We propose a VTOL aircraft (1), comprising:a fuselage (2) for transporting passengers and/or load;a front wing (3) attached to the fuselage (2);a rear wing (4) attached to the fuselage (2), behind the front wing (3) in a direction of forward flight (FF);a right connecting beam (5a) and a left connecting beam (5b), which connecting beams (5a, 5b) structurally connect the front wing (3) and the rear wing (4), which connecting beams (5a, 5b) are spaced apart from the fuselage (2); and at least two lifting units (M1-M6) on each one of the connecting beams (5a, 5b), which lifting units (M1-M6) each comprise at least one propeller (6b) and at least one motor (6a) driving said propeller (6b), preferably an electric motor, and are arranged with their respective propeller axis in an essentially vertical orientation (z);wherein the front wing (3), at least in portions thereof, has a sweep angle γ between γ = 45° and γ = 135°, preferably γ = 75°, and the rear wing (4), at least in portions thereof, has a forward sweep with sweep angle β ≥ 30°, preferably, β = 65°.
VTOL AIRCRAFT
SENKRECHTSTART- UND -LANDEFLUGZEUG
AÉRONEF ADAV
2022-09-14
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |