Golf club head

Information

  • Patent Grant
  • 10434384
  • Patent Number
    10,434,384
  • Date Filed
    Monday, July 10, 2017
    7 years ago
  • Date Issued
    Tuesday, October 8, 2019
    5 years ago
Abstract
A golf club head having a flexible channel to improve the performance of the club head, and a channel tuning system to reduce undesirable club head characteristics introduced, or heightened, via the flexible channel. The channel tuning system includes a sole engaging channel tuning element in contact with the sole and the channel. The club head may include an aerodynamic configuration, as well as a body tuning system.
Description
INCORPORATIONS BY REFERENCE

Additional related applications concerning golf clubs include U.S. patent application Ser. Nos. 13/839,727, 13/956,046, 14/260,328, 14/330,205, 14/259,475, 14/488,354, 14/734,181, 14/472,415, 14/253,159, 14/449,252, 14/658,267, 14/456,927, 14/227,008, 14/074,481, and 14/575,745, all of which are incorporated by reference herein in their entireties.


FIELD

The present application concerns golf club heads, and more particularly, golf club heads having increased striking face flexibility and unique relationships between golf club head variables to ensure club head attributes work together to achieve desired performance.


BACKGROUND

Golf club manufacturers often must choose to improve one performance characteristic at the expense of another. In fact, the incorporation of new technologies that improve performance may necessitate changes to other aspects of a golf club head so that the features work together rather than reduce the associated benefits. Further, it is often difficult to identify the tradeoffs and changes that must be made to ensure aspects of the club head work together to achieve the desired performance. The disclosed embodiments tackle these issues.


SUMMARY

This application discloses, among other innovations, golf club heads that provide improved sound, durability, ball speed, forgiveness, and playability. The club head may include a flexible channel to improve the performance of the club head, and a channel tuning system to reduce undesirable club head characteristics introduced, or heightened, via the flexible channel. The channel tuning system includes a sole engaging channel tuning element in contact with the sole and the channel. The club head may also include an aerodynamic configuration, as well as a body tuning system. The foregoing and other features and advantages of the golf club head will become more apparent from the following detailed description, which proceeds with reference to the accompanying figures.





BRIEF DESCRIPTION OF THE DRAWINGS


FIG. 1 is a top plan view of one embodiment of a golf club head.



FIG. 2 is a side elevation view from a toe side of the golf club head of FIG. 1.



FIG. 3 is a front elevation view of the golf club head of FIG. 1.



FIG. 4 is a bottom plan view of one embodiment of a golf club head.



FIG. 5 is a bottom perspective view of one embodiment of a golf club head.



FIG. 6 is a top plan view of one embodiment of a golf club head.



FIG. 7 is a side elevation view of one embodiment of a golf club head.



FIG. 8 is a front elevation view of one embodiment of a golf club head.



FIG. 9 is a cross-sectional view of one embodiment of a golf club head.



FIG. 10 is a cross-sectional view of one embodiment of a golf club head.



FIG. 11 is a cross-sectional view of one embodiment of a golf club head.



FIG. 12 is a cross-sectional view of one embodiment of a golf club head.



FIG. 13 is a cross-sectional view of one embodiment of a golf club head.



FIG. 14 is a cross-sectional view of one embodiment of a golf club head.



FIG. 15 is a cross-sectional view of one embodiment of a golf club head.



FIG. 16 is a cross-sectional view of one embodiment of a golf club head.



FIG. 17 is a cross-sectional view of one embodiment of a golf club head.



FIG. 18 is a cross-sectional view of one embodiment of a golf club head.



FIG. 19 is a cross-sectional view of one embodiment of a golf club head.



FIG. 20 is a cross-sectional view of one embodiment of a golf club head.



FIG. 21 is a cross-sectional view of one embodiment of a golf club head.



FIG. 22 is a cross-sectional view of one embodiment of a golf club head.



FIG. 23 is a cross-sectional view of one embodiment of a golf club head.



FIG. 24 is a rear elevation view of one embodiment of a golf club head.



FIG. 25 is a perspective view of one embodiment of a golf club head.



FIG. 26 is a perspective view of one embodiment of a golf club head.



FIG. 27 is a bottom plan view of one embodiment of a golf club head.



FIG. 28 is a bottom plan view of one embodiment of a golf club head.



FIG. 29 is a cross-sectional view of one embodiment of a golf club head.



FIG. 30 is a cross-sectional view of one embodiment of a golf club head.



FIG. 31 is a cross-sectional view of one embodiment of a golf club head.



FIG. 32 is a cross-sectional view of one embodiment of a golf club head.



FIG. 33 is a cross-sectional view of one embodiment of a golf club head.



FIG. 34 is an enlarged cross-sectional view of a golf club head having a removable shaft, in accordance with another embodiment.



FIG. 35 is a front elevation view of a shaft sleeve of the assembly shown in FIG. 28.



FIG. 36 is a cross-sectional view of a shaft sleeve of the assembly shown in FIG. 28.



FIG. 37 is an exploded view of a golf club head, according to another embodiment.



FIG. 38A is a bottom view of the golf club head of FIG. 31.



FIG. 38B is an enlarged bottom view of a portion of the golf club head of FIG. 31.



FIG. 38C is a cross-sectional view of the golf club head of FIG. 32A, taken along line C-C.



FIG. 38D is a cross-sectional view of the golf club head of FIG. 32A, taken along line D-D.



FIG. 38E is a cross-sectional view of the golf club head of FIG. 32A, taken along line E-E.



FIG. 39 is a cross-sectional view of one embodiment of a golf club head.





DETAILED DESCRIPTION

The following describes embodiments of golf club heads for metalwood type golf clubs, including drivers, fairway woods, rescue clubs, hybrid clubs, and the like. Several of the golf club heads incorporate features that provide the golf club heads and/or golf clubs with increased moments of inertia and low centers of gravity, centers of gravity located in preferable locations, improved club head and face geometries, increased sole and lower face flexibility, desirable club head tuning, higher coefficients or restitution (“COR”) and characteristic times (“CT”), and/or decreased backspin rates relative to other golf club heads that have come before.


The following makes reference to the accompanying drawings which form a part hereof, wherein like numerals designate like parts throughout. The drawings illustrate specific embodiments, but other embodiments may be formed and structural changes may be made without departing from the intended scope of this disclosure. Directions and references (e.g., up, down, top, bottom, left, right, rearward, forward, heelward, toeward, etc.) may be used to facilitate discussion of the drawings but are not intended to be limiting. For example, certain terms may be used such as “up,” “down,”, “upper,” “lower,” “horizontal,” “vertical,” “left,” “right,” and the like. These terms are used, where applicable, to provide some clarity of description when dealing with relative relationships, particularly with respect to the illustrated embodiments. Such terms are not, however, intended to imply absolute relationships, positions, and/or orientations. For example, with respect to an object, an “upper” surface can become a “lower” surface simply by turning the object over. Nevertheless, it is still the same object.


Accordingly, the following detailed description shall not to be construed in a limiting sense and the scope of property rights sought shall be defined by the appended claims and their equivalents.


Normal Address Position


Club heads and many of their physical characteristics disclosed herein will be described using “normal address position” as the club head reference position, unless otherwise indicated.



FIGS. 1-3 illustrate one embodiment of a golf club head at normal address position. FIG. 1 illustrates a top plan view of the club head 2, FIG. 2 illustrates a side elevation view from the toe side of the club head 2, and FIG. 3 illustrates a front elevation view. By way of preliminary description, the club head 2 includes a hosel 20 and a ball striking club face 18. At normal address position, the club head 2 rests on the ground plane 17, a plane parallel to the ground.


As used herein, “normal address position” means the club head position wherein a vector normal to the club face 18 substantially lies in a first vertical plane (i.e., a vertical plane is perpendicular to the ground plane 17), the centerline axis 21 of the club shaft substantially lies in a second vertical plane, and the first vertical plane and the second vertical plane substantially perpendicularly intersect.


Club Head


A golf club head, such as the golf club head 2, includes a hollow body 10 defining a crown portion 12, a sole portion 14 and a skirt portion 16. A striking face, or face portion, 18 attaches to the body 10. The body 10 can include a hosel 20, which defines a hosel bore 24 adapted to receive a golf club shaft. The body 10 further includes a heel portion 26, a toe portion 28, a front portion 30, and a rear portion 32.


The club head 2 also has a volume, typically measured in cubic-centimeters (cm3), equal to the volumetric displacement of the club head 2, assuming any apertures are sealed by a substantially planar surface. (See United States Golf Association “Procedure for Measuring the Club Head Size of Wood Clubs,” Revision 1.0, Nov. 21, 2003). In some implementations, the golf club head 2 has a volume between approximately 120 cm3 and approximately 460 cm3, and a total mass between approximately 185 g and approximately 245 g. Additional specific implementations having additional specific values for volume and mass are described elsewhere herein.


As used herein, “crown” means an upper portion of the club head above a peripheral outline 34 of the club head as viewed from a top-down direction and rearward of the topmost portion of the striking face 18, as seen in FIG. 1. FIGS. 11-22 and 39 illustrate embodiments of a cross-sectional view of the golf club head of FIG. 1 taken along line 11-11 of FIG. 2 showing internal features of the golf club head. FIGS. 9-10 and 29-31 illustrate embodiments of a cross-sectional view of the golf club head of FIG. 1 taken along line 9-9 of FIG. 1 showing internal features of the golf club head. FIG. 23 illustrates an embodiment of a cross-sectional view of the golf club head of FIG. 1 taken along line 23-23 of FIG. 2 showing internal features of the golf club head. As used herein, “sole” means a lower portion of the club head 2 extending upwards from a lowest point of the club head when the club head is at normal address position. In other implementations, the sole 14 extends upwardly from the lowest point of the golf club body 10 a shorter distance than the sole 14 of golf club head 2. Further, the sole 14 can define a substantially flat portion extending substantially horizontally relative to the ground 17 when in normal address position. In some implementations, the bottommost portion of the sole 14 extends substantially parallel to the ground 17 between approximately 5% and approximately 70% of the depth Dch of the golf club body 10. In some implementations, an adjustable mechanism is provided on the sole 14 to “decouple” the relationship between face angle and hosel/shaft loft, i.e., to allow for separate adjustment of square loft and face angle of a golf club. For example, some embodiments of the golf club head 2 include an adjustable sole portion that can be adjusted relative to the club head body 2 to raise and lower the rear end of the club head relative to the ground. Further detail concerning the adjustable sole portion is provided in U.S. patent application Ser. No. 14/734,181, which is incorporated herein by reference. As used herein, “skirt” means a side portion of the club head 2 between the crown 12 and the sole 14 that extends across a periphery 34 of the club head, excluding the face 18, from the toe portion 28, around the rear portion 32, to the heel portion 26.


As used herein, “striking surface” means a front or external surface of the striking face 18 configured to impact a golf ball (not shown). In several embodiments, the striking face or face portion 18 can be a striking plate attached to the body 10 using conventional attachment techniques, such as welding, as will be described in more detail below. In some embodiments, the striking surface 22 can have a bulge and roll curvature. As illustrated by FIG. 9, the average face thickness for the illustrated embodiment is in the range of from about 1.0 mm to about 4.5 mm, such as between about 2.0 mm and about 2.2 mm.


The body 10 can be made from a metal alloy (e.g., an alloy of titanium, an alloy of steel, an alloy of aluminum, and/or an alloy of magnesium), a composite material, such as a graphitic composite, a ceramic material, or any combination thereof (e.g., a metallic sole and skirt with a composite, magnesium, or aluminum crown). The crown 12, sole 14, and skirt 16 can be integrally formed using techniques such as molding, cold forming, casting, and/or forging and the striking face 18 can be attached to the crown, sole and skirt by known means. For example, in some embodiments, the body 10 can be formed from a cup-face structure, with a wall or walls extending rearward from the edges of the inner striking face surface and the remainder of the body formed as a separate piece that is joined to the walls of the cup-face by welding, cementing, adhesively bonding, or other technique known to those skilled in the art.


Referring to FIGS. 7 and 8, the ideal impact location 23 of the golf club head 2 is disposed at the geometric center of the face 18. The ideal impact location 23 is typically defined as the intersection of the midpoints of a height Hss and a width Wss of the face 18. Both Hss and Wss are determined using the striking face curve Sss. The striking face curve is bounded on its periphery by all points where the face transitions from a substantially uniform bulge radius (face heel-to-toe radius of curvature) and a substantially uniform roll radius (face crown-to-sole radius of curvature) to the body. In the illustrated example, Hss is the distance from the periphery proximate to the sole portion of Sss to the periphery proximate to the crown portion of Sss measured in a vertical plane (perpendicular to ground) that extends through the geometric center of the face 18 (e.g., this plane is substantially normal to the x-axis). Further, as seen in FIGS. 8 and 10, the face 18 has a top edge elevation, Hte, measured from the ground plane. Similarly, Wss is the distance from the periphery proximate to the heel portion of Sss to the periphery proximate to the toe portion of Sss measured in a horizontal plane (e.g., substantially parallel to ground) that extends through the geometric center of the face (e.g., this plane is substantially normal to the z-axis). See USGA “Procedure for Measuring the Flexibility of a Golf Clubhead,” Revision 2.0 for the methodology to measure the geometric center of the striking face. In some implementations, the golf club head face 18 has a height (Hss) between approximately 20 mm and approximately 45 mm, and a width (Wss) between approximately 60 mm and approximately 120 mm. In one specific implementation, the face 18 has a height Hss of approximately 26 mm, width Wss of approximately 71 mm, and total striking surface area of approximately 2050 mm2. Additional specific implementations having additional specific values for face height Hss, face width Wss, and total striking surface area are described elsewhere herein.


In some embodiments, the striking face 18 is made of a composite material such as described in U.S. patent application Ser. No. 14/154,513, which is incorporated herein by reference. In other embodiments, the striking face 18 is made from a metal alloy (e.g., an alloy of titanium, steel, aluminum, and/or magnesium), ceramic material, or a combination of composite, metal alloy, and/or ceramic materials. Examples of titanium alloys include 3-2.5, 6-4, SP700, 15-3-3-3, 10-2-3, or other alpha/near alpha, alpha-beta, and beta/near beta titanium alloys. Examples of steel alloys include 304, 410, 450, or 455 stainless steel.


In still other embodiments, the striking face 18 is formed of a maraging steel, a maraging stainless steel, or a precipitation-hardened (PH) steel or stainless steel. In general, maraging steels have high strength, toughness, and malleability. Being low in carbon, they derive their strength from precipitation of inter-metallic substances other than carbon. The principle alloying element is nickel (15% to nearly 30%). Other alloying elements producing inter-metallic precipitates in these steels include cobalt, molybdenum, and titanium. In some embodiments, a non-stainless maraging steel contains about 17-19% nickel, 8-12% cobalt, 3-5% molybdenum, and 0.2-1.6% titanium. Maraging stainless steels have less nickel than maraging steels, but include significant amounts of chromium to prevent rust.


An example of a non-stainless maraging steel suitable for use in forming a striking face 18 includes NiMark® Alloy 300, having a composition that includes the following components: nickel (18.00 to 19.00%), cobalt (8.00 to 9.50%), molybdenum (4.70 to 5.10%), titanium (0.50 to 0.80%), manganese (maximum of about 0.10%), silicon (maximum of about 0.10%), aluminum (about 0.05 to 0.15%), calcium (maximum of about 0.05%), zirconium (maximum of about 0.03%), carbon (maximum of about 0.03%), phosphorus (maximum of about 0.010%), sulfur (maximum of about 0.010%), boron (maximum of about 0.003%), and iron (balance). Another example of a non-stainless maraging steel suitable for use in forming a striking face 18 includes NiMark® Alloy 250, having a composition that includes the following components: nickel (18.00 to 19.00%), cobalt (7.00 to 8.00%), molybdenum (4.70 to 5.00%), titanium (0.30 to 0.50%), manganese (maximum of about 0.10%), silicon (maximum of about 0.10%), aluminum (about 0.05 to 0.15%), calcium (maximum of about 0.05%), zirconium (maximum of about 0.03%), carbon (maximum of about 0.03%), phosphorus (maximum of about 0.010%), sulfur (maximum of about 0.010%), boron (maximum of about 0.003%), and iron (balance). Other maraging steels having comparable compositions and material properties may also be suitable for use.


In several specific embodiments, a golf club head includes a body 10 that is formed from a metal (e.g., steel), a metal alloy (e.g., an alloy of titanium, an alloy of aluminum, and/or an alloy of magnesium), a composite material, such as a graphitic composite, a ceramic material, or any combination thereof, as described above. In some of these embodiments, a striking face 18 is attached to the body 10, and is formed from a non-stainless steel, such as one of the maraging steels described above. In one specific example, a golf club head includes a body 10 that is formed from a stainless steel (e.g., Custom 450® Stainless) and a striking face 18 that is formed from a non-stainless maraging steel (e.g., NiMark® Alloy 300).


In several alternative embodiments, a golf club head includes a body 10 that is formed from a non-stainless steel, such as one of the maraging steels described above. In some of these embodiments, a striking face 18 is attached to the body 10, and is also formed from a non-stainless steel, such as one of the maraging steels described above. In one specific example, a golf club head includes a body 10 and a striking face 18 that are each formed from a non-stainless maraging steel (e.g., NiMark® Alloy 300 or NiMark® Alloy 250).


When at normal address position as seen in FIG. 3, the club head 2 is disposed at a lie-angle 19 relative to the club shaft axis 21 and the club face has a loft angle 15. The lie-angle 19 refers to the angle between the centerline axis 21 of the club shaft and the ground plane 17 at normal address position. Lie angle for a fairway wood typically ranges from about 54 degrees to about 62 degrees, most typically about 56 degrees to about 60 degrees. Referring to FIG. 2, loft-angle 15 refers to the angle between a tangent line 27 to the club face 18 and a vector normal to the ground plane 29 at normal address position. Loft angle for a driver is typically greater than about 7 degrees, and the loft angle for a fairway wood is typically greater than about 13 degrees. For example, loft for a driver typically ranges from about 7 degrees to about 13 degrees, and the loft for a fairway wood typically ranges from about 13 degrees to about 28 degrees, and more preferably from about 13 degrees to about 22 degrees.


