Disclosed is a hydraulic system (300) for an aircraft. The hydraulic system (300) comprises a backup hydraulic pressure source (216) to provide hydraulic pressure to a brake (222) in the event of a failure condition of a primary hydraulic brake pressure source. The hydraulic system (300) also comprises a landing gear backup system to provide hydraulic pressure to enable extension and/or retraction of landing gear (100). The backup hydraulic pressure source (216) is arranged to provide hydraulic pressure to the landing gear backup system in the event of a failure condition of a primary landing gear hydraulic pressure source.


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    Titel :

    AIRCRAFT HYDRAULICS


    Weitere Titelangaben:

    FLUGZEUGHYDRAULIK
    SYSTÈME HYDRAULIQUE D'AÉRONEF


    Beteiligte:
    HOWELL GEORGE (Autor:in) / CRANE NICHOLAS (Autor:in)

    Erscheinungsdatum :

    26.12.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRCRAFT HYDRAULICS

    HOWELL GEORGE / CRANE NICHOLAS | Europäisches Patentamt | 2018

    Freier Zugriff

    Aircraft hydraulics

    GEORGE HOWELL / NICHOLAS CRANE | Europäisches Patentamt | 2018

    Freier Zugriff



    Aircraft hydraulics

    Adams, H.W. | Engineering Index Backfile | 1943