Propulseur aéronautique (40) d’axe longitudinal (X) et comprenant une rangée rotorique amont et une rangée statorique aval (16) de pales (18) non carénées. Figure de l’abrégé : Figure 5
The invention relates to an aeronautical propulsion unit (40) having a longitudinal axis (X) and comprising an upstream rotor row and a downstream stator row (16) of unducted blades (18), wherein at least two stator blades (18) are at different axial positions (Tl, T2,) with respect to one other along the longitudinal axis (X).
PROPULSEUR AERONAUTIQUE A ACOUSTIQUE AMELIOREE
2024-10-18
Patent
Electronic Resource
French