A hydraulic system of an aircraft, the system comprising at least one servo-control, each servo-control comprising at least one cylinder together with a drive rod and a piston arranged in each cylinder. Between each cylinder of servo-control and the drive rod of that servo-control, at least one servo-control presents main sealing means with controlled leakage allowing a hydraulic fluid to leak out from the cylinder, the hydraulic system further comprising at least one enclosure, each cylinder of the servo-control being arranged inside the enclosure so that the fluid is collected in the enclosure.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft hydraulic system comprising at least one servo-control, and an associated rotor and aircraft


    Beteiligte:
    BIHEL JEAN-ROMAIN (Autor:in) / COIC CLEMENT (Autor:in) / MARGER THIBAUT (Autor:in) / COUDERC GERARD (Autor:in)

    Erscheinungsdatum :

    30.08.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    AIRCRAFT HYDRAULIC SYSTEM COMPRISING AT LEAST ONE SERVO-CONTROL, AND AN ASSOCIATED ROTOR AND AIRCRAFT

    BIHEL JEAN-ROMAIN / COIC CLEMENT / MARGER THIBAUT et al. | Europäisches Patentamt | 2015

    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

    Hydraulic servo actuation system and method for aircraft

    WANG XIAOYING / LIU ZHIYU / HONG QIAN | Europäisches Patentamt | 2024

    Freier Zugriff