Granted Patent B2

US 8,163,119 · App. 12/970,804 · Granted Apr 24, 2012

Abstract

Claims (33)

1. A method for making a composite face plate for a club-head of a golf club, the method comprising:

forming a lay-up of multiple prepreg plies, each prepreg ply comprising at least one layer of reinforcing fibers impregnated with a resin, the lay-up comprising a central portion and a sacrificial portion surrounding the central portion;

at least partially curing the lay-up in a mold so as to form an at least partially cured lay-up having a bulge and roll;

removing the at least partially cured lay-up from the mold; and

after removing the at least partially cured lay-up from the mold, removing the sacrificial portion from the central portion of the at least partially cured lay-up to form a composite part having specified dimensions and shape for use as a face plate or part of a face plate in a club-head, wherein the central portion of the lay-up has first and second opposing surfaces and a thickness measured from the first surface to the second surface, and the act of removing the sacrificial portion forms an outer peripheral edge of the composite part that extends from the first surface to the second surface.

2. The method of claim 1 , wherein the act of at least partially curing the lay-up leaves no more than one void in the central portion of the partially cured lay-up.

3. The method of claim 1 , wherein, prior to the act of removing, the fibers of each ply have opposite end portions that extend into the sacrificial portion, and the act of removing the sacrificial portion is effective to separate the end portions of the fibers from the plies forming the composite part.

4. The method of claim 1 , wherein, prior to the act of removing, the sacrificial portion completely surrounds the central portion.

5. The method of claim 1 , wherein the part, after removing the sacrificial portion, has a void content of about 1.7×10 −6 percent or less by volume.

6. The method of claim 1 , wherein the part, after removing the sacrificial portion, does not have any voids.

7. The method of claim 1 , wherein the act of removing the sacrificial portion comprises water-jet cutting the sacrificial portion from the central portion.

8. The method of claim 1 , further comprising placing an outer layer on the composite part, the outer layer defining a striking surface of the face plate.

9. The method of claim 8 , wherein the outer layer comprises a polymeric layer.

10. The method of claim 8 , wherein the outer layer comprises a metal layer.

11. The method of claim 10 , wherein the metal layer is made of titanium, aluminum, magnesium, steel, or alloys thereof.

12. The method of claim 1 , wherein the lay-up has a varying thickness.

13. The method of claim 1 , wherein the resin comprises a thermoset resin.

14. The method of claim 1 , further comprising mounting the composite part to the club-head.

15. The method of claim 1 , wherein the club-head defines a front opening and the method further comprises mounting the composite part to the club-head so as to cover the front opening.

16. A method for making a composite part, the method comprising:

forming a lay-up of multiple prepreg plies, each prepreg ply comprising at least one layer of reinforcing fibers impregnated with a resin, the lay-up comprising a central portion and a sacrificial portion surrounding the central portion;

at least partially curing the lay-up in a mold, the mold forming at least one curved surface on the central portion of the lay-up;

removing the at least partially cured lay-up from the mold; and

after removing the partially cured lay-up from the mold, removing the sacrificial portion from the central portion of the at least partially cured lay-up to form the composite part, wherein the central portion of the lay-up has first and second opposing surfaces and a thickness measured from the first surface to the second surface, and the act of removing the sacrificial portion forms an outer peripheral edge of the composite part that extends from the first surface to the second surface.

17. The method of claim 16 , wherein the part, after removing the sacrificial portion, has a void content of about 1.7×10 −6 percent or less by volume.

18. The method of claim 16 , wherein the part, after removing the sacrificial portion, does not have any voids.

19. The method of claim 16 , wherein, prior to the act of removing the sacrificial portion, the sacrificial portion completely surrounds the central portion.

20. The method of claim 16 , wherein the resin cross-links during curing.

21. A method for making a composite face plate for a club-head of a golf club, the method comprising:

forming a lay-up of multiple prepreg plies, each prepreg ply comprising at least one layer of reinforcing fibers impregnated with a resin, the lay-up comprising a central portion and a sacrificial portion surrounding the central portion;

at least partially curing the lay-up; and

removing the sacrificial portion from the central portion of the at least partially cured lay-up to form a composite part having specified dimensions and shape for use as a face plate or part of a face plate in a club-head;

wherein at least some of the plies comprise elongated prepreg strips that are narrower in width than the width of the central portion, each strip having opposite end portions that extend into the sacrificial portion, and the act of removing the sacrificial portion is effective to separate the end portions of the strips from the remaining portions of the strips forming the composite part.

Assignments (12)