (2014). Prepreg lay-up technology for manufacturing of lattice structure fuselage sections. ECCM16 - 16th European Conference on Composite Materials. Seville.
- Giusto, G., Totaro, G., Spena, P., De Nicola, F., Di Caprio, F., Zallo, A. et. al. (2021). Composite grid structure technology for space applications. Materials Today: Proceedings, 34, 332–340. doi: https://doi.org/10.1016/j.matpr.2020.05.754
- Gagauz, F., Kryvenda, S., Shevtsova, M., Smovziuk, L., Taranenko, I. (2014). Manufacturing and testing of composite wafer components with dual-purpose integrated semi-loop joints. ECCM16 - 16th European Conference on Composite Materials. Seville.
- Cerqueira, J., Faria, H., Funck, R. (2014). Fabrication of composite cylinders with integrated lattice structure using filament winding. ECCM16 - 16th European Conference on Composite Materials. Seville.
- Vasiliev, V. V., Razin, A. F. (2006). Anisogrid composite lattice structures for spacecraft and aircraft applications. Composite Structures, 76 (1-2), 182–189. doi: https://doi.org/10.1016/j.compstruct.2006.06.025
- Sugiyama, K., Matsuzaki, R., Malakhov, A. V., Polilov, A. N., Ueda, M., Todoroki, A., Hirano, Y. (2020). 3D printing of optimized composites with variable fiber volume fraction and stiffness using continuous fiber. Composites Science and Technology, 186, 107905. doi: https://doi.org/10.1016/j.compscitech.2019.107905
- Zhu, J.-H., Zhang, W.-H., Xia, L. (2015). Topology Optimization in Aircraft and Aerospace Structures Design. Archives of Computational Methods in Engineering, 23 (4), 595–622. doi: https://doi.org/10.1007/s11831-015-9151-2
- Hu, Z., Vambol, O., Sun, S. (2021). A hybrid multilevel method for simultaneous optimization design of topology and discrete fiber orientation. Composite Structures, 266, 113791. doi: https://doi.org/10.1016/j.compstruct.2021.113791
- Hu, Z., Vambol, O. (2020). Topological designing and analysis of the composite wing rib. Aerospace Technic and Technology, 6, 4–14. doi: https://doi.org/10.32620/aktt.2020.6.01
- Fu, J., Yun, J., Jung, Y., Lee, D. (2017). Generation of filament-winding paths for complex axisymmetric shapes based on the principal stress field. Composite Structures, 161, 330–339. doi: https://doi.org/10.1016/j.compstruct.2016.11.022
- Li, N., Link, G., Wang, T., Ramopoulos, V., Neumaier, D., Hofele, J. et. al. (2020). Path-designed 3D printing for topological optimized continuous carbon fibre reinforced composite structures. Composites Part B: Engineering, 182, 107612. doi: https://doi.org/10.1016/j.compositesb.2019.107612
- Chen, Y., Ye, L. (2021). Topological design for 3D-printing of carbon fibre reinforced composite structural parts. Composites Science and Technology, 204, 108644. doi: https://doi.org/10.1016/j.compscitech.2020.108644
- Wang, T., Li, N., Link, G., Jelonnek, J., Fleischer, J., Dittus, J., Kupzik, D. (2021). Load-dependent path planning method for 3D printing of continuous fiber reinforced plastics. Composites Part A: Applied Science and Manufacturing, 140, 106181. doi: https://doi.org/10.1016/j.compositesa.2020.106181
- Bendsoe, M. P., Sigmund, O. (2004). Topology optimization: theory, methods, and applications. Springer, 370. doi: https://doi.org/10.1007/978-3-662-05086-6
- Kabir, S. M. F., Mathur, K., Seyam, A.-F. M. (2020). A critical review on 3D printed continuous fiber-reinforced composites: History, mechanism, materials and properties. Composite Structures, 232, 111476. doi: https://doi.org/10.1016/j.compstruct.2019.111476
- Sorrentino, L., Marchetti, M., Bellini, C., Delfini, A., Del Sette, F. (2017). Manufacture of high performance isogrid structure by Robotic Filament Winding. Composite Structures, 164, 43–50. doi: https://doi.org/10.1016/j.compstruct.2016.12.061
- Sorrentino, L., Anamateros, E., Bellini, C., Carrino, L., Corcione, G., Leone, A., Paris, G. (2019). Robotic filament winding: An innovative technology to manufacture complex shape structural parts. Composite Structures, 220, 699–707. doi: https://doi.org/10.1016/j.compstruct.2019.04.055
- Carrino, L., Polini, W., Sorrentino, L. (2003). Modular structure of a new feed-deposition head for a robotized filament winding cell. Composites Science and Technology, 63 (15), 2255–2263. doi: https://doi.org/10.1016/s0266-3538(03)00174-x
Downloads
Published
How to Cite
Issue
Section
License
Copyright (c) 2021 Zheng Hu, Oleksii Vambol, Shiping Sun, Qinglong Zeng
This work is licensed under a Creative Commons Attribution 4.0 International License.
The consolidation and conditions for the transfer of copyright (identification of authorship) is carried out in the License Agreement. In particular, the authors reserve the right to the authorship of their manuscript and transfer the first publication of this work to the journal under the terms of the Creative Commons CC BY license. At the same time, they have the right to conclude on their own additional agreements concerning the non-exclusive distribution of the work in the form in which it was published by this journal, but provided that the link to the first publication of the article in this journal is preserved.
A license agreement is a document in which the author warrants that he/she owns all copyright for the work (manuscript, article, etc.).
The authors, signing the License Agreement with TECHNOLOGY CENTER PC, have all rights to the further use of their work, provided that they link to our edition in which the work was published.
According to the terms of the License Agreement, the Publisher TECHNOLOGY CENTER PC does not take away your copyrights and receives permission from the authors to use and dissemination of the publication through the world's scientific resources (own electronic resources, scientometric databases, repositories, libraries, etc.).
In the absence of a signed License Agreement or in the absence of this agreement of identifiers allowing to identify the identity of the author, the editors have no right to work with the manuscript.
It is important to remember that there is another type of agreement between authors and publishers – when copyright is transferred from the authors to the publisher. In this case, the authors lose ownership of their work and may not use it in any way.