A servo-control having at least one movable cylinder that includes a hydraulic directional control valve. The hydraulic valve includes a control shaft that is rotatable about a longitudinal axis, the control shaft being connected to a distributor slide. The servo-control including a stationary abutment member secured to a cylinder and an input lever situated outside the cylinder. The input lever is connected to the control shaft and includes a stop portion arranged in the abutment member. The servo-control includes movement means for moving the input lever longitudinally, a first abutment surface of the abutment member limiting a travel amplitude of the stop portion when the input lever is in a first position.


    Access

    Download


    Export, share and cite



    Title :

    Servo-control and an aircraft having such a servo-control


    Contributors:

    Publication date :

    2017-08-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen / B64C AEROPLANES , Flugzeuge / F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein



    SERVO-CONTROL AND AN AIRCRAFT HAVING SUCH A SERVO-CONTROL

    BIHEL JEAN-ROMAIN / MARGER THIBAUT / PUJOL CHRISTOPHE et al. | European Patent Office | 2016

    Free access

    Servo control, rotor and aircraft

    COIEC CLEMENT / BIHEL JEAN-ROMAIN / GROLL ARNAUD | European Patent Office | 2020

    Free access

    SERVO CONTROL, ROTOR AND AIRCRAFT

    COIEC CLEMENT / BIHEL JEAN-ROMAIN / GROLL ARNAUD | European Patent Office | 2019

    Free access

    Servo Drone safety servo control system

    BAE KEUK DO | European Patent Office | 2022

    Free access

    SERVO ACTUATOR FOR AIRCRAFT

    GAIANO ANTONIO / TCHAVDAROV LUDMIL | European Patent Office | 2017

    Free access