A fuel tank inerting system including: a catalytic reactor (222) comprising an inlet, an outlet, a reactive flow path between the inlet and the outlet, a catalyst on the reactive flow path, and a temperature sensor located between the inlet and outlet, wherein the catalytic reactor is arranged to receive fuel from a fuel source and air from an air source that are mixed to form a combined flow, and to react the combined flow along the reactive flow path to generate an inert gas.
CATALYST DEACTIVATION MONITORING OF CATALYTIC INERTING SYSTEM
KATALYSATORDEAKTIVIERUNGSÜBERWACHUNG EINES KATALYTISCHEN INERTISIERUNGSSYSTEMS
SURVEILLANCE DE DÉSACTIVATION DE CATALYSEUR DE SYSTÈME D'INERTAGE CATALYTIQUE
17.11.2021
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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