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 tocontrol 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).

    提供了一种用于飞机的液压致动系统(10),所述液压致动系统(10)包括:致动器(A);主致动布置(100),所述主致动布置用于提供液压流体以控制所述致动器(A),其中所述液压致动系统(10)被配置为检测所述致动器(A)中的故障。所述液压致动系统(10)还包括辅致动布置(200)以用于响应于对所述致动器(A)中的故障的检测而提供液压流体以控制所述致动器(A)。


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    Title :

    HYDRAULIC ACTUATION SYSTEM


    Additional title:

    液压致动系统


    Contributors:

    Publication date :

    2021-01-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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