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).
ENSEMBLE MOTEUR POUR AERONEF COMPRENANT UN MOTEUR AINSI QU'UN MAT D'ACCROCHAGE D'UN TEL MOTEUR
ENGINE ASSEMBLY FOR AN AIRCRAFT COMPRISING AN ENGINE AS WELL AS AN ENGINE MOUNTING STRUCTURE
MOTORANORDNUNG FÜR EIN FLUGZEUG MIT EINEM MOTOR SOWIE EINER MOTORMONTAGESTRUKTUR
2017-09-06
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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