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Simultaneous topology, shape, and layer optimization of jointed isotropic components and fiber composite laminates considering material damage and fail-safety

Subject Area Lightweight Construction, Textile Technology
Mechanics
Term from 2019 to 2025
Project identifier Deutsche Forschungsgemeinschaft (DFG) - Project number 406315228
 
Final Report Year 2025

Final Report Abstract

In structural mechanics (particularly in aviation), certain components are required to be failsafe, which means that the structure must be able to withstand a certain proportion of the intended load despite the absence of a primary load path. Furthermore, optimization methods are increasingly being used in the design process of load-bearing structures, for example to save as much weight as possible. In conventional design optimization, it is possible to take failure safety into account as a secondary condition within the optimization. For this purpose, structural elements are removed during the optimization and the reliability is checked. In topology optimization, on the other hand, a structure is only created during the optimization process. As a result, failure safety could previously only be taken into account during optimization at extremely high computing costs. During the first phase of the project, a method was initially developed to identify load paths during optimization and thus specifically take their failures into account and reduce computing times. However, it turned out that the resulting continuous change of the optimization problem usually prevents convergence. Therefore, an approach was developed in which a cost-efficient topology optimization generates a redundant design, which is then shape-optimized. Since load paths do not change during the shape optimization, a reduced set of damage scenarios can be considered. Furthermore, it was investigated how the consideration of stresses affects the topology optimization considering fail safety. It was found that the shape of the assumed damage has a surprisingly small influence on the optimization result. In addition, fail safety was taken into account in the simultaneous optimization of two components and their connecting elements. This work formed the basis for the second project funding phase. In this phase, the connection of an isotropic component and a fiber composite shell was considered. An approach was developed in which the isotropic component is topologically optimized, while at the same time the locations of the connecting elements and the fiber composite laminate are optimized. It was shown that the consideration of a damage criterion in the fiber composite shell alone has a significant influence on the topology of the isotropic component. These results underline the importance of a holistic approach when optimizing assemblies of components.

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