Additive manufacturing methods for golf club components
Methods of creating golf club components with complex structures that would be difficult, impossible, or cost prohibitive to produce, such as lattice structures, beam structures, and complex surface-based structures, are described herein. In particular, a binder jet machine is used create complex structures to optimize weighting, sound, and performance of golf club heads. The method preferably includes the steps of designing a golf club head component in CAD using optimization software, printing the component from a powdered material, and then removing excess powder from the component via port holes that extend into an external surface of the component and communicate with interior voids within the component.
1. A method comprising the steps of:
inputting into an optimization software at least one parameter, wherein the at least one parameter is selected from the group consisting of individual player measurements, club head delivery data, impact location, and historical player data;
using the optimization software to prepare, modify, influence, or guide the design of a golf club component comprising at least one port hole extending into an external surface of the golf club component;
providing a powdered material;
binder jetting said golf club component from the powdered material based on the design; and
removing excess powdered material from the golf club component via the at least one port hole;
wherein the powdered material is a polymer selected from the group consisting of polyetherimide, polyetheretherketone, and polyetherketoneketone.
2. The method of claim 1 , wherein the step of removing excess powdered material from the golf club component via the at least one port hole comprises the steps of shaking the golf club component and polishing the golf club component.
3. The method of claim 1 , wherein the golf club component comprises a plurality of interconnected interior voids, and wherein the at least one port hole communicates with at least one of the plurality of interconnected interior voids.
4. The method of claim 1 , further comprising the step of covering up the at least one port hole.
5. The method of claim 4 , wherein the step of covering up the at least one port hole comprises the step of permanently affixing the golf club component to another golf club part.
6. The method of claim 1 , wherein the golf club component is a golf club head.
7. The method of claim 1 , wherein the step of utilizing optimization software comprises capturing the design in a CAD model, and wherein the step of binder jetting utilizes the CAD model.
8. A method comprising the steps of:
spreading layers of powdered material across a portion of a binder jet machine;
depositing liquid binder on regions of each layer of powder so that the binder bonds adjacent particles of powdered material together;
repeating the spreading and depositing steps until a green part is formed; and
sintering the green part to create a final part,
wherein the final part is a golf club component;
wherein the powdered material is a polymer selected from the group consisting of polyetherimide, polyetheretherketone, and polyetherketoneketone.
9. The method of claim 8 , further comprising the step of removing binder via a debinding process, wherein the removing step occurs prior to the sintering step.
10. The method of claim 9 , wherein the removing step and the sintering step occur in the same furnace.
11. The method of claim 8 , further comprising the step of preparing design parameters for the golf club component using optimization software, wherein the preparing step occurs before all other steps of the method.
12. The method of claim 11 , wherein the preparing step comprises inputting into the optimization software at least one parameter, wherein the parameter is selected from the group consisting of individual player measurements, club head delivery data, impact location, and historical player data.
13. The method of claim 8 , wherein the final part is 5-50% smaller than the green part.
14. The method of claim 13 , wherein the final part is 10-25% smaller than the green part.
15. The method of claim 8 , wherein the final part has a material density greater than 90%.