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:
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