The control device (10) has a rotational drive and a linear control movement, which has load transmitting components for transferring a force or a torque, where a part of the load transmitting components is redundant. A load path is formed by a set of load-bearing components, where the rotational drive is comprised of a rotational portion of a gear, which is part of the load path. Another load path is formed by another set of load-bearing components. A monitoring unit with an actively actuated brake unit is provided for error detection, particularly for detecting functional disorders. An independent claim is provided for a method for detecting faults in a control device for an aircraft.


    Access

    Download


    Export, share and cite



    Title :

    DISPOSITIF DE REGLAGE, EN PARTICULIER DISPOSITIF DE REGLAGE POUR UN AERONEF


    Contributors:

    Publication date :

    2017-10-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16H Getriebe , GEARING




    Dispositif de réglage angulaire pour siège de véhicule

    TIMON MICHEL | European Patent Office | 2023

    Free access

    DISPOSITIF DE REGLAGE DE FIXATION POUR VEHICULE UTILITAIRE

    VIRY PATRICK / VAZQUEZ RUBEN / VAZQUEZ SABARIEGO JOSE IGNACIO | European Patent Office | 2020

    Free access

    DISPOSITIF DE REGLAGE D'ENTREE D'AIR

    STEE LUCIEN / PARIS PIERRE YVES / BOURIAUD DAVID | European Patent Office | 2019

    Free access