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.


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    Title :

    SERVOCOMMANDE ET AERONEF MUNI D'UNE TELLE SERVOCOMMANDE


    Additional title:

    A SERVO-CONTROL AND AN AIRCRAFT HAVING SUCH A SERVO-CONTROL
    SERVOSTEUERUNG UND LUFTFAHRZEUG, DAS MIT EINER SOLCHEN SERVOSTEUERUNG AUSGESTATTET IST


    Contributors:

    Publication date :

    2017-03-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein



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