A hard landing indicator assembly (202) is disclosed herein. The hard landing indicator assembly includes a pressure relief valve (230), a hydraulic tube (232) having a first end and a second end, the first end coupled to the pressure relief valve (230), and a plunger (238) having a top portion and a shaft (23 8b), the plunger disposed in the hydraulic tube (232), wherein a portion of the shaft (23 8b) is a hard landing indicator (234) that extends outward from the hydraulic tube (232) in response to a hard landing event.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT HARD LANDING INDICATOR


    Additional title:

    INDIKATOR FÜR HARTE LANDUNGEN IN FLUGZEUGEN
    INDICATEUR D'ATTERRISSAGE DUR POUR AVION


    Contributors:

    Publication date :

    2024-06-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    AIRCRAFT HARD LANDING INDICATOR

    M N HEMANTH / BODKI BASAVARAJ | European Patent Office | 2024

    Free access

    Aircraft hard landing indicator

    M N HEMANTH / BODKI BASAVARAJ | European Patent Office | 2024

    Free access

    AIRCRAFT HARD LANDING INDICATOR

    MN HEMANTH / BODKI BASAVARAJ | European Patent Office | 2024

    Free access

    HARD LANDING INDICATOR FOR AN AIRCRAFT LANDING GEAR

    FERNELEY JOHN | European Patent Office | 2025

    Free access

    HARD LANDING INDICATOR FOR AN AIRCRAFT LANDING GEAR

    FERNELEY JOHN J C | European Patent Office | 2020

    Free access