SUSPENSION ASSEMBLY FOR AN AIRCRAFT TURBOJET ENGINE

摘要

The invention relates to a suspension assembly for an aircraft turbojet engine (3), including a pylon (1) and connecting rods (13a, 13b) for taking up the thrust of the turbojet engine (3) and connected to the pylon (1), remarkable in that the assembly includes means (19a, 19b; 25) separate from said pylon for thermally insulating the connecting rods (13a, 13b) from the turbojet engine (3).