An aerial vehicle includes a fuselage supporting a pair of wings, with each of wings having a pair of booms attached thereto. A tilt rotor is positioned at each of the forward ends of each of the booms, to provide the aerial vehicle with at least four tilt rotors. A fixed rotor is positioned at and secured to the aft (or trailing) ends of each of the booms, to provide the aerial vehicle with at least four fixed rotors.
TILT ROTOR VERTICAL TAKE-OFF AND LANDING AERIAL VEHICLE
2024-09-19
Patent
Electronic Resource
English
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