Airflow-dependent deployable fences for aircraft wings

Patent metadata

Field	Value
Publication number	US-11059565-B2
Application number	US-201816197933-A
Country	US
Kind code	B2
Filing date	Nov 21, 2018
Priority date	Nov 21, 2018
Publication date	Jul 13, 2021
Grant date	Jul 13, 2021

Abstract

Airflow-dependent deployable fences for aircraft wings are described. An example apparatus includes a fence coupled to a wing of an aircraft. The fence is movable relative to the wing between a stowed position in which a panel of the fence extends along a skin of the wing, and a deployed position in which the panel extends at an upward angle away from the skin. The panel is configured to impede a spanwise airflow along the wing when the fence is in the deployed position. The fence is configured to move from the stowed position to the deployed position in response to an aerodynamic force exerted on a deployment vane of the fence.

First claim

What is claimed is:

1. An apparatus comprising:
a fence coupled to a wing of an aircraft, the fence having a leading end oriented toward a leading edge of the wing and a trailing end oriented toward a trailing edge of the wing, the fence being movable relative to the wing between a stowed position in which a panel of the fence extends along a skin of the wing, and a deployed position in which the panel extends at an upward angle away from the skin, the panel configured to impede a spanwise airflow along the wing when the fence is in the deployed position, the fence configured to move from the stowed position to the deployed position in response to an aerodynamic force exerted on a deployment vane of the fence, the deployment vane oriented at an angle to the panel, the deployment vane coupled to the panel and located between the leading edge and the trailing edge of the panel.

2. The apparatus of claim 1 , wherein the deployment vane is substantially orthogonal to the panel.

3. The apparatus of claim 1 , wherein the panel is further configured to generate a vortex along the wing when the fence is in the deployed position.

4. The apparatus of claim 1 , further comprising an actuator configured to move the fence from the deployed position to the stowed position.

5. The apparatus of claim 4 , wherein the actuator is configured to move the fence from the deployed position to the stowed position in response to the aerodynamic force being less than a threshold force value.

6. The apparatus of claim 5 , wherein the actuator includes a spring-loaded axle operatively coupled to the fence and mounted to the wing, the spring-loaded axle including an axle and a spring coiled around the axle.

7. The apparatus of claim 6 , wherein the spring is configured to wind around the axle in response to the aerodynamic force being greater than the threshold force value, and the spring is further configured to unwind around the axle in response to the aerodynamic force being less than the threshold force value.

8. The apparatus of claim 6 , wherein the axle has a central axis that is substantially parallel to a chordwise direction of the wing.

9. The apparatus of claim 8 , wherein the panel extends in an inboard direction away from the central axis when the fence is in the stowed position.

10. The apparatus of claim 8 , wherein the deployment vane extends in an outboard direction away from the central axis when the fence is in the deployed position.

11. The apparatus of claim 1 , wherein the panel is recessed within the wing when the fence is in the stowed position.

12. The apparatus of claim 1 , wherein the panel: is a first panel of the fence, the first panel having a first orientation relative to a chord of the wing when the fence is in the stowed position, the fence further including a second panel located aft of the first panel, the second panel having a second orientation relative to the chord of the wing when the fence is in the stowed position, the second orientation differing from the first orientation, the first panel and the second panel configured to extend along the skin of the wing when the fence is in the stowed position, the first panel and the second panel configured to impede the spanwise airflow along the wing when the fence is in the deployed position.

13. A method for moving a fence coupled to a wing of an aircraft, the method comprising:
moving the fence between a stowed position in which a panel of the fence extends along a skin of the wing, and a deployed position in which the panel extends at an upward angle away from the skin, the fence having a leading end oriented toward a leading edge of the wing and a trailing end oriented toward a trailing edge of the wing, the panel impeding a spanwise airflow along the wing when the fence is in the deployed position, the moving including moving the fence from the stowed position to the deployed position in response to an aerodynamic force exerted on a deployment vane of the fence, the deployment vane oriented at an angle to the panel, the deployment vane coupled to the panel and located between the leading edge and the trailing edge of the panel.

14. The method of claim 13 , wherein the deployment vane is substantially orthogonal to the panel.

15. The method of claim 13 , wherein the panel generates a vortex along the wing when the fence is in the deployed position.

16. The method of claim 13 , wherein the aerodynamic force is generated via a substantially spanwise airflow along a spanwise direction of the wing.

17. The method of claim 16 , wherein the fence is rotatably coupled to the wing via an axle having a central axis.

18. The method of claim 17 , wherein the central axis is substantially parallel to a chordwise direction of the wing.

19. The method of claim 18 , wherein the panel extends in an inboard direction away from the central axis when the fence is in the stowed position.

20. The method of claim 18 , wherein the deployment vane extends in an outboard direction away from the central axis when the fence is in the deployed position.

Assignees

• Boeing Co

Inventors

• Tillotson Brian
• Kettering Chris

Classifications

• B64C5/10 Primary

  adjustable · CPC title

• B64C3/58 Primary

  provided with fences or spoilers (adjustable for control purposes B64C9/00) · CPC title

• B64C9/02

  Mounting or supporting thereof · CPC title

• B64C5/08

  mounted on, or supported by, wings · CPC title