ENGINE ASSEMBLY FOR AN AIRCRAFT COMPRISING AN ENGINE AS WELL AS AN ENGINE MOUNTING STRUCTURE

摘要

The invention concerns an engine assembly (1) for an aircraft comprising an engine (2) and an engine mounting structure (4), said structure comprising a rigid structure (10) including a structure box (24) and a mounting system (11) interposed between the engine and the rigid structure, said mounting system including in particular a rear attachment (8), the assembly being further provided with a system for thermal protection (58) of the structure box comprising a duct (60) preferably ventilated and forming a thermal barrier and extending between said structure box and the engine. The invention is characterized in that the duct extends towards the rear beyond the rear engine attachment.