A club shaft is received within the hosel bore 24 and is aligned with the centerline axis 21. In some embodiments, a connection assembly is provided that allows the shaft to be easily disconnected from the club head 2. In still other embodiments, the connection assembly provides the ability for the user to selectively adjust the loft-angle 15 and/or lie-angle 19 of the golf club. For example, in some embodiments, a sleeve is mounted on a lower end portion of the shaft and is configured to be inserted into the hosel bore 24. The sleeve has an upper portion defining an upper opening that receives the lower end portion of the shaft, and a lower portion having a plurality of longitudinally extending, angularly spaced external splines located below the shaft and adapted to mate with complimentary splines in the hosel opening 24. The lower portion of the sleeve defines a longitudinally extending, internally threaded opening adapted to receive a screw for securing the shaft assembly to the club head 2 when the sleeve is inserted into the hosel opening 24. Further detail concerning the shaft connection assembly is provided in U.S. patent application Ser. No. 14/074,481, which is incorporated herein by reference, and some embodiments are described later herein.


Golf Club Head Coordinates


Referring to FIGS. 6-8, a club head origin coordinate system can be defined such that the location of various features of the club head (including, e.g., a club head center-of-gravity (CG) 50) can be determined. A club head origin 60 is illustrated on the club head 2 positioned at the ideal impact location 23, or geometric center, of the face 18.


The head origin coordinate system defined with respect to the head origin 60 includes three axes: a z-axis 65 extending through the head origin 60 in a generally vertical direction relative to the ground 17 when the club head 2 is at normal address position; an x-axis 70 extending through the head origin 60 in a toe-to-heel direction generally parallel to the face 18, e.g., generally tangential to the face 18 at the ideal impact location 23, and generally perpendicular to the z-axis 65; and a y-axis 75 extending through the head origin 60 in a front-to-back direction and generally perpendicular to the x-axis 70 and to the z-axis 65. The x-axis 70 and the y-axis 75 both extend in generally horizontal directions relative to the ground 17 when the club head 2 is at normal address position. The x-axis 70 extends in a positive direction from the origin 60 to the heel 26 of the club head 2. The y-axis 75 extends in a positive direction from the origin 60 towards the rear portion 32 of the club head 2. The z-axis 65 extends in a positive direction from the origin 60 towards the crown 12. An alternative, above ground, club head coordinate system places the origin 60 at the intersection of the z-axis 65 and the ground plane 17, providing positive z-axis coordinates for every club head feature. As used herein, “Zup” means the CG z-axis location determined according to the above ground coordinate system. Zup generally refers to the height of the CG 50 above the ground plane 17.


In several embodiments, the golf club head can have a CG with an x-axis coordinate between approximately −2.0 mm and approximately 6.0 mm, such as between approximately −2.0 mm and approximately 3.0 mm, a y-axis coordinate between approximately 15 mm and approximately 40 mm, such as between approximately 20 mm and approximately 30 mm, or between approximately 23 mm and approximately 28 mm, and a z-axis coordinate between approximately 0.0 mm and approximately −12.0 mm, such as between approximately −1.0 mm and approximately −9.0 mm, or between approximately −1.0 mm and approximately −5.0 mm. In certain embodiments, a z-axis coordinate between about 0.0 mm and about −12.0 mm provides a Zup value of between approximately 10 mm and approximately 30 mm. Additional specific implementations having additional specific values for the CG x-axis coordinate, CG y-axis coordinate, CG z-axis coordinate, and Zup are described elsewhere herein.


Another alternative coordinate system uses the club head center-of-gravity (CG) 50 as the origin when the club head 2 is at normal address position. Each center-of-gravity axis passes through the CG 50. For example, the CG x-axis 90 passes through the center-of-gravity 50 substantially parallel to the ground plane 17 and generally parallel to the origin x-axis 70 when the club head is at normal address position. Similarly, the CG y-axis 95 passes through the center-of-gravity 50 substantially parallel to the ground plane 17 and generally parallel to the origin y-axis 75, and the CG z-axis 85 passes through the center-of-gravity 50 substantially perpendicular to the ground plane 17 and generally parallel to the origin z-axis 65 when the club head is at normal address position.


Mass Moments of Inertia


Referring to FIGS. 6-7, golf club head moments of inertia are typically defined about the three CG axes that extend through the golf club head center-of-gravity 50.


For example, a moment of inertia about the golf club head CG z-axis 85 can be calculated by the following equation

Izz=∫(x2+y2)dm

where x is the distance from a golf club head CG yz-plane to an infinitesimal mass, dm, and y is the distance from the golf club head CG xz-plane to the infinitesimal mass, dm. The golf club head CG yz-plane is a plane defined by the golf club head CG y-axis 95 and the golf club head CG z-axis 85.


The moment of inertia about the CG z-axis (Izz) is an indication of the ability of a golf club head to resist twisting about the CG z-axis. Greater moments of inertia about the CG z-axis (Izz) provide the golf club head 2 with greater forgiveness on toe-ward or heel-ward off-center impacts with a golf ball. In other words, a golf ball hit by a golf club head 2 on a location of the striking face 18 between the toe 28 and the ideal impact location 23 tends to cause the golf club head to twist rearwardly and the golf ball to draw (e.g., to have a curving trajectory from right-to-left for a right-handed swing). Similarly, a golf ball hit by a golf club head 2 on a location of the striking face 18 between the heel 26 and the ideal impact location 23 causes the golf club head 2 to twist forwardly and the golf ball to slice (e.g., to have a curving trajectory from left-to-right for a right-handed swing). Increasing the moment of inertia about the CG z-axis (Izz) reduces forward or rearward twisting of the golf club head, reducing the negative effects of heel or toe mis-hits.


A moment of inertia about the golf club head CG x-axis 90 can be calculated by the following equation

Ixx=∫(y2+z2)dm

where y is the distance from a golf club head CG xz-plane to an infinitesimal mass, dm, and z is the distance from a golf club head CG xy-plane to the infinitesimal mass, dm. The golf club head CG xz-plane is a plane defined by the golf club head CG x-axis 90 and the golf club head CG z-axis 85. The CG xy-plane is a plane defined by the golf club head CG x-axis 90 and the golf club head CG y-axis 95.


As the moment of inertia about the CG z-axis (Izz) is an indication of the ability of a golf club head to resist twisting about the CG z-axis, the moment of inertia about the CG x-axis (Ixx) is an indication of the ability of the golf club head to resist twisting about the CG x-axis. Greater moments of inertia about the CG x-axis (Ixx) improve the forgiveness of the golf club head 2 on high and low off-center impacts with a golf ball. In other words, a golf ball hit by a golf club head 2 on a location of the striking surface 18 above the ideal impact location 23 causes the golf club head 2 to twist upwardly and the golf ball to have a higher trajectory than desired. Similarly, a golf ball hit by a golf club head 2 on a location of the striking face 18 below the ideal impact location 23 causes the golf club head 2 to twist downwardly and the golf ball to have a lower trajectory than desired. Increasing the moment of inertia about the CG x-axis (Ixx) reduces upward and downward twisting of the golf club head 2, reducing the negative effects of high and low mis-hits.


Discretionary Mass


Desired club head mass moments of inertia, club head center-of-gravity locations, and other mass properties of a golf club head can be attained by distributing club head mass to particular locations. Discretionary mass generally refers to the mass of material that can be removed from various structures providing mass that can be distributed elsewhere for tuning one or more mass moments of inertia and/or locating the club head center-of-gravity.


Club head walls provide one source of discretionary mass. In other words, a reduction in wall thickness reduces the wall mass and provides mass that can be distributed elsewhere. For example, in some implementations, one or more walls of the club head can have a thickness (constant or average) less than approximately 0.7 mm, such as between about 0.55 mm and about 0.65 mm. In some embodiments, the crown 12 can have a thickness (constant or average) of approximately 0.60 mm or approximately 0.65 mm throughout more than about 70% of the crown, with the remaining portion of the crown 12 having a thickness (constant or average) of approximately 0.76 mm or approximately 0.80 mm. See for example FIG. 9, which illustrates a back crown thickness 905 of about 0.60 mm and a front crown thickness 901 of about 0.76 mm. In addition, the skirt 16 can have a similar thickness and the wall of the sole 14 can have a thickness of between approximately 0.6 mm and approximately 2.0 mm. In contrast, many conventional club heads have crown wall thicknesses in excess of about 0.75 mm, and some in excess of about 0.85 mm.


Thin walls, particularly a thin crown 12, provide significant discretionary mass compared to conventional club heads. For example, a club head 2 made from an alloy of steel can achieve about 4 grams of discretionary mass for each 0.1 mm reduction in average crown thickness. Similarly, a club head 2 made from an alloy of titanium can achieve about 2.5 grams of discretionary mass for each 0.1 mm reduction in average crown thickness. Discretionary mass achieved using a thin crown 12, e.g., less than about 0.65 mm, can be used to tune one or more mass moments of inertia and/or center-of-gravity location.


To achieve a thin wall on the club head body 10, such as a thin crown 12, a club head body 10 can be formed from an alloy of steel or an alloy of titanium. Thin wall investment casting, such as gravity casting in air for alloys of steel and centrifugal casting in a vacuum chamber for alloys of titanium, provides one method of manufacturing a club head body with one or more thin walls.


Weights and Weight Ports


Various approaches can be used for positioning discretionary mass within a golf club head 2. For example, many club heads 2 have integral sole weight pads cast into the head 2 at predetermined locations that can be used to lower, to move forward, to move rearward, or otherwise to adjust the location of the club head's center-of-gravity. Also, epoxy can be added to the interior of the club head 2 through the club head's hosel opening to obtain a desired weight distribution. Alternatively, weights formed of high-density materials can be attached to the sole, skirt, and other parts of a club head. With such methods of distributing the discretionary mass, installation is critical because the club head endures significant loads during impact with a golf ball that can dislodge the weight. Accordingly, such weights are usually permanently attached to the club head and are limited to a fixed total mass, which of course, permanently fixes the club head's center-of-gravity and moments of inertia.


Alternatively, as seen in FIGS. 27-28 the golf club head 2 can define one or more weight ports 40 formed in the body 10 that are configured to receive one or more weights. For example, one or more weight ports 40 can be disposed in the crown 12, skirt 16 and/or sole 14. The weight port 40 can have any of a number of various configurations to receive and retain any of a number of weights or weight assemblies, such as described in U.S. Pat. Nos. 7,407,447 and 7,419,441, which are incorporated herein by reference. For example, the weight port 40 may provide the capability of a weight to be removably engageable with the sole 14. In some embodiments, a single weight port 40 and engageable weight is provided, while in others, a plurality of weight ports 40 (e.g., two, three, four, or more) and engageable weights are provided. In one embodiment the weight port 40 defines internal threads that correspond to external threads formed on the weight. Weights and/or weight assemblies configured for weight ports in the sole can vary in mass from about 0.5 grams to about 20 grams.


Inclusion of one or more weights in the weight port(s) 40 provides a customizable club head mass distribution, and corresponding mass moments of inertia and center-of-gravity 50 locations. Adjusting the location of the weight port(s) 40 and the mass of the weights and/or weight assemblies provides various possible locations of center-of-gravity 50 and various possible mass moments of inertia using the same club head 2.


As discussed in more detail below, in some embodiments, a playable fairway wood club head can have a low, rearward center-of-gravity. Placing one or more weight ports 40 and weights rearward in the sole helps desirably locate the center-of-gravity. In the foregoing embodiments, a center of gravity of the weight is preferably located rearward of a midline of the golf club head along the y-axis 75, such as, for example, within about 40 mm of the rear portion 32 of the club head, or within about 30 mm of the rear portion 32 of the club head, or within about 20 mm of the rear portion of the club head. In other embodiments a playable fairway wood club head can have a center-of-gravity that is located to provide a preferable center-of-gravity projection on the striking surface 22 of the club head. In those embodiments, one or more weight ports 40 and weights are placed in the sole portion 14 forward of a midline of the golf club head along the y-axis 75. For example, in some embodiments, a center of gravity of one or more weights placed in the sole portion 14 of the club head is located within about 30 mm of the nearest portion of the forward edge of the sole, such as within about 20 mm of the nearest portion of the forward edge of the sole, or within about 15 mm of the nearest portion of the forward edge of the sole, or within about 10 mm of the nearest portion of the forward edge of the sole. Although other methods (e.g., using internal weights attached using epoxy or hot-melt glue) of adjusting the center-of-gravity can be used, use of a weight port and/or integrally molding a discretionary weight into the body 10 of the club head reduces undesirable effects on the audible tone emitted during impact with a golf ball.


Club Head Height and Length


In addition to redistributing mass within a particular club head envelope as discussed immediately above, the club head center-of-gravity location 50 can also be tuned by modifying the club head external envelope. Referring now to FIG. 8, the club head 2 has a maximum club head height Hch defined as the maximum above ground z-axis coordinate of the outer surface of the crown 12. Similarly, a maximum club head width Wch can be defined as the distance between the maximum extents of the heel and toe portions 26, 28 of the body measured along an axis parallel to the x-axis when the club head 2 is at normal address position and a maximum club head depth Dch, or length, defined as the distance between the forwardmost and rearwardmost points on the surface of the body 10 measured along an axis parallel to the y-axis when the club head 2 is at normal address position. Generally, the height and width of club head 2 should be measured according to the USGA “Procedure for Measuring the Clubhead Size of Wood Clubs” Revision 1.0. The heel portion 28 of the club head 2 is broadly defined as the portion of the club head 2 from a vertical plane passing through the origin y-axis 75 toward the hosel 20, while the toe portion 26 is that portion of the club head 2 on the opposite side of the vertical plane passing through the origin y-axis 75.


In some fairway wood embodiments, the golf club head 2 has a height Hch less than approximately 55 mm. In some embodiments, the club head 2 has a height Hch less than about 50 mm. For example, some implementations of the golf club head 2 have a height Hch less than about 45 mm. In other implementations, the golf club head 2 has a height Hch less than about 42 mm. Still other implementations of the golf club head 2 have a height Hch less than about 40 mm. Further, some examples of the golf club head 2 have a depth Dch greater than approximately 75 mm. In some embodiments, the club head 2 has a depth Dch greater than about 85 mm. For example, some implementations of the golf club head 2 have a depth Dch greater than about 95 mm. In other implementations, as discussed in more detail below, the golf club head 2 can have a depth Dch greater than about 100 mm.


Forgiveness of Club Heads


Golf club head “forgiveness” generally describes the ability of a club head to deliver a desirable golf ball trajectory despite a mis-hit (e.g., a ball struck at a location on the striking face 18 other than the ideal impact location 23). As described above, large mass moments of inertia contribute to the overall forgiveness of a golf club head. In addition, a low center-of-gravity improves forgiveness for golf club heads used to strike a ball from the turf by giving a higher launch angle and a lower spin trajectory. Providing a rearward center-of-gravity reduces the likelihood of a slice or fade for many golfers. Accordingly, forgiveness of club heads, such as the club head 2, can be improved using the techniques described above to achieve high moments of inertia and low center-of-gravity compared to conventional fairway wood golf club heads.


For example, a club head 2 with a crown thickness less than about 0.65 mm throughout at least about 70% of the crown can provide significant discretionary mass. A 0.60 mm thick crown can provide as much as about 8 grams of discretionary mass compared to a 0.80 mm thick crown. The large discretionary mass can be distributed to improve the mass moments of inertia and desirably locate the club head center-of-gravity. Generally, discretionary mass should be located sole-ward rather than crown-ward to maintain a low center-of-gravity, forward rather than rearward to maintain a forwardly positioned center of gravity, and rearward rather than forward to maintain a rearwardly positioned center-of-gravity. In addition, discretionary mass should be located far from the center-of-gravity and near the perimeter of the club head to maintain high mass moments of inertia.


For example, in some of the embodiments described herein, a comparatively forgiving golf club head 2 for a fairway wood can combine an overall club head height (Hch) of less than about 46 mm and an above ground center-of-gravity location, Zup, less than about 19 mm. Some examples of the club head 2 provide an above ground center-of-gravity location, Zup, less than about 16 mm. In additional fairway wood embodiments, a thin crown 12 as described above provides sufficient discretionary mass to allow the club head 2 to have a volume less than about 240 cm3and/or a front to back depth (DCH) greater than about 85 mm. Without a thin crown 12, a similarly sized golf club head would either be overweight or would have an undesirably located center-of-gravity because less discretionary mass would be available to tune the CG location. In addition, in some embodiments of a comparatively forgiving golf club head 2, discretionary mass can be distributed to provide a mass moment of inertia about the CG z-axis 85, Izz, greater than about 300 kg-mm2. In some instances, the mass moment of inertia about the CG z-axis 85, Izz, can be greater than about 320 kg-mm2, such as greater than about 340 kg-mm2 or greater than about 360 kg-mm2. Distribution of the discretionary mass can also provide a mass moment of inertia about the CG x-axis 90, Ixx, greater than about 150 kg-mm2. In some instances, the mass moment of inertia about the CG x-axis 85, Ixx, can be greater than about 170 kg-mm2, such as greater than about 190 kg-mm2.


Alternatively, some examples of a forgiving club head 2 combine an above ground center-of-gravity location, Zup, less than about 19 mm and a high moment of inertia about the CG z-axis 85, Izz. In such club heads, the moment of inertia about the CG z-axis 85, Izz, specified in units of kg-mm2, together with the above ground center-of-gravity location, Zup, specified in units of millimeters (mm), can satisfy the relationship

Izz≥13·Zup+105.


Alternatively, some forgiving fairway wood club heads have a moment of inertia about the CG z-axis 85, Izz, and a moment of inertia about the CG x-axis 90, Ixx, specified in units of kg-mm2, together with an above ground center-of-gravity location, Zup, specified in units of millimeters, that satisfy the relationship

Ixx+Izz≥20·Zup+165.


As another alternative, a forgiving fairway wood club head can have a moment of inertia about the CG x-axis, Ixx, specified in units of kg-mm2, and, an above ground center-of-gravity location, Zup, specified in units of millimeters, that together satisfy the relationship

Ixx≥7·Zup+60.

Coefficient of Restitution, Characteristic Time, and Center of Gravity Projection


Another parameter that contributes to the forgiveness and successful playability and desirable performance of a golf club 2 is the coefficient of restitution (COR) and Characteristic Time (CT) of the golf club head 2. Upon impact with a golf ball, the club head's face 18 deflects and rebounds, thereby imparting energy to the struck golf ball. The club head's coefficient of restitution (COR) is the ratio of the velocity of separation to the velocity of approach. A thin face plate generally will deflect more than a thick face plate. Thus, a properly constructed club with a thin, flexible face plate can impart a higher initial velocity to a golf ball, which is generally desirable, than a club with a thick, rigid face plate. In order to maximize the moment of inertia (MOI) about the center of gravity (CG) and achieve a high COR, it typically is desirable to incorporate thin walls and a thin face plate into the design of the club head. Thin walls afford the designers additional leeway in distributing club head mass to achieve desired mass distribution, and a thinner face plate may provide for a relatively higher COR.


Thus, selective use of thin walls is important to a club's performance. However, overly thin walls can adversely affect the club head's durability. Problems also arise from stresses distributed across the club head upon impact with the golf ball, particularly at junctions of club head components, such as the junction of the face plate with other club head components (e.g., the sole, skirt, and crown). One prior solution has been to provide a reinforced periphery about the face plate, such as by welding, in order to withstand the repeated impacts. Another approach to combat stresses at impact is to use one or more ribs extending substantially from the crown to the sole vertically, and in some instances extending from the toe to the heel horizontally, across an inner surface of the face plate. These approaches tend to adversely affect club performance characteristics, e.g., diminishing the size of the sweet spot, and/or inhibiting design flexibility in both mass distribution and the face structure of the club head. Thus, these club heads fail to provide optimal MOI, CG, and/or COR parameters, and as a result, fail to provide much forgiveness for off-center hits for all but the most expert golfers.


In addition to the thickness of the face plate and the walls of the golf club head, the location of the center of gravity also has a significant effect on the COR of a golf club head. For example, a given golf club head having a given CG will have a projected center of gravity or “balance point” or “CG projection” that is determined by an imaginary line passing through the CG and oriented normal to the striking face 18. The location where the imaginary line intersects the striking face 18 is the CG projection, which is typically expressed as a distance above or below the center of the striking face 18. When the CG projection is well above the center of the face, impact efficiency, which is measured by COR, is not maximized. It has been discovered that a fairway wood with a relatively lower CG projection or a CG projection located at or near the ideal impact location on the striking surface of the club face, as described more fully below, improves the impact efficiency of the golf club head as well as initial ball speed. One important ball launch parameter, namely ball spin, is also improved.


The CG projection above centerface of a golf club head can be measured directly, or it can be calculated from several measurable properties of the club head.


Fairway wood shots typically involve impacts that occur below the center of the face, so ball speed and launch parameters are often less than ideal. This results because most fairway wood shots are from the ground and not from a tee, and most golfers have a tendency to hit their fairway wood ground shots low on the face of the club head. Maximum ball speed is typically achieved when the ball is struck at the location on the striking face where the COR is greatest.


For traditionally designed fairway woods, the location where the COR is greatest is the same as the location of the CG projection on the striking surface. This location, however, is generally higher on the striking surface than the below center location of typical ball impacts during play. In contrast to these conventional golf clubs, it has been discovered that greater shot distance is achieved by configuring the club head to have a CG projection that is located near to the center of the striking surface of the golf club head. In some embodiments, the golf club head 2 has a CG projection that is less than about 2.0 mm from the center of the striking surface of the golf club head, i.e. −2.0 mm<CG projection<2.0 mm. For example, some implementations of the golf club head 2 have a CG projection that is less than about 1.0 mm from the center of the striking face of the golf club head (i.e., −1.0 mm<CG projection<1.0 mm), such as about 0.7 mm or less from the center of the striking surface of the golf club head (i.e., −0.7 mm≤CG projection≤0.7 mm), or such as about 0.5 mm or less from the center of the striking surface of the golf club head (i.e., −0.5 mm≤CG projection≤0.5 mm). In other embodiments, the golf club head 2 has a CG projection that is less than about 2.0 mm (i.e., the CG projection is below about 2.0 mm above the center of the striking face), such as less than about 1.0 mm (i.e., the CG projection is below about 1.0 mm above the center of the striking face), or less than about 0.0 mm (i.e., the CG projection is below the center of the striking face), or less than about −1.0 mm (i.e., the CG projection is below about 1.0 mm below the center of the striking face). In each of these embodiments, the CG projection is located above the bottom of the striking face.


In still other embodiments, an optimal location of the CG projection is related to the loft 15 of the golf club head. For example, in some embodiments, the golf club head 2 has a CG projection of about 3 mm or less above the center of the striking face for club heads where the loft angle is at least 15.8 degrees. Similarly, greater shot distance is achieved if the CG projection is about 1.4 mm or less above the center of the striking face for club heads where the loft angle is less than 15.8 degrees. In still other embodiments, the golf club head 2 has a CG projection that is below about 3 mm above the center of the striking face for club heads where the loft angle 15 is more than about 16.2 degrees, and has a CG projection that is below about 2.0 mm above the center of the striking face for club heads where the loft angle 15 is 16.2 degrees or less. In still other embodiments, the golf club head 2 has a CG projection that is below about 3 mm above the center of the striking face for golf club heads where the loft angle 15 is more than about 16.2 degrees, and has a CG projection that is below about 1.0 mm above the center of the striking face for club heads where the loft angle 15 is 16.2 degrees or less. In still other embodiments, the golf club head 2 has a CG projection that is below about 3 mm above the center of the striking face for golf club heads where the loft angle 15 is more than about 16.2 degrees, and has a CG projection that is below about 1.0 mm above the center of the striking face for club heads where the loft angle 15 is between about 14.5 degrees and about 16.2 degrees. In all of the foregoing embodiments, the CG projection is located above the bottom of the striking face. Further, greater initial ball speeds and lower backspin rates are achieved with the lower CG projections.


A golf club head Characteristic Time (CT) can be described as a numerical characterization of the flexibility of a golf club head striking face. The CT may also vary at points distant from the center of the striking face, but may not vary greater than approximately 20% of the CT as measured at the center of the striking face. The CT values for the golf club heads described in the present application were calculated based on the method outlined in the USGA “Procedure for Measuring the Flexibility of a Golf Clubhead,” Revision 2.0, Mar. 25, 2005, which is incorporated by reference herein in its entirety. Specifically, the method described in the sections entitled “3. Summary of Method,” “5. Testing Apparatus Set-up and Preparation,” “6. Club Preparation and Mounting,” and “7. Club Testing” are exemplary sections that are relevant. Specifically, the characteristic time is the time for the velocity to rise from 5% of a maximum velocity to 95% of the maximum velocity under the test set forth by the USGA as described above.


Increased Striking Face Flexibility and Select Tuning


It is known that the coefficient of restitution (COR) of a golf club may be increased by increasing the height Hs, of the striking face 18 and/or by decreasing the thickness of the striking face 18 of a golf club head 2. However, in the case of a fairway wood, hybrid, or rescue golf club, and to a lesser degree even with a driver, increasing the face height may be considered undesirable because doing so will potentially cause an undesirable change to the mass properties of the golf club (e.g., center of gravity location) and to the golf club's appearance.



FIGS. 1-39 show golf club heads that provide increased COR by introducing a flexible channel 212 to increase or enhance the perimeter flexibility of the striking face 18 of the golf club without necessarily increasing the height or decreasing the thickness of the striking face 18. The flexible channel 212 allows for improved performance on mis-hits by increasing the coefficient of restitution (COR) and Characteristic Time (CT) across the face 18 and not just at the center of the face 18, and selectively reducing the amount of spin imparted on a golf ball at impact. The golf club head 2 may include a sole 14 defining a bottom portion of the club head 2, a crown 12 defining a top portion of the club head 2, a skirt portion 16 defining a periphery of the club head 2 between the sole 14 and crown 12, a face 18 defining a forward portion of the club head 2, and a hosel 20 defining a hosel bore 24, thereby defining an interior cavity, or hollow body 10. Some club head 2 embodiments include a flexible channel 212 positioned in the sole 14 of the club head 2 and extending into the interior cavity, or hollow body 10, of the club head 2, and in some embodiments the channel 212 extends substantially in a heel-to-toe direction and has a channel length Lg, a channel width Wg, a channel depth Dg, a channel wall thickness 221, an internal channel structure elevation 224, and a channel setback distance 223 from a leading edge of the club head 2.


One skilled in the art will appreciate that the leading edge is the forwardmost portion of the club head 2 in a particular vertical section that extends in a face-to-rear direction through the width of the striking face Wss, and the leading edge varies across the width of the striking face Wss. Further, as seen in FIG. 4, the channel setback distance 223 may vary across the width of the striking face Wss, although some embodiments may have a constant channel setback distance 223. Thus the club head 2 will have a maximum channel setback distance 223, which in the embodiment of FIG. 4 occurs near the center of the face 18, and a minimum channel setback distance 223, which occurs toward the heel 26 or toe 28 of the club head 2 in the embodiment of FIG. 4, although other embodiments may have a constant channel setback distance 223 in which case the maximum and minimum will be equal. One particular embodiment experiences preferential face flexibility, while maintaining sufficient durability, when the minimum channel setback distance 223 is less than the maximum channel width Wg, while an even further embodiment has a minimum channel setback distance 223 is less than 75% of the maximum channel width Wg, and an even further embodiment has a minimum channel setback distance 223 is 25-75% of the maximum channel width Wg. In another embodiment the minimum channel setback distance 223 is less than 15 mm, while in a further embodiment the minimum channel setback distance 223 is less than 10 mm, while in an even further embodiment the minimum channel setback distance 223 is 3-8 mm. In another embodiment the maximum channel setback distance 223 is less than 30 mm, while in a further embodiment the maximum channel setback distance 223 is less than 20 mm.


While preferential face flexibility and durability may be enhanced as the size of the channel 212 increases, along with the unique relationships disclosed herein, thereby reducing the stresses in the channel 212, increasing the size of the channel 212, particularly the channel depth Dg and channel width Wg, may produce less than desirable sound and vibration upon impact with a golf ball. Additional embodiments further improve the performance via a center-of-gravity CG that is low and forward in conjunction with the channel 212, as well as aerodynamic embodiments having a particularly bulbous crown 12 which may include irregular contours and very thin areas, any of which may further heighten these less than desirable characteristics. Such undesirable attributes associated with the channel 212, particularly a large channel 212, and/or a low and forward CG position, and/or a bulbous aerodynamic crown, may be mitigated with the introduction of a channel tuning system 1100, such as the embodiments seen in FIGS. 11-22, and/or a body tuning system 1400, as seen in FIG. 9. The channel depth Dg is easily measure by filling the channel 212 with clay until the club head 2 has a smooth continuous exterior surface as if the channel 212 does not exist. A blade oriented in the front-to-back direction may then be inserted vertically to section the clay. The clay may then be removed and the vertical thickness measure to reveal the channel depth Dg at any point along the length of the channel 212.


Referring again go FIGS. 11-22, the channel tuning system 1100 may include a longitudinal channel tuning element 1200 and/or a sole engaging channel tuning element 1300. The longitudinal channel running element 1200 is in contact with the channel 212 and the sole engaging channel tuning element 1300 is in contact with the channel 212; which in one embodiment means that they are integrally cast with the channel 212, while in another embodiment they are attached to the channel 212 via available joining methods including welding, brazing, and adhesive attachment. The longitudinal channel tuning element 1200 extends along a portion of the length of the channel 212, and in one embodiment it extends substantially in a heel-to-toe direction, which may be a linear fashion, a zig-zag or sawtooth type fashion, or a curved fashion. As seen best in FIGS. 10, 11, and 29, the longitudinal channel tuning element 1200 has a longitudinal tuning element toe end 1210, a longitudinal element heel end 1220, a longitudinal tuning element length 1230, a longitudinal tuning element height 1240, a longitudinal tuning element width 1250, a top edge elevation 1260, and a lower edge elevation 1270.


As seen in FIG. 11, in one embodiment the aforementioned undesirable attributes associated with the club head 2 are reduced when the longitudinal tuning element length 1230 is greater than the maximum channel width Wg, and in another embodiment when the longitudinal tuning element length 1230 is greater than 50% of the channel length Lg, while in an even further embodiment the longitudinal tuning element length 1230 is greater than 75% of the channel length Lg. The longitudinal tuning element length 1230 is measured in a straight line along the ground plane from a vertical projection of the longitudinal tuning element toe end 1210 on the ground plane to a vertical projection of the longitudinal element heel end 1220 on the ground plane, which is the same manner the channel length Lg is measured.


In another embodiment tuning of the club head 2 is further improved when, in at least one front-to-rear vertical section passing through the longitudinal channel tuning element 1200, a portion of the longitudinal tuning element top edge elevation 1260 is greater than the internal channel structure elevation 224, as seen in FIG. 29. As with all the disclosed embodiments, these unique embodiments and relationships among the channel 212, the attributes of the channel tuning system 1100, the aerodynamic crown, thicknesses, and the club head mass properties selectively mitigate the undesirable characteristics without unduly reducing the performance advantages associated with the channel 212, aerodynamic and mass property features, or sacrificing the durability of the club head 2. Unique placement of the longitudinal tuning element top edge elevation 224 aids in tuning the channel 212 to achieve desirable sound and vibration upon the impact of the club head 2 with a golf ball while not significantly impacting the flexibility of the channel 212 or durability of the club head 2.


In a further embodiment, in at least one front-to-rear vertical section passing through the longitudinal channel tuning element 1200, a portion of the longitudinal tuning element top edge elevation 1260 is at least 10% greater than the internal channel structure elevation 224, while in an even further embodiment a portion of the longitudinal tuning element top edge elevation 1260 is than the internal channel structure elevation 224 by a distance that is greater than the maximum channel wall thickness 221. While the prior embodiments are directed to characteristics in at least one front-to-rear vertical section passing through the longitudinal channel tuning element 1200, in further embodiments the relationships are true through at least 25% of the channel length (Lg), and in even further embodiments through at least 50% of the channel length (Lg), and at least 75% in yet another embodiment. Another embodiment, seen in FIG. 33, has a portion of the longitudinal tuning element top edge elevation 1260 above the elevation of the ideal impact location 23, while in another embodiment a portion of the longitudinal tuning element top edge elevation 1260 is greater than the Zup value. In an even further embodiment, seen best in FIG. 33, at least a portion of the longitudinal channel tuning element 1200 is in contact with both the channel 212 and the hosel bore 24, further tuning the club head 2 without unduly adding rigidity to the channel 212.


In another embodiment at least a portion of the longitudinal channel tuning element 1200 is positioned along the top edge of the channel 212, as seen in FIG. 10, such as in at least one front-to-rear vertical section passing through the longitudinal channel tuning element 1200 the lower edge elevation 1270 is equal to the internal channel structure elevation 224, seen in FIG. 29. While the prior embodiment is directed to characteristics in at least one front-to-rear vertical section passing through the longitudinal channel tuning element 1200, in further embodiments the relationships are true through at least 25% of the channel length Lg, and in even further embodiments through at least 50% of the channel length Lg, and at least 75% in yet another embodiment. As seen in FIG. 10, at least a portion of the longitudinal channel tuning element 1200 may be oriented substantially vertically from the channel 212, oriented at an angle toward the rear of the club head 2 as seen in FIG. 29, or even at an angle toward the face 18, not shown but easily understood. A substantial vertical orientation reduces the impact that the longitudinal channel tuning element 1200 has on the stiffness of the channel 212, and therefore in another embodiment the orientation is substantially vertical through at least 25% of the channel length Lg, and in even further embodiments through at least 50% of the channel length Lg, and at least 75% in yet another embodiment. Further, the substantial vertical orientation aids in the manufacturability of the club head 2 and reduces the likelihood of adding areas of significantly increased rigidity in the channel 212, and the associated peak stress throughout the channel 212, thereby improving the durability of the club head 2, which is also true for the disclosed sizes of the longitudinal channel tuning element, namely the longitudinal tuning element height 1240, the longitudinal tuning element width 1250, and the longitudinal tuning element length 1230.


A further embodiment has a longitudinal tuning element height 1240, seen in FIG. 32, is at least 20% of the channel depth Dg in at least one front-to-rear vertical section passing through the longitudinal channel tuning element, while in a further embodiment this relationship is true throughout at least 25% of the channel length Lg, and in even further embodiments through at least 50% of the channel length Lg, and at least 75% in yet another embodiment. A further embodiment balances the aforementioned tradeoff with the longitudinal tuning element height being 20-70% of the channel depth Dg throughout at least 50% of the longitudinal tuning element length 1230.


As with the length 1230 and height 1240, the longitudinal tuning element width 1250, seen in FIG. 10, plays a role in balancing the benefits and negative effects of the longitudinal channel tuning element 1200. In one embodiment at least a portion of the longitudinal channel tuning element 1200 has a longitudinal tuning element width 1250 of less than the maximum channel wall thickness 221. In a further embodiment the longitudinal tuning element width 1250 is less than the maximum channel wall thickness 221 throughout at least 50% of the longitudinal tuning element length 1230, while in an even further embodiment this is true throughout at least 75% of the longitudinal tuning element length 1230. In an even further embodiment at least a portion of the longitudinal tuning element width 1250 of less than 70% of the maximum channel wall thickness 221. In a further embodiment the longitudinal tuning element width 1250 is less than 70% of the maximum channel wall thickness 221 throughout at least 50% of the longitudinal tuning element length 1230, while in an even further embodiment this is true throughout at least 75% of the longitudinal tuning element length 1230. Yet an even further embodiment has at least a portion of the longitudinal tuning element width 1250 of less than 70% of the maximum channel wall thickness 221. In a further embodiment the longitudinal tuning element width 1250 of 25-60% of the maximum channel wall thickness 221 throughout at least 50% of the longitudinal tuning element length 1230, while in an even further embodiment this is true throughout at least 75% of the longitudinal tuning element length 1230.


