Weight reduction of components and systems is of utmost importance in Aerospace industry. Reducing weight translates into higher performance and lower fuel consumption. In this paper we identify two components as candidates for weight reduction. In order to achieve this goal without sacrificing the current performance of these components we use ATOM optimization software within Abaqus environment. Current geometry models are simulated with the specified load cases to establish a baseline performance in term of stiffness and stresses. We then generate design envelopes representing the available space for topology optimization.
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