Methods and tools for forming contoured composite structures with shape memory alloy

• US 9,808,997 B1
• Filed: 12/30/2016
• Issued: 11/07/2017
• Est. Priority Date: 11/06/2013
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Rotter, Daniel M., Nelson, Paul E.
• Primary Examiner(s): Hindenlang, Alison L
• Assistant Examiner(s): Ahmed Ali, Mohamed K
• Application Number:
  US15/396,170
• Publication Number:
  US 20170320274A1
• Time in Patent Office: 312 Days
• Field of Search: 264230, 425403
• CPC Class Codes: B29C 53/04 of plates or sheets B29C63/04 takes precedence; bending or folding paper B31F1/0003; folding films B65H45/00
• CPC Class Codes: B29C 70/44 using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
• CPC Class Codes: B29C 70/46 using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
• CPC Class Codes: B29K 2105/0872 Prepregs
• CPC Class Codes: C22F 1/006 Resulting in heat recoverable alloys with a memory effect
• CPC Class Codes: Y02T 50/40 Weight reduction

Abstract

Methods and tools for forming contoured composite structures are disclosed. Methods include positioning a sheet of composite material relative to a structure of shape memory alloy, heating the structure of shape memory alloy to deform the structure of shape memory alloy to a deformed conformation and thereby conform the sheet of composite material to a desired contour corresponding to the deformed conformation of the structure of shape memory alloy. Tools include a structure of shape memory alloy and a heat source for heating the structure of shape memory alloy to conform a sheet of composite material to a desired contour corresponding to the deformed conformation of the structure of shape memory alloy.

Claims

1. A tool for forming a contoured composite structure, the tool comprising:

a structure of shape memory alloy configured to deform from a first conformation to a second conformation when heated to within an activated temperature range, wherein the second conformation corresponds to a desired contour of a sheet of composite material, and wherein the structure of shape memory alloy is configured to operatively receive the sheet of composite material;

a heat source configured to heat the structure of shape memory alloy to within the activated temperature range to actively deform the structure of shape memory alloy from the first conformation to the second conformation, thus resulting in conformation of the sheet of composite material to the desired contour at least partially corresponding to the second conformation of the shape memory alloy, wherein the sheet of composite material is maintained in the desired conformation when the structure of shape memory alloy returns to the first conformation; and

a retention structure configured to selectively retain the sheet of composite material relative to the structure of shape memory alloy when the heat source heats the structure of shape memory alloy to within the activated temperature range.

2. The tool of claim 1, in combination with the sheet of composite material in operative relation to the structure of shape memory alloy.

3. The combination of claim 2, wherein the sheet of composite material includes one or more pre-preg composite plies.

4. The tool of claim 1, wherein the structure of shape memory alloy includes a first body and a second body positioned relative to the first body, wherein the first body and the second body are configured to cooperatively and actively conform the sheet of composite material to the desired contour when the structure of shape memory alloy is heated to within the activated temperature range and thus when the structure of shape memory alloy is deformed to the second conformation.

5. The tool of claim 1, wherein the structure of shape memory alloy includes a plurality of bodies, wherein the plurality of bodies defines a die configuration when the structure of shape memory alloy is deformed to the second conformation.

6. The tool of claim 5, wherein the bodies of the plurality of bodies are configured to be translated relative to each other to conform the sheet of composite material to the desired contour when the structure of shape memory alloy is heated to within the activated temperature range.

7. The tool of claim 1, further comprising:

a substrate, wherein the structure of shape memory alloy is operatively positioned within the substrate, and wherein the substrate is not constructed of shape memory alloy.

8. The tool of claim 1, wherein the heat source includes one or more heating plates in operative engagement with the structure of shape memory alloy.

9. The tool of claim 1, wherein the heat source includes one or more resistive heating elements that are integral with the structure of shape memory alloy.

10. The tool of claim 1, wherein the heat source includes an autoclave or an oven.

11. The tool of claim 1, wherein the structure of shape memory alloy includes a plurality of sub-regions, and wherein the heat source is configured to operatively heat fewer than all of the plurality of sub-regions.

12. The tool of claim 1, wherein the structure of shape memory alloy includes a plurality of sub-regions, and wherein the heat source is configured to heat a first subset of the plurality of sub-regions to within the activated temperature range and to not heat a second subset of the plurality of sub-regions to within the activated temperature range.

13. The tool of claim 1, wherein the heat source is configured to sequentially heat predetermined sub-regions of the structure of shape memory alloy in a predetermined sequence.

14. The tool of claim 1, further comprising:

a controller configured to operatively control the heat source to sequentially heat predetermined sub-regions of the structure of shape memory alloy in a predetermined sequence.

15. The tool of claim 1, wherein the retention structure includes a vacuum bagging assembly.

16. The tool of claim 1, further comprising:

a mechanical impeder operatively coupled to the structure of shape memory alloy, wherein the mechanical impeder is configured to operatively resist deformation of the structure of shape memory alloy from the first conformation to the second conformation.

17. The tool of claim 1, wherein the second conformation defines a complex contour.

18. The tool of claim 17, wherein the first conformation is planar.

19. A tool for forming a contoured composite structure, the tool comprising:

a structure of shape memory alloy configured to deform from a first conformation to a second conformation when heated to within an activated temperature range, wherein the second conformation corresponds to a desired contour of a sheet of composite material, and wherein the structure of shape memory alloy is configured to operatively receive the sheet of composite material;

a heat source configured to heat the structure of shape memory alloy to within the activated temperature range to actively deform the structure of shape memory alloy from the first conformation to the second conformation, thus resulting in confirmation of the sheet of composite material to the desired contour at least partially corresponding to the second conformation of the shape memory alloy, wherein the sheet of composite material is maintained in the desired conformation when the structure of shape memory alloy returns to the first conformation; and

a controller configured to operatively control the heat source to sequentially heat predetermined sub-regions of the structure of shape memory alloy in a predetermined sequence.

20. A tool for forming a contoured composite structure, the tool comprising:

a structure of shape memory alloy configured to deform from a first conformation to a second conformation when heated to within an activated temperature range, wherein the second conformation corresponds to a desired contour of a sheet of composite material, and wherein the structure of shape memory alloy is configured to operatively receive the sheet of composite material; and

a heat source configured to heat the structure of shape memory alloy to within the activated temperature range to actively deform the structure of shape memory alloy from the first conformation to the second conformation, thus resulting in confirmation of the sheet of composite material to the desired contour at least partially corresponding to the second conformation of the shape memory alloy, wherein the sheet of composite material is maintained in the desired conformation when the structure of shape memory alloy returns to the first conformation;

wherein the structure of shape memory alloy includes a plurality of sub-regions, and wherein the heat source is configured to operatively heat fewer than all of the plurality of sub-regions.