A landing detection system (300) for a landing gear assembly of an aircraft may comprise a moveable member (309) mechanically coupled between an aircraft wheel and a strut piston (212), wherein the moveable member (309) is in communication with a strut chamber pressure of the landing gear assembly, wherein the moveable member (309) moves relative to the strut piston (212) in response to a first force applied to the aircraft wheel and the strut piston (212) strokes in response to a second force applied to the aircraft wheel.


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    Title :

    TWO STAGE STRUT ALLOWING LOW INITIAL COMPRESSION LOAD


    Additional title:

    ZWEISTUFIGES FEDERBEIN, DAS EINE GERINGE ANFÄNGLICHE DRUCKBELASTUNG ERLAUBT
    JAMBE À AMORTISSEUR À DEUX ÉTAGES PERMETTANT UNE CHARGE DE COMPRESSION INITIALE FAIBLE


    Contributors:

    Publication date :

    2020-05-13


    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



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