An electric vertical take-off and landing aircraft comprises a fuselage (1) and a tilt wing (7). The tilt wing (7) is tiltable relative to the fuselage (1) in a range of tilt wing angles. Control surfaces (13) are arranged at the tilt wings (7). The aircraft comprises a horizontal stabilizer (8) with an elevator, in particular a stabilator, a vertical stabilizer (9) with a rudder, in particular a fully movable stabilizer (9), at least one electric engine (12) for powering main propellers (11) arranged at the tilt wing (7) and at least one software control device (15). The control device (15) is configured to control at least the control surfaces (13), the main propellers (11) and the tilt wing angle during hover and transition between hover and cruise flight.
ELECTRIC VERTICAL TAKE-OFF AND LANDING AIRCRAFT
VERTIKAL STARTENDES UND LANDENDES ELEKTRISCHES FLUGZEUG
AÉRONEF ÉLECTRIQUE À DÉCOLLAGE ET ATTERRISSAGE VERTICAUX
2025-06-18
Patent
Electronic Resource
English