Monitoring of high-lift systems for aircraft. In one configuration, a method for monitoring a high-lift system includes monitoring a first current draw of a first drive station of the high-lift system, and monitoring a second current draw of a second drive station of the high-lift system. The method further includes comparing the first current draw and the second current draw to determine if a differential between the first current draw and the second current draw exceeds a threshold, and generating a failure signal if the differential between the first current draw and the second current draw exceeds the threshold.


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    Titel :

    MONITORING OF HIGH-LIFT SYSTEMS FOR AIRCRAFT


    Beteiligte:
    MOY GEORGE (Autor:in) / PADILLA PETER A (Autor:in)

    Erscheinungsdatum :

    2015-07-16


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / G01R Messen elektrischer Größen , MEASURING ELECTRIC VARIABLES



    MONITORING OF HIGH-LIFT SYSTEMS FOR AIRCRAFT

    MOY GEORGE / PADILLA PETER A | Europäisches Patentamt | 2018

    Freier Zugriff

    MONITORING OF HIGH-LIFT SYSTEMS FOR AIRCRAFT

    MOY GEORGE / PADILLA PETER A | Europäisches Patentamt | 2019

    Freier Zugriff

    Monitoring of high-lift systems for aircraft

    MOY GEORGE / PADILLA PETER A | Europäisches Patentamt | 2015

    Freier Zugriff

    Condition monitoring of aircraft high lift systems

    Chan, K.W. / Southcombe, G. / Trmal, G.J. et al. | Tema Archiv | 1990


    Condition Monitoring of Aircraft High Lift Systems

    Chan, K W / Southcombe, G / Trmal, G J et al. | SAGE Publications | 1990