Composite panel adapted for point compressive loads and method for making same

• US 6,755,998 B1
• Filed: 10/26/2000
• Issued: 06/29/2004
• Est. Priority Date: 10/26/1999
• Status: Active Grant

• Current Assignee: Composites Intellectual Holdings, Inc.
• Original Assignee: Compsys, Inc.
• Inventors: Lewit, Scott M., Mackaness, Miles P., Reichard, Ronnal P., Rohan, Neil A.
• Primary Examiner(s): Kuhns, Allan R.
• Application Number:
  US09/697,465
• Time in Patent Office: 1,342 Days
• Field of Search: 264/46.5, 264/46.7, 264/257, 264/258
• US Class Current: 264/46.5
• CPC Class Codes: B29C 44/12 Incorporating or moulding on preformed parts, e.g. inserts or reinforcements
• CPC Class Codes: B29C 44/14 the preformed part being a lining B29C44/1209 takes precedence
• CPC Class Codes: B32B 17/067 of fibres or filaments
• CPC Class Codes: B32B 2262/0276 Polyester fibres
• CPC Class Codes: B32B 2315/085 Glass fiber cloth or fabric
• CPC Class Codes: B32B 2323/10 Polypropylene
• CPC Class Codes: B32B 2375/00 Polyureas; Polyurethanes
• CPC Class Codes: B32B 2605/00 Vehicles
• CPC Class Codes: B32B 5/022 Non-woven fabric
• CPC Class Codes: B32B 5/18 characterised by features of a layer of foamed material
• 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

Abstract

A method for making a composite panel includes the step (26) of providing a panel having elongated channels (14) that are positioned along areas of anticipated point compression loading. The panel (10) has a reinforcing fabric layer (41) attached to a non-woven fabric layer (43) forming an outside layer (12). The composite panel has foam core (8,9) within the outside layer. The method further comprises the step (27) of providing structural foam channel inserts (16) having an outer fabric layer (18), wherein the channel inserts have a cross section which matches the cross-sectional profile of each of the elongated channels of the panel. Resin is then applied to the outside layer of the panel and outer fabric layer of the channel inserts such the channel inserts are positioned within the channels of the panel (29 and 31). The resin is then allowed to cure (33) forming a composite structure.

Claims

1. A method of forming high strength panels suitable for use in applications requiring a capability to withstand point compression loading without deformation, comprising the steps of:

positioning a first fabric layer spaced from a second fabric layer to form opposing panel surfaces;

fixing a foam core between at least a portion of said fabric layers to form said panel;

defining in at least one of said opposing panel surfaces an elongated channel having a cross-sectional profile;

forming a rigid point compressive load bearing member having a structural foam core, an outer fabric layer including fabric flaps and said cross-sectional profile of said elongated channel;

applying resin to said flaps and mating surfaces of the rigid point oppressive load bearing member and said elongated channel;

positioning said rigid point compressive load bearing member in said elongated channel after said applying step; and

allowing said resin to cure to provide along a length of said rigid point compressive load bearing member a greater resistance to point compression as compared to a remaining portion of said panel exclusive of said rigid point compressive load bearing member.

2. The method according to claim 1 further comprising the step of forming at a periphery of said opposing panel surfaces a plurality of fabric tabs attached to at least one of said first and second fabric layers.

3. The method according to claim 1 further comprising the step of laminating said panel into a composite boat hull to form a transom.

4. The method according to claim 1 further comprising the step of injecting a curable structural foam in a space between said opposing panel surfaces while constraining the first and second fabric layers from movement so as to form said foam core.

5. The method according to claim 4, further comprising the step of constraining said foam under a molding pressure selected to cause said foam to penetrate only partially through an inner thickness of said first and second fabric layers so as to leave an outer exposed portion of said fabric layer free of said structural foam.

6. The method according to claim 4 further comprising the step of attaching a non-woven fabric layer to a reinforcing fabric layer to form each of said first and second fabric layers.

7. The method according to claim 6 further comprising the step of arranging said first and second fabric layers so that said reinforcing fabric layer forms an outer panel surface and said non-woven fabric layer forms an inner panel surface.

8. The method of claim 6, further comprising the step of selecting said reinforcing fabric layer from the group consisting of fiberglass, carbon fibers, aramid fibers, linear polyurethane fiber, polypropylene fibers, and polyester.

9. The method of claim 6, further comprising the step of selecting the non-woven fabric layer from the group consisting of polyester staple mat, glass fiber mat, a continuous thermoplastic fiber which is needle punched to form a felt-like fabric, or other organic and inorganic fiber mats and fabrics.

