Method of fabricating a curved composite structure using composite prepreg tape

• US 9,387,657 B2
• Filed: 01/07/2013
• Issued: 07/12/2016
• Est. Priority Date: 11/12/2010
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Darrow, Donald Chester, Smith, Daniel Richard Jr., Modin, Andrew E., Depase, Edoardo, Klewiada, Mark
• Primary Examiner(s): LEE, EDMUND H
• Application Number:
  US13/736,021
• Publication Number:
  US 20140065354A1
• Time in Patent Office: 1,282 Days
• Field of Search: None
• US Class Current: 1/1
• CPC Class Codes: B29C 70/302 Details of the edges of fibre composites, e.g. edge finishing or means to avoid delamination
• CPC Class Codes: B29C 70/541 Positioning reinforcements in a mould, e.g. using clamping means for the reinforcement positioning inserts in moulds B29C33/12; lay-up on a mould B29C70/30
• CPC Class Codes: B32B 38/0012 Mechanical treatment, e.g. roughening, deforming, stretching
• CPC Class Codes: Y10T 156/1002 with permanent bending or reshaping or surface deformation of self sustaining lamina
• CPC Class Codes: Y10T 428/2419 Fold at edge
• CPC Class Codes: Y10T 428/24628 Nonplanar uniform thickness material

Abstract

A method is provided of fabricating a composite stiffener having a curved web and at least one curved flange. A substantially straight length of unidirectional prepreg tape is placed on a carrier. The at least one curved flange is formed by using the carrier to steer a first portion of the tape onto a first curved tool surface. The curved web is formed by using the carrier to form a second portion of the tape onto a second curved tool surface.

Claims

1. A method of laying up a composite part on a tool, comprising:

providing a composite resin tape reinforced with unidirectional fibers having a substantially zero degree fiber orientation;

placing the composite resin tape on a deformable carrier film;

forming the composite resin tape and the carrier film onto a first curved surface on a forming tool;

forming the composite resin tape and the carrier film about a curved axis onto a second curved surface on the forming tool; and

removing the carrier film from the composite resin tape;

wherein forming the composite resin tape and the carrier film includes deforming the composite resin tape and the carrier film by stretching the carrier film, stretching comprising changing one of a length or a width of the carrier film.

2. The method of claim 1, wherein placing the composite resin tape on the carrier film includes compacting the composite resin tape against the carrier film.

3. The method of claim 1, further comprising:

contouring at least one edge of the composite resin tape along its length.

4. The method of claim 3, wherein contouring the at least one edge of the composite resin tape is performed by cutting the composite resin tape along the edge.

5. The method of claim 1, wherein deforming the carrier film is performed as the composite resin tape and the carrier film are being formed onto the second curved surface of the forming tool.

6. A method of fabricating a curved composite structure having at least two curved legs, comprising:

providing a composite prepreg tape having unidirectional reinforcing fibers with a substantially zero degree fiber orientation;

adhering the composite prepreg tape to a film;

forming a first leg of the curved composite structure by forming the film and a first portion of a width of the composite prepreg tape over a first curved surface of a forming tool;

forming a second leg of the curved composite structure by forming the film and a second portion of the width of the composite prepreg tape onto a second curved surface of the forming tool;

removing the film from the composite prepreg tape formed over the forming tool; and

curing the composite prepreg tape formed over the forming tool;

wherein forming the film and the composite prepreg tape includes deforming the film and the composite prepreg tape by stretching the film, stretching comprising changing one of a length or a width of the film.

7. The method of claim 6, wherein forming the second leg is performed by pressing the film and shearing the second portion of the width of the composite prepreg tape about a curved bend line onto the second curved surface of the forming tool.

8. The method of claim 6, further comprising:

contouring at least one edge of the composite prepreg tape along its length.

9. The method of claim 8, wherein contouring the at least one edge of the composite prepreg tape is performed by cutting the tape along the at least one edge.

10. A method of fabricating a composite stiffener having a curved web and at least one curved flange, comprising:

placing a substantially straight unidirectional prepreg tape on a carrier;

forming the at least one curved flange by using the carrier to steer a first portion of the unidirectional prepreg tape onto a first curved tool surface; and

forming the curved web by using the carrier to form a second portion of the unidirectional prepreg tape onto a second curved tool surface;

wherein forming the curved web includes deforming the carrier and the unidirectional prepreg tape by stretching the carrier, stretching comprising changing one of a length or a width of the carrier.

11. The method of claim 10, wherein forming the curved web includes deforming the carrier as the second portion of the unidirectional prepreg tape is being formed onto the second curved tool surface.

12. The method of claim 10, wherein:

steering the first portion of the unidirectional prepreg tape includes a steering a first portion of a width of the unidirectional prepreg tape, and

forming the second portion of the unidirectional prepreg tape includes forming a second portion of the width of the unidirectional prepreg tape.

13. The method of claim 10, wherein a single width of the unidirectional prepreg tape is used to form the at least one curved flange and the curved web.

14. The method of claim 10, wherein forming the curved web includes shearing a portion of a width of the unidirectional prepreg tape about a curved bend line onto the second curved tool surface.

15. The method of claim 10, further comprising:

removing the carrier from the unidirectional prepreg tape after the curved web and the at least one curved flange have been formed; and

curing the unidirectional prepreg tape.

16. The method of claim 10, further comprising:

clamping the at least one curved flange against the first curved tool surface, and

wherein forming the curved web is performed while the at least one curved flange is clamped against the first curved tool surface.

17. The method of claim 10, wherein placing the unidirectional prepreg tape on the carrier includes forming overlapping segments of the unidirectional prepreg tape on the carrier by sequentially forming offset segments of the unidirectional prepreg tape on the carrier.

18. The method of claim 17, wherein placing the unidirectional prepreg tape on the carrier includes overlapping the segments.

19. The method of claim 16, further comprising:

contouring an edge of the unidirectional prepreg tape along its length before the at least one curved flange and the curved web are formed.

20. A method of laying up a multi-ply composite part on a tool having contoured surfaces to which a layup is to conform, comprising:

providing a deformable carrier film;

reinforcing a portion of the carrier film against deforming, including impregnating the carrier film with reinforcing fibers;

placing a composite doubler on a surface of the carrier film;

placing a strip of release film on the surface of the carrier film;

placing a zero degree prepreg ply on the surface of the carrier film overlying the composite doubler and the strip of release film, including laying down a plurality of courses of unidirectional prepreg fiber tape in a side-by-side relationship on the surface of the carrier film;

compacting the zero degree prepreg ply, the composite doubler and the strip of release film against the carrier film;

using the carrier film to transport the zero degree prepreg ply to tool;

using the carrier film to layup the composite doubler, the strip of release film and the zero degree prepreg ply on the tool, including deforming the zero degree prepreg ply by deforming the carrier film to cause the zero degree prepreg ply to conform to contoured areas of the tool wherein deforming the carrier film includes deforming the carrier film and the zero degree prepreg ply by stretching the carrier film, stretching comprising changing one of a length or a width of the carrier film; and

removing the carrier film from the zero degree prepreg ply when the zero degree prepreg ply has been laid up and conformed to the tool.