A method of determining whether a landing event of an aircraft is hard may comprise: receiving, by a controller (230) via a stroke position sensor (116), a stroke profile as a function of time for a shock strut; receiving, by the controller via a gas pressure sensor (110), a gas pressure in a gas chamber of the shock strut; receiving, by the controller via a wheel speed sensor (120), a wheel speed of a tire in a landing gear assembly; calculating, by the controller, multiple time dependent functions based on the stroke profile of the shock strut, based on the gas pressure, a shock strut temperature, and the wheel speed; and comparing, by the controller, the multiple time dependent functions to respective predetermined thresholds to determine whether the landing event is hard.


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    Titel :

    HARD-LANDING DETECTION SYSTEM


    Weitere Titelangaben:

    SYSTEM ZUR DETEKTION VON HARTEN LANDUNGEN
    SYSTÈME DE DÉTECTION D'ATTERRISSAGE BRUTAL


    Beteiligte:
    FAZELI AMIR (Autor:in) / KIELSTRA EBENEZER (Autor:in) / CEPIC ADNAN (Autor:in)

    Erscheinungsdatum :

    22.06.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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