Device for the attachment of an engine to an aircraft

Details Device for the attachment of an engine to an aircraft Device for the attachment of an engine to an aircraft

B - Operations, Transporting

64

D

B64D 27/26 (2006.01) F02C 7/20 (2006.01)

Patent

CA 2394462

Device for attaching an engine to an aircraft. The attachment device (10) is inserted between the engine (14) and a pylon (12) designed to be attached to an aircraft structure, such as a wing or fuselage section. The attachment device (10) generally includes two brackets (18a, 18b) joined together and secured to the pylon (12) and two pairs of rods (20a, 20b, 22a, 22b) inserted between the two brackets (18a, 18b) and a part (24) of the structure of the engine (14). Thus the integrity of the link between the pylon (16) and the engine (14) is preserved in the event of failure of any of the parts which constitute the device, without there being any need for a backup attachment system.

La présente concerne un dispositif de fixation d'un moteur à un aéronef. Le dispositif de fixation (10) est inséré entre le moteur (14) et un pylône (12) conçu pour être attaché à une structure d'aéronef, comme une aile ou une section de fuselage. Le dispositif de fixation (10) comprend généralement deux supports (18a, 18b) réunis et fixés au pylône (12) et deux paires de tiges (20a, 20b, 22a, 22b) insérées entre les deux supports (18a, 18b) et une partie (24) de la structure du moteur (14). Ainsi, l'intégrité de la liaison entre le pylône (16) et le moteur (14) est conservée en cas de défaillance de l'une des pièces qui constituent le dispositif, sans qu'il soit nécessaire d'avoir un système de fixation d'appoint.

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