An aircraft comprising: a fuselage; and a plurality of lift rotors disposed on opposite sides of the fuselage, wherein each lift rotor is oriented at a corresponding non-zero angle to a substantially horizontal plane of the aircraft, wherein the non-zero angle for at least one pair of lift rotors on each side of the fuselage is such that the at least one pair of lift rotors tilt outboard away from the fuselage.
Multicopter with angled rotors
21.09.2023
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |