IP Library Granted Patent US 11,925,844
Granted Patent B2
US 11,925,844 · App. 17/485,049 · Granted Mar 12, 2024

Multi-component golf club head with tuning element

Inventor: Travis D. Milleman (Portland, OR)
Assignee: Karsten Manufacturing Corporation
A63B60/54A63B53/0412A63B53/0437A63B53/0466A63B60/002B32B5/02B32B7/12B32B27/12A63B2053/0491A63B53/08A63B2209/00B32B2262/101B32B2274/00B32B2307/10B32B2307/54
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Quick Facts
Patent No.
US 11,925,844
App. No.
17/485,049
Granted
Mar 12, 2024
Kind
B2
Abstract

Embodiments of a multi-material wood-type golf club head comprising a tuning element to damp dominant vibrations are described herein. The multi-material wood-type club head comprises a first, metallic component forming the striking face, and portions of the crown, the heel, the toe, and sole, and a second, non-metallic component forming a majority of the crown and portions of the heel, toe, and sole. The club head further comprises a tuning element secured to the interior surface of the crown, wherein the tuning element damps the amplitude vibration at a vibration hotspot in the club head by between 1-7 decibels.

Claims (94)

1. A golf club head comprising:

a crown, a sole opposite the crown, a heel end, a toe end opposite the heel end, a front end comprising a leading edge, a rear end, and a skirt extending between the crown and the sole;

a first component formed of a metal and comprising a striking face, a return portion extending rearward from the striking face, and a sole rear extension extending rearward from the return portion;

a second component formed of a non-metal and configured to be secured to the first component to enclose a hollow interior cavity, wherein the second component forms a majority of the crown and wraps around the skirt to form at least a portion of the heel end, the toe end, and the sole;

wherein the striking face comprises a striking face center defining an origin for a coordinate system including an x-axis extending horizontally through the striking face center in a direction extending from the heel end to the toe end when the club head is at an address position, a y-axis extending vertically through the striking face center in a direction extending from the crown to the sole, wherein the y-axis is perpendicular to the x-axis, a z-axis extending horizontally through the striking face center in a direction extending from the striking face to the rear end, wherein the z-axis is perpendicular to both the x-axis and the y-axis;

a front end reference plane tangent to the leading edge and perpendicular to a ground plane, the ground plane being defined as tangent to the sole at the address position;

a rear end reference plane tangent to the rear end and parallel to the front end reference plane;

a midplane perpendicular to the ground plane and located halfway between the front end reference plane and the rear end reference plane;

a YZ plane extending along the y-axis and the z-axis perpendicular to the ground plane;

wherein when viewing the club head from a top view, an intersection of the midplane and the YZ plane divides the club head into a quadrant system having a front-toe quadrant, a front-heel quadrant, a rear-toe quadrant, and a rear-heel quadrant;

a tuning element secured to an interior surface of the second component within the rear-heel quadrant;

wherein the tuning element comprises an adhesive layer, a stiffening layer opposite the adhesive layer, and a damping layer sandwiched between the adhesive layer and the stiffening layer;

wherein the stiffening layer comprises a glass cloth;

wherein the damping layer comprises a thermoplastic elastomer;

wherein the second component comprises a recess formed in an exterior surface of the crown, the recess being located within the rear-heel quadrant;

wherein the recess comprises a recess edge separating the recess from a non-recessed surface of the crown adjacent the recess;

wherein the recess forms a corresponding protrusion extending into the hollow interior cavity from an internal surface of the crown;

wherein the club head comprises a hotspot within the rear-heel quadrant and located proximate the recess, the hotspot being defined as a location of maximum amplitude of a natural frequency when the club head is devoid of the tuning element;

wherein said natural frequency is between 5000 Hz and 6500 Hz;

wherein the tuning element is positioned on the protrusion, the tuning element is configured to damp the maximum amplitude of the natural frequency; and

wherein when the club head comprising the tuning element vibrates at the natural frequency, the maximum amplitude is reduced by at least 2 decibels when compared to a similar club head devoid of the tuning element.

2. The golf club head of claim 1 , wherein the tuning element further comprises a tuning element center point located halfway between a heel-most portion of the tuning element and a toe-most portion of the tuning element, and halfway between a forwardmost portion of the tuning element and a rearward-most portion of tuning element; and

wherein the tuning element center point is located within the rear-heel quadrant.

3. The golf club head of claim 2 , wherein an offset distance measured parallel to the z-axis and between the front end reference plane and the tuning element center point is between 1.5 inches and 2.0 inches.

