The detecting means (1) comprise measuring means (2) adapted to measure and provide at least one raw data corresponding to an aircraft parameter, computing means (3) adapted to estimate at least one derivative of said raw data, and detecting means (4) adapted to detect a failure with the aid of said derivative, said computing means (3) being adapted to estimate said derivative by differentiation.


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    Titel :

    Method and device for detecting a failure on an aircraft


    Beteiligte:
    GHEORGHE ANCA (Autor:in) / GOUPIL PHILIPPE (Autor:in) / DAYRE RÉMY (Autor:in) / ZOLGHADRI ALI (Autor:in) / CIESLAK JÉRÔME (Autor:in) / EFIMOV DENIS (Autor:in)

    Erscheinungsdatum :

    19.02.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / B64C AEROPLANES , Flugzeuge / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL