Shape-changing control surface

• US 8,382,045 B2
• Filed: 07/21/2009
• Issued: 02/26/2013
• Est. Priority Date: 07/21/2009
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Manley, David J., Grip, Robert E.
• Primary Examiner(s): Ellis, Christopher P
• Assistant Examiner(s): Badawi, Medhat
• Application Number:
  US12/506,462
• Publication Number:
  US 20110017876A1
• Time in Patent Office: 1,316 Days
• Field of Search: 244/219, 244/201, 244/215, 244/135.R, 244/38, 244/213
• US Class Current: 244/219
• CPC Class Codes: B64C 3/48 by relatively-movable parts of wing structures
• CPC Class Codes: B64C 9/16 at the rear of the wing

Abstract

A method and apparatus for controlling the shape of a control surface. A structure is rotated about an axis. The structure is located between a flexible skin and a skin located substantially opposite of the flexible skin. An assembly is moved to change the shape of the control surface in response to a rotation of the structure. The assembly is movably connected to the structure and is configured to move such that the flexible skin forms a plurality of curvatures.

Claims

1. An apparatus comprising:

a flexible skin of a control surface;

a skin of the control surface, the skin associated with the flexible skin and located substantially opposite of the flexible skin;

a structure located between the flexible skin and the skin; and

an assembly, wherein the assembly is moveably connected to the structure, and is configured to move such that the flexible skin changes between a plurality of curvatures while a curvature of the skin, extending from a base of the control surface to a tip of the control surface, remains rigid during movement of the assembly.

2. The apparatus of claim 1, wherein the flexible skin, the skin, the structure, and the assembly form a control surface.

3. The apparatus of claim 2, wherein the control surface is selected from one of a flap, a rudder, and an elevator.

4. The apparatus of claim 2 further comprising:

a first number of hinge points located on the structure, wherein the structure is configured to move around an axis through the first number of hinge points.

5. The apparatus of claim 4 further comprising:

a second number of hinge points located on the structure, wherein the assembly is moveably connected to the second number of hinge points and is configured to move such that the flexible skin changes between the plurality of curvatures in response to movement of the structure around the axis.

6. The apparatus of claim 5, wherein the assembly comprises:

a plurality of rigid structures moveably connected to the second number of hinge points located on the structure, wherein the plurality of rigid structures is connected in series to a number of fixed points.

7. The apparatus of claim 6, wherein the assembly further comprises:

a first plurality of connecting members moveably connected to the plurality of rigid structures and connecting the plurality of rigid structures in series to the number of fixed points.

8. The apparatus of claim 7, wherein the assembly further comprises:

a second plurality of connecting members having first ends moveably connected to the plurality of rigid structures and second ends connected to the flexible skin.

9. The apparatus of claim 4 further comprising:

a number of actuators connected to the structure, wherein the number of actuators is configured to move the structure around the axis.

10. The apparatus of claim 1, wherein changes in the flexible skin between the plurality of curvatures change a degree of flow turning.

11. The apparatus of claim 4, wherein movement of the structure around the axis and wherein changes in the flexible skin between the plurality of curvatures both change a degree of flow turning.

12. The apparatus of claim 8, wherein movement of the structure around the axis causes a first portion of change in the degree of flow turning, and wherein changes in the flexible skin between the plurality of curvatures cause a second portion of change in the degree of flow turning.

13. The apparatus of claim 2 further comprising:

a sliding joint located around a base of the control surface, wherein the sliding joint is configured to allow a surface of the flexible skin to slide relative to a surface of the skin.

14. The apparatus of claim 6, wherein the structure further comprises:

a number of ribs, wherein the plurality of rigid structures is connected to the number of ribs at the second number of hinge points.

15. The apparatus of claim 1, wherein the structure is connected to the skin and the flexible skin.

16. The apparatus of claim 1, wherein the skin is comprised of a material selected from at least one of aluminum, titanium, and a composite material.

17. The apparatus of claim 6, wherein the plurality of rigid structures is a plurality of linkages capable of rotating about the second number of hinge points.