A multilayer bleed duct and its manufacturing method. The duct, configured to direct a flow of exhaust gases from an aircraft, includes an inner thermal insulating layer having a tubular surface which defines a passageway for the exhaust gases, comprises at least two edges, substantially parallel to each other, superposing or at least partially superposing along a longitudinal direction of the tubular surface, an outer layer made of fiber-reinforced composite material, an intermediate adhesive layer positioned between the inner layer and the outer layer.
MULTILAYER TUBULAR DUCT AND MANUFACTURING METHOD
2023-09-14
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |