ABSTRACT 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. Date Recue/Date Received 2021-01-07
TURBOFAN ENGINE, NACELLE THEREOF, AND ASSOCIATED METHOD OF OPERATION
2021-05-28
Patent
Electronic Resource
English
TURBOFAN ENGINE, NACELLE THEREOF, AND ASSOCIATED METHOD OF OPERATION
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