Methods for improving conformability of non-crimp fabric and contoured composite components made using such methods

• US 8,234,990 B2
• Filed: 07/31/2008
• Issued: 08/07/2012
• Est. Priority Date: 07/31/2008
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Xie, Ming, Stephens, Brian, Schulte, Elliott, Gentry, Johnny Ray
• Primary Examiner(s): Izaguirre, Ismael
• Application Number:
  US12/183,187
• Publication Number:
  US 20100024179A1
• Time in Patent Office: 1,468 Days
• Field of Search: 11247501-47509, 112/475.15, 112/475.17, 112/413, 112/415, 66/82.S, 661/92, 661/70, 661/90, 428 98-113, 428/221, 281/40, 281/43, 281/64, 281/65, 264/292, 264/324, 442/183, 442/189, 442/226, 442/350
• US Class Current: 112/475.17
• CPC Class Codes: D04B 21/16 incorporating synthetic threads
• CPC Class Codes: D04B 21/165 with yarns stitched through one or more layers or tows, e.g. stitch-bonded fabrics layered products not united by stitch loops B32B5/22
• CPC Class Codes: D04H 3/002 Inorganic yarns or filaments
• CPC Class Codes: D04H 3/004 Glass yarns or filaments
• CPC Class Codes: D04H 3/005 Synthetic yarns or filaments D04H3/013 takes precedence
• CPC Class Codes: D04H 3/04 in rectilinear paths, e.g. crossing at right angles
• CPC Class Codes: D04H 3/115 by applying or inserting filamentary binding elements
• CPC Class Codes: D10B 2403/02412 including several arrays of unbent yarn, e.g. multiaxial fabrics
• CPC Class Codes: Y10T 428/24033 including stitching and discrete fastener[s], coating or bond

Abstract

Methods for making a self-conforming non-crimp fabric involving tailoring at least a first parameter to anchor the fabric and at least a second parameter to provide conformability of the fabric, the first and second parameters selected from stitch type, stitch spacing, stitch density, stitch material, stitch weight, stitch tension, and combinations of the same.

Claims

1. A method comprising:

forming a self-conforming non-crimp fabric comprising layers of unidirectional fibers and stitching by tailoring at least a first parameter of the stitching to anchor the fabric and at least a second parameter of the stitching to provide conformability of the fabric, the first and second parameters selected from the group consisting of stitch type, stitch spacing, stitch density, stitch material, stitch weight, stitch tension, and combinations thereof;

infusing the fabric with a resin; and

then

curing the resin to form a component containing the layers and the stitching, the component comprising an anchoring region including the stitching tailored by the first parameter and a conforming region including the stitching tailored by the second parameter.

2. The method of claim 1 wherein the non-crimp fabric comprises fibers selected from the group consisting of carbon fibers, graphite fibers, glass fibers, ceramic fibers, aromatic polyamide fibers, and combinations thereof.

3. The method of claim 1, wherein the tailoring of the first and second parameters comprises tailoring the first parameter to utilize a simple stitch type to anchor the fabric, or tailoring the second parameter to utilize a complex stitch type to provide conformability of the fabric, or a combination thereof.

4. The method of claim 1, wherein the tailoring of the first and second parameters comprises tailoring the first parameter to utilize a smaller stitch spacing to anchor the fabric, or tailoring the second parameter to utilize a larger stitch spacing to provide conformability of the fabric, or a combination thereof.

5. The method of claim 4 wherein the smaller stitch spacing comprises a stitch spacing of about 10 ppi to about 2.5 ppi and the larger stitch spacing comprises stitch spacing of about 2.49 ppi to about 0.1 ppi.

6. The method of claim 1, wherein the tailoring of the first and second parameters comprises tailoring the first parameter to utilize a high stitch density to anchor the fabric, or tailoring the second parameter to utilize a low stitch density to provide conformability of the fabric, or a combination thereof.