Like the length 1230, height 1240, width 1250, longitudinal tuning element top edge elevation 1260, seen in FIGS. 29 and 32-33, and orientation, the location of the longitudinal channel tuning element 1200 plays a role in balancing the benefits and negative effects. As seen in FIG. 11, in one embodiment the longitudinal channel tuning element 1200 extends throughout a channel central region 225, which in one embodiment is defined as the portion of the channel 212 within ½ inch on either side of the ideal impact location 23. Deflection of the channel 212 in this channel central region 225 is not as important to improving the performance of the club head 2 and therefore is a good location for a longitudinal channel tuning element 1200 to influence the tuning of the club head 2 while having minimal effect on enhanced performance associated with the channel 212, which is also why further embodiments, described elsewhere in detail, have increased channel wall thickness 221 in the channel central region 225. Another embodiment capitalizes on tuning gains afforded by having at least a portion of the longitudinal channel tuning element 1200 is in contact with both the channel 212 and the hosel bore 24, further tuning the club head 2 without unduly adding rigidity to the channel 212, as seen in FIGS. 12 and 33. An alternative embodiment is seen in FIG. 13 whereby the longitudinal channel tuning element 1200 is located on the toe portion of the channel 212. In some embodiment the channel 212 extends high up the skirt portion 16, as seen in FIG. 33, and therefore enables the previously described embodiment in which a portion of the longitudinal tuning element top edge elevation 1260 is above the elevation of the ideal impact location 23, and the embodiment having a portion of the longitudinal tuning element top edge elevation 1260 is greater than the Zup value. A common mishit involves striking the golf ball high on the toe portion of the face and these embodiments achieve preferential tuning so that the pitch and vibrations associated with such mishits is not as significantly different from impacts at the ideal impact location 23 as may be experienced with a club head 2 having a channel 212 without a channel tuning system 1100. This improved consistency in pitch and vibration is also heightened in embodiments having a portion of the longitudinal channel tuning element 1200 joining a heel portion of the channel 212 with a portion of the hosel bore 24, also seen in FIG. 33. Yet another embodiment seen in FIG. 14 has a longitudinal channel tuning element 1200 on the toe side of the channel 212, like the embodiment of FIG. 13, and a second longitudinal channel tuning element 1280 on the heel side of the channel 212, like the embodiment of FIG. 14. Still further embodiments such as those seen in FIGS. 19-22 have a longitudinal channel tuning element 1200 extending continuously from the heel to the toe of the channel 212.


As previously mentioned, the channel tuning system 1100 may further includes a sole engaging channel tuning element 1300 in contact with the sole 14 and the channel 212, seen best in FIGS. 15 and 10, which may be in addition to, or in lieu of, the longitudinal channel tuning element 1200. The sole engaging channel tuning element 1300 has a face end 1310, a rear end 1320, a sole engaging tuning element length 1330, seen in FIG. 15, a sole engaging tuning element height 1340, seen in FIG. 10, a sole engaging tuning element width 1350, seen in FIG. 16, a sole engaging portion 1360 in contact with the sole 14 and having a sole engaging portion length 1362, seen in FIG. 30, and a channel engaging portion 1370 in contact with the channel 212 and having a channel engaging portion length 1372 and a channel engaging portion elevation 1374, also seen in FIG. 30. As with the longitudinal channel tuning element 1200, the unique relationships disclosed strike a delicate balance in reducing the undesirable attributes associated with the channel 212 with preferential tuning, while not significantly compromising the performance and flexibility of the channel 212, as well as the durability of the club head 2.


With continued reference to FIG. 30, in one such embodiment the goals are achieved with a sole engaging portion length 1362 is at least 50% of the maximum channel width Wg. A further embodiment achieves the goals when the sole engaging portion 1360 has a sole engaging tuning element height 1340 of at least 15% of the maximum channel depth Dg. Still further, another embodiment, seen in FIG. 31, has a channel engaging portion 1370 that extends up the channel 212 to a channel engaging portion elevation 1374 that is at least 50% of the channel depth Dg in the same vertical plane as the channel engaging portion 1370, while another embodiment has a channel engaging portion 1370 that extends up the channel 212 to a channel engaging portion elevation 1374 that is at least 50-100% of the channel depth Dg in the same vertical plane as the channel engaging portion 1370. In such embodiments the channel engaging portion 1370 does not extend along more than 50% of the channel 212, as also illustrated in FIG. 16, in a face-to-rear vertical section, and serves to tune the club head 2 while also supporting the rear channel wall 218, yet facilitating significant deflection of the channel 212 for improved performance. Still further, another embodiment has a channel engaging portion 1370 that extends up the channel 212 to a channel engaging portion elevation 1374 greater than the internal channel structure elevation 224, as seen in FIG. 30. In fact in some embodiments such as that seen in FIGS. 30, 15, and 18 the channel engaging portion 1370 extends all the way over the channel 212, and in some embodiments engages a portion of the sole 14 between the channel 212 and the face 18, as seen in FIG. 30. In one such entirely over the channel embodiment the channel engaging portion 1370 is located in the channel central region 225 to have a significant influence on the tuning of the club head 2 while having minimal effect on enhanced performance associated with the channel 212 because the slight decrease in potential deflection of the channel 212 in the channel central region 225 is not as impactful on overall club head 2 performance.


Likewise, the channel engaging portion length 1372, seen in FIGS. 30-31, and the sole engaging tuning element width 1350, seen in FIG. 16, play a role in achieving the goals without unduly limiting the performance benefits gained through the addition of the channel 212. For example, in one embodiment the channel engaging portion length 1372 is greater than the maximum channel depth Dg. The channel engaging portion length 1372 is measured along the intersection of the channel engaging portion 1370 and the channel 212. In yet another embodiment the channel engaging portion length 1372 is less than the sum of the maximum channel depth Dg and the maximum channel width Wg, further controlling the amount of rigidity that is added to the flexible channel 212. Still further, in another embodiment the sole engaging portion length 1362 is less than 150% of the maximum channel width Wg, thereby further controlling the amount of rigidity that is added to the channel 212. Similarly, in another embodiment the goals are further enhanced when the sole engaging tuning element width 1350 is less than 70% of the maximum channel wall thickness 221, and even further in an embodiment in which the sole engaging tuning element width 1350 is 25-60% of the maximum channel wall thickness 221.


The orientation and location of the sole engaging channel tuning element 1300 also influences the tuning goals. The sole engaging channel tuning element 1300 is preferably oriented in a direction that is plus, or minus, 45 degrees from a vertical face-to-rear plane passing through the ideal impact location 23, as can be easily visualized in FIGS. 15-18, however in a further embodiment the sole engaging channel tuning element 1300 is oriented in a direction that is plus, or minus, 20 degrees from a vertical face-to-rear plane passing through the ideal impact location 23, and in yet another embodiment the sole engaging channel tuning element 1300 extends in a substantially face-to-rear direction. In the embodiment of FIG. 15 the location of the sole engaging channel tuning element 1300 is substantially aligned with a vertical face-to-rear plane passing through the ideal impact location 23, while in another embodiment, seen in FIG. 16, the sole engaging channel tuning element 1300 is located in a heel portion 26 of the club head 2, and in yet another embodiment, seen in FIG. 17, the sole engaging channel tuning element 1300 is located in a toe portion 26 of the club head 2. Each location achieves different tuning levels, and influences the performance of the channel 212 differently. Embodiments having both a longitudinal channel tuning element 1200 and at least one sole engaging channel tuning element 1300 may have the elements exist independently, as seen in FIGS. 16-18, or they may intersect, as seen in FIGS. 15 and 19-22. Some embodiments may incorporate multiple sole engaging channel tuning elements, such as two, namely the sole engaging channel tuning element 1300 and a second sole engaging channel tuning element 1380, as seen in FIG. 20, or even three, namely the sole engaging channel tuning element 1300, the second sole engaging channel tuning element 1380, and a third sole engaging channel tuning element 1390, as seen in FIG. 19. The quantity and location of each achieves different tuning levels, and influence the performance of the channel 212 differently. One particular embodiment has a sole engaging channel tuning element 1300 within the channel central region 225 to provide a degree of tuning in the area that has a low impact on performance, and a second sole engaging channel tuning element 1380 located in a toe portion of the club head 2, outside of the channel central region 2, where the channel thickness 221 and club head thickness is less thereby having a greater impact on the tuning.


Preferably, the overall frequency of the golf club head 2, i.e., the average of the first mode frequencies of the crown, sole and skirt portions of the golf club head, generated upon impact with a golf ball is greater than 3,000 Hz. Frequencies above 3,000 Hz provide a user of the golf club with an enhanced feel and satisfactory auditory feedback, while in some embodiments frequencies above 3,200 Hz are obtained and preferred. However, a golf club head 2 having relatively thin walls, a channel 212, and/or a thin bulbous crown 12, can reduce the first mode vibration frequencies to undesirable levels. The addition of the channel tuning system 1100 described herein can significantly increase the first mode vibration frequencies, thus allowing the first mode frequencies to approach a more desirable level and improving the feel of the golf club 2 to a user.


For example, golf club head 2 designs were modeled using commercially available computer aided modeling and meshing software, such as Pro/Engineer by Parametric Technology Corporation for modeling and Hypermesh by Altair Engineering for meshing. The golf club head 2 designs were analyzed using finite element analysis (FEA) software, such as the finite element analysis features available with many commercially available computer aided design and modeling software programs, or stand-alone FEA software, such as the ABAQUS software suite by ABAQUS, Inc.


The golf club head 2 design was made of titanium and shaped similar to the club head 2 shown in the figures, except that several iterations were run in which the golf club head 2 had different combinations of the channel tuning system 1100 present or absent. The predicted first or normal mode frequency of the golf club head 2, i.e., the frequency at which the head will oscillate when the golf club head 2 impacts a golf ball, was obtained using FEA software for the various embodiments. A first mode frequency for the club head 2 without any form of a channel tuning system 1100 is below the preferred lower limit of 3000 Hz.


Table 1 below, and reference to FIG. 39, illustrates the significant tuning capabilities associated with the channel tuning system 1100. First, the channel tuning system 1100 includes a longitudinal channel tuning element 1200, a sole engaging channel tuning element 1300, a second sole engaging channel tuning element 1380, and a third sole engaging channel tuning element 1390, the first mode frequency is increased to 3530 Hz and the second mode frequency is increased to 3729 Hz. The next embodiment removes the third sole engaging channel tuning element 1390, leaving the longitudinal channel tuning element 1200, the sole engaging channel tuning element 1300, and the second sole engaging channel tuning element 1380 to produce a club head 2 with a first mode frequency of 3328 Hz and a second mode frequency of 3727 Hz; thus removal of the third sole engaging channel tuning element 1390 located toward the toe resulted in a first mode frequency drop of 202 Hz and a second mode frequency drop of 2 Hz. The next embodiment removes the sole engaging channel tuning element 1300, leaving the longitudinal channel tuning element 1200, the second sole engaging channel tuning element 1380, and the third sole engaging channel tuning element 1390, to produce a club head 2 with a first mode frequency of 3322 Hz and a second mode frequency of 3694 Hz; thus removal of the centrally located sole engaging channel tuning element 1300 resulted in a first mode frequency drop of 208 Hz and a second mode frequency drop of 35 Hz. The next embodiment removes the second sole engaging channel tuning element 1380, leaving the longitudinal channel tuning element 1200, the sole engaging channel tuning element 1300, and the third sole engaging channel tuning element 1390 to produce a club head 2 with a first mode frequency of 3377 Hz and a second mode frequency of 3726 Hz; thus removal of the centrally located second sole engaging channel tuning element 1380 resulted in a first mode frequency drop of 153 Hz and a second mode frequency drop of 3 Hz. The last embodiment removes the longitudinal channel tuning element 1200, leaving the sole engaging channel tuning element 1300, the second sole engaging channel tuning element 1380, and the third sole engaging channel tuning element 1390 to produce a club head 2 with a first mode frequency of 3503 Hz and a second mode frequency of 3728 Hz; thus removal of the longitudinal channel tuning element 1200 resulted in a first mode frequency drop of 27 Hz and a second mode frequency drop of 1 Hz.













TABLE 1





Elements of the


Mode 1
Mode 2


Channel Tuning
Mode 1
Mode 2
Drop
Drop


System (1100) Present
(Hz)
(Hz)
(Hz)
(Hz)



















1200 + 1300 + 1380 + 1390
3530
3729




1200 + 1300 + 1380
3328
3727
202
2


1200 + 1380 + 1390
3322
3694
208
35


1200 + 1300 + 1390
3377
3726
153
3


1300 + 1380 + 1390
3503
3728
27
1









Another advantage of the channel tuning system 1100 is that it is located in the forward half of the club head 2, further promoting a low forward location of the club head 2 center-of-gravity.


Yet a further embodiment incorporates a body tuning system 1400 having a body tuning element 1500, seen best in FIGS. 9-10, 19-23, which may be used in addition to the longitudinal channel tuning element 1200 and/or the sole engaging channel tuning element 1300, or entirely independent of them. The body tuning system 1400 is able to tune the club head 2 and reduce some of the undesirable attributes associated with the introduction of the channel 212 and does so without contacting the channel 212 and therefore without influencing the flexibility of the channel 212. The body tuning system 1400 is particularly beneficial in embodiments having irregular contours of the crown 12, such as the embodiments seen best in FIGS. 1-2 and 23-25, or a particularly bulbous crown 12 that extends significantly above the top edge of the face 18, as seen in FIG. 8.


In one body tuning system 1400 embodiment the body tuning element 1500 includes a body tuning element toe end 1510, a body tuning element heel end 1520, a body tuning element length 1530, a body tuning element height 1540, and a body tuning element width 1550, seen best in FIGS. 9-10, 19, 23, and 31. As seen in FIG. 23, an embodiment of the body tuning element 1500 has a body tuning element sole portion 1570 in contact with the sole 14 and extending in a substantially heel-to-toe direction. The body tuning element 1500 is separated from the channel 212 by a body tuning separation distance 1560, seen in FIG. 10, which is greater than the maximum channel width Wg. The body tuning element length 1530 is measured in a straight line along the ground plane from a vertical projection of the body tuning element toe end 1510 on the ground plane to a vertical projection of the body tuning element heel end 1520 on the ground plane. Similarly, the body tuning separation distance 1560 is measured in a straight line along the ground plane from a vertical projection of a location on the body tuning element 1500 to the nearest vertical projection of the channel 212 onto the ground plane. In another embodiment the body tuning separation distance 1560 is greater than the maximum channel width Wg throughout at least 50% of the body tuning element length 1530; whereas in another embodiment the body tuning separation distance 1560 is at least twice the maximum channel width Wg throughout at least 50% of the body tuning element length 1530; in yet a further embodiment the body tuning separation distance 1560 is 150-300% of the maximum channel width Wg throughout at least 50% of the body tuning element length 1530; and in a further embodiment the body tuning separation distance 1560 is 175-250% of the maximum channel width Wg throughout at least 50% of the body tuning element length 1530


Beneficial tuning is achieved in a further embodiment without adding undue rigidity to the club head 2 and limiting beneficial flexing of the club head 2 when at least a portion of the body tuning element height 1540 is at least 15% of the maximum channel depth Dg, and in a further embodiment at least a portion of the body tuning element height 1540 is no more than 75% of the maximum channel depth Dg, while in an even further embodiment at least a portion of the body tuning element height 1540 is 25-50% of the maximum channel depth Dg. While the prior embodiments are directed to characteristics in at least one front-to-rear vertical section passing through the body tuning element 1500, in further embodiments the relationships are true through at least 25% of the body tuning element length 1530, and in even further embodiments through at least 50% of the body tuning element length 1530, and at least 75% in yet another embodiment.


The delicate balance of beneficial tuning, and avoidance of undue rigidity, is further achieved in embodiments having a body tuning element length 1530, as seen in FIG. 19, of at least 50% of the channel length Lg, while in another embodiment the body tuning element length 1530 is at least 75% of the channel length Lg. Even further embodiments having a longitudinal channel tuning element 1200 link the body tuning element length 1530 to the longitudinal tuning element length 1230 such that in one embodiment the body tuning element length 1530 is at least 50% of the longitudinal tuning element length 1230, while in a further embodiment the body tuning element length 1530 is at least 75% of the longitudinal tuning element length 1230. Thus, any of the described relationships of the body tuning element 1500 with respect to percentages of the body tuning element length 1530, may also be applied throughout the indicated percentages of the longitudinal tuning element length 1230 and/or the channel length Lg to achieve the desired tuning and avoidance of undue club head 2 rigidity.


