Morphing Wing Prototype (Exploded Parts Set)

Create a small educational ARCS-inspired morphing wing prototype for a college engineering project. Overall dimensions: Half-span: 150 mm Root chord: 100 mm Tip chord: 75 mm Taper ratio: 0.75 Approximate airfoil: NACA 0012 Design: Five ribs positioned at 0, 37.5, 75, 112.5 and 150 mm along the span. Rigid front wing section covering 65% of the chord. Flexible rear trailing-edge section covering 35% of the chord. Main spar: 5 × 5 mm. Rear torsion shaft: 4 mm diameter. Five rear support arms, approximately 8 mm long. One MG90S micro-servo mounted near the root. Include servo mount, pushrod, crank, shaft supports and mechanical travel stops. The servo should rotate the torsion shaft, moving the rear support arms to bend the flexible trailing edge upward and downward. Generate separate editable mechanical parts and a complete assembly. Keep all dimensions in millimetres. Make the components suitable for an educational FDM 3D-printing prototype using PLA and TPU. Export individual STL files and a STEP assembly if supported. Do not simplify the mechanism into a decorative model. Show the moving mechanism and component connections. Treat the geometry as a preliminary design requiring fit and movement validation.

Parameters

Every value above is a live dimension. Open a model like this in the editor and each one becomes a slider you can drag before exporting.