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
19.09.2024
Patent
Elektronische Ressource
Englisch
Tilt rotor vertical take-off and landing unmanned aerial vehicle
Europäisches Patentamt | 2023
|Tilt rotor canard vertical take-off and landing unmanned aerial vehicle
Europäisches Patentamt | 2022
|Tailstock type tilt rotor vertical take-off and landing unmanned aerial vehicle
Europäisches Patentamt | 2024
|Electric vertical take-off and landing tilt rotor aircraft
Europäisches Patentamt | 2025
|Vertical take-off and landing rotor type unmanned aerial vehicle
Europäisches Patentamt | 2024
|