Tilt-Rotor VTOL Mechanism Design & Build
CATIA V5
Overview
Designed and prototyped a tilt-rotor mechanism for a hybrid VTOL delta-wing aircraft. The system enabled controlled transition between vertical lift and forward flight configurations.
Technical Snapshot
Application
Hybrid VTOL / Fixed-Wing Aircraft
Actuation
Servo-driven gear mechanism
Structure
Aluminum mounting + 3D-printed housing
Propulsion
Brushless motor + propeller
Manufacturing
Additive manufacturing + CNC components
Scope of Work
• 3D modeling and full assembly in CATIA V5
• Design of tilt-rotor housing and gear interface
• Integration of servo actuation for controlled rotation
• Structural mounting to main spar / fuselage
• 3D printing and physical assembly of mechanism
• Functional testing for transition stability
Outcome
Tilt mechanism achieved controlled rotation under motor load and was validated through ground and transition testing.