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

Patent metadata

Field	Value
Publication number	US-9566746-B2
Application number	US-201414188252-A
Country	US
Kind code	B2
Filing date	Feb 24, 2014
Priority date	Nov 6, 2013
Publication date	Feb 14, 2017
Grant date	Feb 14, 2017

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.

First claim

The invention claimed is:

1. A method of forming a contoured composite structure, the method comprising:
positioning a sheet of composite material in operative relation to a structure of shape memory alloy, wherein the structure of shape memory alloy is configured to deform between a first conformation and a second conformation when heated to within an activated temperature range;
following the positioning, heating the structure of shape memory alloy to within the activated temperature range, thereby resulting in deforming the structure of shape memory alloy from the first conformation to the second conformation, and thereby resulting in conforming the sheet of composite material to a desired contour at least partially corresponding to the second conformation and resulting in a conformed sheet of composite material; and
following the heating, cooling the structure of shape memory alloy to below the activated temperature range, thereby deforming the structure of shape memory alloy from the second conformation to the first conformation, while maintaining the sheet of composite material in the desired contour.

2. The method of claim 1 ,
wherein the structure of shape memory alloy includes a first body and a second body;
wherein the positioning includes positioning the sheet of composite material between the first body and the second body; and
wherein the first body and the second body are positioned relative to each other to cooperatively conform the sheet of composite material to the desired contour during the heating.

3. The method 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, the method further comprising:
operatively translating the plurality of bodies, and collectively with the heating, conforming the sheet of composite material to the desired contour and resulting in the conformed sheet of composite material.

4. The method of claim 1 , wherein the structure of shape memory alloy is operatively positioned within a substrate, wherein the substrate is not constructed of shape memory alloy.

5. The method of claim 1 , wherein the heating at least partially sets the conformed sheet of composite material in the desired contour.

6. The method of claim 1 , wherein the heating includes heating the structure of shape memory alloy with one or more heating plates in operative engagement with the structure of shape memory alloy.

7. The method of claim 1 , wherein the structure of shape memory alloy includes one or more integral resistive heating elements, and wherein the heating is performed by the one or more integral resistive heating elements.

8. The method of claim 1 , further comprising:
positioning the sheet of composite material and the structure of shape memory alloy in an autoclave or an oven, wherein the heating is performed by the autoclave or the oven.

9. The method of claim 1 , wherein the structure of shape memory alloy includes a plurality of sub-regions, and wherein the heating includes operatively heating fewer than all of the plurality of sub-regions.

10. The method of claim 1 , wherein the heating includes sequentially heating sub-regions of the structure of shape memory alloy in a predetermined sequence.

11. The method of claim 1 , wherein the heating includes curing the conformed sheet of composite material, thereby resulting in a cured composite structure.

12. The method of claim 1 , further comprising:
following the cooling, curing the conformed sheet of composite material, thereby resulting in a cured composite structure.

13. The method of claim 1 , further comprising:
following the positioning and prior to the heating, retaining the sheet of composite material relative to the structure of shape memory alloy.

14. The method of claim 13 , wherein the retaining includes vacuum bagging the sheet of composite material to the structure of shape memory alloy.

15. The method of claim 1 , further comprising:
concurrently with the heating, impeding the deforming so that the second conformation corresponds to the desired contour.

16. The method of claim 1 , wherein the second conformation defines a complex contour.

17. The method of claim 1 , wherein the first conformation is generally planar.

18. The method of claim 1 , wherein the conformed sheet of composite material defines a complex contour.

19. A method of forming a contoured composite structure, the method comprising:
positioning a sheet of composite material in operative relation to a structure of shape memory alloy, wherein the structure of shape memory alloy is configured to deform between a first conformation and a second conformation when heated to within an activated temperature range;
following the positioning, retaining the sheet of composite material relative to the structure of shape memory alloy, wherein the retaining includes vacuum bagging the sheet of composite material to the structure of shape memory alloy;
following the positioning, heating the structure of shape memory alloy to within the activated temperature range, thereby resulting in deforming the structure of shape memory alloy from the first conformation to the second conformation, and thereby resulting in conforming the sheet of composite material to a desired contour at least partially corresponding to the second conformation and resulting in a conformed sheet of composite material, wherein the heating at least partially sets the conformed sheet of composite material in the desired contour, and wherein the desired contour has a complex contour;
following the heating, cooling the structure of shape memory alloy to below the activated temperature range, thereby deforming the structure of shape memory alloy from the second conformation to the first conformation, while maintaining the sheet of composite material in the desired contour; and
following the cooling, curing the conformed sheet of composite material, thereby resulting in a cured composite structure.

Assignees

• Boeing Co

Inventors

• Rotter Daniel M
• Nelson Paul E

Classifications

• C22F1/006

  Resulting in heat recoverable alloys with a memory effect · CPC title

• B29C70/46

  using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs · CPC title

• Y02T50/433

  Cross-Sectional Technologies · mapped topic

• B29K2105/0872

  Prepregs · CPC title

• B29C53/04

  of plates or sheets {(B29C63/04 takes precedence; bending or folding paper B31F1/0003; folding films B65H45/00)} · CPC title