Fabrication of composite laminates using temporarily stitched preforms

Patent metadata

Field	Value
Publication number	US-11046050-B2
Application number	US-201715622444-A
Country	US
Kind code	B2
Filing date	Jun 14, 2017
Priority date	Mar 19, 2014
Publication date	Jun 29, 2021
Grant date	Jun 29, 2021

Abstract

A composite structure is fabricated using a preform comprising a stack of unidirectional prepreg plies that are stitched together. During curing of the prepreg, the stitches melt and dissolve.

First claim

What is claimed is:

1. A method of fabricating a composite structure, the method comprising:
laying up a dry fiber preform having dry fiber layers;
stitching the dry fiber layers together with thermoplastic threads into a stitched stack of dry fiber layers having varying fiber orientations;
infusing the stack of dry fiber layers with a polymer resin;
thermally curing the stitched stack of dry fiber layers;
melting the thermoplastic threads after resin infusion is commenced to produce a matrix resin, wherein melting the thermoplastic threads takes place during thermal curing of the stitched stack of dry fiber layers, wherein the thermoplastic threads begin to melt and dissolve into the polymer resin only after a viscosity of the polymer resin begins to increase as the polymer resin begins to harden during an initial stage of curing; and wherein a vacuum is used to debulk the layers together without movement while the stitches melt into the resin and the structure cures and consolidates; and
subjecting the stack of dry fiber layers, the polymer resin, and the thermoplastic threads with pressure causing the thermoplastic threads and the resin to mix together.

2. The method of claim 1 , wherein the stack has a thickness, and stitching the dry fiber layers together is performed by using the thermoplastic threads that pass substantially through the thickness of the stack.

3. The method of claim 1 , further comprising:
forming the stack of dry fiber layers into a desired shape corresponding to a shape of the composite structure before stitching the dry fiber layers together.

4. The method of claim 1 , wherein forming the stack of dry fiber layers includes placing the stack in a mold, and infusing the stack of dry fiber layers includes introducing a polymer resin into the mold under a vacuum.

5. The method of claim 1 , wherein the stitching the dry fiber layers together with thermoplastic threads into a stitched stack of dry fiber layers having varying fiber orientations is performed prior to curing of the polymer resin.

6. The method of claim 1 , wherein melting of the thermoplastic stitches during a cure process effectively dissolves the stitches and avoids crimping between the stitches and reinforcing fibers.

7. The method of claim 6 , wherein dissolution of the thermoplastic stitches reduces or eliminates stress concentrations in a cured stack of fiber layers caused by fiber crimping.

8. The method of claim 7 , wherein the dissolution of the thermoplastic stitches improves a mechanical performance of the composite structure and reduces crack propagation through the composite structure.

9. The method of claim 1 , wherein the thermoplastic stitches have a melt temperature that is below a cure temperature of the polymer resin.

10. The method of claim 1 , wherein the melted thermoplastic stitches are distributed generally uniformly across the stack of fiber layers.

11. The method of claim 1 , wherein:
each of the fiber layers includes a resin matrix, and
the melted thermoplastic stitches are compatible with the resin matrix.

12. The method of claim 11 , wherein:
the resin matrix is a thermoset resin, and
the thermoplastic stitches comprise a thermoplastic resin.

13. The method of claim 1 , wherein each of the layers including unidirectional reinforcing fibers.

14. The method of claim 1 , wherein the thermoplastic threads melt when heated to a predetermined temperature.

15. The method of claim 1 , further comprising:
varying a tightness of the stitches depending upon a number of plies in the stack and a complexity of a dry fiber structure being fabricated so that for a highly contoured composite structure relatively loose stitches are made in order to allow the number of plies to slip slightly in-plane relative to each other as they are being formed over a tooling and allow the stack to better conform to contoured tool surfaces and avoid ply wrinkling and bunching.

16. The method of claim 1 , wherein the polymer resin is selected such that the stitched stack of dry fiber layers assists in toughening the matrix resin and increases mechanical properties of a cured composite structure of the matrix resin.

17. The method of claim 16 , wherein the mechanical properties include impact resistance.

18. The method of claim 1 , wherein stitching comprises extending the thermoplastic stitches diagonally through a thickness of the stitched stack.

19. The method of claim 1 , wherein a thermoplastic material of each stitch comprises a thermoplastic resin selected from a group consisting of PEI (polyetherimide) PPS (polyphenylene sulphide), PES (polyethersulfone), PEKK (polyetheretherketone), and PEKK-FC (polyetherketoneketone-fc grade).

20. The method of claim 1 , wherein each stitch comprises a thermoplastic material that has a melt temperature of about 150 degrees.

Assignees

• Boeing Co

Inventors

• Coxon Brad Andrew

Classifications

• B32B5/06 Primary

  characterised by a fibrous {or filamentary} layer {mechanically connected, e.g. by needling} to another layer, e.g. of fibres, of paper · CPC title

• B29C66/73941

  characterised by the materials of both parts being thermosets · CPC title

• B29C70/42

  for producing articles of definite length, i.e. discrete articles · CPC title

• B29C66/72141

  Fibres of continuous length · CPC title

• Y10T428/24826

  Spot bonds connect components · CPC title