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.
HYBRID FIXED ANGLE ROTOR UNMANNED AERIAL VEHICLE WITH VERTICAL TAKEOFF AND LANDING CAPABILITIES
UNBEMANNTES LUFTFAHRZEUG MIT HYBRIDEM FESTWINKELROTOR MIT VERTIKALEN START- UND LANDEFÄHIGKEITEN
VÉHICULE AÉRIEN SANS PILOTE À ROTOR À ANGLE FIXE HYBRIDE AYANT DES CAPACITÉS DE DÉCOLLAGE ET D'ATTERRISSAGE VERTICAUX
2024-03-20
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 | 2022
|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
|