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

The assembly (1) has an engine mounting structure (4) comprising a rigid structure (10) with a shell (24) and a mounting system interposed between a jet engine (2) and structure (10), where the system includes front engine attachment and rear engine attachment (8). A thermal protection system (58) p...

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Bibliographische Detailangaben
Hauptverfasser:	LAFONT, Laurent, JOURNADE, Frédéric
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	The assembly (1) has an engine mounting structure (4) comprising a rigid structure (10) with a shell (24) and a mounting system interposed between a jet engine (2) and structure (10), where the system includes front engine attachment and rear engine attachment (8). A thermal protection system (58) protects the shell and has a ventilated duct (60) forming a thermal barrier. The duct extends, between the shell and engine, towards a rear beyond the rear engine attachment. The duct has a rear end (71) arranged on a detachment or break in an external wall of a fairing (66) of the structure (4).