Abstract
Additive manufactured parts have a high potential in weight saving for aerospace applications. In the Bavarian-funded project BayLu25 – BLANCA, the Universität der Bundeswehr München, the test house GMA, the small and medium enterprise GERG and the aircraft manufacturer Boeing are working together to investigate and develop additive manufactured load introductions into sandwich parts. Certification is taken as a basis for the developments and therefore, 3D simulation methods are used to verify and validate the structure. Current metal parts are commonly certified using the von-Mises yield criterion. The advantages in higher compression and shear allowable as well as the orthotropic behavior of additive manufactured metals are not considered. To further decrease weight and therefore save CO2, the 3D material behavior of Ti-6Al-4 V is investigated in the current project. The material characterization was done by means of a test program, in which the 3D material properties for tension, compression and shear loading were determined. Furthermore, the build orientation influence on the strength and stiffness values of the specimens was evaluated. For modeling the material behavior, the Cuntze-Bold model was adapted for metallic parts.
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References
European Union Aviation Safety Agency: Certification Specifications and Acceptable Means of Compliance for large Aeroplanes CS-25. Amendment 26 (2020).
European Union Aviation Safety Agency: Acceptable Means of Compliance AMC 20–29, Appendix 2 (2020).
United States Department of Defense: Metallic Materials and Elements for Aerospace Vehicle Structures, MIL-HDBK-5C. Vol 1, Revision C (1976).
Riebensahm, P., Träger, L.: Werkstoffprüfung (Metalle). Springer, Heidelberg (1928).
Mises, R. v.: Mechanik der festen Körper im plastisch-deformablen Zustand. Nachrichten der königlichen Gesellschaft der Wissenschaft in Göttingen, Mathematisch-Physikalische Klasse, 582 (1913).
Ramberg, W., Osgood, W.R.: Description of stress-strain curves by three parameters. NACA, Washington, D.C. (1943).
Tsai, S. W., Wu, E. M.: A General Theory of Strength for Anisotropic Materials. Journal of Composite Materials, 5, 58-80 (1971).
Cuntze, R.: Comparison between experimental and theoretical results using Cuntze's failure mode concept model for composites under triaxial loadings. Journal of Composite Materials, SAGE Publications (2012).
Bold, J.: Vergleich des Impaktverhaltens von monolithischer und hybrider CFK-Platte unter Verwendung eines neuen Werkstoffmodells. PhD Thesis, Deutsches Zentrum für Luft- und Raumfahrt e.V., Köln (2019).
Acknowledgements
This study is part of the research project BLANCA, which is funded by the Bavarian Ministry of Economic affairs, Regional development and Energy (StMWi) within the program BayLu-25.
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Ertürk, E., Bold, J., Höfer, P., Stark, C., Höhn, W. (2023). 3D Material Model for Additive Manufactured Metallic Parts. In: Rieser, J., Endress, F., Horoschenkoff, A., Höfer, P., Dickhut, T., Zimmermann, M. (eds) Proceedings of the Munich Symposium on Lightweight Design 2021. Springer Vieweg, Berlin, Heidelberg. https://doi.org/10.1007/978-3-662-65216-9_16
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DOI: https://doi.org/10.1007/978-3-662-65216-9_16
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