An indicator assembly (300) for an aircraft landing gear for providing indication of a hard landing. The indicator assembly including an actuator member (314) pivotably movable when the pressure on a shock strut of the aircraft landing gear exceeds a desired load and stroke threshold indicative of a hard landing. A shear pin (306) is coupled to the actuator member which is configured to shear when a desired level of force is applied to at least a portion of the shear pin. A visibly recognizable indicator (308) is moved from a non-indicating position to an indicating position upon shearing of the shear pin.


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    Titel :

    System for indicating an airplane hard landing


    Weitere Titelangaben:

    System zur Anzeige einer harten Flugzeuglandung
    Système pour indiquer un atterrissage brutal d'avion


    Beteiligte:
    MARTIN DENNIS W (Autor:in) / ACKS JAMES P (Autor:in)

    Erscheinungsdatum :

    28.10.2015


    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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