Nacelle with simplified cowling arrangement

Details Nacelle with simplified cowling arrangement Nacelle with simplified cowling arrangement

B - Operations, Transporting

64

D

B64D 29/06 (2006.01) B64D 29/08 (2006.01)

Patent

CA 2707838

The invention relates to a nacelle (1) that comprises a first cowling (7) and a second cowling (9) capable of covering in particular the area (15) located around the casing of the fan (19) of a turbojet engine (3). The nacelle further includes an intermediate cowling (23) attached to said first cowling (7) so as to sandwich a mast (5) holding said turbojet engine (3). The second cowling (9) is mounted onto the intermediate cowling (23) via removable fastening means.

Cette nacelle (1) comprend un premier capot (7) et un deuxième capot (9) aptes à couvrir notamment la zone (15) située autour du carter de soufflante (19) d'un turboréacteur (3). Cette nacelle comprend en outre un capot intermédiaire (23) fixé audit premier capot (7) de manière prendre en sandwich un mât (5) de support dudit turboréacteur (3). Ledit deuxième capot (9) est rapporté sur ledit capot intermédiaire (23) par des moyens de fixation démontables.

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