Aircraft ventral fairing partition wall and aircraft...

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 7/00 (2006.01)

Patent

CA 2628618

The invention relates to a vertical partition wall (10) for the ventral fairing of an aircraft comprising a plurality of vertical panels (11, 12, 12~, 13, 13~), each panel being connected to an adjacent panel by a vertical stake (14, 15, 16). At least one outer panel (13, 13~) is fixedly mounted on at least one associated vertical stake (14, 16). The top end of the said vertical stake is equipped with a means of fixing in transverse rotation intended to be fixed to the structure (8) of an aircraft, the means of fixing in transverse rotation being able to allow the structure of the aircraft to move (Dy) with respect to the fixed partition wall. It is also possible for at least one intermediate panel (12, 12~) to be mounted in a floating manner on at least one associated vertical stake (15, 16) so that it can have a travel parallel and perpendicular to the adjacent panels.

L'invention concerne un mur (10) de cloisonnement vertical pour carénage ventral d'aéronef comportant une pluralité de panneaux (1 1 , 12, 12', 13, 13') verticaux, chaque panneau étant relié à un panneau adjacent par un piquet vertical (14, 15, 16). Au moins un panneau extérieur (13, 13') est monté fixe sur au moins un piquet vertical (14, 16) associé. L'extrémité haute dudit piquet vertical est munie d'un moyen de fixation en rotation transversale destiné à être fixé à la structure (8) d'un aéronef, le moyen de fixation en rotation transversale étant apte à autoriser le déplacement (Dy) de la structure de l'aéronef par rapport au mur de cloisonnement fixe. Il est également possible qu'au moins un panneau intermédiaire (12, 12') soit monté flottant sur au moins un piquet vertical (15, 16) associé, de manière à avoir un débattement parallèlement et perpendiculairement aux panneaux adjacents.

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