An aircraft is provided which includes a fuselage having a first wing with curved wingtips positioned above a second wing having curved wingtips. Rotor assemblies located in between the curved wingtips of the first and second wing, are employable to both provide vertical thrust for vertical take off of the aircraft and auto rotation to generate electric energy to recharge an onboard electric power supply. The first wing may be formed in a V-shape, and additional rotor assemblies to provide forward and vertical thrust to the airplane can be included on rotatable canards.
AIRCRAFT WITH WINGTIP POSITIONED PROPELLERS
FLUGZEUGE MIT PROPELLERN, DIE AN DEN FLÜGELSPITZEN POSITIONIERT SIND
AÉRONEF À HÉLICES POSITIONNÉES EN BOUT D'AILE
2023-12-13
Patent
Elektronische Ressource
Englisch