There is provided an hydraulic actuation system (10) for an aircraft, the hydraulic actuation system (10) includes an actuator (A), a primary actuation arrangement (100) to provide hydraulic fluid to control the actuator (A), wherein the hydraulic actuation system (10) is configured to detect a fault in the actuator (A). The hydraulic actuation system (10) also includes a secondary actuation arrangement (200) to provide hydraulic fluid to control the actuator (A) in response to a detection of a fault in the actuator (A).


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    Title :

    HYDRAULIC ACTUATION SYSTEM


    Additional title:

    SYSTEME D`ACTIONNEMENT HYDRAULIQUE


    Contributors:

    Publication date :

    2021-01-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F15B SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL , Druckmittelbetriebene Systeme allgemein



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