A rotorcraft having a fuselage surmounted by a main rotor. The rotorcraft has a first propeller and a second propeller driven in rotation respectively about a first secondary axis of rotation and a second secondary axis of rotation. A mobility system turns the second propeller relative to the fuselage, the mobility system turning the second secondary axis of rotation relative to the fuselage from a first position where the second propeller exerts thrust in a first direction to a second position where the second propeller exerts thrust in a second direction opposite to the first direction.
GIRAVION MUNI D'UNE VOILURE TOURNANTE ET D'UNE HELICE ORIENTABLE, ET PROCEDE APPLIQUE PAR CE GIRAVION
2018-08-17
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
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