An aerodynamic element to a nacelle of the aircraft and the nacelle of the aircraft

摘要

An aerodynamic element to a nacelle of the aircraft and the nacelle of the aircraft. The invention relates to a nacelle (1), which comprises a fixed cover (9) and a flap of entry (8) that can move axially with respect to the cover (9) between an operating position and a maintenance position rear front.The aerodynamic element (15) is flexible and has a substantially cylindrical shape in general, and the element comprises: an ascending portion (16) designed to be fixed on the inner wall (17) of the flap (8) of the nacelle inlet; and a descending portion (20) projected pair The bear radially against the internal face (31) of the cover (9).The descending portion (20) of the element (15) includes an annular collar (24) that protrudes to the outside of the element (15), and a blade terminal (25) which, at rest, is inclined to outside of the element (15) in the direction of its free end.