A landing gear system may include: a casing coupled to a fuselage of an aircraft, such as an urban air mobility vehicle; a steering , one side of which is inserted into the casing and the other side of which is connected to a tire; a magnetorheological (MR) damper including a cylinder coupled to the casing and a piston coupled to the steering rod; a sensor unit configured to measure a condition of the urban air mobility vehicle; and a controller configured to control damping force of the MR damper based on measurement data of the sensor unit. The sensor unit may include a first sensor for measuring a stroke of the MR damper and a second sensor for measuring an acceleration of the casing.


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    Titel :

    LANDING GEAR SYSTEM WITH MAGNETORHEOLOGICAL DAMPER


    Weitere Titelangaben:

    FAHRWERKSYSTEM MIT MAGNETORHEOLOGISCHEM DÄMPFER
    SYSTÈME DE TRAIN D'ATTERRISSAGE AVEC AMORTISSEUR MAGNÉTORHÉOLOGIQUE


    Beteiligte:
    KIM CHOUNG HYOUNG (Autor:in) / LEE JUNG HYUN (Autor:in) / HWANG EUGENE (Autor:in)

    Erscheinungsdatum :

    2024-06-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



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