(EN) An engine assembly includes a nacelle configured to at least partially surround an engine and a thrust reverser coupled to the nacelle. The thrust reverser includes: a thrust-reversing element movable relative to the nacelle between a stowed position and a deployed position; a hydraulic actuator operably coupled to move the thrust-reversing element; and a fluid control system configured to operate the hydraulic actuator. The fluid control system includes: a directional control unit including a directional control valve operable to selectively route fluid between a pressurized fluid source, the actuator, and a fluid return reservoir; one or more bypass fluid lines providing fluid communication between the actuator and the fluid return reservoir independent of the directional control valve; and a flow limiter residing between the pressurized fluid source and the directional control valve, the flow limiter configured to inhibit a pressure draw by the actuator from surpassing a predetermined threshold.
(ZH) 发动机组件包括被构造成至少部分地包围发动机的机舱和联接到机舱的推力反向器。推力反向器包括：可相对于机舱在收起位置和展开位置之间移动的推力反向元件；可操作地联接以使推力反向元件移动的液压致动器；和被构造成操作液压致动器的流体控制系统。流体控制系统包括：方向控制单元，其包括可操作以在加压流体源、致动器和流体返回贮器之间选择性地引导流体的方向控制阀；一条或更多条旁路流体管线，其独立于方向控制阀在致动器和流体返回贮器之间提供流体连通；以及位于加压流体源和方向控制阀之间的限流器，该限流器被构造成阻止由致动器抽取的压力超过预定阈值。
