Compliant Morphing Wing System
grabcad
Software: Autodesk Inventor Pro 2018Size: 1500 x 600 mmTime: 4 months, 3 iterations with FEM & CFD analysis each.Abstract: * This was my B.E. undergraduate project. It is a wing design that can change it's shape to predetermined configurations based on circumstances.* It is actuated using monolithic, flexible Compliant Mechanism.* It includes Leading Edge, Trailing Edge and Sweep Morphing Mechanisms in a single design.Note:* Aerofoil rib actuation of Aileron and Flap region differ from each other.* Had to create 14 unique aerofoil ribs.* Used NACA 2415 aerofoil for all ribs.* Used a Swastika design for Leading Edge Camber Morphing.* Used a motor at the center connected to aileron sections to achieve Sweep Morphing.* Used a Fish Skeleton design for Trailing Edge Camber Morphing.
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