An aircraft has a fire suppression control system for a plurality of enclosures within the aircraft. The aircraft comprises a directional valve for each enclosure, sensors provided for each enclosure, for monitoring variables of the enclosure, one or more fire suppression agent bottles and a control unit for regulating the discharge of the fire suppression agent. The sensors are operatively linked by the control unit to a warning system in a cockpit of the aircraft.


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    Title :

    AIRCRAFT WITH FIRE SUPPRESSION CONTROL SYSTEM


    Contributors:

    Publication date :

    2017-01-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    A62C FIRE-FIGHTING , Feuerbekämpfung / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G08B SIGNALLING OR CALLING SYSTEMS , Signalisier- oder Rufsysteme



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