Rear section of an aircraft including an engine mounting...

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 1/16 (2006.01) B64D 27/08 (2006.01) B64D 27/14 (2006.01) B64D 27/26 (2006.01)

Patent

CA 2756345

The invention relates to a rear section of an aircraft including two connecting rods (66) symmetrically arranged on either side of a vertical median plane (P), each connecting rod having an end mounted on an engine mounting structure (14) and another end mounted on the fuselage (6), said section being designed so as to enable, by rotating the connecting rods (66) about the rotational axes thereof, a limited amplitude swinging movement of the assembly (23) formed by the mounting structure and the engines, relative to the fuselage (6), through first and second openings (18) of the fuselage.

L' invention se rapporte à une partie arrière d'aéronef comprenant deux bielles (66) disposées symétriquement de part et d'autre d'un plan médian vertical (P), chaque bielle présentant une extrémité montée sur une structure de support (14) des moteurs et une autre extrémité montée sur le fuselage (6), cette partie étant conçue de manière à autoriser, par rotation des bielles (66) autour de leurs axes de rotation, un mouvement oscillant d'amplitude limitée de l'ensemble (23) formé par la structure de support et les moteurs, par rapport au fuselage (6), à travers des première et seconde ouvertures (18) de fuselage.

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