The disclosure relates to hybrid unmanned aerial vehicle (UAV) having vertical take-off and landing (VTOL) capabilities. Specifically, the disclosure relates to a stable hybrid fixed angle rotor arrays UAV having VTOL capabilities with hovering capabilities using rotors and cruising using fixed wing.
L'invention concerne un véhicule aérien sans pilote hybride (UAV) ayant des capacités de décollage et d'atterrissage verticaux (VTOL). De façon spécifique, l'invention concerne des AUV à réseaux de rotors à angle fixe hybrides stables ayant des capacités VTOL avec des capacités de vol stationnaire à l'aide de rotors ainsi que de croisière à l'aide d'une aile fixe.
HYBRID FIXED ANGLE ROTOR UNMANNED AERIAL VEHICLE WITH VERTICAL TAKEOFF AND LANDING CAPABILITIES
VÉHICULE AÉRIEN SANS PILOTE À ROTOR À ANGLE FIXE HYBRIDE AYANT DES CAPACITÉS DE DÉCOLLAGE ET D'ATTERRISSAGE VERTICAUX
2022-12-22
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
HYBRID FIXED ANGLE ROTOR UNMANNED AERIAL VEHICLE WITH VERTICAL TAKEOFF AND LANDING CAPABILITIES
European Patent Office | 2024
|HYBRID FIXED ANGLE ROTOR UNMANNED AERIAL VEHICLE WITH VERTICAL TAKEOFF AND LANDING CAPABILITIES
European Patent Office | 2024
|HYBRID FIXED ANGLE ROTOR UNMANNED AERIAL VEHICLE WITH VERTICAL TAKEOFF AND LANDING CAPABILITIES
European Patent Office | 2022
|Hybrid fixed angle rotor unmanned aerial vehicle with vertical take-off and landing capabilities
European Patent Office | 2024
|VERTICAL TAKEOFF AND LANDING FIXED-WING UNMANNED AERIAL VEHICLE
European Patent Office | 2022
|