Method of laying up prepreg plies on contoured tools using a deformable carrier film

• US 9,701,067 B2
• Filed: 10/07/2013
• Issued: 07/11/2017
• Est. Priority Date: 11/12/2010
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Hawkins, Robert D., Willden, Kurtis S., Depase, Edoardo, Mussi, Benjamin Adam, Kismarton, Max U., Modin, Andrew E., Glain, Michael L.
• Primary Examiner(s): LEE, EDMUND H
• Application Number:
  US14/048,009
• Publication Number:
  US 20140027048A1
• Time in Patent Office: 1,373 Days
• Field of Search: None
• CPC Class Codes: B29C 70/021 Combinations of fibrous reinforcement and non-fibrous material
• CPC Class Codes: B29C 70/20 oriented in a single direction, e.g. roofing or other parallel fibres B29C70/083, B29C70/226 take precedence
• CPC Class Codes: B29C 70/30 Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
• 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: B29D 99/0003 Producing profiled members, e.g. beams

Abstract

A method is presented. The method comprises identifying a desired shape of a ply on a tool, in which the ply has a fiber orientation; identifying a cut shape for the ply, in which the cut shape is different than the desired shape; cutting a composite prepreg ply to have the cut shape, the composite prepreg ply having the fiber orientation; using a deformable carrier to apply the composite prepreg ply having the cut shape to the tool such that the composite prepreg ply has the desired shape on the tool.

Claims

1. A method comprising:

identifying a desired shape of a ply on a tool, in which the ply has a fiber orientation;

identifying a cut shape for the ply, in which the cut shape is different than the desired shape;

cutting a composite prepreg ply to have the cut shape, the composite prepreg ply having the fiber orientation;

applying the composite prepreg ply having the cut shape over a deformable carrier;

deforming the composite prepreg by stretching the deformable carrier, stretching comprising changing one of a length or a width of the deformable carrier; and

using deformable carrier to apply the composite prepreg ply having the cut shape to the tool such that the composite prepreg ply has the desired shape on the tool.

2. The method of claim 1, further comprising:

using the carrier to transport and locate the composite prepreg ply over a tool.

3. The method of claim 2, further comprising:

removing the carrier from the composite prepreg ply.

4. The method of claim 2, wherein:

applying the composite prepreg ply over the carrier includes compacting the composite prepreg ply against the carrier; and

the carrier is removed from the composite prepreg ply after the composite prepreg ply has been applied to the tool.

5. The method of claim 2, further comprising:

applying at least one of a release film and a ply doubler on the carrier before the composite prepreg ply is applied to the carrier.

6. The method of claim 2, wherein applying the composite prepreg ply over the carrier includes:

laying down courses of unidirectional prepreg fiber tape in side-by-side relationship on the carrier; and

compacting the courses against the carrier.

7. The method of claim 1, wherein the fiber orientation is a 45 degree orientation.

8. The method of claim 1, wherein the fiber orientation is a 0 degree orientation.

9. The method of claim 1 further comprising:

deforming the composite prepreg ply by stretching the carrier, stretching comprising changing one of a length or a width of carrier.

10. The method of claim 9, wherein stretching the carrier is performed as the composite prepreg ply is being applied to the tool.

11. The method of claim 9, wherein the carrier comprises an elastic material that returns substantially to its original size and shape following stretching.

12. The method of claim 1, wherein the cut shape compensates for a shearing effect in the composite prepreg ply while applying the composite prepreg ply to the tool.

13. The method of claim 1, wherein the cut shape compensates for a fanning effect in the composite prepreg ply.

14. A method comprising:

identifying a desired shape of a ply on a tool, in which the ply has a fiber orientation;

identifying a cut shape for the ply, in which the cut shape is different than the desired shape;

cutting a composite prepreg ply to have the cut shape, the composite prepreg ply having the fiber orientation;

placing the composite prepreg ply having the cut shape on a carrier; and

using the carrier to apply the composite prepreg ply to the tool, including deforming the composite prepreg ply by stretching the carrier, stretching comprising changing one of a length or a width of the carrier.

15. The method of claim 14, wherein placing the composite prepreg ply on a carrier film comprising:

laying down courses of unidirectional prepreg fiber tape in side-by-side relationship on the carrier; and

compacting the courses against the carrier.

16. The method of claim 14, wherein placing composite prepreg plies on the carrier and using the carrier to apply the composite prepreg plies are repeated to form a multiple ply part layup.

17. The method of claim 14, wherein deforming the composite prepreg ply includes:

stretching the carrier in a direction transverse to the fiber orientation of the composite prepreg ply.