A sensor system for a wing panel assembly of an aircraft includes a first end of a linkage assembly operatively coupled to a first slat panel. Also included is a second end of the linkage assembly operatively coupled to a second slat panel with a first ball joint. Further included is a block having a cutout portion surrounding the first ball joint. Yet further included is a sensing element disposed proximate the block to detect rotation of the block beyond a predetermined angle.


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    Titel :

    Sensor system for a wing panel assembly and method of monitoring a wing panel assembly


    Beteiligte:
    CARBONE MICHAEL (Autor:in) / BONNETT SCOTT C (Autor:in)

    Erscheinungsdatum :

    2018-08-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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