Adaptive composite structure using shape memory alloys

Patent metadata

Field	Value
Publication number	US-11110647-B2
Application number	US-201815963890-A
Country	US
Kind code	B2
Filing date	Apr 26, 2018
Priority date	Jul 16, 2014
Publication date	Sep 7, 2021
Grant date	Sep 7, 2021

Abstract

Systems and processes that integrate thermoplastic and shape memory alloy materials to form an adaptive composite structure capable of changing its shape. For example, the adaptive composite structure may be designed to serve as a multifunctional adaptive wing flight control surface. Other applications for such adaptive composite structures include in variable area fan nozzles, winglets, fairings, elevators, rudders, or other aircraft components having an aerodynamic surface whose shape is preferably controllable. The material systems can be integrated by means of overbraiding (interwoven) with tows of both thermoplastic and shape memory alloy materials or separate layers of each material can be consolidated (e.g., using induction heating) to make a flight control surface that does not require separate actuation.

First claim

The invention claimed is:

1. An aerodynamic device comprising first and second skins, each of the first and second skins comprising shape memory alloy and thermoplastic material, wherein the shape memory alloy is embedded in the thermoplastic material and wrapped around an inner mold line of the aerodynamic device, and further comprising a first heating blanket adhered to an interior surface of the first skin, wherein the shape memory alloy of the first skin comprises an active portion embedded in the thermoplastic material of the first skin in an area overlapping the first heating blanket, and the first heating blanket comprises conductive foil in a serpentine pattern.

2. The aerodynamic device as recited in claim 1 , wherein the first skin is a lamination comprising an inner layer comprising shape memory alloy and an outer layer comprising thermoplastic material without shape memory alloy, the inner layer being disposed inside the outer layer.

3. The aerodynamic device as recited in claim 2 , wherein the inner layer comprises thermoplastic material and tapes made of shape memory alloy at least partly embedded in the thermoplastic material of the inner layer and wrapped around the inner mold line of the aerodynamic device.

4. The aerodynamic device as recited in claim 2 , wherein the inner layer comprises thermoplastic material and wires made of shape memory alloy at least partly embedded in the thermoplastic material of the inner layer and wrapped around the inner mold line of the aerodynamic device.

5. The aerodynamic device as recited in claim 1 , wherein the shape memory alloy of the first skin comprises tapes made of shape memory alloy material embedded in the thermoplastic material and wrapped around the inner mold line of the aerodynamic device.

6. The aerodynamic device as recited in claim 1 , wherein the shape memory alloy of the first skin comprises wires made of shape memory alloy material embedded in the thermoplastic material and wrapped around the inner mold line of the aerodynamic device.

7. The aerodynamic device as recited in claim 1 , further comprising a second heating blanket adhered to an interior surface of the second skin, wherein the shape memory alloy of the second skin comprises an active portion embedded in the thermoplastic material of the second skin in an area overlapping the second heating blanket, and the second heating blanket comprises conductive foil in a serpentine pattern.

8. The aerodynamic device as recited in claim 7 , wherein the first and second skins form an airfoil-shaped body having a chord and a forward portion.

9. The aerodynamic device as recited in claim 8 , wherein the active portions of the shape memory alloy are capable of producing chordwise changes in the contours of the upper and lower skins when the shape memory alloy is heated.

10. The aerodynamic device as recited in claim 8 , wherein the forward portion is made of a material which is not susceptible to heat-induced shape change.

11. The aerodynamic device as recited in claim 10 , wherein the forward portion is made of shape memory alloy which has not been trained to change shape at a transition temperature.

12. The aerodynamic device as recited in claim 1 , wherein at least some of the shape memory alloy of the first skin and at least some of the shape memory alloy of the second skin has been trained to deform in a specified manner in response to being heated.

13. The aerodynamic device as recited in claim 12 , wherein the trained shape memory alloy has been trained to change shape in a manner that produces a constrained motion of the aerodynamic device in response to being heated.

14. The aerodynamic device as recited in claim 1 , wherein the first and second skins have an outer mold line which changes shape as the thermoplastic material deforms in response to heating of the shape memory alloy.

15. The aerodynamic device as recited in claim 1 , wherein the first skin comprises a woven or continuous layer of shape memory alloy material sandwiched between two woven or continuous layers of thermoplastic material.

16. The aerodynamic device as recited in claim 1 , wherein the thermoplastic material comprises polyetherketoneketone resin and polyester fibers.

17. The aerodynamic device as recited in claim 1 , wherein the shape memory alloy of the first skin is not exposed on an exterior surface of the first skin.

18. The aerodynamic device as recited in claim 1 , wherein the shape memory alloy of the first skin is configured to form a pair of mutually antagonistic one-way shape memory alloy actuators.

19. The aerodynamic device as recited in claim 1 , wherein the shape memory alloy of the first skin is configured to form a two-way shape memory alloy actuator.

20. The aerodynamic device as recited in claim 1 , wherein the conductive foil is embedded in a dielectric matrix.

Assignees

• Boeing Co

Inventors

• Marcoe Jeffery L
• Apdalhaliem Sahrudine
• Shome Moushumi

Classifications

• F03G7/06143

  Wires · CPC title

• F03G7/066

  Actuator control or monitoring · CPC title

• F03G7/06147

  Magnetic shape memory alloys, e.g. ferro-magnetic alloys · CPC title

• B29C61/0625 Primary

  Preforms comprising incorporated or associated heating means · CPC title

• B29C70/302 Primary

  Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination · CPC title