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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

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


    Beteiligte:

    Erscheinungsdatum :

    2016-07-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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

    BIHEL JEAN-ROMAIN / MARGER THIBAUT / PUJOL CHRISTOPHE et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    SERVO CONTROL, ROTOR AND AIRCRAFT

    COIEC CLEMENT / BIHEL JEAN-ROMAIN / GROLL ARNAUD | Europäisches Patentamt | 2019

    Freier Zugriff

    Servo control, rotor and aircraft

    COIEC CLEMENT / BIHEL JEAN-ROMAIN / GROLL ARNAUD | Europäisches Patentamt | 2020

    Freier Zugriff

    Servo Drone safety servo control system

    BAE KEUK DO | Europäisches Patentamt | 2022

    Freier Zugriff

    SERVO ACTUATOR FOR AIRCRAFT

    GAIANO ANTONIO / TCHAVDAROV LUDMIL | Europäisches Patentamt | 2017

    Freier Zugriff