An inerting fuel tank system comprising a closed tank and any number of flow impingement valves. The flow impingement valve allows uninhibited flow in one direction. In the reverse direction, the fluid flows back into the input flow stream thereby slowing / preventing the fluid flow outward. The flow impingement valve resists reverse flow of fluid out of a fuel tank vent due to sloshing or other flow dynamics.


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    Title :

    INERTING TANK SYSTEM


    Contributors:

    Publication date :

    2023-10-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B01D SEPARATION , Trennen



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