A fuel tank inerting system including: a catalytic reactor 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
2020-06-11
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G01K MEASURING TEMPERATURE , Messen der Temperatur / G07C TIME OR ATTENDANCE REGISTERS , Zeit- oder Anwesenheitskontrollgeräte |
CATALYST DEACTIVATION MONITORING OF CATALYTIC INERTING SYSTEM
European Patent Office | 2021
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