As previously noted, the body tuning system 1400 is particularly beneficial in embodiments having irregular contours of the crown 12, such as the embodiments seen best in FIGS. 1-2 and 23-25, and embodiments having a bulbous crown with an apex that is significantly above a top edge of the face 18, therefore some embodiments may have a body tuning system 1500 that further includes a body tuning element crown portion 1580 in contact with the crown 12, as seen in FIG. 23. One such embodiment has a body tuning element crown portion 1580 in contact with the crown 12 throughout at least 50% of the longitudinal tuning element length 1230 and/or at least 50% of the channel length Lg; while a further embodiment has the body tuning element crown portion 1580 in contact with the crown 12 throughout at least 75% of the longitudinal tuning element length 1230 and/or at least 75% of the channel length Lg. One particular embodiment has at least a portion of the body tuning element crown portion 1580 connected to the body tuning element sole portion 1570, while in an even further embodiment the body tuning element crown portion 1580 is connected to the body tuning element sole portion 1570 at both the heel portion 26 and the toe portion 28, as seen in FIG. 23. One embodiment having irregular crown contours has a body tuning element crown portion 1580 with at least one section that is concave downward toward the sole 14 and at least one section that is concave upward toward the crown 12, while the embodiment of FIG. 23 includes one section that is concave downward toward the sole 14 and two sections that are concave upward toward the crown 12 separated by the concave downward section. In one embodiment the concave downward section is integrally formed with at least one concave upward section. As seen in FIG. 26, the crown 12 may be a crown insert attached to the club head 2, and in such embodiments the crown insert may be constructed of a different, generally lighter, material, which may further contribute to the need for a channel tuning system 1100 and/or a body tuning system 1400.


As with the longitudinal channel tuning element 1200 and the sole engaging channel tuning element 1300 being in contact with the channel 212 either integrally or via a number of joining methods, portions of the body tuning system 1400 are in contact with the sole 14 and/or crown 12, which in one embodiment means that they are integrally cast with the sole 14 and/or crown 12, while in another embodiment they are attached to the sole 14 and/or crown 12 via available joining methods including welding, brazing, and adhesive attachment.


The body tuning element 1500 is preferably oriented in a direction that is plus, or minus, 45 degrees from a vertical heel-to-toe plane parallel to a vertical heel-to-toe plane containing the centerline axis 21, however in a further embodiment the body tuning element 1500 is preferably oriented in a direction that is plus, or minus, 20 degrees from a vertical heel-to-toe plane parallel to a vertical heel-to-toe plane containing the centerline axis 21, and in an even further embodiment the body tuning element 1500 is preferably oriented in a direction that is substantially parallel to a vertical heel-to-toe plane containing the centerline axis 21. The body tuning element 1500 may traverse a portion of the club head 2 a linear fashion, a zig-zag or sawtooth type fashion, or a curved fashion.


Another embodiment incorporates the aerodynamic benefits of a uniquely shaped crown 12 as disclosed in U.S. patent application Ser. Nos. 14/260,328, 14/330,205, 14/259,475, and 14/88,354, all of which are incorporated by reference in their entirety herein. One such embodiment has a club head depth Dch, seen in FIG. 7, that is at least 4.4 inches, while in a further embodiment the club head depth Dch is at least 4.5 inches, and at least 4.6 inches in yet a further embodiment. Aerodynamic characteristics are particularly beneficial in embodiments having a maximum top edge elevation, Hte, of at least 2.0 inches, while in a further embodiment the maximum top edge elevation, Hte, is at least 2.2 inches, and at least 2.4 inches in yet a further embodiment. The highest point on the crown 12 establishes the club head height, Hch, above the ground plane, as seen in FIGS. 8 and 10, and this highest point on the crown 12 is referred to as the crown apex. An apex ratio is the ratio of club head height, Hch, to the maximum top edge elevation, Hte. In one embodiment the apex ratio is at least 1.13, thereby encouraging airflow reattachment and reduced aerodynamic drag, while the apex ratio is at least 1.15 in a further embodiment, at least 1.17 in an even further embodiment, and at least 1.19 in yet another embodiment.


While such bulbous crown embodiments are aerodynamically beneficial, it is desirable to control the center-of-gravity of the club head 2 so that it does not increase significantly due to the bulbous crown 12. One manner of controlling the height of the CG is to incorporate a crown structure such as that disclosed in U.S. patent application Ser. No. 14/734,181, which is incorporated by reference in its entirety herein. Therefore, in one embodiment majority of the crown 12 has a thickness of 0.7 mm or less, while in a further embodiment majority of the crown 12 has a thickness of 0.65 mm or less. In another embodiment at least a portion of the crown 12 has a thickness of 0.5 mm or less, while in yet a further embodiment at least a portion of the crown 12 has a thickness of 0.4 mm or less; in another embodiment such crown 12 embodiments having thin portions may also have a portion with a thickness of at least 0.7 mm. For instance, the crown 12 may have a front crown portion 901, as seen in FIG. 9, with a relatively greater thickness than a back crown portion 905 in order to provide greater durability to the golf club head 2. In some embodiments, the front crown portion 901 has a thickness of from about 0.6 to about 1.0 mm, such as from about 0.7 to about 0.9 mm, or about 0.8 mm. In a further embodiment at least a portion of the back crown portion 905 has a thickness that is less than 60% of the front crown portion 901.


Now looking at just the portion of the crown 12 located at an elevation above the maximum face top edge elevation, Hte, in one embodiment majority of this portion of the crown 12 has a thickness of 0.7 mm or less, while in a further embodiment majority of this portion of the crown 12 has a thickness of 0.6 mm or less, while in yet another embodiment majority of this portion of the crown 12 has a thickness of 0.5 mm or less. The foregoing thicknesses refer to the components of the golf club head 2 after all manufacturing steps have been taken, including construction (e.g., casting, stamping, welding, brazing, etc.), finishing (e.g., polishing, etc.), and any other steps. Another manner of controlling the height of the CG, while still incorporating an aerodynamically bulbous crown, is to incorporate at least one recessed area into the crown, as seen in FIGS. 1 and 2, in lieu of a traditional crown 12 of relatively consistent curvature.


Such bulbous crown embodiments, and the associated thin-crown embodiments and recessed area crown embodiments, are designed to reduce the impact of the bulbous crown on the CG location, often introduce new less desirable characteristics to the club head 2, similar to those discussed with the introduction of the channel 212. Fortunately embodiments incorporating a body tuning system 1400 may reduce the less desirable characteristics. For instance, one embodiment incorporates a body tuning element crown portion 1580 that is partially above the maximum top edge elevation, Hte, of the face 18, as seen in FIG. 10, while a further embodiment has at least a portion of the body tuning element crown portion 1580 at an elevation that is at least 5% greater than the maximum top edge elevation, Hte, of the face 18, and yet another embodiment has at least a portion of the body tuning element crown portion 1580 at an elevation that is at least 10% greater than the maximum top edge elevation, Hte, of the face 18. Another embodiment incorporates a body tuning element crown portion 1580 that extends continuously across the portion of the crown 12 that is located at an elevation above the maximum face top edge elevation, Hte, of the face 18. Such embodiments, along with the previously disclosed embodiments disclosing relationships of the body tuning separation distance 1560 to other club head 2 variables, effectively establish the portion of the crown 12 that lies above the maximum face top edge elevation, Hte, of the face 18.


In yet a further embodiment the body tuning system 1400 further includes a body tuning element connecting element 1600 having a connecting element sole end 1610 engaging the body tuning element sole portion 1570, and a connecting element crown end 1620 engaging the body tuning element crown portion 1580, as seen in FIG. 23. In one embodiment the body tuning element connecting element 1600, or a portion of it, may be integrally cast with the body tuning element sole portion 1570 and/or the body tuning element crown portion 1580, while in another embodiment the attachment may be made via available joining methods including welding, brazing, and adhesive attachment, or mechanically attached such as in an embodiment like FIG. 26 having a crown insert. In such crown insert embodiment the body tuning element connecting element 1600 may be a single piece connected to either the body tuning element sole portion 1570 and/or the body tuning element crown portion 1580 that then engages the other portion when the crown insert is installed, or the body tuning element connecting element 1600 may be composed of multiple sections that then engages the other section when the crown insert is installed. Thus, either, or both, the body tuning element sole portion 1570 and/or the body tuning element crown portion 1580 may be formed to include a receiver to cooperate and receive an end of the body tuning element connecting element 1600. The body tuning element connecting element 1600 effectively joins the crown 12 and sole 14 to further tune the club head 2 and reduce undesirable vibrations.


The location of the body tuning element connecting element 1600 is largely dictated by the location of the body tuning element sole portion 1570 and the body tuning element crown portion 1580, and therefore all the relationships disclosed regarding their location with respect to the channel 212 also apply to the location of the body tuning element connecting element 1600. Further, one particular embodiment provides preferred performance when the body tuning element connecting element 1600 is located on the toe side of the club head 2, or between the ideal impact location 23 and the toe 28. In another embodiment the body tuning element connecting element 1600 is located on the toe side of the club head 2 and in the rear half of the club head 2, using the club head depth Dch seen in FIG. 7 to determine the rear half. Still further, in another embodiment the connecting element crown end 1620 engages the body tuning element crown portion 1580 at an elevation below the maximum face top edge elevation, Hte, of the face 18.


Likewise, the orientation and construction of the body tuning element connecting element 1600 influences the benefits associated with it. In one embodiment the body tuning element connecting element 1600 is oriented at an angle that is plus, or minus, 10 degrees from vertical; while in a further embodiment the orientation is plus, or minus, 5 degrees from vertical; and in an even further embodiment the orientation is substantially vertical. The cross-sectional shape of the body tuning element connecting element 1600 in a plane perpendicular to a longitudinal axis of the body tuning element connecting element 1600 is round in one embodiment. Further, in one embodiment the body tuning element connecting element 1600 is solid, while in an alternative embodiment the body tuning element connecting element 1600 is hollow. Regardless, the minimum cross-sectional dimension of the body tuning element connecting element 1600 is at least as great as the minimum body tuning element width 1550, while in a further embodiment it is at least as great as the maximum body tuning element width 1500, while in yet another embodiment it is at least twice the maximum body tuning element width 1500, and in still a further embodiment it is 2-5 times the maximum body tuning element width 1500. In hollow body tuning element connecting element 1600 embodiments the minimum wall thickness of the body tuning element connecting element 1600 is at least as great as the minimum body tuning element width 1550. A further embodiment includes a bridge 1700, seen in FIG. 23, connecting the body tuning element 1500 with the sole engaging channel tuning element 1300, and in one embodiment the bridge 1700 engages the body tuning element 1500 at the connecting element sole end 1610.


The benefits of the channel tuning system 1100 and/or body tuning system 1400 are heightened as the size of the channel 212 increases. For example in one embodiment the disclosed embodiments are used in conjunction with a channel 212 having a volume that is at least 3% of the club head 2 volume, while in a further embodiment the channel 212 has a volume that is 4-10% of the club head 2 volume, and in an even further embodiment the channel 212 has a volume that is at least 5% of the club head 2 volume. In one particular embodiment the channel 212 has a volume that is at least 15 cubic centimeters (cc), while a further embodiment has a channel 212 volume that is 15-40 cc, and an even further embodiment has a channel 212 volume of at least 20 cc. One skilled in the art will know how to determine such volumes by submerging at least a portion of the club head in a liquid, and then doing the same with the channel 212 covered, or by filling the channel 212 with clay or other malleable material to achieve a smooth exterior profile of the club head and then removing and measuring the volume of the malleable material.


Further, the benefits of the channel tuning system 1100 and/or body tuning system 1400 are heightened as the channel width Wg, channel depth Dg, and/or channel length Lg increase. As previously disclosed, beneficial flexing of the club head 2, and reduced stress in the channel 212, may be achieved as the size of the channel 212 increases, however there is a point at which the negatives outweigh the positives, yet the channel tuning system 1100 and/or body tuning system 1400, as well as the upper channel wall radius of curvature 222R, beneficially shift, or control, when the negatives outweigh the positives. In one embodiment any of the disclosed embodiments are used in conjunction with a channel 212 that has a portion with a channel depth Dg that is at least 20% of the Zup value, while a further embodiment has a portion with the channel depth Dg being at least 30% of the Zup value, and an even further embodiment has a portion with the channel depth Dg being 30-70% of the Zup value. In another embodiment any of the disclosed embodiments are used in conjunction with a channel 212 that has a portion with a channel depth Dg that is at least 8 mm, while a further embodiment has a portion with the channel depth Dg being at least 10 mm, while an even further embodiment has a portion with the channel depth Dg being at least 12 mm, and yet another embodiment has a portion with the channel depth Dg being 10-15 mm. One embodiment has a Zup value that is less than 30 mm. The length Lg of the channel 212 may be defined relative to the width of the striking face Wss. For example, in some embodiments, the length Lg of the channel 212 is from about 70% to about 140%, or about 80% to about 140%, or about 100% of the width of the striking face Wss.


Further, the configuration of the crown 12, including the shape, and in some embodiments the amount of the bulbous crown 12 at an elevation above the maximum face top edge elevation, Hte, of the face 18, as well as the crown thickness, influence the overall rigidity, or alternatively the flexibility, of the club head 2, which must compliment the benefits associated with the channel 212, and vice versa, rather than fight the benefits associated with the channel 212 and/or crown thickness, and in some embodiments the relationships further serve to achieve the desired tuning characteristics of the club head 2. As such, in one bulbous crown embodiment the difference between the maximum club head height, Hch, or apex height, and the maximum face top edge elevation, Hte, of the face 18, is at least 50% of the maximum channel depth, Dg, while in a further embodiment the difference is at least 70% of the maximum channel depth, Dg, in yet another embodiment the difference is 70-125% of the maximum channel depth, Dg, and in still a further embodiment the difference is 80-110% of the maximum channel depth, Dg. In another bulbous crown embodiment the difference between the maximum club head height, Hch, or apex height, and the maximum face top edge elevation, Hte, of the face 18, is at least 25% of the maximum channel width, Wg, while in a further embodiment the difference is at least 50% of the maximum channel width, Wg, in yet another embodiment the difference is 60-120% of the maximum channel width, Wg, and in still a further embodiment the difference is 70-110% of the maximum channel width, Wg. A further bulbous crown embodiment has an apex ratio of at least 1.13 and the maximum channel depth, Dg, is at least 10% of the difference between the maximum club head height, Hch, or apex height, and the maximum face top edge elevation, Hte, of the face 18; while in a further embodiment the apex ratio is at least 1.15 and the maximum channel depth, Dg, is at least 20% of the difference between the maximum club head height, Hch, or apex height, and the maximum face top edge elevation, Hte, of the face 18; and in yet another embodiment the apex ratio is at least 1.15 and the maximum channel depth, Dg, is 60-120% of the difference between the maximum club head height, Hch, or apex height, and the maximum face top edge elevation, Hte, of the face 18.


In a further embodiment wherein a majority of the portion of the crown 12 located at an elevation above the maximum face top edge elevation, Hte, has a crown thickness of 0.7 mm or less; while in another embodiment majority of the portion of the crown 12 located at an elevation above the maximum face top edge elevation, Hte, has a crown thickness that is less than a maximum channel wall thickness 221; and in yet an even further embodiment majority of the portion of the crown 12 located at an elevation above the maximum face top edge elevation, Hte, has a crown thickness that is less than a minimum channel wall thickness 221. In another embodiment majority of the portion of the crown 12 located at an elevation above the maximum face top edge elevation, Hte, has a crown thickness that is 25-75% of a minimum channel wall thickness 221.


Now turning to the channel width Wg, in one embodiment any of the disclosed embodiments are used in conjunction with a channel 212 that has a portion with a channel width Wg that is at least 20% of the Zup value, while a further embodiment has a portion with the channel width Wg being at least 30% of the Zup value, and an even further embodiment has a portion with the channel width Wg being 25-60% of the Zup value. In one driver embodiment the Zup value is 20-36 mm, while in a further embodiment the Zup value is 24-32 mm, while in an even further embodiment the Zup value is 26-30 mm. In one fairway wood embodiment the Zup value is 8-20 mm, while in a further embodiment the Zup value is 10-18 mm, while in an even further embodiment the Zup value is 12-16 mm.


Another embodiment further improves the stress distribution in the channel 212 when any of the disclosed embodiments are used in conjunction with a channel 212 that has a portion with an upper channel wall radius of curvature 222R, seen in FIG. 9, that is at least 20% of the maximum channel width Wg, while a further embodiment has a portion with an upper channel wall radius of curvature 222R that is at least 25% of the maximum channel width Wg, and an even further embodiment has a portion with an upper channel wall radius of curvature 222R that is at least 30% of the maximum channel width Wg. While the embodiments described immediately above in this paragraph are directed to characteristics in at least one front-to-rear vertical section passing through the longitudinal channel tuning element 1200, in further embodiments the relationships are true through at least 25% of the channel length Lg, and in even further embodiments through at least 50% of the channel length Lg, and at least 75% in yet another embodiment. Now turning to the channel length Lg, in one embodiment any of the disclosed embodiments are used in conjunction with a channel 212 that has a channel length Lg that is at least 50% of the face width Wss, while in another embodiment any of the disclosed embodiments are used in conjunction with a channel 212 that has a channel length Lg that is at least 75% of the face width Wss, and in an even further embodiment any of the disclosed embodiments are used in conjunction with a channel 212 that has a channel length Lg that is greater than the face width Wss.


The channel 212 may further include an aperture as disclosed in U.S. patent application Ser. No. 14/472,415, which is incorporated herein by reference. Further, the crown 12 may include a post apex attachment promoting region as disclosed in U.S. patent application Ser. No. 14/259,475, which is incorporated herein by reference, a drop contour area as disclosed in U.S. patent application Ser. No. 14/488,354, which is incorporated herein by reference, a trip step as disclosed in U.S. patent application Ser. No. 14/330,205, which is incorporated herein by reference, and/or unique crown curvature as disclosed in U.S. patent application Ser. No. 14/260,328, which is incorporated herein by reference


Another embodiment introduces a thickened channel central region 225, seen best in FIGS. 6 and 11, to further complement the benefits of the channel tuning system 1100 and/or body tuning system 1400. In one embodiment the channel central region 225 is the portion of the channel 212 within ½ inch on either side of the ideal impact location 23, and within the channel central region 225 a portion of the channel 212 has a wall thickness 221 that is at least twice the thinnest portion of the channel 212 located outside of the channel central region 225, while in a further embodiment the wall thickness 221 through the entire channel central region 225 is at least twice the thinnest portion of the channel 212 located outside of the channel central region 225. In one embodiment a portion of the channel 212 within the channel central region 225 has a wall thickness 221 that is at least 2.0 mm, and a portion of the channel 212 located outside of the channel central region 225 has a wall thickness 221 that is 1.0 mm or less, while in another embodiment the channel central region 225 has a wall thickness 221 that is at least 2.5 mm, and in yet another embodiment no portion of the channel central region 225 has a wall thickness 221 greater than 3.5 mm. In a further embodiment the portion of the sole 14 in front of the channel central region 225 has a sole thickness that is at least as thick as the maximum channel wall thickness 221 in the channel central region 225, while in an even further embodiment the portion of the sole 14 in front of the channel central region 225 has a sole thickness that is at least twice the thinnest portion of the channel 212 located outside of the channel central region 225, while in another embodiment the portion of the sole 14 in front of the channel central region 225 has a sole thickness that is at least 2.0 mm, and in yet another embodiment the entire portion of the sole 14 in front of the channel central region 225 has a sole thickness that is 2.5-3.5 mm. In addition to the benefits of the channel tuning system 1100 and/or body tuning system 1400 disclosed, the embodiments of this paragraph also stabilize the face 18, lower the peak stress in the channel 212, and reduce the spin imparted on a golf ball at impact.


