A system (104) includes a turbo pump (206) to convert compressed gas into power, a storage tank (200, 202, 204) to store the compressed gas, and a fire suppression control valve (208) having a closed position in which the compressed gas is prevented from flowing to the cargo compartment (102) and an open position in which the compressed gas is ported to the cargo compartment (102) to suppress a fire. The system (104) also includes a pump control valve (212) having a closed position in which the compressed gas is prevented from flowing to the turbo pump (206) and an open position in which the compressed gas is ported to the turbo pump (206) to cause the turbo pump (206) to convert the compressed gas into the power. The system also includes an OBIGGS (118) to convert bleed air from a gas turbine engine (114) into an inert gas to provide low rate discharge (LRD) fire suppression to the cargo compartment (102).


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    Title :

    SYSTEMS AND METHODS FOR PROVIDING POWER AND FIRE SUPPRESSION USING A TURBO PUMP, COMPRESSED GAS, AND AN OBIGGS


    Additional title:

    SYSTEME UND VERFAHREN ZUR BEREITSTELLUNG VON ENERGIE- UND BRANDUNTERDRÜCKUNG UNTER VERWENDUNG EINER TURBOPUMPE, EINES DRUCKGASES UND EINES OBIGGS
    SYSTÈMES ET PROCÉDÉS POUR FOURNIR UNE PUISSANCE ET UNE SUPPRESSION D'INCENDIE À L'AIDE D'UNE POMPE DE TURBOCOMPRESSEUR, GAZ COMPRIMÉ ET OBIGGS


    Contributors:

    Publication date :

    2024-02-28


    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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