Air intake structure for aircraft engine

B - Operations – Transporting – 64 – D

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B64D 33/02 (2006.01) B64D 29/06 (2006.01) F02C 7/045 (2006.01)

Patent

CA 2292914

Dans une structure d'entrée d'air (14) d'une nacelle de moteur d'aéronef, la liaison entre la lèvre d'entrée d'air (15), le cadre de renfort avant (16) et le panneau acoustique (17) est réalisée de façon telle que la lèvre (15) puisse être démontée sans rompre la liaison entre le cadre (16) et le panneau (17). De plus, la partie arrière interne (15a) de la lèvre (15) recouvre normalement la partie avant (17a) du panneau (17), ainsi que les organes (22,24), assurant la liaison entre ce dernier et le cadre (16).

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