The rear channel wall 218 and front channel wall 220 define a channel angle β therebetween. In some embodiments, the channel angle β can be between about 10° to about 30°, such as about 13° to about 28°, or about 13° to about 22°. In some embodiments, the rear channel wall 218 extends substantially perpendicular to the ground plane when the club head 2 is in the normal address position, i.e., substantially parallel to the z-axis 65. In still other embodiments, the front channel wall 220 defines a surface that is substantially parallel to the striking face 18, i.e., the front channel wall 220 is inclined relative to a vector normal to the ground plane (when the club head 2 is in the normal address position) by an angle that is within about ±5° of the loft angle 15, such as within about ±3° of the loft angle 15, or within about ±1° of the loft angle 15.


In the embodiment shown, the heel channel wall 214, toe channel wall 216, rear channel wall 218, and front channel wall 220 each have a thickness 221 of from about 0.7 mm to about 1.5 mm, e.g., from about 0.8 mm to about 1.3 mm, or from about 0.9 mm to about 1.1 mm.


As seen in FIGS. 27-28, a weight port 40 may be located on the sole portion 14 of the golf club head 2, and is located adjacent to and rearward of the channel 212. In a further embodiment the weight port 40 is located on the sole portion 14 of the golf club head 2, and is located adjacent to and rearward of the body tuning system 1500. Still a further embodiment has at least one weight port 40 is located on the sole portion 14 of the golf club head 2, and located adjacent to and between the channel 212 and the body tuning system 1500; while an even further embodiment has at least two weight ports 40 is located on the sole portion 14 of the golf club head 2, and located adjacent to and between the channel 212 and the body tuning system 1500. By positioning the weight port 40 rearward of the channel 212, and in some embodiments forward of the body tuning system 1500, the deformation is localized in the area of the channel 212, since the club head 2 is much stiffer in the area of the at least one weight port 40. As a result, the ball speed after impact is greater for the club head having the channel 212 and at least one weight port 40 than for a conventional club head, which results in a higher COR. The weight port 40 may be located adjacent to and rearward of the rear channel wall 218. One or more mass pads may also be located in a forward position on the sole 14 of the golf club head 2, contiguous with both the rear channel wall 218 and the weight port 40. As discussed above, the configuration of the channel 212 and its position near the face 18 allows the face plate to undergo more deformation while striking a ball than a comparable club head without the channel 212, thereby increasing both COR and the speed of golf balls struck by the golf club head. In some embodiments the weight port 40, or ports, are located adjacent to and rearward of the rear channel wall 218. The weight ports 40 are separated from the rear channel wall 218 by a distance of approximately 1 mm to about 10 mm, such as about 1.5 mm to about 8 mm. As discussed above, the configuration of the channel 212 and its position near the face 18 allows the face plate to undergo more deformation while striking a ball than a comparable club head without the channel 212, thereby increasing both COR and the speed of golf balls struck by the golf club head. As a result, the ball speed after impact is greater for the club head having the channel 212 than for a conventional club head, which results in a higher COR.


In some embodiments, the slot 212 has a substantially constant width Wg, and the slot 212 is defined by a radius of curvature for each of the forward edge and rearward edge of the slot 212. In some embodiments, the radius of curvature of the forward edge of the slot 212 is substantially the same as the radius of curvature of the forward edge of the sole 14. In other embodiments, the radius of curvature of each of the forward and rearward edges of the slot 212 is from about 15 mm to about 90 mm, such as from about 20 mm to about 70 mm, such as from about 30 mm to about 60 mm. In still other embodiments, the slot width Wg changes at different locations along the length of the slot 212.


Connection Assembly


Now referencing FIGS. 34-38, a club shaft is received within the hosel bore 24 and is aligned with the centerline axis 21. In some embodiments, a connection assembly is provided that allows the shaft to be easily disconnected from the club head 2. In still other embodiments, the connection assembly provides the ability for the user to selectively adjust the loft-angle 15 and/or lie-angle 19 of the golf club. For example, in some embodiments, a sleeve is mounted on a lower end portion of the shaft and is configured to be inserted into the hosel bore 24. The sleeve has an upper portion defining an upper opening that receives the lower end portion of the shaft, and a lower portion having a plurality of longitudinally extending, angularly spaced external splines located below the shaft and adapted to mate with complimentary splines in the hosel opening 24. The lower portion of the sleeve defines a longitudinally extending, internally threaded opening adapted to receive a screw for securing the shaft assembly to the club head 2 when the sleeve is inserted into the hosel opening 24. Further detail concerning the shaft connection assembly is provided in U.S. patent application Ser. No. 14/074,481, which is incorporated herein by reference.


For example, FIG. 34 shows an embodiment of a golf club assembly that includes a club head 3050 having a hosel 3052 defining a hosel opening 3054, which in turn is adapted to receive a hosel insert 2000. The hosel opening 3054 is also adapted to receive a shaft sleeve 3056 mounted on the lower end portion of a shaft (not shown in FIG. 28) as described in U.S. patent application Ser. No. 14/074,481. The hosel opening 3054 extends from the hosel 3052 through the club head and opens at the sole, or bottom surface, of the club head. Generally, the club head is removably attached to the shaft by the sleeve 3056 (which is mounted to the lower end portion of the shaft) by inserting the sleeve 3056 into the hosel opening 3054 and the hosel insert 2000 (which is mounted inside the hosel opening 3054), and inserting a screw 4000 upwardly through an opening in the sole and tightening the screw into a threaded opening of the sleeve, thereby securing the club head to the sleeve 3056.


The shaft sleeve 3056 has a lower portion 3058 including splines that mate with mating splines of the hosel insert 2000, an intermediate portion 3060 and an upper head portion 3062. The intermediate portion 3060 and the head portion 3062 define an internal bore 3064 for receiving the tip end portion of the shaft. In the illustrated embodiment, the intermediate portion 3060 of the shaft sleeve has a cylindrical external surface that is concentric with the inner cylindrical surface of the hosel opening 3054. In this manner, the lower and intermediate portions 3058, 3060 of the shaft sleeve and the hosel opening 3054 define a longitudinal axis B. The bore 3064 in the shaft sleeve defines a longitudinal axis A to support the shaft along axis A, which is offset from axis B by a predetermined angle 3066 determined by the bore 3064. As described in more detail in U.S. patent application Ser. No. 14/074,481, inserting the shaft sleeve 3056 at different angular positions relative to the hosel insert 2000 is effective to adjust the shaft loft and/or the lie angle.


In the embodiment shown, because the intermediate portion 3060 is concentric with the hosel opening 3054, the outer surface of the intermediate portion 3060 can contact the adjacent surface of the hosel opening, as depicted in FIG. 34. This allows easier alignment of the mating features of the assembly during installation of the shaft and further improves the manufacturing process and efficiency. FIGS. 35 and 36 are enlarged views of the shaft sleeve 3056. As shown, the head portion 3062 of the shaft sleeve (which extends above the hosel 3052) can be angled relative to the intermediate portion 3060 by the angle 3066 so that the shaft and the head portion 3062 are both aligned along axis A. In alternative embodiments, the head portion 3062 can be aligned along axis B so that it is parallel to the intermediate portion 3060 and the lower portion 3058.


Further embodiments incorporate a club head 2 having a shaft connection assembly like that described above in relation to FIGS. 34-36. In some embodiments, the club head 2 includes a shaft connection assembly and a channel or slot, such as those described above. For example, FIGS. 37 and 38A-E show an embodiment of a golf club head 2 having a shaft connection assembly that allows the shaft to be easily disconnected from the club head 2, and that provides the ability for the user to selectively adjust the loft-angle 15 and/or lie-angle 19 of the golf club. The club head 2 includes a hosel 20 defining a hosel bore 24, which in turn is adapted to receive a hosel insert 2000. The hosel bore 24 is also adapted to receive a shaft sleeve 3056 mounted on the lower end portion of a shaft (not shown in FIGS. 34 and 38A-F) as described in U.S. patent application Ser. No. 14/074,481. A recessed port 3070 is provided on the sole, and extends from the bottom portion of the golf club head into the interior of the body 10 toward the crown portion 12. The hosel bore 24 extends from the hosel 20 through the club head 2 and opens within the recessed portion 3070 at the sole of the club head.


The club head 2 is removably attached to the shaft by the sleeve 3056 (which is mounted to the lower end portion of the shaft) by inserting the sleeve 3056 into the hosel bore 24 and the hosel insert 2000 (which is mounted inside the hosel bore 24), and inserting a screw 4000 upwardly through the recessed port 3070 and through an opening in the sole and tightening the screw into a threaded opening of the sleeve, thereby securing the club head to the sleeve 3056. A screw capturing device, such as in the form of an o-ring or washer 3036, can be placed on the shaft of the screw 4000 to retain the screw in place within the club head when the screw is loosened to permit removal of the shaft from the club head.


The recessed port 3070 extends from the bottom portion of the golf club head into the interior of the outer shell toward the top portion of the club head (400), as seen in FIGS. 37 and 38A-E. In the embodiment shown, the mouth of the recessed port 3070 is generally rectangular, although the shape and size of the recessed port 3070 may be different in alternative embodiments. The recessed port 3070 is defined by a port toe wall 3072, a port fore-wall 3074, and/or a port aft-wall 3076, as seen in FIG. 37. In this embodiment, a portion of the recessed port 3070 connects to the channel 212 at an interface referred to as a port-to-channel junction 3080, seen best in the sections FIGS. 38D-E taken along section lines seen in FIG. 38A. In this embodiment, the portion of the channel 212 located near the heel portion of the club head 2 does not have a distinct rear wall at the port-to-channel junction 3080 and the port fore-wall 3074 supports a portion of the channel 212 located near the heel and serves to stabilize the heel portion of the channel 212 while permitting deflection of the channel 212. Similarly, the port-to-channel junction 3080 may be along the port aft-wall 3076 or the port toe wall 3072. Such embodiments allow the recessed port 3070 and the channel 212 to coexist in a relatively tight area on the club head while providing a stable connection and preferential deformation of the portion of the channel 212 located toward the heel of the club head.


As shown in FIGS. 38A-E, the channel 212 extends over a portion of the sole 14 of the golf club head 2 in the forward portion of the sole 14 adjacent to or near the striking face 18. The channel 212 extends into the interior of the club head body 10 and may have an inverted “V” shape, a length Lg, a width Wg, and a depth Dg as discussed above. The channel 212 may merge with the recessed port 3070 at the port-to-channel junction 3080.


In the embodiment shown in FIG. 38B, the channel width Wg is from about 3.5 mm to about 8.0 mm, such as from about 4.5 mm to about 7.0 mm, such as about 6.5 mm. A pair of distance measurements L1 and L2 are also shown in FIG. 38B, with L1 representing a distance from the toe channel wall 216 to a point within the channel corresponding with the port-to-channel junction 3080, and with L2 representing a distance from a point representing an intersection of the upper channel wall 222 and the toe channel wall 216 to a point on the upper channel wall 222 adjacent to the bore for the screw 4000. In the embodiment shown, the L1 distance is about 58 mm and the L2 distance is about 63 mm.


Also shown in FIG. 38B are measurements for the port width Wp and port length Lp, which define the generally rectangular shape of the recessed port 3070 in the illustrated embodiment. The port width Wp is measured from a midpoint of the mouth of the port fore-wall 3074 to a midpoint of the mouth of the port aft-wall 3076. The port length Lp is measured from a midpoint of the heel edge of the recessed port 3070 to a midpoint of the mouth of the port toe wall 3072. In the embodiment shown, the port width Wp is from about 8 mm to about 25 mm, such as from about 10 mm to about 20 mm, such as about 15.5 mm. In the embodiment shown, the port length Lp is from about 12 mm to about 30 mm, such as from about 15 mm to about 25 mm, such as about 20 mm.


In alternative embodiments, the recessed portion 3070 has a shape that is other than rectangular, such as round, triangular, square, or some other regular geometric or irregular shape. In each of these embodiments, a port width Wp may be measured from the port fore-wall 3074 to a rearward-most point of the recessed port. For example, in an embodiment that includes a round recessed port (or a recessed port having a rounded aft-wall), the port width W.sub.p may be measured from the port fore-wall 3074 to a rearward-most point located on the rounded aft-wall. In several embodiments, a ratio Wp/Wg of the port width Wp to an average width of the channel Wg may be from about 1.1 to about 20, such as about 1.2 to about 15, such as about 1.5 to about 10, such as about 2 to about 8.


Turning to the cross-sectional views shown in FIGS. 38C-E, the transition from the area and volume comprising the recessed port 3070 to the area and volume comprising the channel 212 is illustrated. In FIG. 38C, the hosel opening 3054 is shown in communication with the recessed port 3070 via a passage 3055 through which the screw 400 of the shaft attachment system is able to pass. In FIG. 38D, a bottom wall 3078 of the recessed port 3070 forms a transition between the port fore-wall 3074 and the port aft-wall 3076. In FIG. 38E, the port-to-channel junction 3080 defines the transition from the recessed port 3070 to the channel 212.


In the embodiment shown in FIGS. 37 and 38A-E, a weight port 40 is located on the sole portion 14 of the golf club head 2, and is located adjacent to and rearward of the channel 212. As described previously, the weight port 40 can have any of a number of various configurations to receive and retain any of a number of weights or weight assemblies, such as described in U.S. Pat. Nos. 7,407,447 and 7,419,441, which are incorporated herein by reference. In the embodiment shown, the weight port 40 is located adjacent to and rearward of the rear channel wall 218. One or more mass pads may also be located in a forward position on the sole 14 of the golf club head 2, contiguous with both the rear channel wall 218 and the weight port 40. As discussed above, the configuration of the channel 212 and its position near the face 18 allows the face 18 to undergo more deformation while striking a ball than a comparable club head without the channel 212, thereby increasing both COR and the speed of golf balls struck by the golf club head. By positioning the mass pad rearward of the channel 212, the deformation is localized in the area of the channel 212, since the club head is much stiffer in the area of the mass pad. As a result, the ball speed after impact is greater for the club head having the channel 212 and mass pad than for a conventional club head, which results in a higher COR.


Whereas the invention has been described in connection with representative embodiments, it will be understood that it is not limited to those embodiments. On the contrary, it is intended to encompass all alternatives, modifications, combinations, and equivalents as may be included within the spirit and scope of the invention as defined by the appended claims.

