An aircraft fuel tank system includes at least one fuel tank having a plurality of interconnected bays and a vent arranged so as to allow an inward venting of atmospheric air. The system is arranged so as to direct the inwardly vented air along a vent duct. The vent duct is arranged so as to convey the inwardly vented air to substantially each one of the interconnected bays.
AIRCRAFT FUEL TANK INERTING SYSTEM
INERTISIERUNGSSYSTEM FÜR EINEN FLUGZEUGTREIBSTOFFTANK
SYSTÈME D'INERTAGE DE RÉSERVOIR À CARBURANT POUR AVION
2023-01-18
Patent
Electronic Resource
English