Method and apparatus for composite rib and rib-and-sheet molding

Patent metadata

Field	Value
Publication number	US-11059239-B2
Application number	US-201916653592-A
Country	US
Kind code	B2
Filing date	Oct 15, 2019
Priority date	Oct 15, 2018
Publication date	Jul 13, 2021
Grant date	Jul 13, 2021

Abstract

Rib-and-sheet structures include a rib comprising continuous, aligned fibers. The rib is fabricated via compression molding from continuous, aligned fiber, thereby providing an aligned, continuously reinforced rib. In one embodiment, rib-and-sheet structures are produced in a two-step compression-molding process, wherein a near net-shape rib is molded, in a first mold, from fiber-bundle based preforms, and then a rib-and-sheet part is molded by placing, in a second mold, the rib with either: (i) a preformed sheet, (ii) plies that form a laminate/sheet or (iii) chopped fibers that form a sheet during the molding process. In another embodiment, rib-and-sheet structures are fabricated in a one-step compression-molding process, wherein fiber-bundle-based preforms and (i) a preformed sheet, (ii) plies that form a laminate/sheet, or (iii) chopped fibers are combined in a single mold and molded in a single step.

First claim

What is claimed:

1. A method for molding, via compression molding, a rib-and-sheet part, the method comprising:
forming a plurality of continuous-fiber preforms, each preform comprising a bundle of unidirectionally aligned fibers impregnated with a first thermoplastic polymer resin;
organizing the preforms into an assemblage thereof, the assemblage having a first shape, wherein the assemblage consists of multiple layers, each layer comprising at least one of the preforms, and wherein at least some of the layers have the first shape;
compression molding, in a first mold, the assemblage, thereby subjecting it to heat that is sufficient to melt the first thermoplastic polymer resin and pressure that is sufficient to fully consolidate the assemblage of preforms into a rib having the first shape;
compression molding, in the first mold or in a second mold, a first material selected from the group consisting of a preformed sheet of prepreg, plural plies of prepreg, and chopped fibers, wherein heat and pressure applied via the compression molding is sufficient to consolidate the first material with the consolidated assemblage; and
cooling the consolidated first material and rib, thereby forming a rib-and-sheet part.

2. The method of claim 1 wherein the first shape comprises a loop, and wherein the loop comprises the unidirectionally aligned fibers.

3. The method of claim 1 wherein the first shape comprises a perimeter portion and an internal portion, the perimeter portion defining a loop, and the internal portion comprising one or more members disposed within the perimeter portion and that intersect the perimeter portion.

4. The method of claim 2 wherein the rib is discontinuous.

5. The method of claim 1 wherein at least some of the layers having the first shape have a gap therein, and when the layers having the gap are directly adjacent one another in overlying relation, organizing the preforms further comprises offsetting the gaps in the adjacent layers.

6. The method of claim 4 wherein for at least some of the layers having the first shape, the loop shape is formed from two “L”-shaped preforms.

7. The method of claim 1 and further comprising tacking together the assemblage of preforms, thereby forming a preform charge having the first shape.

8. The method of claim 1 wherein organizing the preforms into an assemblage further comprises:
organizing the preforms into an assemblage in a fixture physically adapted to organize them into the first shape;
tacking together the assemblage of preforms, thereby forming a preform charge having the first shape; and
removing the preform charge from the fixture and placing it in the first mold.

9. The method of claim 1 wherein compression molding, the assemblage in the first mold comprises:
cooling the consolidated assemblage, thereby forming the rib; and
placing the rib in the second mold.

10. The method of claim 9 wherein the second mold is configured to dispose at least a portion of the rib at a perimeter of the rib-and-sheet part.

11. The method of claim 1 wherein the first material and the assemblage are subjected to the heat and the pressure of compression molding in the first mold, and at the same time.

12. A method for molding, via compression molding, a rib-and-sheet part, the method comprising:
placing constituents in a mold cavity, the constituents comprising:
(i) a first material selected from the group consisting of a preformed sheet of prepreg, plural plies of prepreg, and chopped fibers; and
(ii) a plurality of continuous-fiber preforms, each preform comprising a bundle of unidirectionally aligned fibers impregnated with thermoplastic polymer resin, wherein placing the continuous-fiber preforms in the mold cavity further comprises arranging the plurality of preforms into an assemblage thereof, the assemblage having a first shape;

consolidating the constituents by compression molding the constituents; and
cooling the constituents, thereby forming a rib-and-sheet part, the rib containing the continuous, unidirectionally aligned fibers.

13. The method of claim 12 and further comprising tacking together the assemblage of preforms, thereby forming a preform charge having the first shape.

14. The method of claim 12 wherein the first shape comprises a loop.

15. The method of claim 12 wherein the first shape comprises a perimeter portion and an internal portion, the perimeter portion defining a loop, and the internal portion comprising one or more members disposed within the perimeter portion and that intersect the perimeter portion.

16. The method of claim 12 wherein the rib is discontinuous.

17. The method of claim 12 wherein the assemblage consists of multiple layers, each layer comprising at least one of the preforms, and wherein at least some of the layers have the first shape, and wherein at least some of the layers having the first shape have a gap therein, and when the layers having the gap are directly adjacent one another in overlying relation, arranging the preforms further comprises offsetting the gaps in the adjacent layers.

18. A method for molding, via compression molding, a rib-and-sheet part, the method comprising:
placing, in a first mold cavity, a preform charge having a first shape, the preform charge comprising an assemblage of a plurality of continuous-fiber preforms that are adhered to one another, each preform comprising a bundle of unidirectionally aligned fibers and thermoplastic polymer resin;
consolidating, by compression molding subjecting the preform charge in the first mold cavity, thereby forming a rib having the first shape;
compression molding, in the first mold cavity or in a second mold cavity, a first material selected from the group consisting of a preformed sheet of prepreg, plural plies of prepreg, and chopped fibers, in the presence of the rib, thereby consolidating the first material with the rib; and
cooling the consolidated first material and the rib, thereby forming a rib-and-sheet part, wherein the rib and the sheet are not coplanar.

19. The method of claim 18 wherein the first shape is a loop.

20. The method of claim 19 wherein the loop is discontinuous.

21. The method of claim 19 wherein the first shape comprises a perimeter portion and an internal portion, the perimeter portion defining a loop, and the internal portion comprising one or more members disposed within the perimeter portion and that intersect the perimeter portion.

Assignees

• Arris Composites Inc

Inventors

• Davidson Erick
• Reese Riley
• Escowitz Ethan
• Perkins J Scott

Classifications

• C08J5/24

  Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs · CPC title

• B29D99/0014 Primary

  provided with ridges or ribs, e.g. joined ribs · CPC title

• B29C70/46

  using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs · CPC title

• B29C70/345 Primary

  using matched moulds · CPC title

• B29C70/44

  using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding · CPC title