Thrust reverser velocity control valve

A turbofan engine assembly comprising:

• a turbofan engine;
• a nacelle surrounding the turbofan engine and defining an annular bypass duct through the turbofan engine to define a generally forward-to-aft bypass air flow path;
• a thrust reverser comprising:
• a first moveable element, moveable to and from a reversing position where at least a portion of bypass air flow is reversed;
• a hydraulic actuator coupled to the first moveable element to move the first moveable element into and out of the reversing position;
• and
• a second moveable element, configured to move in synchronicity with the first moveable element and into and out of a predetermined position;
• a first hydraulic valve operable to control a flow of hydraulic fluid for actuation of the hydraulic actuator;
• and
• a second hydraulic valve operably coupled to the second moveable element and moveable in synchronicity with the second moveable element between a restricted condition when the second moveable element is in the predetermined position wherein the flow of hydraulic fluid is restricted, and a permit condition when the second moveable element is out of the predetermined position wherein the flow of hydraulic fluid is permitted.