The invention is related to a rotorcraft (1) with a fuselage (4) and at least one main rotor (2), said at least one main rotor (2) being drivable for controlling an associated pitch attitude of said rotorcraft (1) in operation, and said fuselage (4) being equipped with at least one passive wing-type aerodynamic device (6) that is adapted for generating independently of said associated pitch attitude a lift force (14a) acting on said fuselage (4), said lift force (14a) being oriented perpendicular to an air flow (12) that is directed in operation of said rotorcraft (1) against said passive wing-type aerodynamic device (6).
Rotorcraft with a fuselage and at least one main rotor
Hubschrauber mit einem Rumpf und mindestens einem Hauptrotor
Hélicoptère comprenenat un fuselage et au moins un rotor principal
2019-01-16
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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