A swivel axis for an aircraft engine attachment, comprising a tubular main axis which has, at a first end, a head and, at a second end, a threaded portion onto which is screwed a first nut. A fail-safe axis is configured to be mounted to swivel inside the main axis. The fail-safe axis has, at a first end, a head and, at a second end, a threaded portion onto which is screwed a second nut. The fail-safe axis is linked by an axial link to the first nut. Since the fail-safe axis is linked to the first nut, it is necessarily inserted into the main axis when the first nut is screwed onto the main axis.


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    Title :

    AXE DE PIVOTEMENT AMELIORE POUR UNE ATTACHE-MOTEUR D'AERONEF


    Additional title:

    IMPROVED PIVOTING AXIS FOR AN AIRCRAFT ENGINE ATTACHMENT
    VERBESSERTE SCHWENKACHSE FÜR EINE MOTORBEFESTIGUNG EINES LUFTFAHRZEUGS


    Contributors:

    Publication date :

    2020-02-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16C SHAFTS , Wellen



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