Engine mounting structure for an aircraft

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 27/26 (2006.01)

Patent

CA 2613191

The invention relates to an engine mounting structure for an aircraft, said structure comprising a rear engine mount (8) which is provided with a rear mount body (54) and a first shear slug (66) that can take over the effort exerted in a transversal direction (Y) of the structure. Said first slug (66) crosses a lower strut (20) of the rigid structure and the lower end (70) thereof is inserted into the rear mount body. According to the invention, the lower end (70) is provided with a borehole (76) crossed by a first pin (74) which also crosses the rear mount body (54).

L'invention se rapporte à un mât d'accrochage de moteur pour aéronef comportant une attache moteur arrière (8) équipée d'un corps d'attache arrière (54) et d'un premier pion de cisaillement (66) capable d'assurer la reprise des efforts s'exerçant selon une direction transversale (Y) du mât, ce premier pion (66) traversant un longeron inférieur (20) de la structure rigide du mât et disposant d'une extrémité inférieure (70) logée dans le corps d'attache arrière. Selon l'invention, l'extrémité inférieure (70) est pourvue d'un alésage (76) traversé par une première goupille (74) traversant également le corps d'attache arrière (54).

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