Engine mount for an aircraft, to be placed between an engine...

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 27/26 (2006.01)

Patent

CA 2613194

The invention relates to an engine mount for an aircraft, to be placed between an engine and an engine mounting structure, said mount comprising a shackle (20) which is connected to a first fixing device (34) comprising a fork (36) provided with two arms (36a, 36b), and an axle (44) which passes through the shackle (20) and the two arms. Said two arms each have an opening (48a, 48b) which is respectively provided with a first ring (50) and a second ring (60) for receiving the axle. According to the invention, the first ring has a bottom (54) which forms an abutment for a first end (44a) of the axle, and the first fixing device also comprises means for stopping the axle (64) in translation, co-operating with a second end (44b) of said axle.

L'invention se rapporte à une attache moteur pour aéronef destinée à être interposée entre un moteur et un mât d'accrochage, l'attache comprenant une manille (20) raccordée à un premier dispositif de fixation (34) comportant une chape (36) pourvue de deux bras (36a, 36b) et un axe (44) traversant la manille (20) ainsi que ces deux bras, ces deux derniers disposant chacun d'un orifice (48a, 48b) équipé respectivement d'une première bague (50) ainsi que d'une seconde bague (60) de réception de l'axe. Selon l'invention, la première bague est équipée d'un fond (54) formant butée pour une première extrémité (44a) de l'axe, et le premier dispositif de fixation comporte en outre des moyens d'arrêt en translation de l'axe (64) coopérant avec une seconde extrémité (44b) de cet axe.

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