A hard landing indicator assembly is disclosed herein. The hard landing indicator assembly includes a pressure relief valve, a hydraulic tube having a first end and a second end, the first end coupled to the pressure relief valve, and a plunger having a top portion and a shaft, the plunger disposed in the hydraulic tube, wherein a portion of the shaft is a hard landing indicator that extends outward from the hydraulic tube in response to a hard landing event.


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    Titel :

    Aircraft hard landing indicator


    Beteiligte:
    M N HEMANTH (Autor:in) / BODKI BASAVARAJ (Autor:in)

    Erscheinungsdatum :

    2024-07-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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