An intake duct assembly for an auxiliary power unit system is provided. A first inlet adapter (210) includes at least one hole (332) through the duct wall. A fire containment apparatus (230) forms a first passage to direct intake air between exterior wall of the aircraft and the enclosure. An inner duct (500) mounted on the first inlet adapter (210) at a first position downstream of the at least one hole and mounted on a second inlet adapter (220). An outer sheath (550) is mounted on the first inlet adapter (210) at a second position upstream of the at least one hole and mounted on the second inlet adapter (220). The outer sheath (550) circumscribes the inner duct (500) to form at least a portion of a barrier annulus between the inner duct (500) and outer sheath (550) in fluid communication with the first passage via the at least one hole in the first inlet adapter (210).
FIRE CONTAINMENT APPARATUSES FOR AIRCRAFT DUCT ASSEMBLIES
BRANDEINDÄMMUNGSVORRICHTUNGEN FÜR FLUGZEUGLEITUNGSKANALBAUGRUPPEN
APPAREILS DE CONFINEMENT D'INCENDIE POUR ENSEMBLES DE CONDUIT D'AÉRONEF
2019-02-20
Patent
Electronic Resource
English
FIRE CONTAINMENT APPARATUSES FOR AIRCRAFT DUCT ASSEMBLIES
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