B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 27/14 (2006.01) B64D 27/20 (2006.01) B64D 27/26 (2006.01)
Patent
CA 2736777
The invention relates to a rear part of an aircraft (1) comprising a structure for supporting engines (14), extending through the fuselage, through a first opening and a second opening (18, 18). Said rear part comprises connection means connecting the structure (14) to the fuselage (6), with first connection means connecting the structure to a first casing (50) forming the first opening (18) and second connection means connecting the structure to a second casing (50) forming the second opening (18). According to the invention, the connection means also comprise at least one effort recovery connecting rod (66), the first end of which is mounted on the structure (14) and the opposite end is mounted on the fuselage, at a distance from the first and second openings.
L'invention se rapporte à une partie arrière d'aéronef (1) comprenant une structure de support des moteurs (14), traversant ledit fuselage au niveau d'une première et d'une seconde ouvertures (18, 18). Elle dispose de moyens d'attache raccordant la structure (14) au fuselage (6), comprenant des premiers moyens d'attache raccordant la structure à un premier encadrement (50) formant la première ouverture (18) et des seconds moyens d'attache raccordant la structure à un second encadrement (50) formant la seconde ouverture (18). Selon l'invention, les moyens d'attache comprennent aussi au moins une bielle de reprise d'efforts (66) dont une première extrémité est montée sur la structure (14), et dont l'extrémité opposée est montée sur le fuselage, à distance des première et seconde ouvertures.
Bardou Etienne
Jalbert Delphine
Journade Frederic
Lafont Laurent
Airbus Operations (societe Par Actions Simplifiee)
Robic
LandOfFree
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