Composite structures and method of making composite structures

• US 5,429,066 A
• Filed: 01/14/1994
• Issued: 07/04/1995
• Est. Priority Date: 01/14/1994
• Status: Expired due to Term

• Current Assignee: Compsys, Inc.
• Original Assignee: Compsys, Inc.
• Inventors: Lewit, Scott, Rohan, Neil
• Primary Examiner(s): BASINGER, SHERMAN D
• Application Number:
  US08/181,321
• Time in Patent Office: 536 Days
• Field of Search: 114/357, 264/258, 264/46.4, 264/46.6
• US Class Current: 114/357
• CPC Class Codes: B29C 2791/001 Shaping in several steps
• CPC Class Codes: B29C 44/1209 by impregnating a preformed part, e.g. a porous lining
• CPC Class Codes: B29C 44/1261 Avoiding impregnation of a preformed part
• CPC Class Codes: B29C 44/60 Measuring, controlling or regulating
• CPC Class Codes: B29K 2105/0809 Fabrics
• CPC Class Codes: B29K 2105/0854 in the form of a non-woven mat
• CPC Class Codes: B32B 1/00 Layered products having a non-planar shape
• CPC Class Codes: B32B 2262/0253 Polyolefin fibres vinyl or acrylic copolymers B32B2262/0223 or B32B2262/0246
• CPC Class Codes: B32B 2262/0269 Aromatic polyamide fibres
• CPC Class Codes: B32B 2262/0276 Polyester fibres
• CPC Class Codes: B32B 2262/101 Glass fibres
• CPC Class Codes: B32B 2262/106 Carbon fibres, e.g. graphite fibres
• CPC Class Codes: B32B 2266/0278 Polyurethane
• CPC Class Codes: B32B 2605/12 Ships
• CPC Class Codes: B32B 5/022 Non-woven fabric
• CPC Class Codes: B32B 5/06 characterised by a fibrous or filamentary layer mechanically connected, e.g. by needling to another layer, e.g. of fibres, of paper
• CPC Class Codes: B32B 5/18 characterised by features of a layer of foamed material
• CPC Class Codes: B32B 5/20 foamed in situ
• CPC Class Codes: B32B 5/24 one layer being a fibrous or filamentary layer
• CPC Class Codes: B32B 5/245 another layer next to it being a foam layer
• CPC Class Codes: B32B 5/26 : another layer next to it also being fibrous or filamentary relative arrangement of fibres or filaments of different layers B32B5/12
• CPC Class Codes: B63B 2231/50 : Foamed synthetic materials
• CPC Class Codes: B63B 2231/52 : Fibre reinforced plastics materials
• CPC Class Codes: B63B 5/24 : made predominantly of plastics surf boards B63B32/57

Abstract

A composite structure and method of making the composite structure are disclosed. A reinforcing fabric such as fiberglass is mechanically attached, for example, by stitching to a non-woven polyester fabric. The attached fabrics are placed in a mold with the non-woven fabric facing the inside of the mold. A self-expanding, self-curing foam is filled into the mold in an amount sufficient so that upon expansion in the closed mold, the foam penetrates into the interstices of the non-woven fabric which upon curing forms a bond therewith. The resulting structure can be used in a number of applications wherein the reinforcing fabric is later impregnated, for example, with a resin, and allowed to cure. Typical use of such a structure is as a stringer in fiberglass boat construction.

Claims

1. A composite structure having an exposed reinforcing fabric layer free of structural foam and curable resin, said structure comprising:

a reinforcing fabric layer;

a non-woven fabric layer attached to said reinforcing fabric layer; and

a structural foam attached to said non-woven fabric layer on the side of said non-woven fabric layer opposite said reinforcing fabric layer by having filled interstices of said non-woven fabric layer without penetrating into the reinforcing fabric layer;

wherein said reinforcing fabric layer of said composite structure is capable of being saturated with curable resin after said structural foam has been attached to said non-woven fabric layer.

2. A composite structure as in claim 1 wherein said reinforcing fabric layer is a directional reinforcing fabric.

3. A composite structure as in claim 1 wherein said reinforcing fabric layer is composed of organic or inorganic fibers.

4. A composite structure as in claim 1 wherein said reinforcing fabric layer is one of fiberglass, carbon fiber, aramid fiber, linear polyethylene or polypropylene fiber, and polyester fiber.

5. A composite structure as in claim 1 wherein said non-woven fabric layer is one of nonwoven fabric composed of continuous thermoplastic fibers, needle punched together as a felt-like fiber.

6. A composite structure as in claim 5 wherein said reinforcing fabric is mechanically attached to said non-woven fabric by stitching.

7. A composite structure as in claim 1 wherein said non-woven fabric layer is one of polyester staple mat, glass fiber mat, organic fiber mat and inorganic fiber mat.

8. A composite structure as in claim 1 wherein said reinforcing fabric is mechanically attached to said non-woven fabric.

9. A composite structure as in claim 7 wherein said structural foam is a two-part, self-expanding, self-curing urethane foam which has been expanded and cured to attach itself to said non-woven fabric by having expanded into the interstices of said non-woven fabric.

