Device for recovery of forces generated by an aircraft engine

Details Device for recovery of forces generated by an aircraft engine Device for recovery of forces generated by an aircraft engine

B - Operations, Transporting

64

D

B64D 27/00 (2006.01) B64D 27/26 (2006.01)

Patent

CA 2389881

Device for recovering forces generated by an aircraft engine. The device comprises an engine strut (10), capable of being fixed to a wing or a fuselage of an aircraft, and an attachment device (12) fixed to the engine strut (10) and on which the engine is mounted. An intermediate fitting (24) of large dimensions, capable of recovering exceptionally high forces is fixed to several strut fittings (30) independent from each other, for example by bolts (28), across a lower spar (14) of the engine strut (10).

Un dispositif servant à la récupération des forces que génère le moteur d'un aéronef. Le dispositif comprend un mât de liaison (10) qui se fixe à une aile ou au fuselage d'un aéronef, ainsi qu'un dispositif de fixation (12) assujetti au mât de liaison (10) et sur lequel le moteur est monté. Une pièce de fixation intermédiaire (24) de grande taille, capable de récupérer des forces exceptionnellement élevées, est retenue à plusieurs pièces de fixation (30) du mât de liaison, indépendantes les unes des autres et retenues en place, par exemple, par des boulons (28) le long d'un longeron inférieur du mât de liaison (10).

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