Air intake for aircraft nacelle, and propulsion assembly...

Details Air intake for aircraft nacelle, and propulsion assembly... Air intake for aircraft nacelle, and propulsion assembly...

B - Operations, Transporting

64

D

B64D 29/00 (2006.01) B64D 33/02 (2006.01)

Patent

CA 2708106

The invention relates to an air intake for an aircraft nacelle that comprises a shroud (19) that can be mounted on the fan casing (15) of a turbojet engine (1). The shroud (19) is sized so as to define a circumferential gap (J) relative to the casing (15). Punctual linking means (27, 33) between the shroud (19) and the casing (15) are discretely distributed at the periphery of said shroud (19).

Cette entrée d'air pour nacelle d'aéronef comprend une virole (19) apte à être montée sur le carter de soufflante (15) d'un turboréacteur (1). Cette virole (19) est dimensionnée pour définir un jeu circonférentiel (J) par rapport au carter (15). Des moyens de liaison ponctuelle (27; 33) de cette virole (19) au carter (15) sont répartis de manière discrète à la périphérie cette virole (19).

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