A method for testing a component in a high lift system of an aircraft comprises the steps of activating a brake coupled with at least one hydraulic motor, commanding a rotation of the at least one hydraulic motor for a predetermined period of time, wherein the brake remains activated, acquiring a sensor output of a motion sensor coupled with a central power control unit for moving a high lift surface during the commanded rotation of the at least one hydraulic motor, determining a motion of the power control unit from the acquired sensor output, comparing the determined motion with a predetermined threshold value, and generating a brake indication signal if the determined motion exceeds the predetermined motion threshold value.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    METHOD FOR TESTING A COMPONENT IN A HIGH LIFT SYSTEM OF AN AIRCRAFT


    Beteiligte:

    Erscheinungsdatum :

    2016-06-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



    METHOD FOR TESTING COMPONENT IN HIGH LIFT SYSTEM OF AIRCRAFT

    ANDREAS FLEDDERMANN / VINCENT MAIRE / JAN-AREND VAN BRUGGEN | Europäisches Patentamt | 2016

    Freier Zugriff


    METHOD FOR DETERMINING STATE OF COMPONENT IN HIGH LIFT SYSTEM OF AIRCRAFT, HIGH LIFT SYSTEM OF AIRCRAFT AND AIRCRAFT HAVING SUCH HIGH LIFT SYSTEM

    EUGEN NEB / JAN-AREND VAN BRUGGEN / MICHAEL BRADY et al. | Europäisches Patentamt | 2016

    Freier Zugriff


    METHOD FOR TESTING A COMPONENT IN A HIGH LIFT SYSTEM OF AN AIRCRAFT

    FLEDDERMANN ANDREAS / MAIRE VINCENT / VAN BRUGGEN JAN-AREND | Europäisches Patentamt | 2023

    Freier Zugriff