B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 27/26 (2006.01) F02C 7/20 (2006.01)
Patent
CA 2715734
The invention relates to an aircraft engine assembly comprising an annular load-transfer structure surrounding the central casing (16) and connected to a plurality of substantially planar structures arranged externally with respect to this annular structure, and acting upon it at a plurality of load application points (68a, 68b, 68c). According to the invention, at least one connecting link is associated with each of the load application points, the said link being positioned tangentially with respect to the casing (16) and having an inner end (62a) connected to this casing and an outer end (62b) connected to the structure (60) so that it has passing through it an imaginary plane (66a, 66b, 66c) in which said structure is located and which passes through the load application point.
invention se rapporte à un ensemble moteur pour aéronef comprenant une structure annulaire de transfert d'efforts entourant le carter central (16) et étant raccordée à une pluralité de structures sensiblement planes agencées extérieurement par rapport à celle-ci, et la sollicitant en une pluralité de points d'introduction d'efforts (68a, 68b, 68c). Selon l'invention, au moins une bielle de raccordement est associée à chacun des points d'introduction d'efforts, ladite bielle étant disposée tangentiellement par rapport au carter (16), et présentant une extrémité intérieure (62a) raccordée sur ce carter, ainsi qu'une extrémité extérieure (62b) raccordée sur la structure (60) de manière à être traversée par un plan fictif (66a, 66b, 66c) dans lequel se trouve ladite structure, et passant par le point d'introduction d'efforts.
Jalbert Delphine
Journade Frederic
Airbus Operations
Goudreau Gage Dubuc
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