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


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    Titel :

    Two stage strut allowing low initial compression load


    Beteiligte:
    LUCE WILLIAM E (Autor:in)

    Erscheinungsdatum :

    2019-08-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16F SPRINGS , Federn



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