A check device is provided for a flight actuator primary load path failure detection device 13 of the type that disconnects a position sensor 15 from the primary load path 1 in the event of a primary load path failure. The check device comprises: a mechanical linkage 40, 42, 44 for simulating disconnection of the position sensor 15 by permitting relative movement of at least first and second mechanical parts 32, 34 of the actuator that are unable to move relative to one another in normal use without failure of the primary load path 1, wherein these first and second mechanical parts 32, 34 include a first mechanical part 32 with movement detected by the position sensor 15 of the primary load path failure detection device 13.


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    Title :

    CHECK DEVICE FOR A FLIGHT ACTUATOR PRIMARY LOAD PATH FAILURE DETECTION DEVICE


    Additional title:

    PRÜFVORRICHTUNG FÜR EINE VORRICHTUNG ZUR FEHLERERKENNUNG DES PRIMÄREN LASTPFADES EINES FLUGAKTUATORS
    DISPOSITIF DE VÉRIFICATION POUR UN DISPOSITIF DE DÉTECTION DE DÉFAILLANCE D'UN TRAJET DE CHARGE PRIMAIRE D'UN ACTIONNEUR DE VOL


    Contributors:
    MOULON THOMAS (author) / AMARAL RUI (author)

    Publication date :

    2016-10-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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