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
MEHRSCHICHTIGER ROHRFÖRMIGER KANAL UND HERSTELLUNGSVERFAHREN
CONDUIT TUBULAIRE MULTICOUCHE ET PROCÉDÉ DE FABRICATION
2023-06-07
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |