Side-opening jet engine nacelle

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 29/06 (2006.01) B64D 15/12 (2006.01) B64D 29/08 (2006.01) F02K 1/72 (2006.01)

Patent

CA 2666614

The invention relates to a nacelle including an air intake upstream from the jet engine (1), a medium section surrounding the fan of the jet engine (1), and a downstream section. The nacelle further includes at least one pair of mobile cowlings (3) provided on both sides of a vertical longitudinal symmetry plane of the nacelle and hinged essentially parallel to a longitudinal axis (A) of the nacelle so they can be opened to provide access to the jet engine (1). The mobile cowlings (3) are paired by fastening means (8) so that they can be hinged on each other about separate or overlapping axes (6). Each mobile cowling (3) comprises permanent connection means or means (14, 15) for connecting it temporarily by rotation and in closed position to a fixed structure (7) of the nacelle.

La nacelle comprend une entrée d'air en amont du turboréacteur (1 ), une section médiane entourant une soufflante du turboréacteur (1) et une section aval. La nacelle comporte en outre au moins une paire de capots mobiles (3) disposés de part et d'autre d'un plan vertical longitudinal de symétrie de la nacelle et articulés sensiblement parallèlement à un axe longitudinal (A) de la nacelle de manière à pouvoir s'ouvrir pour donner accès au turboréacteur (1). Les capots mobiles (3) sont appariés par des moyens d'attache (8) permettant leur articulation l'un sur l'autre autour d'axes (6) distincts ou confondus. Chaque capot mobile (3) comporte des moyens de liaison permanente ou des moyens (14, 15) pour le lier temporairement, lorsqu'il est fermé, en rotation avec une structure fixe (7) de la nacelle.

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