An aircraft comprises an aircraft structure, a flight control surface attached to the aircraft structure, and a local hydraulic power pack disposed proximal to the flight control surface. The local hydraulic power pack is configured to provide pressurized hydraulic fluid for actuating the flight control surface. The local hydraulic power pack comprises a reservoir for the hydraulic fluid and two hydraulic pumps for pressurizing the hydraulic fluid.


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    Title :

    AIRCRAFT WITH DISTRIBUTED HYDRAULIC SYSTEM


    Additional title:

    FLUGZEUG MIT VERTEILTEM HYDRAULIKSYSTEM
    AÉRONEF AVEC SYSTÈME HYDRAULIQUE DISTRIBUÉ


    Contributors:

    Publication date :

    2023-10-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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