The invention is related to a rotorcraft 1 with at least one main rotor 1 a and at least one counter-torque rotor 11a, comprising: at least one duct-type portion 10 provided with a shroud 3 that defines at least one transverse duct 6, said at least one counter-torque rotor 11a comprising a plurality of counter-torque rotor blades 13 and being rotatably arranged within said at least one transverse duct 6, and said shroud 3 being equipped in the region of said at least one transverse duct 6 at least partly with a liner arrangement 3a, said liner arrangement 3a being at least adapted for reducing generation of aerodynamic noise resulting from blade tip clearance vortices occurring during rotation of said at least one counter-torque rotor 11a inside said at least one transverse duct 6 in operation of said rotorcraft 1.
Rotorcraft with at least one main rotor and at least one counter-torque rotor
Drehflügler mit mindestens einem Hauptrotor und mindestens einem rotor zum Drehmomentausgleich
Giravion avec au moins un rotor principal et au moins un rotor anti-couple
2015-09-02
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
ROTORCRAFT WITH AT LEAST ONE MAIN ROTOR AND AT LEAST ONE COUNTER-TORQUE ROTOR
Europäisches Patentamt | 2015
|ROTORCRAFT WITH AT LEAST ONE MAIN ROTOR AND AT LEAST ONE COUNTER-TORQUE ROTOR
Europäisches Patentamt | 2015
|Rotorcraft with at least one main rotor and at least one counter-torque rotor
Europäisches Patentamt | 2019
|Rotorcraft with a fuselage and at least one main rotor
Europäisches Patentamt | 2016
|ROTORCRAFT WITH A FUSELAGE AND AT LEAST ONE MAIN ROTOR
Europäisches Patentamt | 2015
|