A mechanical position indicator for providing a visual indication that a first part of an aircraft landing gear has assumed a predetermined position relative to a second part, the position indicator being arranged to be coupled to a first one of the first and second parts and in a first state arranged to hold an indicator element in a deployed position, the position indicator being arranged such that upon the first part assuming the predetermined position relative to the second part, a second one of the first and second parts changes the position indicator from the first state to a second state in which the indicator element is displaced from the deployed position, the position indicator being arranged to inhibit the indicator element thereafter returning to the deployed position.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Mechanical position indicator


    Beteiligte:

    Erscheinungsdatum :

    01.03.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / G01L Messen von Kraft, mechanischer Spannung, Drehmoment, Arbeit, mechanischer Leistung, mechanischem Wirkungsgrad oder des Drucks von Fluiden , MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE



    MECHANICAL POSITION INDICATOR FOR AN AIRCRAFT LANDING GEAR

    HODGKINSON BEN / LACY STUART / WEBB CHRIS et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    Crane Position Indicator

    CRANNEY III RICHARD A | Europäisches Patentamt | 2021

    Freier Zugriff

    TAILGATE POSITION INDICATOR

    KROB MONTI | Europäisches Patentamt | 2023

    Freier Zugriff

    POSITION INDICATOR BEACON

    SAMARAI FARIS | Europäisches Patentamt | 2016

    Freier Zugriff

    Rudder position indicator

    ZIMMERMAN ROSS M | Europäisches Patentamt | 2016

    Freier Zugriff