Patent ID: 8727268

Claim:
An attachment device for an aircraft engine comprising: a rigid structure; and attachment means for the engine on the rigid structure, the attachment means including a device to take-up thrust forces generated by the engine, the thrust take-up device including: a spreader, two connecting rods mechanically connected to the spreader at an aft end through a first mechanical link, a connection fitting fixed to the rigid structure to which the spreader is mechanically connected by a junction fitting by a connection pin inserted orthogonal to a vertical and longitudinal median plane of the attachment device, and an additional fitting to which the connecting rods, the spreader, and the connection fitting are mechanically connected, a clearance being provided at a second mechanical link between the connecting rods and the additional fitting, a link between the additional fitting and the connection fitting being made using the connection pin connecting the connection fitting and the junction fitting, the connection pin being inserted laterally, orthogonal to the median plane of the attachment device.