Thrust reverser flow limiting valve

Patent metadata

Field	Value
Publication number	US-11053889-B2
Application number	US-201916294111-A
Country	US
Kind code	B2
Filing date	Mar 6, 2019
Priority date	Feb 2, 2017
Publication date	Jul 6, 2021
Grant date	Jul 6, 2021

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 method of operating a thrust reverser element, the method comprising:
flowing hydraulic fluid to a deploy port of a hydraulic actuator to move the thrust reverser element from a stowed position to a deployed position;
receiving a flow of hydraulic fluid from a stow port of the hydraulic actuator through a restrictor and a velocity fuse;
automatically closing the velocity fuse when a flow rate of the flow of hydraulic fluid from the hydraulic actuator through the velocity fuse exceeds a threshold value, the flow of hydraulic fluid from the hydraulic actuator passing through the restrictor alone; and
automatically opening the velocity fuse when the thrust reverser element reaches the deployed position and the flow of hydraulic fluid from the stow port of the hydraulic actuator is below a minimum value.

2. The method of claim 1 , comprising:
with the thrust reverser element in the deployed position, flowing hydraulic fluid through the restrictor and the velocity fuse to the stow port of the hydraulic actuator to move the thrust reverser element from the deployed position to the stowed position; and
receiving, at a fluid return, a flow of hydraulic fluid from the deploy port of the hydraulic actuator.

3. The method of claim 1 , wherein a two-speed thrust reverser actuation system comprises:
the thrust reverser element, configured to move between the stowed position and the 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 toward the deployed position,
an isolation valve configured to supply hydraulic fluid under pressure;
the hydraulic actuator, configured to move the thrust reverser element between the stowed position and the deployed position, the hydraulic actuator comprising:
the deploy port, through which hydraulic fluid under pressure from the isolation valve is admitted to a first side of the hydraulic actuator during operation of the hydraulic actuator in a thrust reverser element deploy mode to displace the thrust reverser element from the stowed position to the deployed position, and
the stow port, through which hydraulic fluid is displaced from a second side of the hydraulic 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 hydraulic actuator is returned to the first side of the hydraulic actuator in addition to the hydraulic fluid supplied from the isolation valve during operation in the deploy mode, the regeneration feature comprising:
the restrictor, and
the velocity fuse, arranged in parallel with the restrictor and configured to close when the flow rate of hydraulic fluid through the velocity fuse in a first direction exceeds the threshold value.

4. The method of claim 3 , 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.

5. The method of claim 3 , further comprising regenerating hydraulic fluid from a stow line to a supply line during the deploy mode, wherein the directional control valve is configured to supply the hydraulic fluid to the hydraulic actuator via the supply line and receive the hydraulic fluid from the hydraulic actuator via the stow line.

6. The method of claim 3 , further comprising supplying, by the isolation valve, the hydraulic fluid to the directional control valve from a source of hydraulic fluid under pressure.

7. The method of claim 3 , wherein the threshold value of the velocity fuse corresponds to a maximum deploy rate of the thrust reverser element.

8. The method of claim 3 , further comprising opening the velocity fuse based on the flow rate of hydraulic fluid through the regeneration feature dropping below the minimum value.

9. The method of claim 8 , wherein the velocity fuse is configured to open when the flow rate of hydraulic fluid through the regeneration feature is zero.

10. The method of claim 9 , further comprising:
admitting hydraulic fluid under pressure from the isolation valve through the stow port to the second side of the hydraulic actuator, where a stow side of the hydraulic actuator is a high pressure side during operation of the hydraulic actuator in a thrust reverser element stow mode;
displacing the thrust reverser element from the deployed position toward the stowed position;
displacing hydraulic fluid from the first side of the hydraulic actuator through the deploy port during operation in the deploy mode; and
moving, by the hydraulic actuator, the thrust reverser element from the deployed position to the stowed position in the thrust reverser element stow mode.

11. The method of claim 10 , further comprising: reversing the hydraulic fluid flow through the regeneration feature; switching, by the reversing, the hydraulic actuator from the thrust reverser element deploy mode to the thrust reverser element stow mode; and flowing the hydraulic fluid through the velocity fuse in a second direction opposite the first direction.

12. The method of claim 11 , further comprising opening the velocity fuse based on the hydraulic fluid flowing through the velocity fuse in the second direction.

13. The method of claim 1 , further comprising:
opening the velocity fuse during a deploy mode;
flowing hydraulic fluid through both the restrictor and the velocity fuse during the deploy mode;
moving the thrust reverser element at a first speed during the deploy mode;
closing the velocity fuse during the deploy mode;
flowing hydraulic fluid through the restrictor alone during the deploy mode; and
moving the thrust reverser element at a second speed during the deploy mode.

14. The method of claim 13 , further comprising:
receiving an assisting load at the thrust reverser element;
urging, by the assisting load, the flow rate of hydraulic fluid through the velocity fuse;
exceeding, by the flow rate, the threshold value;
closing, based on the exceeding, the velocity fuse; and
switching from the first speed to the second speed based on the closing of the velocity fuse.

15. The method of claim 14 , further comprising:
increasing, by the assisting load on the thrust reverser element, a deploy rate of the thrust reverser element; and
increasing, by the assisting load on the thrust reverser element, the flow rate of hydraulic fluid through the velocity fuse in a first movement speed mode.

16. The method of claim 14 , 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.

17. The method 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 b

Assignees

• Woodward Inc

Inventors

• Kopecek Joseph Thomas

Classifications

• F05D2270/64

  Hydraulic actuators · CPC title

• F05D2270/331

  Mechanical loads · CPC title

• F02K1/58

  Reversers mounted on the inner cone or the nozzle housing {or the fuselage} · CPC title

• F02K1/62

  by blocking the rearward discharge by means of flaps · CPC title

• F02K1/763 Primary

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