A multicopter with angled rotors is disclosed. In various embodiments, a multicopter as disclosed herein includes a fuselage and a plurality of rotors. At least some of the rotors are disposed on opposite sides of the fuselage and each is oriented at a corresponding angle to a substantially horizontal plane of the aircraft, the angle being of a magnitude such that a plane of rotation of the rotor does not intersect at least a critical portion of the fuselage.
MULTICOPTER WITH ANGLED ROTORS
MULTIKOPTER MIT ABGEWINKELTEN ROTOREN
MULTICOPTÈRE À ROTORS INCLINÉS
2024-03-13
Patent
Elektronische Ressource
Englisch