To design and fabricate a mechanically actuated wing system capable of converting rotational motion into controlled flapping movement using linkage-based mechanical design principles.
Translating rotational input into smooth, repeatable flapping motion
Maintaining structural stability while minimizing system weight
Preventing excessive stress concentrations and mechanical binding during operation
Achieving consistent alignment between pivot points and moving joints
Designed and iterated linkage geometries in CAD to optimize motion range and efficiency
Tested multiple pivot placements and joint configurations to improve mechanical performance
Reinforced high-stress regions and refined tolerances to reduce binding and instability
Fabricated and tested physical prototypes to validate structural durability and movement consistency
CAD Modeling, Mechanical Linkages, Rapid Prototyping, Mechanical Testing, Structural Design