Claims
  • 1. A golf club head comprising: a club head body having a crown, a sole, a heel, a toe, a striking face, and a rear portion opposite the striking face, with the club head body defining an interior cavity;one or more body tuning element connecting elements positioned within the interior cavity toeward of a geometric center of the striking face and connecting the crown to the sole, the one or more body tuning element connecting elements each having a first end attached to a first internal surface and a second end attached to a second internal surface, and an intermediate portion spanning across the interior cavity from the first end to the second end;wherein the intermediate portion does not contact any portion of the crown or the sole and the one or more body tuning element connecting elements do not contact the rear portion of the club head body;wherein the one or more body tuning element connecting elements are permanently secured to the club head body;at least one weight configured to engage the sole at two or more positions;a channel positioned in the sole portion of the club head body and having a volume that is at least 3% of the club head volume;wherein the golf club head has a CG with a head origin x-axis (CGx) coordinate between about −2 mm and about 6 mm and a head origin y-axis (CGy) coordinate between about 15 mm and about 40 mm, and a head origin z-axis (CGz) less than 0 mm;wherein the channel extends in a substantially heel-to-toe lengthwise direction and has a channel internal surface located within the interior cavity of the club head body, and at least one widthwise rib extending across the channel internal surface in a widthwise direction, wherein the widthwise direction is substantially transverse to the lengthwise direction of the channel.
  • 2. The golf club head according to claim 1, further comprising at least two widthwise ribs extending across the channel internal surface in the widthwise direction and spaced apart in the lengthwise direction.
  • 3. The golf club head according to claim 2, wherein a first rib of the at least two widthwise ribs is angled with respect to a second rib of the at least two widthwise ribs.
  • 4. The golf club head according to claim 2, further comprising at least one lengthwise rib extending along the channel internal surface in the lengthwise direction and engaging at least two widthwise ribs.
  • 5. The golf club head of claim 2, further comprising a crown insert formed from a different material than the rest of the club head body.
  • 6. The golf club head according to claim 5, wherein the lengthwise direction of the channel is curved.
  • 7. The golf club head of claim 5, wherein at least a portion of the crown is non-metallic and the crown has an average thickness between about 0.6 mm and about 1.0 mm.
  • 8. The golf club head of claim 5, further comprising an adjustable head-shaft connection assembly that is operable to adjust at least one of the loft angle or lie angle of a golf club formed when the golf club head is attached to a golf club shaft via the head-shaft connection assembly.
  • 9. The golf club head of claim 5, wherein the channel has a volume between 15 cc and 40 cc.
  • 10. The golf club head of claim 5, wherein the golf club head has a mass moment of inertia about the CG z-axis, Izz, greater than 360 kg-mm2.
  • 11. The golf club head of claim 5, wherein the golf club head has an above ground center-of-gravity location Zup measured in mm; wherein the golf club head has a moment of inertia about the center-of-gravity z-axis Izz measured in kg-mm2 greater than 360 kg-mm2;wherein the golf club head has a moment of inertia about the center-of-gravity x-axis Ixx measured in kg-mm2; andwherein Izz and Ixx are related to the above ground center-of-gravity location Zup by the equation Ixx+Izz≥20·Zup+165.
  • 12. The golf club head according to claim 5, wherein a coefficient of restitution of the golf club head measured at the center of the face is 0.80 or greater;wherein a mass of the golf club head is between about 185 grams and about 245 grams;wherein a maximum dimension from a forward portion to a rearward portion of the golf club head is greater than about 75 mm;wherein the golf club head has a mass moment of inertia about the CG z-axis, Izz, greater than 360 kg-mm2.
  • 13. The golf club head according to claim 12, wherein the crown insert has a central raised section.
  • 14. The golf club head according to claim 1, further comprising at least one lengthwise rib extending along the channel internal surface in the lengthwise direction.
  • 15. The golf club head according to claim 1, wherein the at least one widthwise rib extends across the channel internal surface and engages at least one internal surface of the sole.
  • 16. The golf club head according to claim 1, further comprising at least one lengthwise rib extending along the channel internal surface in the lengthwise direction and engaging the at least one widthwise rib.
  • 17. The golf club head of claim 1, wherein at least one of the one or more body tuning element connecting elements is angled.
  • 18. The golf club head of claim 1, wherein the channel has a volume that is at least 5% of the club head volume.
  • 19. The golf club head of claim 1, wherein the two or more positions include a toe-ward position and a heel-ward position such that the at least one weight is movable between an engagement position in a toe portion of the sole and an engagement position in a heel portion of the sole.
  • 20. The golf club head of claim 1, further comprising: a body tuning element sole portion in contact with the sole and extending in a substantially heel-to-toe direction; anda body tuning element crown portion in contact with the crown and connected to a body tuning element sole portion at both the heel portion and the toe portion;wherein the body tuning element sole portion and the body tuning element crown portion engage at least one of the one or more body tuning element connecting elements connecting the crown to the sole.
  • 21. The golf club head of claim 1, wherein the golf club head has an above ground center-of-gravity location Zup measured in mm; wherein the golf club head has a moment of inertia about the center-of-gravity z-axis Izz measured in kg-mm2;wherein the golf club head has a moment of inertia about the center-of-gravity x-axis Ixx measured in kg-mm2; andwherein Izz and Ixx are related to the above ground center-of-gravity location Zup by the equation Ixx+Izz≥20·Zup+165.
  • 22. A golf club head comprising: a club head body having a crown, a sole, a heel, a toe, a striking face, and a rear portion opposite the striking face, with the club head body defining an interior cavity;one or more body tuning element connecting elements positioned within the interior cavity toeward of a geometric center of the striking face and connecting the crown to the sole, the one or more body tuning element connecting elements each having a first end attached to a first internal surface and a second end attached to a second internal surface, and an intermediate portion spanning across the interior cavity from the first end to the second end;wherein the intermediate portion does not contact any portion of the crown or the sole and the one or more body tuning element connecting elements do not contact the rear portion of the club head body;wherein the one or more body tuning element connecting elements are permanently secured to the club head body;at least one weight configured to engage the sole at two or more positions;a channel positioned in the sole portion of the club head;a crown insert formed from a different material than the rest of the club head body;wherein the channel extends in a substantially heel-to-toe lengthwise direction and has a channel internal surface located within the interior cavity of the club head body, and at least two widthwise ribs extending across the channel internal surface in a widthwise direction and spaced apart in the lengthwise direction, wherein the widthwise direction is substantially transverse to the lengthwise direction of the channel;wherein at least one of the widthwise ribs extends across the channel internal surface and engages at least one internal surface of the sole;at least one lengthwise rib extending along the channel internal surface in the lengthwise direction and engaging the at least two widthwise ribs;wherein the golf club head has a mass moment of inertia about the CG z-axis Izz greater than 360 kg-mm2; andwherein the golf club head has a CG with a head origin x-axis (CGx) coordinate between about −2 mm and about 6 mm and a head origin y-axis (CGy) coordinate between about 15 mm and about 40 mm, and a head origin z-axis (CGz) less than 0 mm.
CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation of U.S. patent application Ser. No. 14/939,648, filed Nov. 12, 2015, which is a continuation-in-part of U.S. patent application Ser. No. 14/871,789, filed Sep. 30, 2015, now U.S. Pat. No. 9,700,763, issued Jul. 11, 2017, which is a continuation of U.S. patent application Ser. No. 14/701,476, filed Apr. 30, 2015, now U.S. Pat. No. 9,211,447, issued Dec. 15, 2015, which is a continuation of U.S. patent application Ser. No. 14/495,795, filed Sep. 24, 2014, now U.S. Pat. No. 9,186,560, issued Nov. 17, 2015, which is a continuation of U.S. patent application Ser. No. 13/828,675, filed Mar. 14, 2013, now U.S. Pat. No. 8,888,607, issued Nov. 18, 2014, which is a continuation-in-part of U.S. patent application Ser. No. 13/469,031, filed May 10, 2012, now U.S. Pat. No. 9,220,953, issued Dec. 29, 2015, which is a continuation-in-part of U.S. patent application Ser. No. 13/338,197, filed Dec. 27, 2011, now U.S. Pat. No. 8,900,069, issued Dec. 2, 2014, which claims the benefit of U.S. Provisional Patent Application No. 61/427,772, filed Dec. 28, 2010, all of which applications are incorporated by reference herein in their entireties.

