An aircraft including at least one turbine engine and a monitoring device associated with the turbine engine, the turbine engine being linked firstly to circuits including fluid circuits and electric circuits, and secondly to sensors for monitoring the turbine engine and the circuits, the sensors including at least one fire sensor and sensors for monitoring the fluid circuits, sensors for monitoring the electric circuits and sensors for monitoring the operation of the turbine engine, the monitoring device being linked to the sensors and including a central processing unit to generate a signal indicating the occurrence of a fire on the turbine engine only if a fire sensor and a sensor for monitoring a fluid circuit or an electric circuit or the operation of the turbine engine transmit a signal indicating an anomaly.


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    Title :

    DISPOSITIF DE SURVEILLANCE D'UNE TURBOMACHINE D'UN AERONEF


    Additional title:

    MONITORING SYSTEM OF AN AIRCRAFT TURBINE ENGINE
    ÜBERWACHUNGSSYSTEM EINES TURBOTRIEBWERKS EINES LUFTFAHRZEUGS


    Contributors:

    Publication date :

    2019-08-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / A62C FIRE-FIGHTING , Feuerbekämpfung / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / G08B SIGNALLING OR CALLING SYSTEMS , Signalisier- oder Rufsysteme






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    Free access

    PROCÉDÉ DE COMMANDE D'UN MOTEUR D'UNE COMMANDE D'UN AÉRONEF, DISPOSITIF DE COMMANDE ET AÉRONEF

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    Free access