| 摘要 |
The invention relates to an aircraft engine assembly (1) comprising an engine (2) and an engine mount (4), this engine mount including firstly a rigid structure (10) comprising a box (24) and secondly a mounting system (11) positioned between the engine and the rigid structure, this mounting system notably comprising an aft attachment (8), the assembly also being provided with a thermal protection system (58) for the box, comprising a preferably ventilated duct (60) forming a heat barrier and extending between this box and the engine. According to the invention, the duct extends rearward beyond the aft engine attachment.
|