US Referenced Citations (681)
Number Name Date Kind
411000 Anderson Sep 1889 A
1133129 Govan Mar 1915 A
1135621 Roberts et al. Apr 1915 A
1320163 Fitz Maurice Oct 1919 A
1518316 Ellingham Dec 1924 A
1526438 Scott Feb 1925 A
1538312 Beat May 1925 A
1592463 Marker Jul 1926 A
1658581 Tobia Feb 1928 A
1697846 Anderson Jan 1929 A
1704119 Buhrke Mar 1929 A
1705997 Quynn Mar 1929 A
1854548 Hunt Apr 1932 A
1970409 Wiedemann Aug 1934 A
D107007 Cashmore Nov 1937 S
2214356 Wettlaufer Sep 1940 A
2225930 Sexton Dec 1940 A
2257575 Reach Sep 1941 A
2328583 Reach Sep 1943 A
2360364 Reach Oct 1944 A
2375249 Richer May 1945 A
2460435 Schaffer Feb 1949 A
2652256 Thomas Sep 1953 A
2681523 Sellers Jun 1954 A
2691525 Callaghan Oct 1954 A
3064980 Steiner Nov 1962 A
3084940 Cissel Apr 1963 A
3466047 Rodia et al. Sep 1969 A
3486755 Hodge Dec 1969 A
3556533 Hollis Jan 1971 A
3589731 Chancellor Jun 1971 A
3606327 Gorman Sep 1971 A
3610630 Glover Oct 1971 A
3652094 Glover Mar 1972 A
3672419 Fischer Jun 1972 A
3680868 Jacob Aug 1972 A
3692306 Glover Sep 1972 A
3743297 Dennis Jul 1973 A
3810631 Braly May 1974 A
3860244 Cosby Jan 1975 A
3897066 Belmont Jul 1975 A
3976299 Lawrence et al. Aug 1976 A
3979122 Belmont Sep 1976 A
3979123 Belmont Sep 1976 A
3997170 Goldberg Dec 1976 A
4008896 Gordos Feb 1977 A
4043563 Churchward Aug 1977 A
4052075 Daly Oct 1977 A
4076254 Nygren Feb 1978 A
4085934 Churchward Apr 1978 A
4121832 Ebbing Oct 1978 A
4150702 Holmes Apr 1979 A
4189976 Becker Feb 1980 A
4214754 Zebelean Jul 1980 A
4262562 MacNeill Apr 1981 A
D259698 MacNeill Jun 1981 S
4322083 Imai Mar 1982 A
4340229 Stuff, Jr. Jul 1982 A
4398965 Campau Aug 1983 A
4411430 Dian Oct 1983 A
4423874 Stuff, Jr. Jan 1984 A
4438931 Motomiya Mar 1984 A
4471961 Masghati et al. Sep 1984 A
4489945 Kobayashi Dec 1984 A
4530505 Stuff Jul 1985 A
D284346 Masters Jun 1986 S
4602787 Sugioka et al. Jul 1986 A
4607846 Perkins Aug 1986 A
4712798 Preato Dec 1987 A
4730830 Tilley Mar 1988 A
4736093 Braly Apr 1988 A
4754974 Kobayashi Jul 1988 A
4754977 Sahm Jul 1988 A
4762322 Molitor et al. Aug 1988 A
4795159 Nagamoto Jan 1989 A
4803023 Enomoto et al. Feb 1989 A
4809983 Langert Mar 1989 A
4867457 Lowe Sep 1989 A
4867458 Sumikawa et al. Sep 1989 A
4869507 Sahm Sep 1989 A
4890840 Kobayashi Jan 1990 A
4895371 Bushner Jan 1990 A
4915558 Muller Apr 1990 A
4962932 Anderson Oct 1990 A
4994515 Washiyama et al. Feb 1991 A
5006023 Kaplan Apr 1991 A
5020950 Ladouceur Jun 1991 A
5028049 McKeighen Jul 1991 A
5039267 Wollar Aug 1991 A
5042806 Helmstetter Aug 1991 A
5050879 Sun et al. Sep 1991 A
5058895 Igarashi Oct 1991 A
5067715 Schmidt et al. Nov 1991 A
5076585 Bouquet Dec 1991 A
5078400 Desbiolles et al. Jan 1992 A
5121922 Harsh, Sr. Jun 1992 A
5122020 Bedi Jun 1992 A
5193810 Antonious Mar 1993 A
5213328 Long et al. May 1993 A
5219408 Sun Jun 1993 A
5221086 Antonious Jun 1993 A
5232224 Zeider Aug 1993 A
5244210 Au Sep 1993 A
5251901 Solheim et al. Oct 1993 A
5253869 Dingle et al. Oct 1993 A
D343558 Latraverse et al. Jan 1994 S
5297794 Lu Mar 1994 A
5301941 Allen Apr 1994 A
5306008 Kinoshita Apr 1994 A
5316305 McCabe May 1994 A
5320005 Hsiao Jun 1994 A
5328176 Lo Jul 1994 A
5330187 Schmidt et al. Jul 1994 A
5346216 Aizawa Sep 1994 A
5346217 Tsuchiya et al. Sep 1994 A
5385348 Wargo Jan 1995 A
5395113 Antonious Mar 1995 A
5410798 Lo May 1995 A
5419556 Take May 1995 A
5421577 Kobayashi Jun 1995 A
5429365 McKeighen Jul 1995 A
5439222 Kranenberg Aug 1995 A
5441274 Clay Aug 1995 A
5447309 Vincent Sep 1995 A
5449260 Whittle Sep 1995 A
5451056 Manning Sep 1995 A
5467983 Chen Nov 1995 A
D365615 Shimatani Dec 1995 S
5472201 Aizawa et al. Dec 1995 A
5472203 Schmidt et al. Dec 1995 A
5480152 Schmidt et al. Jan 1996 A
5511786 Antonious Apr 1996 A
5518243 Redman May 1996 A
5533730 Ruvang Jul 1996 A
5538245 Moore Jul 1996 A
5564705 Kobayashi et al. Oct 1996 A
5571053 Lane Nov 1996 A
5573467 Chou et al. Nov 1996 A
5582553 Ashcraft et al. Dec 1996 A
5603668 Antonious Feb 1997 A
5613917 Kobayashi et al. Mar 1997 A
5616088 Aizawa et al. Apr 1997 A
5620379 Borys Apr 1997 A
5624331 Lo et al. Apr 1997 A
5629475 Chastonay May 1997 A
5632694 Lee May 1997 A
5658206 Antonious Aug 1997 A
5669827 Nagamoto Sep 1997 A
5681228 Mikame et al. Oct 1997 A
5683309 Reimers Nov 1997 A
5688189 Bland Nov 1997 A
5709613 Sheraw Jan 1998 A
5718641 Lin Feb 1998 A
5720674 Galy Feb 1998 A
D392526 Nicely Mar 1998 S
5735754 Antonious Apr 1998 A
5746664 Reynolds, Jr. May 1998 A
5749795 Schmidt May 1998 A
5755627 Yamazaki et al. May 1998 A
5762567 Antonious Jun 1998 A
5766095 Antonious Jun 1998 A
5769737 Holladay et al. Jun 1998 A
5776010 Helmstetter et al. Jul 1998 A
5776011 Su et al. Jul 1998 A
5788587 Tseng Aug 1998 A
5798587 Lee Aug 1998 A
5803829 Hayashi Sep 1998 A
RE35955 Lu Nov 1998 E
5851160 Rugge et al. Dec 1998 A
5873791 Allen Feb 1999 A
5888148 Allen Mar 1999 A
D409463 McMullin May 1999 S
5908356 Nagamoto Jun 1999 A
5911638 Parente et al. Jun 1999 A
5913735 Kenmi Jun 1999 A
5916042 Reimers Jun 1999 A
5924938 Hines Jul 1999 A
D412547 Fong Aug 1999 S
5935019 Yamamoto Aug 1999 A
5935020 Stites et al. Aug 1999 A
5941782 Cook Aug 1999 A
5947840 Ryan Sep 1999 A
5967905 Nakahara et al. Oct 1999 A
5971867 Galy Oct 1999 A
5976033 Takeda Nov 1999 A
5997415 Wood Dec 1999 A
6015354 Ahn et al. Jan 2000 A
6017177 Lanham Jan 2000 A
6019686 Gray Feb 2000 A
6023891 Robertson et al. Feb 2000 A
6032677 Blechman et al. Mar 2000 A
6033318 Drajan, Jr. et al. Mar 2000 A
6033321 Yamamoto Mar 2000 A
6042486 Gallagher Mar 2000 A
6056649 Imai May 2000 A
6062988 Yamamoto May 2000 A
6074308 Domas Jun 2000 A
6077171 Yoneyama Jun 2000 A
6086485 Hamada Jul 2000 A
6089994 Sun Jul 2000 A
6120384 Drake Sep 2000 A
6123627 Antonious Sep 2000 A
6139445 Werner et al. Oct 2000 A
6149533 Finn Nov 2000 A
6162132 Yoneyama Dec 2000 A
6162133 Peterson Dec 2000 A
6171204 Starry Jan 2001 B1
6186905 Kosmatka Feb 2001 B1
6190267 Marlowe et al. Feb 2001 B1
6193614 Sasamoto et al. Feb 2001 B1
6203448 Yamamoto Mar 2001 B1
6206789 Takeda Mar 2001 B1
6206790 Kubica et al. Mar 2001 B1
6210290 Erickson et al. Apr 2001 B1
6217461 Galy Apr 2001 B1
6238303 Fite May 2001 B1
6244974 Hanberry, Jr. Jun 2001 B1
6248025 Murphy et al. Jun 2001 B1
6254494 Hasebe et al. Jul 2001 B1
6264414 Hartmann et al. Jul 2001 B1
6270422 Fisher Aug 2001 B1
6277032 Smith Aug 2001 B1
6290609 Takeda Sep 2001 B1
6296579 Robinson Oct 2001 B1
6299546 Wang Oct 2001 B1
6299547 Kosmatka Oct 2001 B1
6306048 McCabe et al. Oct 2001 B1
6319149 Lee Nov 2001 B1
6319150 Werner et al. Nov 2001 B1
6334817 Ezawa et al. Jan 2002 B1
6338683 Kosmatka Jan 2002 B1
6340337 Hasebe et al. Jan 2002 B2
6344000 Hamada Feb 2002 B1
6344001 Hamada et al. Feb 2002 B1
6344002 Kajita Feb 2002 B1
6348012 Erickson et al. Feb 2002 B1
6348013 Kosmatka Feb 2002 B1
6348014 Chiu Feb 2002 B1
6354961 Allen Mar 2002 B1
6364788 Helmstetter et al. Apr 2002 B1
6379264 Forzano Apr 2002 B1
6379265 Hirakawa et al. Apr 2002 B1
6383090 O'Doherty et al. May 2002 B1
6386987 Lejeune, Jr. May 2002 B1
6386990 Reyes et al. May 2002 B1
6390933 Galloway et al. May 2002 B1
6409612 Evans et al. Jun 2002 B1
6422951 Burrows Jul 2002 B1
6425832 Cackett et al. Jul 2002 B2
6434811 Helmstetter et al. Aug 2002 B1
6436142 Paes et al. Aug 2002 B1
6440009 Guibaud et al. Aug 2002 B1
6440010 Deshmukh Aug 2002 B1
6443851 Liberatore Sep 2002 B1
6447405 Chen Sep 2002 B1
6458044 Vincent et al. Oct 2002 B1
6461249 Liberatore Oct 2002 B2
6471604 Hocknell et al. Oct 2002 B2
6475101 Burrows Nov 2002 B2
6475102 Helmstetter et al. Nov 2002 B2
6478692 Kosmatka Nov 2002 B2
6491592 Cackett et al. Dec 2002 B2
6508978 Deshmukh Jan 2003 B1
6514154 Finn Feb 2003 B1
6524197 Boone Feb 2003 B2
6524198 Takeda Feb 2003 B2
6527649 Neher et al. Mar 2003 B1
6530847 Antonious Mar 2003 B1
6530848 Gillig Mar 2003 B2
6533679 McCabe et al. Mar 2003 B1
6547676 Cackett et al. Apr 2003 B2
6558273 Kobayashi et al. May 2003 B2
6565448 Cameron et al. May 2003 B2
6565452 Helmstetter et al. May 2003 B2
6569029 Hamburger May 2003 B1
6569040 Bradstock May 2003 B2
6572489 Miyamoto et al. Jun 2003 B2
6575845 Galloway et al. Jun 2003 B2
6575854 Yang et al. Jun 2003 B1
6582323 Soracco et al. Jun 2003 B2
6592468 Vincent et al. Jul 2003 B2
6602149 Jacobson Aug 2003 B1
6604568 Bliss et al. Aug 2003 B2
6605007 Bissonnette et al. Aug 2003 B1
6607452 Helmstetter et al. Aug 2003 B2
6612938 Murphy et al. Sep 2003 B2
6616547 Vincent et al. Sep 2003 B2
6638180 Tsurumaki Oct 2003 B2
6638183 Takeda Oct 2003 B2
D482089 Burrows Nov 2003 S
D482090 Burrows Nov 2003 S
D482420 Burrows Nov 2003 S
6641487 Hamburger Nov 2003 B1
6641490 Ellemor Nov 2003 B2
6648772 Vincent et al. Nov 2003 B2
6648773 Evans Nov 2003 B1
6652387 Liberatore Nov 2003 B2
D484208 Burrows Dec 2003 S
6663506 Nishimoto et al. Dec 2003 B2
6669571 Cameron et al. Dec 2003 B1
6669578 Evans Dec 2003 B1
6669580 Cackett et al. Dec 2003 B1
6676536 Jacobson Jan 2004 B1
6679786 McCabe Jan 2004 B2
6695712 Iwata et al. Feb 2004 B1
6716111 Liberatore Apr 2004 B2
6716114 Nishio Apr 2004 B2
6719510 Cobzaru Apr 2004 B2
6719641 Dabbs et al. Apr 2004 B2
6739982 Murphy et al. May 2004 B2
6739983 Helmstetter et al. May 2004 B2
6743118 Soracco Jun 2004 B1
6749523 Forzano Jun 2004 B1
6757572 Forest Jun 2004 B1
6758763 Murphy et al. Jul 2004 B2
6773360 Willett et al. Aug 2004 B2
6773361 Lee Aug 2004 B1
6776726 Sano Aug 2004 B2
6800038 Willett et al. Oct 2004 B2
6805643 Lin Oct 2004 B1
6808460 Namiki Oct 2004 B2
6824475 Burnett et al. Nov 2004 B2
6835145 Tsurumaki Dec 2004 B2
D501036 Burrows Jan 2005 S
6855068 Antonious Feb 2005 B2
6860818 Mahaffey et al. Mar 2005 B2
6860823 Lee Mar 2005 B2
6860824 Evans Mar 2005 B2
6875124 Gilbert et al. Apr 2005 B2
6875129 Erickson et al. Apr 2005 B2
6881158 Yang et al. Apr 2005 B2
6881159 Galloway et al. Apr 2005 B2
6887165 Tsurumaki May 2005 B2
6890267 Mahaffey et al. May 2005 B2
6904663 Willett et al. Jun 2005 B2
6923734 Meyer Aug 2005 B2
6926619 Helmstetter et al. Aug 2005 B2
6960142 Bissonnette et al. Nov 2005 B2
6964617 Williams Nov 2005 B2
6969326 De Shiell Nov 2005 B2
6974393 Caldwell et al. Dec 2005 B2
6988960 Mahaffey et al. Jan 2006 B2
6991558 Beach et al. Jan 2006 B2
D515165 Zimmerman et al. Feb 2006 S
6997820 Willett et al. Feb 2006 B2
7004852 Billings Feb 2006 B2
7025692 Erickson et al. Apr 2006 B2
7029403 Rice et al. Apr 2006 B2
7077762 Kouno et al. Jul 2006 B2
7086964 Chen et al. Aug 2006 B2
7134971 Franklin et al. Nov 2006 B2
7137905 Kohno Nov 2006 B2
7137906 Tsunoda et al. Nov 2006 B2
7140974 Chao et al. Nov 2006 B2
7147572 Kohno Dec 2006 B2
7147573 DiMarco Dec 2006 B2
7153220 Lo Dec 2006 B2
7163468 Gibbs et al. Jan 2007 B2
7166038 Williams et al. Jan 2007 B2
7166040 Hoffman et al. Jan 2007 B2
7166041 Evans Jan 2007 B2
7169060 Stevens et al. Jan 2007 B2
7179034 Ladouceur Feb 2007 B2
7186190 Beach et al. Mar 2007 B1
7189169 Billings Mar 2007 B2
7198575 Beach et al. Apr 2007 B2
7201669 Stites et al. Apr 2007 B2
7223180 Willett et al. May 2007 B2
7252600 Murphy et al. Aug 2007 B2
7255654 Murphy et al. Aug 2007 B2
7267620 Chao et al. Sep 2007 B2
7273423 Imamoto Sep 2007 B2
7278926 Frame Oct 2007 B2
7278927 Gibbs et al. Oct 2007 B2
7294064 Tsurumaki et al. Nov 2007 B2
7294065 Liang et al. Nov 2007 B2
7351161 Beach Apr 2008 B2
7377860 Breier et al. May 2008 B2
7396293 Soracco Jul 2008 B2
7407447 Beach et al. Aug 2008 B2
7419441 Hoffman et al. Sep 2008 B2
7445563 Werner Nov 2008 B1
7448963 Beach et al. Nov 2008 B2
D588223 Kuan Mar 2009 S
7500924 Yokota Mar 2009 B2
7520820 Dimarco Apr 2009 B2
7530901 Imamoto et al. May 2009 B2
7530903 Imamoto et al. May 2009 B2
7530904 Beach et al. May 2009 B2
7540811 Beach et al. Jun 2009 B2
7563175 Nishitani et al. Jul 2009 B2
7568985 Beach et al. Aug 2009 B2
7572193 Yokota Aug 2009 B2
7578753 Beach et al. Aug 2009 B2
7582024 Shear Sep 2009 B2
7585233 Horacek Sep 2009 B2
7591737 Gibbs et al. Sep 2009 B2
7591738 Beach et al. Sep 2009 B2
7621823 Beach et al. Nov 2009 B2
7628707 Beach et al. Dec 2009 B2
7632193 Thielen Dec 2009 B2
7632194 Beach et al. Dec 2009 B2
7632196 Reed et al. Dec 2009 B2
7641569 Best et al. Jan 2010 B2
D612440 Oldknow Mar 2010 S
7670235 Lo Mar 2010 B2
7674189 Beach et al. Mar 2010 B2
7682264 Hsu et al. Mar 2010 B2
7717803 DiMarco May 2010 B2
7744484 Chao Jun 2010 B1
7749101 Imamoto et al. Jul 2010 B2
7753806 Beach et al. Jul 2010 B2
7758451 Liang et al. Jul 2010 B2
7771291 Willett et al. Aug 2010 B1
7798914 Noble Sep 2010 B2
7824277 Bennett et al. Nov 2010 B2
7857711 Shear Dec 2010 B2
7857713 Yokota Dec 2010 B2
7867105 Moon Jan 2011 B2
7887431 Beach et al. Feb 2011 B2
7887434 Beach et al. Feb 2011 B2
7896753 Boyd et al. Mar 2011 B2
7914393 Hirsch Mar 2011 B2
7946931 Oyama May 2011 B2
7988565 Abe Aug 2011 B2
8012038 Beach et al. Sep 2011 B1
8012039 Greaney et al. Sep 2011 B2
8016694 Llewellyn et al. Sep 2011 B2
8025587 Beach et al. Sep 2011 B2
8083609 Burnett et al. Dec 2011 B2
8088021 Albertsen et al. Jan 2012 B2
8105175 Breier et al. Jan 2012 B2
8118689 Beach et al. Feb 2012 B2
8147350 Beach et al. Apr 2012 B2
8157672 Greaney et al. Apr 2012 B2
8167737 Oyama May 2012 B2
8177661 Beach et al. May 2012 B2
8182364 Cole et al. May 2012 B2
8197358 Watson Jun 2012 B1
8206244 Honea et al. Jun 2012 B2
8235831 Beach et al. Aug 2012 B2
8235841 Stites et al. Aug 2012 B2
8235844 Albertsen et al. Aug 2012 B2
8241143 Albertsen et al. Aug 2012 B2
8241144 Albertsen et al. Aug 2012 B2
8257195 Erickson Sep 2012 B1
8257196 Abbott et al. Sep 2012 B1
8262498 Beach et al. Sep 2012 B2
8277337 Shimazaki Oct 2012 B2
8292756 Greaney et al. Oct 2012 B2
8303431 Beach et al. Nov 2012 B2
8328659 Shear Dec 2012 B2
8337319 Sargent et al. Dec 2012 B2
8353786 Beach et al. Jan 2013 B2
D675692 Oldknow et al. Feb 2013 S
D678964 Oldknow et al. Mar 2013 S
D678965 Oldknow et al. Mar 2013 S
D678968 Oldknow et al. Mar 2013 S
D678969 Oldknow et al. Mar 2013 S
D678970 Oldknow et al. Mar 2013 S
D678971 Oldknow et al. Mar 2013 S
D678972 Oldknow et al. Mar 2013 S
D678973 Oldknow et al. Mar 2013 S
8398503 Beach et al. Mar 2013 B2
8403771 Rice et al. Mar 2013 B1
D679354 Oldknow et al. Apr 2013 S
8430763 Beach et al. Apr 2013 B2
8435134 Tang et al. May 2013 B2
8496541 Beach et al. Jul 2013 B2
8496544 Curtis et al. Jul 2013 B2
8517855 Beach et al. Aug 2013 B2
8517860 Albertsen et al. Aug 2013 B2
8529368 Rice et al. Sep 2013 B2
8562453 Sato Oct 2013 B2
8579728 Morales et al. Nov 2013 B2
8591351 Albertsen et al. Nov 2013 B2
8602907 Beach et al. Dec 2013 B2
8616999 Greaney et al. Dec 2013 B2
D697152 Harbert et al. Jan 2014 S
8622847 Beach et al. Jan 2014 B2
8628433 Stites et al. Jan 2014 B2
8632419 Tang et al. Jan 2014 B2
8641555 Stites et al. Feb 2014 B2
8663029 Beach et al. Mar 2014 B2
8678949 Shimazaki Mar 2014 B2
8690704 Thomas Apr 2014 B2
8695487 Sakane et al. Apr 2014 B2
8696487 Beach et al. Apr 2014 B2
8696491 Myers Apr 2014 B1
8702531 Boyd et al. Apr 2014 B2
8721471 Albertsen et al. May 2014 B2
8727900 Beach et al. May 2014 B2
D707768 Oldknow et al. Jun 2014 S
D707769 Oldknow et al. Jun 2014 S
D707773 Oldknow et al. Jun 2014 S
8753222 Beach et al. Jun 2014 B2
8753226 Rice et al. Jun 2014 B2
8758153 Sargent et al. Jun 2014 B2
D708281 Oldknow et al. Jul 2014 S
8790195 Myers et al. Jul 2014 B1
8821312 Burnett et al. Sep 2014 B2
8827831 Burnett et al. Sep 2014 B2
8834289 de la Cruz et al. Sep 2014 B2
8834290 Bezilla et al. Sep 2014 B2
8834293 Thomas Sep 2014 B2
8845450 Beach et al. Sep 2014 B2
8845454 Boyd et al. Sep 2014 B2
D714893 Atwell Oct 2014 S
8876622 Beach et al. Nov 2014 B2
8876627 Beach et al. Nov 2014 B2
8888607 Beach et al. Nov 2014 B2
8900069 Beach et al. Dec 2014 B2
D722122 Greensmith Feb 2015 S
8956240 Beach et al. Feb 2015 B2
8956244 Westrum Feb 2015 B1
8986133 Bennett et al. Mar 2015 B2
9033821 Beach et al. May 2015 B2
9101811 Goudarzi Aug 2015 B1
9180348 Beach Nov 2015 B2
9180349 Seluga et al. Nov 2015 B1
9186560 Harbert Nov 2015 B2
9205312 Zimmerman et al. Dec 2015 B2
9211447 Harbert Dec 2015 B2
9220953 Beach Dec 2015 B2
9295885 Matsunaga et al. Mar 2016 B2
9403069 Boyd et al. Aug 2016 B2
9486677 Seluga Nov 2016 B1
9498688 Galvan Nov 2016 B2
9597558 Seluga Mar 2017 B1
9597561 Seluga Mar 2017 B1
9623291 Greensmith Apr 2017 B2
9636552 Cleghorn May 2017 B2
9662545 Beach et al. May 2017 B2
9687701 Seluga Jun 2017 B1
9687702 Seluga Jun 2017 B1
9694257 Seluga Jul 2017 B1
9700763 Harbert Jul 2017 B2
9700769 Beach et al. Jul 2017 B2
9707457 Mata Jul 2017 B2
9717962 Seluga Aug 2017 B1
9776058 Seluga Oct 2017 B2
9795840 Greensmith Oct 2017 B2
9814954 Westrum Nov 2017 B2
9855476 Seluga Jan 2018 B2
9901794 Beno Feb 2018 B2
9908017 Seluga Mar 2018 B2
9914030 Cleghorn Mar 2018 B2
9931549 Seluga Apr 2018 B1
10076688 Harbert et al. Sep 2018 B1
10183202 Harbert et al. Jan 2019 B1
20010049310 Cheng et al. Dec 2001 A1
20020022535 Takeda Feb 2002 A1
20020025861 Ezawa Feb 2002 A1
20020032075 Vatsvog Mar 2002 A1
20020055396 Nishimoto et al. May 2002 A1
20020072434 Yabu Jun 2002 A1
20020123394 Tsurumaki Sep 2002 A1
20020137576 Dammen Sep 2002 A1
20020160854 Beach et al. Oct 2002 A1
20020169036 Boone Nov 2002 A1
20020183134 Allen et al. Dec 2002 A1
20030013545 Vincent et al. Jan 2003 A1
20030032500 Nakahara et al. Feb 2003 A1
20030036442 Chao et al. Feb 2003 A1
20030130059 Billings Jul 2003 A1
20040023729 Nagai et al. Feb 2004 A1
20040087388 Beach et al. May 2004 A1
20040121852 Tsurumaki Jun 2004 A1
20040157678 Kohno Aug 2004 A1
20040176180 Yamaguchi et al. Sep 2004 A1
20040176183 Tsurumaki Sep 2004 A1
20040180730 Franklin et al. Sep 2004 A1
20040192463 Tsurumaki et al. Sep 2004 A1
20040235584 Chao et al. Nov 2004 A1
20040242343 Chao Dec 2004 A1
20050049075 Chen et al. Mar 2005 A1
20050070371 Chen et al. Mar 2005 A1
20050096151 Hou et al. May 2005 A1
20050101404 Long et al. May 2005 A1
20050124435 Gambetta et al. Jun 2005 A1
20050137024 Stites et al. Jun 2005 A1
20050181884 Beach et al. Aug 2005 A1
20050227781 Huang et al. Oct 2005 A1
20050239575 Chao et al. Oct 2005 A1
20050239576 Stites et al. Oct 2005 A1
20050266933 Galloway Dec 2005 A1
20060035722 Beach et al. Feb 2006 A1
20060058112 Haralason et al. Mar 2006 A1
20060073910 Imamoto et al. Apr 2006 A1
20060084525 Imamoto et al. Apr 2006 A1
20060122004 Chen et al. Jun 2006 A1
20060154747 Beach et al. Jul 2006 A1
20060172821 Evans Aug 2006 A1
20060189407 Soracco Aug 2006 A1
20060240908 Adams et al. Oct 2006 A1
20070021234 Tsurumaki et al. Jan 2007 A1
20070026961 Hou Feb 2007 A1
20070049400 Imamoto et al. Mar 2007 A1
20070049415 Shear Mar 2007 A1
20070049417 Shear Mar 2007 A1
20070105646 Beach et al. May 2007 A1
20070105647 Beach et al. May 2007 A1
20070105648 Beach et al. May 2007 A1
20070105649 Beach et al. May 2007 A1
20070105650 Beach et al. May 2007 A1
20070105651 Beach et al. May 2007 A1
20070105652 Beach et al. May 2007 A1
20070105653 Beach et al. May 2007 A1
20070105654 Beach et al. May 2007 A1
20070105655 Beach et al. May 2007 A1
20070117648 Yokota May 2007 A1
20070117652 Beach et al. May 2007 A1
20080020861 Adams et al. Jan 2008 A1
20080146370 Beach et al. Jun 2008 A1
20080161127 Yamamoto Jul 2008 A1
20080261715 Carter Oct 2008 A1
20080261717 Hoffman et al. Oct 2008 A1
20080280698 Hoffman et al. Nov 2008 A1
20090062029 Stites et al. Mar 2009 A1
20090088269 Beach et al. Apr 2009 A1
20090088271 Beach et al. Apr 2009 A1
20090137338 Kajita May 2009 A1
20090170632 Beach et al. Jul 2009 A1
20090264214 De La Cruz et al. Oct 2009 A1
20090286611 Beach et al. Nov 2009 A1
20090286618 Beach et al. Nov 2009 A1
20090318245 Yim et al. Dec 2009 A1
20100016095 Burnett et al. Jan 2010 A1
20100029404 Shear Feb 2010 A1
20100029408 Abe Feb 2010 A1
20100035701 Kusumoto Feb 2010 A1
20100048316 Honea et al. Feb 2010 A1
20100048321 Beach et al. Feb 2010 A1
20100075774 Ban Mar 2010 A1
20100113176 Boyd et al. May 2010 A1
20100144461 Ban Jun 2010 A1
20100167837 Ban Jul 2010 A1
20100197423 Thomas et al. Aug 2010 A1
20100197426 De La Cruz et al. Aug 2010 A1
20100234127 Snyder et al. Sep 2010 A1
20100331103 Takahashi et al. