B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 27/26 (2006.01) B64D 27/16 (2006.01) F02C 7/20 (2006.01)
Patent
CA 2715738
The invention relates to an aircraft engine assembly comprising means for mounting a turbojet (2) on a rigid mounting strut structure, these means comprising first, second and third thrust load-absorbing front engine mounts (6a, 6b, 8) fitted to the fan casing (12) and arranged in such a way that the third mount (8) passes through a first diametral plane (P1) of the turbojet, the first and second mounts (6a, 6b) being arranged one on either side of this first plane (P1). According to the invention, the mounts (6a, 6b) are fitted to the fan casing (12) at two respective points (6'a, 6'b) situated beyond a second diametral plane (P2) of the turbojet which is orthogonal to the first plane (P1), with respect to the third mount (8).
L' invention se rapporte à un ensemble moteur pour aéronef comprenant des moyens d'accrochage d'un turboréacteur (2) sur une structure rigide de mât d'accrochage, ces moyens comportant une première, seconde et troisième attaches moteur avant (6a, 6b, 8) de reprise des efforts de poussée rapportées sur le carter de soufflante (12), et agencées de sorte que la troisième attache (8) passe par un premier plan diamétral (P1) du turboréacteur, les première et seconde attaches (6a, 6b) étant disposées de part et d'autre de ce premier plan (P1). Selon l'invention, les attaches (6a, 6b) sont rapportées sur le carter de soufflante (12) respectivement en deux points (6'a, 6'b) situés au-delà d'un second plan diamétral (P2) du turboréacteur orthogonal au premier plan (P1), par rapport à la troisième attache (8).
Jalbert Delphine
Journade Frederic
Lafont Laurent
Airbus Operations
Goudreau Gage Dubuc
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