4. The golf club head of claim 1 , wherein the second component further comprises:

a second component crown portion forming at least a portion of the crown of the club head;

a second component heel portion wrapping around at least a portion of the heel end of the club head;

a second component toe portion wrapping around at least a portion of the toe end of the club head; and

wherein the tuning element is secured to an interior surface of the crown portion.

5. The golf club head of claim 1 , wherein the natural frequency of the golf club head is between 5500 Hz and 6000 Hz.

6. The golf club head of claim 1 , wherein the tuning element is adhesively coupled to the interior surface of the second component.

7. The golf club head of claim 1 , wherein the tuning element comprises a mass between 0.5 grams and 4 grams.

8. The golf club head of claim 1 , further comprising:

a club head volume less than 200 cc;

wherein the golf club head comprises a center of gravity defining an origin for a coordinate system including a CG x-axis parallel to the ground plane and in a direction from the heel end to the toe end, and a CG y-axis perpendicular to the ground plane and in a direction extending from the sole to the crown when the club head is at the address position;

wherein the golf club head comprises a Ixx moment of inertia about the CG x-axis greater than 1500 g*cm 2 ; and

wherein the golf club head comprises a Iyy moment of inertia about the CG y-axis greater than 2900 g*cm 2 .

9. A golf club head comprising:

a crown, a sole opposite the crown, a heel end, a toe end opposite the heel end, a front end comprising a leading edge, a rear end, and a skirt extending between the crown and the sole;

a first component formed of a metal and comprising a striking face, a return portion extending rearward from the striking face, and a sole rear extension extending rearward from the return portion;

a second component formed of a non-metal and configured to be secured to the first component to enclose a hollow interior cavity, wherein the second component forms a majority of the crown and wraps around the skirt to form at least a portion of the heel end, the toe end, and the sole;

wherein the striking face comprises a striking face center defining an origin for a coordinate system including an x-axis extending horizontally through the striking face center in a direction extending from the heel end to the toe end when the club head is at an address position, a y-axis extending vertically through the striking face center in a direction extending from the crown to the sole, wherein the y-axis is perpendicular to the x-axis, a z-axis extending horizontally through the striking face center in a direction extending from the striking face to the rear end, wherein the z-axis is perpendicular to both the x-axis and the y-axis;

a front end reference plane tangent to the leading edge and perpendicular to a ground plane, the ground plane being defined as tangent to the sole at the address position;

a rear end reference plane tangent to the rear end and parallel to the front end reference plane;

a midplane perpendicular to the ground plane and located halfway between the front end reference plane and the rear end reference plane;

a YZ plane extending along the y-axis and the z-axis perpendicular to the ground plane;

wherein when viewing the club head from a top view, an intersection of the midplane and the YZ plane divides the club head into a quadrant system having a front-toe quadrant, a front-heel quadrant, a rear-toe quadrant, and a rear-heel quadrant;

a tuning element secured to an interior surface of the second component within the rear-toe quadrant;

wherein the tuning element comprises an adhesive layer, a stiffening layer opposite the adhesive layer, and a damping layer sandwiched between the adhesive layer and the stiffening layer;

wherein the stiffening layer comprises a glass cloth;

wherein the damping layer comprises a thermoplastic elastomer;

wherein the second component comprises a recess formed in an exterior surface of the crown, the recess being located within the rear-heel quadrant;

wherein the recess comprises a recess edge separating the recess from a non-recessed surface of the crown adjacent the recess;

wherein the recess forms a corresponding protrusion extending into the hollow interior cavity from an internal surface of the crown;

wherein the club head comprises a hotspot within the rear-heel quadrant and located proximate the recess, the hotspot being defined as a location of maximum amplitude of a natural frequency when the club head is devoid of the tuning element;

wherein said natural frequency is between 5000 Hz and 6500 Hz;

wherein the tuning element is positioned on the protrusion, the tuning element is configured to damp the maximum amplitude of the natural frequency; and

wherein when the club head comprising the tuning element vibrates at the natural frequency, the maximum amplitude is reduced by at least 2 decibels when compared to a similar club head devoid of the tuning element.

10. The golf club head of claim 9 , wherein the natural frequency of the golf club head is between 6000 Hz and 6500 Hz.

11. The golf club head of claim 9 , wherein the tuning element further comprises a tuning element center point located halfway between a heel-most portion of the tuning element and a toe-most portion of the tuning element and halfway between a forwardmost portion of the tuning element and a rearward-most portion of tuning element; and

wherein the tuning element center point is located within the rear-toe quadrant.

