A hydraulic system 300 for an aircraft including 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 includes 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


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

    Erscheinungsdatum :

    01.03.2022


    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