A sensor system for a wing panel assembly of an aircraft includes a first end 14 of a linkage assembly 12 operatively coupled to a first slat panel 16. Also included is a second end 18 of the linkage assembly operatively coupled to a second slat panel 20 with a first ball joint 22. Further included is a block 30 having a cutout portion 34 surrounding the first ball joint. Yet further included is a sensing element 40 disposed proximate the block to detect rotation of the block beyond a predetermined angle.


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    Title :

    SENSOR SYSTEM FOR A WING PANEL ASSEMBLY AND METHOD OF MONITORING A WING PANEL ASSEMBLY


    Additional title:

    SENSORSYSTEM FÜR EINE FLÜGELPLATTENANORDNUNG UND VERFAHREN ZUR ÜBERWACHUNG EINER FLÜGELPLATTENANORDNUNG
    SYSTÈME DE CAPTEUR POUR UN ENSEMBLE DE PANNEAU D'AILE ET PROCÉDÉ DE SURVEILLANCE D'UN ENSEMBLE DE PANNEAU D'AILE


    Contributors:

    Publication date :

    2016-06-01


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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