Toroidal fuselage structure for unmanned aerial vehicles having

Aeronautics and astronautics – Aircraft – heavier-than-air – Airplane and fluid sustained

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B64C 3906

Patent

active

052773809

ABSTRACT:
An unmanned aerial vehicle having a toroidal fuselage structure that surrounds a pair of coaxial, multi-bladed, counter-rotating rotors. The toroidal fuselage structure is optimized to provide a highly efficient structure for reacting aerodynamic flight loads and rotor thrust loads of the UAV. The toroidal fuselage structure is further optimized to provide weight efficiency for minimizing power requirements.

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