A VTOL vehicle includes a forward rotor, an aft rotor and a fuselage, the forward and aft rotor lying in a longitudinal axis of the vehicle, with the fuselage located axially between the forward and aft rotors. The vehicle has an in-flight configuration wherein the forward rotor is tilted downwardly at a negative tilt angle relative to the fuselage and the aft rotor is tilted upwardly at a positive tilt angle relative to the fuselage.
VTOL VEHICLE WITH COAXIALLY TILTED OR TILTABLE ROTORS
VTOL-FAHRZEUG MIT KOAXIAL GENEIGTEN ODER NEIGBAREN ROTOREN
VÉHICULE VTOL À ROTORS COAXIALEMENT BASCULÉS OU BASCULANTS
2017-09-06
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |