FlyUC Frame Design

These were 2 designs for the frame of an electric Vertical Take-off and Landing aircraft. The goal was to maintain rigidity in the frame to account for torsion due to uneven propulsion from quadrotors and to accommodate maximum battery capacity while maintaining overlap between center of gravity and center of mass regions.
Published 8 months ago
battery-pack boeing flyuc gofly structure-design university-project vtol weldment-design

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