An inerting system for aircraft including a gas circuit with successively at least one air inlet, a compressor and an air separation module. The air separation module includes an outlet for oxygen-enriched gas and an outlet for inerting gas. The air separation module includes gas permeation membranes resistant to a temperature greater than or equal to 100° C. and preferably 140° C., and the inerting gas outlet is connected to a turbine for releasing pressure and cooling the inerting gas.
SYSTEME D'INERTAGE ET PROCEDE DE GENERATION D'UN GAZ D'INERTAGE DANS UN AERONEF, FONCTIONNANT SANS PRELEVEMENT D'AIR EXTERIEUR
INERTING SYSTEM AND METHOD FOR GENERATING AN INERTING GAS IN AN AIRCRAFT, OPERATING WITHOUT EXTERNAL AIR COLLECTION
INERTISIERUNGSSYSTEM UND ERZEUGUNGSVERFAHREN VON INERTISIERUNGSGAS IN EINEM LUFTFAHRZEUG, DAS OHNE AUSSENLUFTENTNAHME FUNKTIONIERT
2021-04-28
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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