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)。
HYDRAULIC ACTUATION SYSTEM
液压致动系统
2021-01-12
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |