Strut for locking the engine of an aircraft

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 27/26 (2006.01)

Patent

CA 2623791

The invention concerns a strut for locking (4) the engine of an aircraft, the strut comprising a rigid structure (10) forming a structure box closed at the front by a front closing rib (36), as well as a system for mounting the engine including in particular a front engine fastener (6) comprising a fastener body (46) fixedly mounted on the rigid structure (10). The invention is characterized in that the fastener body (46) is pressed against a front surface (38), and the mast (4) comprises at least one shear pin (68) passing at least partly through the fastener body (46) as well as the front closing rib (36).

L'invention se rapporte à un mât d'accrochage (4) pour moteur d'aéronef, le mât comportant une structure rigide (10) formant un caisson fermé vers l'avant par une nervure de fermeture avant ((36), ainsi qu'un système de montage du moteur comportant notamment une attache moteur avant (6) comprenant un corps d'attache (46) monté fixement sur la structure rigide (10). Selon l'invention, le corps d'attache (46) est plaqué contre une surface avant (38), et le mât (4) comprend au moins un pion de cisaillement (68) traversant au moins partiellement le corps d'attache (46) ainsi que la nervure de fermeture avant (36).

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