7. The method of claim 6 wherein the high stitch density comprises stitches having a density of about 10 stitches/1 inch (about 10 stitches/2.54 cm) to about 5 stitches/1 inch (about 5 stitches/2.54 cm) and the low stitch density comprises stitches having a density of about 4.9 stitches/1 inch (about 4.9 stitches/2.54 cm) to about 1 stitch/1 inch (about 1 stitch/2.54 cm).

8. The method of claim 1, wherein the tailoring of the first and second parameters comprises tailoring the first parameter to utilize a rigid stitch material to anchor the fabric, or tailoring the second parameter to utilize an elastic stitch material to provide conformability of the fabric, or a combination thereof.

9. The method of claim 8 wherein the rigid stitch material comprises nylon filaments and the elastic stitch material comprises thermoplastic elastomers.

10. The method of claim 1, wherein the tailoring of the first and second parameters comprises tailoring the first parameter to utilize a heavy stitch weight to anchor the fabric, or tailoring the second parameter to utilize a light stitch weight to provide conformability of the fabric through controlled stitch breakage, or a combination thereof.

11. The method of claim 10 wherein the heavy stitch weight comprises a stitch weighing about 72 denier or greater and the light stitch weight comprises a stitch weighing less than about 72 denier.

12. The method of claim 1, wherein the tailoring of the first and second parameters comprises tailoring the first parameter to utilize a taut stitch tension to anchor the fabric, or tailoring the second parameter to utilize a slack stitch tension to provide conformability of the fabric, or a combination thereof.

13. The method of claim 1, comprising providing conformability of the fabric by interrupting the stitching of any of the first parameter, the second parameter, or a combination thereof.

14. The component made by the method of claim 1.

21. The composite component of claim 14, wherein the composite component is a contoured containment casing of an engine.

22. The composite component of claim 14, wherein the composite component is a fan blade of an engine or a wind blade of a windmill.

15. A method comprising:

forming a self-conforming non-crimp fabric comprising layers of unidirectional fibers and stitching by tailoring at least one of a first parameter of the stitching to anchor the fabric and at least one of a second parameter of the stitching to provide conformability of the fabric wherein the first parameter is at least one selected from the group consisting of a simple stitch type, smaller stitch spacing, high stitch density, rigid stitch material, heavy stitch weight, taut stitch tension, and combinations thereof, and the second parameter is at least one selected from the group consisting of a complex stitch type, larger stitch spacing, low stitch density, elastic stitch material, light stitch weight, slack stitch tension, and combinations thereof wherein the non-crimp fabric comprises fibers selected from the group consisting of carbon fibers, graphite fibers, glass fibers, ceramic fibers, aromatic polyamide fibers, and combinations thereof;

infusing the fabric with a resin; and

then

curing the resin to form a component containing the layers and the stitching, the component comprising an anchoring region including the stitching tailored by the first parameter and a conforming region including the stitching tailored by the second parameter.

16. The method of claim 15 wherein the first parameter comprises the smaller stitch spacing and stitch spacing of about 10 ppi to about 2.5 ppi and the second parameter comprises the larger stitch spacing and stitch spacing of about 2.49 ppi to about 0.1 ppi.

17. The method of claim 15, wherein the first parameter comprises the high stitch density and stitches having a density of about 10 stitches/1 inch (about 10 stitches/2.54 cm) to about 5 stitches/1 inch (about 5 stitches/2.54 cm) and the second parameter comprises the low stitch density and stitches having a density of about 4.9 stitches/1 inch (about 4.9 stitches/2.54 cm) to about 1 stitch/1 inch (about 1 stitch/2.54 cm).

18. The method of claim 15, wherein the first parameter comprises the heavy stitch weight and a stitch weighing about 72 denier or greater and the second parameter comprises the light stitch weight and a stitch weighing less than about 72 denier.

19. The method of claim 15, further comprising providing conformability of the fabric by interrupting the stitching of any of the first parameter, the second parameter, or a combination thereof.

20. The component made by the method of claim 15.

23. The composite component of claim 20, wherein the composite component is a contoured containment casing of an engine.

24. The composite component of claim 20, wherein the composite component is a fan blade of an engine or a wind blade of a windmill.