A fuel tank inerting system uses a catalytic oxidation unit to combust fuel from the fuel tank to produce inert gas, simultaneously working with a gas separator that removes dissolved carbon dioxide from the fuel before it is cycled to the thermal management system (TMS) or the engine. This prevents cavitation of carbon dioxide (gaseous bubbling) within the fuel at varying temperatures while in flight.


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    Titel :

    CAVITATION MITIGATION IN CATALYTIC OXIDATION FUEL TANK INERTING SYSTEMS


    Beteiligte:

    Erscheinungsdatum :

    2019-09-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B01D SEPARATION , Trennen / B01J Chemische oder physikalische Verfahren, z.B. Katalyse oder Kolloidchemie , CHEMICAL OR PHYSICAL PROCESSES, e.g. CATALYSIS OR COLLOID CHEMISTRY / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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