12. The golf club head of claim 9 , further comprising:

a club head volume less than 200 cc;

wherein the golf club head comprises a center of gravity defining an origin for a coordinate system including a CG x-axis parallel to the ground plane and in a direction from the heel end to the toe end, and a CG y-axis perpendicular to the ground plane and in a direction extending from the sole to the crown when the club head is at the address position;

wherein the golf club head comprises a Ixx moment of inertia about the CG x-axis greater than 1500 g*cm 2 ; and

wherein the golf club head comprises a Iyy moment of inertia about the CG y-axis greater than 2900 g*cm 2 .

13. A golf club head comprising:

a crown, a sole opposite the crown, a heel end, a toe end opposite the heel end, a front end comprising a leading edge, a rear end, and a skirt extending between the crown and the sole;

a first component formed of a metal and comprising a striking face, a return portion extending rearward from the striking face, and a sole rear extension extending rearward from the return portion;

a second component formed of a non-metal and configured to be secured to the first component to enclose a hollow interior cavity, wherein the second component forms a majority of the crown and wraps around the skirt to form at least a portion of the heel end, the toe end, and the sole;

wherein the striking face comprises a striking face center defining an origin for a coordinate system including an x-axis extending horizontally through the striking face center in a direction extending from the heel end to the toe end when the club head is at an address position, a y-axis extending vertically through the striking face center in a direction extending from the crown to the sole, wherein the y-axis is perpendicular to the x-axis, a z-axis extending horizontally through the striking face center in a direction extending from the striking face to the rear end, wherein the z-axis is perpendicular to both the x-axis and the y-axis;

a front end reference plane tangent to the leading edge and perpendicular to a ground plane, the ground plane being defined as tangent to the sole at the address position;

a rear end reference plane tangent to the rear end and parallel to the front end reference plane;

a midplane perpendicular to the ground plane and located halfway between the front end reference plane and the rear end reference plane;

a YZ plane extending along the y-axis and the z-axis perpendicular to the ground plane;

wherein when viewing the club head from a top view, an intersection of the midplane and the YZ plane divides the club head into a quadrant system having a front-toe quadrant, a front-heel quadrant, a rear-toe quadrant, and a rear-heel quadrant;

a tuning element secured to an interior surface of the second component within the rear-heel quadrant;

wherein the tuning element comprises an adhesive layer, a stiffening layer opposite the adhesive layer, and a damping layer sandwiched between the adhesive layer and the stiffening layer;

wherein the stiffening layer comprises a glass cloth;

wherein the damping layer comprises a thermoplastic elastomer;

wherein the second component comprises a recess formed in an exterior surface of the crown, the recess being located within the rear-heel quadrant;

wherein the recess comprises a recess edge separating the recess from a non-recessed surface of the crown adjacent the recess;

wherein the recess forms a corresponding protrusion extending into the hollow interior cavity from an internal surface of the crown;

wherein the club head comprises a hotspot within the rear-heel quadrant and located proximate the recess, the hotspot being defined as a location of maximum amplitude of a natural frequency when the club head is devoid of the tuning element;

wherein said natural frequency is between 5000 Hz and 6500 Hz;

wherein the tuning element is positioned on the hotspot, the tuning element is configured to damp the maximum amplitude of the natural frequency; and

wherein when the club head comprising the tuning element vibrates at the natural frequency, the maximum amplitude is reduced by at least 2 decibels when compared to a similar club head devoid of the tuning element;

wherein the maximum amplitude of the natural frequency is less than or equal to 65 decibels.

14. The golf club head of claim 13 , wherein the natural frequency of the golf club head is between 5500 Hz and 6000 Hz.

15. The golf club head of claim 13 , wherein the tuning element further comprises a tuning element center point located halfway between a heel-most portion of the tuning element and a toe-most portion of the tuning element and halfway between a forwardmost portion of the tuning element and a rearward-most portion of tuning element; and

wherein the tuning element center point is located within the rear-heel quadrant.

16. The golf club head of claim 13 , wherein the tuning element comprises a density between 0.5 g/cm 3 and 1.5 g/cm 3 .

17. The golf club head of claim 13 , wherein the stiffening layer comprises a tensile strength greater than 60 MPa.

18. The golf club head of claim 14 , wherein the natural frequency of the golf club head is approximately 5860 Hz.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 13, 2021
From: MILLEMAN, TRAVIS D.
To: KARSTEN MANUFACTURING CORPORATION
Reel/Frame 057780/0630 →
Continuity (3)
Provisional Application 63127869 · Dec 18, 2020
Provisional Application 63082925 · Sep 24, 2020
Related Publication 20220088450A1 · Mar 24, 2022
Cited By (2)
US 12,186,637 US 12,465,820