An aircraft fuel tank inerting arrangement 1 is provided for providing oxygen-depleted gas to one or more aircraft fuel tanks. The arrangement comprises a gas inlet 2 supplying oxygen-containing gas to an oxygen remover 10 that is configured to remove oxygen to produce an oxygen-depleted gas. A first flow control valve 12 controls the flow of oxygen depleted gas to at least one gas outlet for supply of oxygen-depleted gas to an aircraft fuel tank.
Aircraft fuel tank inerting arrangement
2015-06-03
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |