A fire detection system includes a heat detector controller and a multiplicity of heat detectors. The heat detectors are positioned at predetermined locations along a ceiling of a cargo compartment and/or on an exterior side of a cargo compartment liner from an interior of the cargo compartment. Each of the multiplicity of heat detectors are configured to measure temperature and to transmit temperature measurements to the heat detector controller. The heat detector controller is configured to determine that a fire has breached the cargo compartment liner based on the temperature measurements.


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    Title :

    Airplane fire detection system


    Contributors:

    Publication date :

    2018-06-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G08B SIGNALLING OR CALLING SYSTEMS , Signalisier- oder Rufsysteme



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