Method of producing textile preforms for fiber reinforced composite products from textile semi-finished articles

• US 20030173019A1
• Filed: 03/10/2003
• Published: 09/18/2003
• Est. Priority Date: 03/08/2002
• Status: Active Grant

• Current Assignee: Airbus Operations GmbH (Airbus SE)
• Original Assignee: Airbus Deutschland GmbH (Airbus SE), Fraunhofer Gesellschaft Zur Foerderung Der Angewandten Forsching E.V.
• Inventors: Joern, Paul, Eberth, Ulrich
• Granted Patent: US 7,008,580 B2
• Time in Patent Office: Days
• US Class Current: 156/176
• CPC Class Codes: B29C 70/222 the structure being shaped to form a three dimensional configuration
• 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 70/32 on a rotating mould, former or core
• CPC Class Codes: D04C 1/06 Braid or lace serving particular purposes
• CPC Class Codes: D10B 2505/02 Reinforcing materials; Prepregs

Abstract

A method of producing a textile preform to be used for making a fiber reinforced plastic composite product involves the following steps. A two- or three-dimensional semi-finished textile material or article is produced by essentially any textile production process, such as weaving, knitting or braiding. A binder is applied to the textile material, which is then subjected to a reforming and/or draping process by being applied onto a carrier and reforming tool having a contour or geometry adapted to that of the desired preform that is to be produced. Thereby, the previously unfixed fibers of the textile material are brought into the desired finished orientation and are then fixed, and the cross-sectional shape of the material is changed. This produces the preform having the desired contour, geometry and fiber orientation. The preform may then be subjected to further processing steps to form the finished composite product.

Claims

1. A method of producing a textile preform for the subsequent manufacture of a fiber reinforced plastic composite product, comprising the steps:

a) producing a semi-finished textile material including unfixed fibers that are not yet entirely finally fixed, by a textile production process;

b) by a reforming and/or draping process, reforming and/or draping said semi-finished textile material to re-orient said unfixed fibers into a desired fiber orientation of said preform; and

c) applying said semi-finished textile material onto a carrier having a geometry adapted to a final intended geometry of said preform, to thereby form said preform having said final intended geometry.

2. The method according to claim 1, wherein said step b) is carried out directly following said step a).

3. The method according to claim 1, expressly excluding a step of temporarily arranging said semi-finished textile material on a temporary carrier having a geometry different from and unrelated to said final intended geometry of said preform.

4. The method according to claim 1, wherein said steps b) and c) are achieved concurrently, with said reforming and/or draping of said semi-finished textile material being achieved by performing said applying of said semi-finished textile material onto said carrier.

5. The method according to claim 1, wherein said textile production process is a two-dimensional textile production process.

6. The method according to claim 1, wherein said textile production process is a three-dimensional textile production process.

7. The method according to claim 1, wherein said textile production process is a weaving process, and said semi-finished textile material comprises a woven textile.

8. The method according to claim 1, wherein said textile production process is a braiding process, and said semi-finished textile material comprises a braided textile.

9. The method according to claim 1, wherein said carrier comprises a reforming tool, and wherein said steps b) and c) together comprise drawing said semi-finished textile material through or along said reforming tool, which changes a cross-sectional shape of said semi-finished textile material into said final intended geometry and at least partially changes an orientation of at least a portion of said unfixed fibers whereby said unfixed fibers are re-oriented into said desired fiber orientation of said preform.

10. The method according to claim 9, wherein said reforming tool comprises a curved matrix die onto and around which said semi-finished textile material is draped.

11. The method according to claim 1, wherein said semi-finished textile material includes standing end threads.

12. The method according to claim 1, wherein said carrier comprises a reforming tool, and wherein said steps b) and c) together comprise winding, wrapping or laying-up said semi-finished textile material onto said reforming tool, which changes a cross-sectional shape of said semi-finished textile material into said final intended geometry and at least partially changes an orientation of at least a portion of said unfixed fibers, whereby said unfixed fibers are re-oriented into said desired fiber orientation of said preform.

13. The method according to claim 12, wherein said reforming tool comprises a matrix die.

14. The method according to claim 1, wherein said carrier comprises a reforming tool, and wherein said steps b) and c) together comprise pushing, pressing or squeezing said semi-finished textile material into, onto or along said reforming tool, which changes a cross-sectional shape of said semi-finished textile material into said final intended geometry and at least partially changes an orientation of at least a portion of said unfixed fibers, whereby said unfixed fibers are reoriented into said desired fiber orientation of said preform.

15. The method according to claim 14, wherein said reforming tool comprises a matrix die.

16. The method according to claim 14, wherein said pushing, pressing or squeezing comprises pressing said semi-finished textile material onto said reforming tool using a counter-pressing roller.

17. The method according to claim 1, further comprising fixing said fibers in said desired fiber orientation after said steps b) and c), due to an interengaging friction of said fibers relative to each other, which prevents further movement of said fibers out of said desired fiber orientation.

18. The method according to claim 1, further comprising applying a binder to said fibers before, during or after said reforming and/or draping process, and fixing said fibers in said desired fiber orientation by at least partly curing said binder.

19. The method according to claim 18, further in combination with processing said preform to manufacture said fiber reinforced plastic composite product, comprising applying a resin matrix material to said preform and curing said resin matrix material under an elevated temperature and/or elevated pressure.

20. The method according to claim 1, further comprising applying a resin matrix material to said fibers before, during or after said reforming and/or draping process, and fixing said fibers in said desired fiber orientation by at least partly curing said matrix material.

21. The method according to claim 20, further in combination with processing said preform to manufacture said fiber reinforced plastic composite product, comprising completely curing said resin matrix material under an elevated temperature and/or elevated pressure.

22. The method according to claim 1, further in combination with processing said preform to manufacture said fiber reinforced plastic composite product, comprising applying a resin matrix material to said preform and curing said resin matrix material under an elevated temperature and/or elevated pressure.

23. The method according to claim 1, further comprising pre-orienting said fibers at least partially in said desired fiber orientation of said preform already during said step a).

24. The method according to claim 1, wherein said step a) includes providing respective longitudinally extending fibers of varying lengths in said semi-finished textile material, and said steps b) and c) include forming a curve in said final intended geometry with said varying lengths of said longitudinally extending fibers respectively adapted to varying arc lengths at different radial positions in said curve.