Aircraft Turbofan Engine paramitric design

detailed 3D CAD model of a high-bypass turbofan aircraft engine, designed entirely from the ground up using parametric modeling techniques. The assembly includes the aerodynamic intake, fan blades, spinner, compressor stages, combustion section, turbine, exhaust system, and external nacelle Project Highlights: Complete parametric 3D assembly Individual mechanical components High-bypass turbofan configuration Engineering-oriented modeling workflow Exploded and sectional assembly views Optimized topology for visualization and technical presentations Suitable for educational, aerospace visualization, and engineering portfolio purposes Tools Used: FreeCAD CAD Assembly Modeling Parametric Design Photorealistic Rendering