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.


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    Titel :

    Mechanical position indicator


    Beteiligte:

    Erscheinungsdatum :

    01.03.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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    Navigation position indicator

    Rittenhouse, H.O. | Engineering Index Backfile | 1887


    HEADREST POSITION INDICATOR

    STEPIN ALEKSANDR VALEREVICH / BARINOV MIKHAIL MIKHAJLOVICH / LEONOV KIRILL EDUARDOVICH | Europäisches Patentamt | 2019

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    "Blind" position indicator

    Cruzan, R. C. | NTRS | 1979


    Air position indicator

    Wahl, A. | Engineering Index Backfile | 1945