Rear part of an aircraft comprising two semi-structures for...

B - Operations – Transporting – 64 – D

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Details

B64D 27/14 (2006.01) B64D 27/02 (2006.01) B64D 27/26 (2006.01) B64D 29/06 (2006.01)

Patent

CA 2736911

The invention relates to a rear part of an aircraft (1), comprising a structure for supporting engines (14), extending through the fuselage (6), through two openings (18, 18) distributed either side of a vertical median plane (P) of the aircraft. According to the invention, the support structure (14) consists of a first semi-structure and a second semi-structure (22, 22) respectively extending through the first and second fuselage openings (18, 18), the first and second semi-structures being joined to each other in a dismountable manner in an inside space (8) defined by the fuselage.

L'invention se rapporte à une partie arrière d'aéronef (1) comprenant une structure de support des moteurs (14), traversant le fuselage (6) au niveau de deux ouvertures (18, 18) réparties de part et d'autre d'un plan médian vertical (P) de l'aéronef. Selon l'invention, la structure de support (14) est réalisée à partir d'une première et d'une seconde demi- structures (22, 22) traversant respectivement les première et seconde ouvertures du fuselage (18, 18), les première et seconde demi-structures étant assemblées l'une à l'autre de manière démontable au sein d'un espace intérieur (8) défini par le fuselage.

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