<p>This research addresses a fundamental challenge in aerospace engineering concerning the design and Optimization of the bracket for General Electric (GE) jet engines. The general problem statement revolves around the need for improved structural performance, enhanced fuel efficiency and reduced environmental impact in modern aviation. The proposed work aims to conduct a comprehensive analysis of the GE jet engine bracket through Modal analysis, Structural analysis and Mesh independency studies. The methodological approach includes Optimization of GE bracket using Generative Design within Fusion 360 software. This study focuses on the practical application of established engineering tools to achieve an optimized and structurally efficient bracket design. By integrating simulation-driven design with generative optimization techniques, the study demonstrates an effective approach to achieving a lightweight, structurally sound bracket configuration tailored for aerospace applications. Employing generative design in Fusion 360, this study aims to identify an optimized configuration that maximizes structural integrity while minimizing weight. The anticipated results of this research include a refined GE jet engine bracket design that exhibits improved structural characteristics and contribution to overall efficiency. The outcomes of the research are expected to inform future developments in jet engine technology, paving the way for more sustainable and high-performance aircraft in the aviation industry.</p> Graphical abstract <p></p>