Systems and methods for additive manufacturing of a golf club

Patent metadata

Field	Value
Publication number	US-12269209-B2
Application number	US-202418436759-A
Country	US
Kind code	B2
Filing date	Feb 8, 2024
Priority date	Apr 17, 2020
Publication date	Apr 8, 2025
Grant date	Apr 8, 2025

Abstract

A process of manufacturing a golf club component includes spreading a thin layer of metal powder over a build plane defined over a build platform and bonding, using a laser, portions of the thin layer of metal powder. The spreading and bonding are repeated until the golf club component is formed. The golf club component comprises a lattice structure positioned within an internal cavity of the golf club component and the lattice structure is interrupted by a solid portion that extends along a bottom side of the golf club component from a toe region of the golf club component to a location between the toe region and a heel region of the golf club component.

First claim

We claim:

1. A process of manufacturing a golf club component, comprising:
spreading a thin layer of metal powder over a build plane defined over a build platform;
bonding, using a laser, portions of the thin layer of metal powder, wherein the spreading and bonding are repeated until the golf club component is formed;
cooling the golf club component; and
extracting loose powder from the golf club component,
wherein the golf club component comprises a lattice structure positioned within an internal cavity of the golf club component and the lattice structure is interrupted by a solid portion that extends along a bottom side of the golf club component from a toe region of the golf club component to a location between the toe region and a heel region of the golf club component,
wherein a cavity extends into the solid portion and a weight is positioned within the cavity of the solid portion.

2. The process of manufacturing the golf club component of claim 1 , wherein the weight is attached or secured within the cavity via a sintering process.

3. The process of manufacturing the golf club component of claim 1 , wherein the weight is formed by a metal injection molding process.

4. The process of manufacturing the golf club component of claim 1 , wherein the lattice structure defines a hybrid structure that varies in one or more of unit cell type, unit cell geometry, unit cell size, segment length, segment thickness, segment volume, and unit cell density at one or more locations along the lattice structure.

5. The process of manufacturing the golf club component of claim 1 , wherein the golf club component includes an externally visible lattice structure.

6. The process of manufacturing the golf club component of claim 1 , wherein the step of extracting loose powder from the golf club component includes removing any loose metal powder from the golf club component.

7. The process of manufacturing the golf club component of claim 1 , wherein the build plane is rotationally offset from a ground plane, the ground plane defined as a horizontal plane parallel to the ground when the golf club component is at address.

8. A process of manufacturing a golf club component, comprising:
spreading a thin layer of metal powder over a build plane defined over a build platform; and
bonding, using a laser, portions of the thin layer of metal powder, wherein the spreading and bonding are repeated until the golf club component is formed;
wherein the golf club component comprises a lattice structure positioned within an internal cavity of the golf club component, and wherein the lattice structure is formed by a plurality of segments,
wherein the lattice structure defines a lattice plane L 1 that forms a lattice build angle A 1 with respect to the build plane, and a lattice plane L 2 that forms a lattice build angle A 2 with respect to the build plane, each of the lattice plane L 1 and the lattice plane L 2 is formed by a portion of the plurality of segments that are aligned and orientated at the lattice build angle A 1 and the lattice build angle A 2 , respectively, relative to the build plane, and
wherein each of the lattice build angle A 1 and the lattice build angle A 2 is greater than or equal to 30 degrees.

9. The process of manufacturing the golf club component of claim 8 , wherein the lattice structure defines a lattice plane L 3 that forms a lattice build angle A 3 with respect to the build plane, and a lattice plane L 4 that forms a lattice build angle A 4 with respect to the build plane, each of the lattice plane L 3 and the lattice plane L 4 is formed by a portion of the plurality of segments that are aligned and orientated at the lattice build angle A 3 and the lattice build angle A 4 , respectively, relative to the build plane.

10. The process of manufacturing the golf club component of claim 9 , wherein each of the lattice build angle A 3 and the lattice build angle A 4 is greater than or equal to 30 degrees.

11. The process of manufacturing the golf club component of claim 9 , wherein each of the lattice plane L 1 , the lattice plane L 2 , the lattice plane L 3 , and the lattice plane L 4 extend in varying directions and form a plurality of intersection points where one or more of the plurality of segments that form the lattice plane L 1 , the lattice plane L 2 , the lattice plane L 3 , and the lattice plane L 4 intersect.

12. The process of manufacturing the golf club component of claim 8 , wherein the build plane is orientated parallel to a line that extends perpendicularly through a front face of the golf club component.

13. The process of manufacturing the golf club component of claim 8 , wherein the lattice structure is formed by a plurality of gyroid structures.

14. The process of manufacturing the golf club component of claim 8 , wherein the build plane is rotationally offset from a ground plane, the ground plane defined as a horizontal plane parallel to the ground when the golf club component is at address.

15. The process of manufacturing the golf club component of claim 8 , wherein the golf club component includes an externally visible lattice structure.

16. A process of manufacturing a golf club component, comprising:
printing a material, layer by layer, along a build plane to form a printed part; and
sintering the printed part to form the golf club component, wherein, during the step of sintering, the printed part is resting on a sintering plane that is angled with respect to the build plane.

17. The process of manufacturing the golf club component of claim 16 , wherein the golf club component comprises a lattice structure,
wherein the lattice structure is formed by a plurality of segments,
wherein each of the plurality of segments defines a lattice plane,
wherein each of the lattice planes is angled with respect to the build plane and a ground plane, and
wherein the ground plane is defined as a horizontal plane parallel to the ground when the golf club component is at address.

18. The process of manufacturing the golf club component of claim 16 , wherein the build plane is offset from a ground plane by between about 5 degrees and about 160 degrees,
wherein the ground plane is defined as a horizontal plane parallel to the ground when the golf club component is at address, and
wherein the build plane is not a face angle of the golf club component.

19. The process of manufacturing the golf club component of claim 16 , wherein the sintering plane is defined by a sintering support surface, and
wherein the sintering plane is arranged to be non-parallel relative to the build plane.

20. The process of manufacturing the golf club component of claim 1 , wherein the lattice structure defines a variable structure that varies in one or more of unit cell type, unit cell geometry, unit cell size, segment length, segment thickness, segment volume, and unit cell density at one or more locations along the lattice structure.

Assignees

• Cobra Golf Inc

Inventors

• Roach Ryan L
• Day Cameron J
• Hobbs Bryce W

Classifications

• A63B53/04

  Heads · CPC title

• B22F10/40

  Structures for supporting workpieces or articles during manufacture and removed afterwards · CPC title

• B22F10/68

  Cleaning or washing · CPC title

• A63B2053/0491

  with added weights, e.g. changeable, replaceable · CPC title

• B22F10/38

  to achieve specific product aspects, e.g. surface smoothness, density, porosity or hollow structures · CPC title