A rotorcraft with at least one main rotor and a fuselage, comprising: a tail boom connected to the fuselage, the tail boom extending from the fuselage toward a duct-type portion; a shroud provided at the duct-type portion and forming a transverse duct; at least one ducted tail rotor rotatably arranged in the transverse duct, wherein the at least one ducted tail rotor comprises a plurality of rotor blades mounted to a rotatable rotor hub; and a stator with a gearbox fairing mounted to the shroud for supporting the rotatable rotor hub in the transverse duct, wherein the stator comprises at least one rotatable stator blade connecting the gearbox fairing to the shroud.
Rotorcraft with a ducted tail rotor supported by a stator
20.05.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
ROTORCRAFT WITH A DUCTED TAIL ROTOR SUPPORTED BY A STATOR
Europäisches Patentamt | 2024
|A ROTORCRAFT WITH A DUCTED TAIL ROTOR SUPPORTED BY A STATOR
Europäisches Patentamt | 2024
|A ROTORCRAFT WITH A TAIL BOOM HAVING A DUCTED TAIL ROTOR
Europäisches Patentamt | 2024
|PITCH CONTROL DEVICE FOR A DUCTED TAIL ROTOR OF A ROTORCRAFT
Europäisches Patentamt | 2019
Ducted tail rotor designs for rotorcraft and their low noise features
Tema Archiv | 1996
|