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 2736803
The invention relates to a rear part of an aircraft (1) comprising a structure for supporting engines (14), passing through the fuselage, through a first opening and a second opening (18, 18). Said rear part comprises connection means connecting the support structure (14) to the fuselage (6), with first connection means connecting the structure (14) to a first casing (50) forming the first opening and second connection means connecting the structure (14) to a second casing (50) forming the second opening. According to the invention, the first and second connection means each comprise at least one blocking element (90, 92) of said support structure, under compression loading by being applied to the casing (50) and to the support structure (14).
L'invention se rapporte à une partie arrière d'aéronef (1) comprenant une structure de support des moteurs (14), traversant le fuselage au niveau d'une première et d'une seconde ouvertures (18, 18). Elle dispose de moyens d'attache raccordant la structure de support (14) au fuselage (6), comprenant des premiers moyens d'attache raccordant la structure (14) à un premier encadrement (50) formant la première ouverture et des seconds moyens d'attache raccordant la structure (14) à un second encadrement (50) formant la seconde ouverture. Selon l'invention, les premiers et seconds moyens d'attache comprennent chacun au moins un élément de blocage (90, 92) de ladite structure de support, sollicité en compression en étant en appui d'une part sur l'encadrement (50), et d'autre part sur la structure de support (14).
Journade Frederic
Lafont Laurent
Airbus Operations
Goudreau Gage Dubuc
LandOfFree
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