The nacelle can have an inlet portion having a duct wall and an outer skin, the duct wall being annular around an axis and having a surface forming a radially-outer delimitation to a gas path upstream of a fan area, the duct wall extending from a rounded inlet edge of the nacelle to the fan area, a cavity located inside the inlet portion, a compressed air inlet leading into the cavity, and an outlet fluidly connecting the cavity to the gas path, the outlet having a plurality of apertures disposed circumferentially around the duct wall, the apertures sloping circumferentially.
Turbofan engine, nacelle thereof, and associated method of operation
07.11.2023
Patent
Elektronische Ressource
Englisch
TURBOFAN ENGINE, NACELLE THEREOF, AND ASSOCIATED METHOD OF OPERATION
Europäisches Patentamt | 2021
|TURBOFAN ENGINE, NACELLE THEREOF, AND ASSOCIATED METHOD OF OPERATION
Europäisches Patentamt | 2021
|