Thrust reverser flow limiting valve

Patent metadata

Field	Value
Publication number	US-10288007-B2
Application number	US-201715423249-A
Country	US
Kind code	B2
Filing date	Feb 2, 2017
Priority date	Feb 2, 2017
Publication date	May 14, 2019
Grant date	May 14, 2019

Abstract

The present subject matter can be embodied in, among other things, a two-speed thrust reverser actuation system for actuating a thrust reverser element experiencing an assisting load during movement between a stowed and deployed positions. The system includes a hydraulic actuator to move the thrust reverser element between the stowed and deployed positions, and a directional control valve with a regeneration feature including a restrictor and a velocity fuse arranged in parallel with the restrictor. The velocity fuse is configured to close when the assisting load on the thrust reverser element increases the flow rate of hydraulic fluid through the velocity fuse above threshold value. In operation, the system defines a first movement speed when the velocity fuse is open, and a second movement speed when the velocity fuse is closed, thereby decreasing an effective exit orifice size of the hydraulic actuator when the assisting load increases the deploy rate.

First claim

What is claimed is:

1. A two-speed thrust reverser actuation system comprising:
a thrust reverser element configured to move between a stowed position and a deployed position during normal use in association with a jet engine, and arranged to experience an assisting load during movement of the thrust reverser element from the stowed position towards the deployed position,
an isolation valve configured to supply hydraulic fluid under pressure;
a hydraulic actuator configured to move the thrust reverser element between the stowed and deployed positions, the hydraulic actuator comprising:
a deploy port through which hydraulic fluid under pressure from the isolation valve is admitted to a first side of the actuator during operation of the actuator in a thrust reverser element deploy mode to displace the thrust reverser element from its stowed position to the deployed position, and
a stow port though which hydraulic fluid is displaced from a second side of the actuator during operation in the deploy mode; and

a directional control valve comprising a regeneration feature through which hydraulic fluid displaced from the second side of the actuator is returned to the first side of the actuator in addition to the hydraulic fluid supplied from the isolation valve during operating in the deploy mode, the regeneration feature comprising:
a restrictor, and
a velocity fuse arranged in parallel with the restrictor and configured to close when a flow rate of hydraulic fluid through the velocity fuse in a first direction exceeds a threshold value.

2. The two-speed thrust reverser actuation system of claim 1 , wherein the velocity fuse and restrictor of the regeneration feature define:
a first movement speed mode of the thrust reverser element during the deploy mode whereby the velocity fuse is open and hydraulic fluid flows through both the restrictor and the velocity fuse, and
a second movement speed mode of the thrust reverser element during the deploy mode whereby the velocity fuse is closed and hydraulic fluid flows through the restrictor alone.

3. The two-speed thrust reverser actuation system of claim 2 , wherein the two-speed thrust reverser actuation system is configured to switch from the first movement speed mode to the second movement speed mode when the assisting load at the thrust reverser element causes the flow rate of hydraulic fluid through the velocity fuse to exceed the threshold value and close the velocity fuse.

4. The two-speed thrust reverser actuation system of claim 3 , wherein the assisting load on the thrust reverser element acts to increase a deploy rate of the thrust reverser element and increase the flow rate of hydraulic fluid through the velocity fuse when the two-speed thrust reverser actuation system is in the first movement speed mode.

5. The two-speed thrust reverser actuation system of claim 1 , wherein the assisting load on the thrust reverser element increases during movement of the thrust reverser element from the stowed position towards the deployed position.

6. The two-speed thrust reverser actuation system of claim 1 , wherein the hydraulic actuator comprises a double-acting hydraulic piston and cylinder device.

7. The two-speed thrust reverser actuation system of claim 1 , wherein the threshold value of the velocity fuse corresponds to a maximum deploy rate of the thrust reverser element.

8. The two-speed thrust reverser actuation system of claim 1 , wherein the restrictor defines a first orifice and the velocity fuse defines a second orifice, and the first orifice and the second orifice define an overall orifice of the regeneration feature.

9. The two-speed thrust reverser actuation system of claim 1 , wherein the velocity fuse is configured to open when the flow rate of hydraulic fluid through the regeneration feature is below a minimum value.

10. The two-speed thrust reverser actuation system of claim 9 , wherein the velocity fuse is configured to open when the flow rate of hydraulic fluid through the regeneration feature is zero.

11. The two-speed thrust reverser actuation system of claim 9 , wherein the hydraulic actuator is configured to move the thrust reverser element from the deployed position to the stowed position in a thrust reverser element stow mode wherein:
hydraulic fluid under pressure from the isolation valve is admitted through the stow port to the second side of the actuator, where a stow side of the actuator is a high pressure side during operation of the actuator in the thrust reverser element stow mode to displace the thrust reverser element from its deployed position to the stowed position, and
hydraulic fluid is displaced from the first side of the actuator through the deploy port during operation in the deploy mode.

12. The two-speed thrust reverser actuation system of claim 11 , wherein the hydraulic fluid flow through the regeneration feature is reversed to switch the hydraulic actuator from the thrust reverser element deploy mode to the thrust reverser element stow mode, the hydraulic fluid flowing through the velocity fuse in an opposite direction during the thrust reverser element stow mode.

13. The two-speed thrust reverser actuation system of claim 12 , wherein the velocity fuse is configured to open when the hydraulic fluid flows through the velocity fuse in the opposite direction.

14. The two-speed thrust reverser actuation system of claim 1 , wherein the thrust reverser element comprises:
a translating cowl mounted to a nacelle of a gas turbine engine and adapted to translate a distance in an aft direction of the gas turbine engine, the translating cowl having a radially inner wall that defines a radially outer flow surface of a bypass duct defined by and between the nacelle and a core of the gas turbine engine,
a fixed structure within the nacelle that does not translate with the translating cowl, the fixed structure comprising at least one opening that is exposed to the bypass duct when the translating cowl is translated in the aft direction, and
blocker doors mounted to the nacelle and having blocker door stowed positions and blocker door deployed positions, at least a portion of the blocker doors being disposed in the bypass duct in the deployed position; and
wherein the blocker doors are arranged to experience the assisting load from an airflow in the bypass duct.

15. The two-speed thrust reverser actuation system of claim 14 , wherein the hydraulic actuator is configured to deploy the blocker doors in a first direction and stow the blocker doors in an opposite direction.

16. The two-speed thrust reverser actuation system of claim 1 , wherein the directional control valve is configured to supply the hydraulic fluid to the hydraulic actuator via a supply line and receive the hydraulic fluid from the hydraulic actuator via a stow line, wherein the direction control valve enables regeneration of hydraulic fluid from the stow line to the supply line during the deploy mode.

17. The two-speed thrust reverser actuation system of claim 1 , wherein the isolation valve is configured to supply the hydraulic fluid to the directional control valve from a source of hydraulic fluid under pressure.

18. The two-speed thrust reverser actuation system of claim 1 , wherein the velocity fuse and restrictor are incorporated together into a single cartridge assembly.

19. The two-speed thrust reverser actuation system of claim 1 , wherein the hydraulic actuator comprises the velocity fuse and the restrictor.

Assignees

• Woodward Inc

Inventors

• Kopecek Joseph Thomas

Classifications

• F05D2270/56

  by hydraulic means, e.g. hydraulic valves within a hydraulic circuit · CPC title

• F05D2260/60

  Fluid transfer · CPC title

• F02K1/72

  the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow · CPC title

• F02K1/12

  by means of pivoted flaps · CPC title

• F02K1/763 Primary

  with actuating systems or actuating devices; Arrangement of actuators for thrust reversers · CPC title