CONFORMABLE COMPOSITE STRUCTURAL MEMBER AND METHOD THEREFOR

• US 20020178992A1
• Filed: 05/29/2001
• Published: 12/05/2002
• Est. Priority Date: 05/29/2001
• Status: Active Grant

• Current Assignee: Composites Intellectual Holdings, Inc.
• Original Assignee: Compsys, Inc.
• Inventors: Lewit, Scott M.
• Granted Patent: US 6,497,190 B1
• Time in Patent Office: Days
• US Class Current: 114/357
• CPC Class Codes: B29C 44/0461 by having different chemical compositions in different places, e.g. having different concentrations of foaming agent, feeding one composition after the other
• CPC Class Codes: B29C 44/1209 by impregnating a preformed part, e.g. a porous lining
• CPC Class Codes: B32B 1/00 Layered products having a non-planar shape
• CPC Class Codes: B32B 2262/0253 Polyolefin fibres
• CPC Class Codes: B32B 2262/0276 Polyester fibres
• CPC Class Codes: B32B 2262/0292 Polyurethane 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 5/022 Non-woven fabric
• 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 5/32 at least two layers being foamed and next to each other
• CPC Class Codes: B63B 2231/50 Foamed synthetic materials
• CPC Class Codes: B63B 5/24 made predominantly of plastics surf boards B63B32/57

Abstract

A conformable composite reinforcing member (20) includes a cavity formed at least in part from a fabric layer (12) and at least a first foam core (16) and at least a second foam core (18) positioned within the cavity. The second foam core has a relatively higher rigidity than the first foam core. The first foam core is preferably made from an open cell or flexible foam and the second foam core is preferably made from a rigid open cell foam.

Claims

1. A method of forming a structural member, comprising the steps of:

providing a cavity formed at least in part from a fabric layer;

inserting at least a first foam core within the cavity; and

inserting at least a second foam core within the cavity, the second foam core having a relatively higher rigidity than the first foam core, wherein the second foam penetrates the fabric layer.

2. The method of claim 1, wherein the fabric layer is formed from fabric layers constructed by attaching a reinforcing fabric layer to a non-woven fabric layer forming an outside layer.

3. The method of claim 2, wherein the second foam core only penetrates the non-woven fabric layer.

4. The method of claim 1, wherein outer fabric layer of the structural member further comprises fabric flaps.

5. The method of claim 1, wherein the first foam core is made of a flexible open cell urethane and the second foam core is made of a rigid closed cell urethane.

6. The method of claim 1, wherein the fabric layer is selected among the group of directional reinforcing fabric layers of organic or inorganic structural reinforcing fabrics consisting of fiberglass, carbon fibers, aramid fibers, linear polyurethane fibers, polypropylene fibers, or polyester fibers or any combination thereof.

7. The method of claim 2, wherein the reinforcing fabric layer is an exposed reinforcing fabric layer that is laminated into a larger composite structure.

8. The method of claim 2, wherein the non-woven fabric layer is composed of materials selected from the group including polyester staple mat, glass fiber mat, or other organic and inorganic fiber mats and fabrics.

9. The method of claim 2, wherein the second foam core is formed of a self-expanding, self-curing urethane foam which has been caused to expand into the interstices of an inner one of the fabric layers by having been filled into a mold in an amount sufficient to cause pressure as a result of expansion of the foam cores to penetrate into the interstices of the inner one of the fabric layers.

10. The method of claim 1, wherein the second foam core is an MDI-based rigid polyurethane foam (methylene-diphenyl-methane diisocyanate) using “

hydrogenated chlorofluorocarbons”

(HCFC), water and/or CO₂ as a blowing agent.

11. The method of claim 1, wherein the step of inserting at least a first foam core comprises the step of feeding a soft foam strip into a mold.

12. The method of claim 11, wherein the step of inserting at least a second foam core comprises the step of injecting the second foam core underneath, above, within, or around the soft foam strip.

13. The method of claim 12, wherein the step of inserting at least a first foam core further comprises the step of inserting another soft foam strip underneath the second foam core, forming a rigid foam core sandwiched between two soft foam strips within the cavity.

14. The method of claim 2, wherein the fabric layer is formed from fabric layers constructed by attaching a reinforcing fabric layer to a non-woven fabric layer forming an upper outside layer and mating the upper outside layer with another non-woven fabric layer forming a lower outside layer, wherein the upper outside layer and the lower outside layer form an outside layer.

16. The method in accordance to claim 15, wherein the composite reinforcing member has an exposed reinforcing fabric layer that is laminated into a larger composite structure.

18. The conformable composite reinforcing member of claim 17, wherein the fabric layer is constructed by attaching a reinforcing fabric layer to a non-woven fabric layer forming an outside layer.

19. The conformable composite reinforcing member of claim 18, wherein the second foam core fills interstices of the non-woven fabric layer without penetrating into the reinforcing fabric layer.

20. The conformable composite reinforcing member of claim 17, wherein the second foam core surrounds the first foam core and has a relatively higher rigidity than the first foam core.

21. The conformable composite reinforcing member of claim 17, wherein the second foam core surrounds the first foam core and has a relatively lower rigidity than the first foam core.

15. A method of forming a conformable composite reinforcing member, comprising the steps of:

providing a cavity formed at least in part from a fabric layer by attaching a reinforcing fabric layer to a non-woven fabric layer forming an outside layer;

inserting at least a first foam core within the cavity; and

inserting at least a second foam core within the cavity wherein the second foam core is more rigid than the first foam core and wherein the second foam core penetrates the non-woven fabric layer.

17. A conformable composite reinforcing member, comprising:

a cavity formed at least in part from a fabric layer;

at least a first foam core located within the cavity; and

at least a second foam core positioned within the cavity, wherein the first foam core and the second foam core have relatively different rigidity or density.

22. A method of forming a composite structure requiring a tight curvature using at least a structural member, comprising the steps of:

providing the structural member wherein the structural member comprises a cavity formed at least in part from a fabric layer wherein a first foam core is inserted with the cavity and at least a second foam core is inserted within the cavity, the second foam core having a relatively higher rigidity than the first foam core, wherein the second foam penetrates the fabric layer;

conforming the structural member to the tight curvature of the composite structure;

hardening the structural member once the structural member is conformed to the tight curvature.

23. The method of claim 22, wherein the method of forming a composite structure comprises the method of forming a boat hull.

24. The method of claim 23, wherein the step of forming a boat hull and hardening the structural member within the boat hull comprises the steps of providing a mold having a tight curvature, providing a layer of gel coat on the mold, providing a layer of fiberglass mat on the gel coat, conforming the structural member to the tight curvature of the composite structure layered above the fiberglass mat, wetting out the structural member with resin, and allowing the resin on the structural member to cure.

25. The method of claim 22, wherein the method of forming a composite structure comprises the method of forming a tank.