Limited flow thrust reverser actuating
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.
1. An engine assembly, comprising:
a nacelle configured to at least partially surround an engine; and
a thrust reverser coupled to the nacelle, the thrust reverser comprising:
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 between the stowed position and the deployed position; and
a fluid control system configured to operate the hydraulic actuator, the fluid control system comprising: a directional control unit including a directional control valve operable to selectively route fluid between an isolation valve, the actuator, and a fluid return reservoir;
an isolation control unit comprising the isolation control valve operable to selectively route fluid flow between a pressurized fluid source and the directional control unit; one or more bypass fluid lines providing fluid communication between the actuator and the fluid return reservoir independent of the isolation control valve and 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;
wherein the isolation control valve is operable to selectively inhibit or permit fluid flow between the directional control valve and the pressurized fluid source and the fluid return reservoir; and
wherein the isolation control unit further includes a piloted valve operable in a first stage, where fluid flow from the fluid return reservoir to the actuator through the one or more bypass fluid lines is inhibited, and a second stage, where fluid flow from the fluid return reservoir to the actuator is uninhibited.
2. The engine assembly of claim 1 , wherein the isolation control unit further comprises a solenoid valve coupled to both the isolation control valve and the piloted valve, and configured to concurrently control operation of the isolation control valve and the piloted valve.
3. The engine assembly of claim 2 , wherein the solenoid valve is configured to initiate transition of the piloted valve from the first stage to the second stage in response to receiving a thrust-reverser-deploy command.
4. The engine assembly of claim 1 , wherein the directional control valve is operable in a deploy stage, where fluid from the fluid source is routed to both a deploy chamber and a stow chamber of the actuator, and a stow stage, where fluid from the fluid source is routed only to the stow chamber of the actuator; and
wherein, when the directional control valve is in the deploy stage, the deploy and stow chambers are placed in fluid communication with one another to permit fluid recirculation.
5. The engine assembly of claim 1 , wherein the fluid control system further comprises an anti-cavitation check valve residing on the one or more bypass fluid lines, the check valve configured to permit fluid flow from the fluid return reservoir to the actuator, while inhibiting fluid flow from the actuator to the fluid return reservoir.
6. The engine assembly of claim 5 , wherein the anti-cavitation check valve is configured to permit fluid flow when the pressure in a deploy chamber of the actuator is less than the pressure at the fluid return reservoir.
7. The engine assembly of claim 1 , wherein the flow limiter comprises at least one of a flow regulator or a flow restrictor.
8. The engine assembly of claim 1 , wherein the flow limiter is incorporated in the directional control unit.
9. A fluid control system configured to operate a hydraulic actuator coupled to a thrust-reversing element coupled to a nacelle of an engine assembly, the fluid control system comprising:
a directional control unit including a directional control valve operable to selectively route fluid between an isolation valve, the hydraulic actuator, and a fluid return reservoir,
an isolation control unit comprising an isolation control valve operable to selectively route fluid flow between a pressurized fluid source and the directional control unit;
one or more bypass fluid lines providing fluid communication between the actuator and the fluid return reservoir independent of the isolation control valve and 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;
wherein the isolation control valve is operable to selectively inhibit or permit fluid flow between the directional control valve and the pressurized fluid source and the fluid return reservoir; and
wherein the isolation control unit further includes a piloted valve operable in a first stage, where fluid flow from the fluid return reservoir to the actuator through the one or more bypass fluid lines is inhibited, and a second stage, where fluid flow from the fluid return reservoir to the actuator is uninhibited.
10. The fluid control system of claim 9 , wherein the isolation control unit further comprises a solenoid valve coupled to both the isolation control valve and the piloted valve, and configured to concurrently control operation of the isolation control valve and the piloted valve.
11. The fluid control system of claim 10 , wherein the solenoid valve is configured to initiate transition of the piloted valve from the first stage to the second stage in response to receiving a thrust-reverser-deploy command.
12. The fluid control system of claim 9 , wherein the directional control valve is operable in a deploy stage, where fluid from the fluid source is routed to both a deploy chamber and a stow chamber of the actuator, and a stow stage, where fluid from the fluid source is routed only to the stow chamber of the actuator; and
wherein, when the directional control valve is in the deploy stage, the deploy and stow chambers are placed in fluid communication with one another to permit fluid recirculation.
13. The fluid control system of claim 9 , wherein the fluid control system further comprises an anti-cavitation check valve residing on the one or more bypass fluid lines, the check valve configured to permit fluid flow from the fluid return reservoir to the actuator, while inhibiting fluid flow from the actuator to the fluid return reservoir.
14. The fluid control system of claim 13 , wherein the anti-cavitation check valve is configured to permit fluid flow when the pressure in a deploy chamber of the actuator is less than the pressure at the fluid return reservoir.
15. The fluid control system of claim 9 , wherein the flow limiter comprises at least one of a flow regulator or a flow restrictor.
16. The fluid control system of claim 9 , wherein the flow limiter is incorporated in the directional control unit.