The invention relates to a gear reducer (1) for a cockpit control device of an aircraft, the gear reducer comprising a frame (3) and a fork (5), movable in rotation relative to the frame around a fork axis (X5), the fork comprising two arms (7, 8). The gear reducer comprises two rollers (13, 15), the rollers being respectively mounted at an end (12, 14) of the arms, and a cam (21), movable in rotation relative to the frame around a cam axis (X21) parallel to the fork axis, the rollers being in rolling contact respectively with opposed sides (21 A, 21 B) of the cam, one among the fork and the cam being an input of the gear reducer, the other being an output of the gear reducer.


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    Title :

    GEAR REDUCER FOR A COCKPIT CONTROL DEVICE OF AN AIRCRAFT, AND CONTROL DEVICE COMPRISING SUCH A GEAR REDUCER


    Additional title:

    UNTERSETZUNGSGETRIEBE FÜR EINE COCKPITSTEUERUNGSVORRICHTUNG EINES FLUGZEUGS UND STEUERUNGSVORRICHTUNG MIT SOLCH EINEM UNTERSETZUNGSGETRIEBE
    RÉDUCTEUR À ENGRENAGES POUR DISPOSITIF DE COMMANDE DE COCKPIT D'UN AVION, UN TEL DISPOSITIF COMPRENANT LEDIT ENGRENAGE


    Contributors:

    Publication date :

    2019-10-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / G09B Unterrichts- oder Vorführungsgeräte , EDUCATIONAL OR DEMONSTRATION APPLIANCES



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