A vertical take-off and landing aircraft includes a fuselage, at least one wing connected to the fuselage, a plurality of rotors connected to the at least one wing for providing lift for vertical take-off and landing of the aircraft and a plurality of proprotors connected to the at least one wing and tiltable between lift configurations for providing lift for vertical take-off and landing of the aircraft and propulsion configurations for providing forward thrust to the aircraft
VERTICAL TAKE-OFF AND LANDING AIRCRAFT
SENKRECHT STARTENDES UND LANDENDES FLUGZEUG
AÉRONEF À DÉCOLLAGE ET ATTERRISSAGE VERTICAUX
2024-08-07
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |