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.

    L'invention concerne un aéronef qui comprend une structure d'aéronef, une surface de commande de vol fixée à la structure d'aéronef, et un bloc d'alimentation hydraulique local disposé à proximité de la surface de commande de vol. Le bloc d'alimentation hydraulique local est configuré pour fournir un fluide hydraulique mis sous pression pour actionner la surface de commande de vol. Le bloc d'alimentation hydraulique local comprend un réservoir pour le fluide hydraulique et deux pompes hydrauliques pour mettre le fluide hydraulique sous pression.


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    Title :

    AIRCRAFT WITH DISTRIBUTED HYDRAULIC SYSTEM


    Additional title:

    AÉRONEF AVEC SYSTÈME HYDRAULIQUE DISTRIBUÉ


    Contributors:

    Publication date :

    2017-01-05


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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