10. A method for manufacturing a composite boat transom comprising the steps of:

positioning a first fabric layer spaced from a second fabric layer to form opposing transom surfaces;

positioning elongated rigid channel members between said first and second fabric layers aligned with locations corresponding to areas of anticipated point compressive loading; and

injecting a foam core between said first and second fabric layers.

11. The method according to claim 10 further comprising the step of aligning said elongated rigid channel members with an anticipated location of a bolt for an outboard motor bracket.

12. The method according to claim 11 further comprising the step of selecting said elongated rigid channel members to be formed of metal.

13. The method according to claim 10 further comprising the step of injecting said foam core within said rigid channel members.

14. The method according to claim 10 further comprising the step of forming said first and second fabric layers to include fabric flaps at a periphery of said composite transom.

15. The method according to claim 14 further comprising the step of positioning said composite transom to form part of a composite boat hull and laminating said exposed reinforcing fabric flaps into said composite boat hull.

16. The method according to claim 10 wherein said injecting step further comprises causing said foam core to penetrate at least partially into interstices of said fabric layer to bind said foam core to said fabric layers.

17. A method for manufacturing a composite boat transom comprising the steps of:

positioning a first fabric layer spaced from a second fabric layer to form opposing transom surfaces;

positioning elongated rigid channel members between said first and second fabric layers aligned with locations corresponding to areas of anticipated point compressive loading associated with an outboard motor bracket;

injecting a foam core between said first and second fabric layers; and

causing said foam core to penetrate at least partially into interstices of said fabric layers to bind said foam core to said fabric layers.

18. The method according to claim 17 further comprising the step of selecting said elongated rigid channel members to be formed of metal.

19. The method according to claim 18 further comprising the step of injecting said foam core within said rigid channel members.

20. The method according to claim 17 further comprising the step of forming said first and second fabric layers to include fabric flaps at a periphery of said composite transom.

21. A method of forming high strength panels suitable for use in applications requiring a capability to withstand point compression loading without deformation, comprising the steps of:

positioning a first fabric layer spaced from a second fabric layer to form opposing panel surfaces;

fixing a foam core between at least a portion of said fabric layers to form said panel;

positioning at least one rigid point compressive load bearing member between portions of said foam core along areas of anticipated point compression loading in a location to prevent compression of said foam core when a point compressive load is applied to said point compressive load bearing members; and

selecting said point compressive load bearing member to be an elongated channel formed of a material selected from the group consisting of steel, aluminum and a metal alloy.

22. A method of forming high strength panels suitable for use in applications requiring a capability to withstand point compression loading without deformation, comprising the steps of:

positioning a first fabric layer spaced from a second fabric layer to form opposing panel surfaces;

fixing a foam core between at least a portion of said fabric layers to form said panel;

positioning at least one rigid point compressive load bearing member between portions of said foam core along areas of anticipated point compression loading in a location to prevent compression of said foam core when a point compressive load is applied to said point compressive load bearing members; and

forming at a periphery of said opposing panel surfaces a plurality of fabric tabs attached to at least one of said first and second fabric layers.

23. A method of forming high strength panels suitable for use in applications requiring a capability to withstand point compression loading without deformation, comprising the steps of:

positioning a first fabric layer spaced from a second fabric layer to form opposing panel surfaces;

fixing a foam core between at least a portion of said fabric layers to form said panel;

positioning at least one rigid point compressive load bearing member between portions of said foam core along areas of anticipated point compression loading in a location to prevent compression of said foam core when a point compressive load is applied to said point compressive load bearing members; and

laminating said panel into a composite boat hull to form a transom.

24. A method of forming high strength panels suitable for use in applications requiring a capability to withstand point compression loading without deformation, comprising the steps of:

positioning a first fabric layer spaced from a second fabric layer to form opposing panel surfaces;

positioning a rigid point compressive load bearing member between said first and second fabric layers along areas of anticipated point compression loading; and

injecting a foam core between at least a portion of said first and second fabric layers to form said panel, wherein said rigid point compressive load bearing member prevents compression of said foam core when a point compressive load is applied to said point compressive load bearing member; and

injecting a foam core into said rigid point compressive load bearing member.

25. A method of forming high strength panels suitable for use in applications requiring a capability to withstand point compression loading without deformation, comprising the steps of:

positioning a first fabric layer spaced from a second fabric layer to form opposing panel surfaces;

positioning a rigid point compressive load bearing member between said first and second fabric layers along areas of anticipated point compression loading; and

injecting a foam core between at least a portion of said first and second fabric layers to form said panel, wherein said rigid point compressive load bearing member prevents compression of said foam core when a point compressive load is applied to said point compressive load bearing member; and

selecting said rigid point compressive load bearing member to be an elongated channel formed of a material selected from the group consisting of steel, aluminum and a metal alloy.