Assembly of a metal insert and a sheet of composite material, method for incorporating such an insert into such a sheet and part obtained by molding such a sheet

Patent metadata

Field	Value
Publication number	US-9925738-B2
Application number	US-201314443404-A
Country	US
Kind code	B2
Filing date	Nov 19, 2013
Priority date	Nov 20, 2012
Publication date	Mar 27, 2018
Grant date	Mar 27, 2018

Abstract

The assembly consists of at least one metal insert and one reinforcing sheet. The reinforcing sheet contains reinforcing fibers longer than or equal in length to one centimeter. The metal insert comprises protrusions shaped to traverse the sheet, passing between the reinforcing fibers, and to fold by plastic deformation, enclosing the reinforcing fibers when said protrusions are subjected to a longitudinal compression force.

First claim

What is claimed is:

1. An assembly comprising:
at least one metal insert and at least one reinforcing sheet of composite material, wherein:
at least one reinforcing sheet contains reinforcing fibers longer than or equal in length to one centimeter;
said at least one metal insert comprises protrusions shaped to:
traverse said at least one reinforcing sheet of composite material going between said reinforcing fibers forming projected ends;
fold towards said at least one reinforcing sheet of composite material by plastic deformation so that said projected ends of said protrusions point toward and at least partially embed in said at least one reinforcing sheet, enclosing said reinforcing fibers;

wherein said metal insert further comprises a screw barrel which traverses said at least one reinforcing sheet of composite material by separating said reinforcing fibers.

2. The assembly according to claim 1 , wherein said protrusions have a sharp end.

3. The assembly according to claim 1 , wherein said screw barrel traverses said at least one reinforcing sheet of composite material without damaging said at least one reinforcing sheet of composite material.

4. The assembly according to claim 1 , wherein said reinforcing fibers are a unidirectional sheet of long fibers.

5. The assembly according to claim 1 , wherein said reinforcing fibers consist of cut fibers distributed randomly in said at least one reinforcing sheet of composite material.

6. The assembly according to claim 1 , wherein said reinforcing fibers are carbon, glass or plant fibers.

7. The assembly according to claim 2 , wherein a screw barrel traverses said at least one reinforcing sheet of composite material without damaging said at least one reinforcing sheet of composite material.

8. The assembly according to claim 2 , wherein said reinforcing fibers are a unidirectional sheet of long fibers.

9. The assembly according to claim 2 , wherein said reinforcing fibers are carbon, glass or plant fibers.

10. A method of incorporating a metal insert in at least one reinforcing sheet of composite material wherein said method comprises the steps of:
providing at least one reinforcing sheet of composite material, wherein said at least one reinforcing sheet contains reinforcing fibers longer than or equal in length to one centimeter;
providing at least one metal insert comprising shaped protrusions;
depositing said at least one metal insert on said at least one reinforcing sheet of composite material;
pushing said protrusions through said at least one reinforcing sheet of composite material going between said reinforcing fibers forming projected ends;
folding by plastic deformation said protrusions toward said at least one reinforcing sheet of composite material so that said projected ends of said protrusions point toward and at least partially embed in said at least one reinforcing sheet, enclosing said reinforcing fibers;
wherein said metal insert further comprises a screw barrel which traverses said reinforcing sheet of composite material by separating said reinforcing fibers.

11. The method according to claim 10 , wherein said protrusions are folded by an axial or lateral force.

12. The method according to claim 10 , wherein the step of folding said protrusions is carried out before introducing an assembly in a mold for manufacturing a part made of composite material.

13. The method according to claim 10 , wherein the step of folding said protrusions is carried out in a mold for manufacturing a part made of a composite material.

14. The method according to claim 13 , wherein said protrusions are folded by an axial or lateral force.

15. A part made of composite material wherein said part is obtained by shaping and polymerizing an assembly comprising:
at least one metal insert and at least one reinforcing sheet of composite material, wherein:
at least one reinforcing sheet contains reinforcing fibers longer than or equal in length to one centimeter;
said at least one metal insert comprises protrusions shaped to:
traverse said at least one reinforcing sheet of composite material going between said reinforcing fibers forming projected ends;
fold towards said at least one reinforcing sheet of composite material by plastic deformation so that said projected ends of said protrusions point toward and at least partially embed in said at least one reinforcing sheet, enclosing said reinforcing fibers;

wherein said metal insert further comprises a screw barrel which traverses said at least one reinforcing sheet of composite material by separating said reinforcing fibers.

16. The part made of composite material according to claim 15 ,
wherein said protrusions have a sharp end.

17. The part made of composite material according to claim 15 , said part being a motor vehicle component.

Assignees

• Plastic Omnium Cie

Inventors

• Tresse David

Classifications

• B29C66/0324

  Reforming or reshaping the joint, e.g. folding over (reshaping the burr B29C66/326) · CPC title

• B29C35/02

  Heating or curing, e.g. crosslinking or vulcanizing {during moulding, e.g. in a mould}(cold vulcanisation B29C35/18 {; vulcanising tyres, presses therefor B29D30/0601}) · CPC title

• B32B3/30 Primary

  characterised by a layer formed with recesses or projections, e.g. {hollows, grooves, protuberances, ribs (apertured layer B32B3/266; layer with cavities or internal voids B32B3/26)} · CPC title

• Y10T428/24289

  Embedded or interlocked · CPC title

• B32B2262/101

  Glass fibres · CPC title