The invention is related to a rotorcraft (1) with at least one main rotor (1a) and a fuselage (2), comprising: a tail boom (2a) connected to the fuselage (2), the tail boom (2a) extending from the fuselage (2) toward a duct-type portion (7); a shroud (3) provided at the duct-type portion (7) and forming a transverse duct (6); at least one ducted tail rotor (9) rotatably arranged in the transverse duct (6), wherein the at least one ducted tail rotor (9) comprises a plurality of rotor blades (9a) mounted to a rotatable rotor hub (9b); and a stator (11) with a gearbox fairing (10) mounted to the shroud (3) for supporting the rotatable rotor hub (9b) in the transverse duct (6), wherein the stator (11) comprises at least one rotatable stator blade (11a) connecting the gearbox fairing (10) to the shroud (3).
A ROTORCRAFT WITH A DUCTED TAIL ROTOR SUPPORTED BY A STATOR
DREHFLÜGELFLUGZEUG MIT EINEM HECKROTOR MIT KANALFÜHRUNG, DER VON EINEM STATOR GESTÜTZT WIRD
GIRAVION AVEC UN ROTOR ARRIÈRE CARÉNÉ SUPPORTÉ PAR UN STATOR
28.08.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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