An aircraft assembly (10) having an indicator (20) configured to provide an indication of when an element of the aircraft assembly has received a predetermined load or traveled to a predetermined position.

    Un assemblage daéronef (10) comportant un indicateur (20) configuré pour fournir une indication du moment où un élément de lassemblage a reçu une charge prédéterminée ou quil sest déplacé à une position prédéterminée.


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    Title :

    AN AIRCRAFT ASSEMBLY WITH LOAD AND POSITION INDICATOR


    Additional title:

    UN MECANISME D'AERONEF DOTE D'UN INDICATEUR DE CHARGE ET DE POSITION


    Contributors:

    Publication date :

    2018-03-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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 / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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