A fire-suppression system includes an aviation vehicle and a fluid transport and delivery system. The fluid transport and delivery system is coupled to a vehicle frame of the aviation vehicle and is located within a cabin of the vehicle frame. The fluid transport and delivery system includes a tank having an exit aperture formed in a bottom wall of the tank, a plug aligned with the exit aperture of the tank, and a plug actuator configured to move the plug along an axis from an open position, in which the fluid stored in the tank passes around the plug and through the exit aperture, to a closed position, in which fluid is blocked from exiting through the exit aperture.


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    Title :

    FIRE SUPPRESSION SYSTEM FOR AVIATION VEHICLE


    Contributors:

    Publication date :

    2021-09-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    A62C FIRE-FIGHTING , Feuerbekämpfung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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