A fuel tank inerting system (20) is provided including an air flow comprising air from a first source (24) having a first temperature and air from a second source (32) having a second temperature. The second temperature is cooler than the first temperature. At least one air separating module (30) is configured to separate an inert gas from the air flow.
TEMPERATURE CONTROL SYSTEM FOR FUEL TANK INERTING SYSTEM
TEMPERATURSTEUERUNGSSYSTEM FÜR KRAFTSTOFFTANKINERTISIERUNGSSYSTEM
SYSTÈME DE RÉGULATION DE TEMPÉRATURE POUR SYSTÈME D'INERTAGE DE RÉSERVOIR DE CARBURANT
2022-01-05
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
FUEL TANK INERTING SYSTEM AND METHOD FOR FUEL TANK INERTING
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