A hydraulic system for an aircraft having an engine and an auxiliary power unit includes a first hydraulic subsystem including a first hydraulic pump and a first set of hydraulic-powered components in fluid communication with the first hydraulic pump. The first hydraulic pump is powered by the engine to pump shared hydraulic fluid to the first set of hydraulic-powered components. The hydraulic system includes a second hydraulic subsystem including a second hydraulic pump and a second set of hydraulic-powered components in fluid communication with the second hydraulic pump. The second hydraulic pump is powered by the auxiliary power unit to pump the shared hydraulic fluid to the second set of hydraulic-powered components. A shared return line subsystem and reservoir is in fluid communication with the first and second hydraulic subsystems to return the shared hydraulic fluid to the first and second hydraulic pumps.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft Hydraulic Systems Having Shared Components



    Erscheinungsdatum :

    2018-09-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Aircraft hydraulic systems having shared components

    ELVING CARL THEODORE / REYNOLDS ROBERT PAUL / HAWTHORNE DAVID ALAN et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    AIRCRAFT HYDRAULIC SYSTEMS HAVING SHARED COMPONENTS

    ELVING CARL THEODORE / REYNOLDS ROBERT PAUL / HAWTHORNE DAVID ALAN et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    GERMAN AIRCRAFT and HYDRAULIC SYSTEMS Their Components

    DAVIES, R. H. | SAE Technical Papers | 1946


    Hydraulic control systems and methods for components of an aircraft

    THOMPSON DREW M / FAHEY PATRICK M / SMITH PAUL et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Aircraft hydraulic systems

    Neese, William A. | TIBKAT | 1987