A hydraulic system (14) in an aircraft (10) and configured to supply hydraulic power to one or more hydraulic components (16) in the aircraft (10) by means of an operating hydraulic fluid, the hydraulic system (14) including a system pumping device (26) for priming and pumping the operating hydraulic fluid from a system inlet (24) of the hydraulic system (14) and to the hydraulic components.


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    Title :

    HYDRAULIC SYSTEM FOR AN AIRCRAFT, HYDRAULIC ARRANGEMENT, AIRCRAFT, AIRCRAFT ARRANGEMENT, AND METHOD FOR TESTING SUCH HYDRAULIC SYSTEM


    Contributors:
    KLOSE JULIAN (author) / HAMM MARTIN (author) / GÖSSING ROLF (author)

    Publication date :

    2025-05-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64C AEROPLANES , Flugzeuge / F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein




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