An aircraft including a fuselage and a propulsion assembly. The propulsion assembly includes at least one fan rotor placed behind the fuselage as an extension thereof along a longitudinal axis, and a nacelle which forms a fairing of the at least one fan rotor through which at least one air flow passes. The aircraft comprises a plurality of stator radial arms mounted upstream of the at least one fan rotor and extending between the fuselage and the nacelle. The radial arms comprise at least one variable-pitch movable portion configured to axially divert the air flow.
AERONEF COMPRENANT UN PROPULSEUR ARRIERE CARENE AVEC STATOR D'ENTREE A VOLETS MOBILES
AIRCRAFT INCLUDING A STREAMLINED REAR THRUSTER WITH AN INPUT STATOR HAVING MOVABLE FLAPS
LUFTFAHRZEUG MIT EINEM STROMLINIENFÖRMIGEN HINTEREN TRIEBWERK MIT EINEM EINGANGSSTATOR MIT BEWEGLICHEN KLAPPEN
2023-03-22
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02K JET-PROPULSION PLANTS , Strahltriebwerke / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS |
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