10. A composite structure as in claim 9 wherein said urethane foam is buoyant.

11. A composite structure as in claim 1 shaped in the form of a stringer for boat construction.

12. A method of making a composite structure having an exposed reinforcing fabric layer free of structural foam and curable resin, said method comprising the steps of:

attaching a reinforcing fabric layer to a non-woven fabric layer on one side thereof;

laying said attached fabric layers into a mold with the non-woven fabric layer facing the interior of the mold;

filling said mold with a self-expanding, self-curable, uncured structural foam; and

allowing said foam to expand and cure to attach itself to said non-woven fabric layer by filling interstices of said non-woven fabric layer in a manner such that said foam does not penetrate into the reinforcing fabric layer to thereby result in said composite structure, and

wherein said reinforcing fabric layer of said composite structure is capable of being subsequently saturated with curable resin after said structural foam has been attached to said non-woven fabric layer.

13. A method as in claim 12 wherein said attaching step is conducted by mechanically attaching said reinforcing fabric layer to said non-woven fabric layer.

14. A method as in claim 13 wherein said mechanical attaching is conducted by stitching.

15. A method as in claim 12 wherein said reinforcing fabric layer is a directional reinforcing fabric layer.

16. A method as in claim 12 wherein said reinforcing fabric layer is made of one of fiberglass, carbon fiber, aramid fiber, linear polyethylene or polypropylene fiber, and polyethylene fiber.

17. A method as in claim 12 wherein said reinforcing fabric layer is composed of organic or inorganic fibers.

18. A method as in claim 12 wherein said non-woven fabric layer is a non-woven fabric composed of continuous thermoplastic fiber needle, punched together as a felt-like fiber.

19. A method as in claim 18 further comprising the step of laying a separate layer of non-woven fabric on the layer of non-woven fabric attached to said reinforcing fabric layer prior to adding said foam to said mold, with said separate layer of non-woven fabric being of sufficient thickness to allow said foam to penetrate therethrough and into the layer of non-woven fabric attached to said reinforcing fabric layer, without penetrating into said reinforcing fabric layer.

20. A method as in claim 12 wherein said non-woven fabric layer is one of polyester staple mat, glass fiber mat, organic fiber mat and inorganic fiber mat.

21. A method as in claim 12 wherein said structural foam is a two-part, self-expanding, self-curing urethane foam, and further comprising allowing said foam to partially expand before filling said foam into said mold, and filling said mold with an amount of foam sufficient to cause said foam to penetrate into interstices of said non-woven fabric as it expands and cures without penetrating into said reinforcing fabric layer.

22. A method as in claim 12 wherein said structural foam is a two-part, self-expanding, self-curing urethane foam and further comprising filling said mold with an amount of foam sufficient to cause said foam to penetrate into interstices of said non-woven fabric as it expands and cures.

23. A method as in claim 22 wherein said non-woven fabric layer is of sufficient thickness to allow said foam to penetrate into interstices thereof without penetrating into said reinforcing fabric layer.

24. A method as in claim 12 wherein said mold is shaped as a stringer for use in boat construction.

25. A method as in claim 24 wherein said mold has rounded edges and corners.

26. A method as in claim 25 wherein said reinforcing fabric layer is woven fiberglass.

27. A method of manufacturing a boat, comprising the steps of:

spraying a layer of gelcoat into a boat-hull mold and allowing said gelcoat layer to cure;

laying a structural skin coat of fiberglass;

laying stringers throughout said mold in a reinforcing arrangement on said structural skin coat of fiberglass, said stringers being made as a composite structure comprising, a reinforcing fabric layer, a non-woven fabric layer attached to said reinforcing fabric layer, a structural foam attached to said non-woven fabric layer on the side of said non-woven fabric layer opposite said reinforcing fabric layer by having filled interstices of said non-woven fabric layer, and said stringers having flaps of said attached reinforcing fabric layer and non-woven fabric layer extending therefrom and not attached to said foam, with said stringers being laid so that said flaps lay on said structural skin coat of fiberglass;

impregnating said structural skin coat of fiberglass and said stringers with curable resin; and

curing said resin to result in a boat hull having said stringers attached thereto.

28. A method as in claim 27 wherein said structural skin coat of fiberglass is impregnated with resin and cured prior to laying said stringers therein, and further comprising the steps of;

laying layers of chopped fiberglass on said cured skin coat at the locations where said stringers are to be laid;

impregnating said chopped fiberglass and stringers with resin;

laying the stringers on said layers of chopped fiberglass; and

curing said resin.

29. A method as in claim 27 wherein said reinforcing fabric layer of said stringers is fiberglass.

30. A method as in claim 27 wherein said structural skin layer of fiberglass laid in said mold is one of chopped strand mat, chopped roving, woven roving and stitch bonded fiberglass.

32. A method as in claim 27 wherein the reinforcing fabric layer and non-woven fabric layer of said stringers are mechanically attached.

31. A method as in clam 27 wherein said impregnation with resin is conducted prior to laying said stringers in said mold.