A method of monitoring a high-lift system (200) on an aircraft (100) having a first drive station (201, 202, 203, or 204) installed on a first side of a flap (114 or 115) and a second drive station (201, 202, 203, or 204) installed on a second side of the flap, the method comprising: monitoring a current draw (11,12,13, or 14) of the first drive station for actuating the flap; identifying an expected current draw of the first drive station; comparing the monitored current draw of the first drive station to the expected current draw of the first drive station to determine if a differential between the monitored current draw and the expected current draw exceeds a first threshold; and generating a failure signal if the differential between the monitored current draw and the expected current draw exceeds the first threshold.


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    Titel :

    MONITORING OF HIGH-LIFT SYSTEMS FOR AIRCRAFT


    Weitere Titelangaben:

    ÜBERWACHUNG VON AUFTRIEBERHÖHENDEN SYSTEMEN FÜR FLUGZEUGE
    SURVEILLANCE DE SYSTÈMES HYPERSUSTENTATEURS POUR AVION


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

    Erscheinungsdatum :

    2019-03-06


    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



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    MOY GEORGE / PADILLA PETER A | Europäisches Patentamt | 2018

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    MOY GEORGE / PADILLA PETER A | Europäisches Patentamt | 2015

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    Condition Monitoring of Aircraft High Lift Systems

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


    Monitoring of high-lift systems for aircraft

    MOY GEORGE / PADILLA PETER A | Europäisches Patentamt | 2015

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