A monitor system for monitoring the reliability of at least one piece of electronic equipment installed in an aircraft. In order to monitor each piece of electronic equipment, such a monitor system comprises: monitor means for measuring variations of at least one state parameter P as a function of time t; concatenation means for generating data groups (ti, Pi, Sj); transmission means for transmitting the data groups (ti, Pi, Sj) to a centralized unit; first computation means for determining an observed reliability Robs of the or each piece of electronic equipment; second computation means for determining an expected reliability Rexp of the or each piece of electronic equipment; comparator means for comparing the observed reliability Robs with the expected reliability Rexp of the or each piece of electronic equipment; and warning means.


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    Title :

    PROCEDE ET SYSTEME DE CONTROLE DE LA FIABILITE D'AU MOINS UN EQUIPEMENT ELECTRONIQUE INSTALLE DANS UN AERONEF


    Contributors:

    Publication date :

    2017-12-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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