DEVICE FOR ATTACHING AN AIRCRAFT ENGINE INCLUDING A THRUST FORCE COLLECTION DEVICE WITH REDUCED OVERALL DIMENSIONS

摘要

The invention mainly relates to a device for attaching an aircraft engine that comprises a rigid structure (10) and a means for attaching the engine on said rigid structure, said attachment means including a rear engine fastener (8) and a device (9) for collecting the thrust forces generated by the engine, the rear engine fastener (8) being attached on the rigid structure by two side brackets attached to the rigid structure, said force collecting device (9) including two connecting rods (26a, 26b) mechanically connected to a rudder bar (28) by a mechanical link, a connection bracket (49) attached on the rear engine fastener (8) and mechanically connected to the rigid structure (10) by a thrust axis (60) wherein the side brackets include abutment means limiting the tilting of the rudder bar (28) in the case of breakage of a connecting rod (26a, 26b) and ensuring the transmission of the thrust forces to the rigid structure (10).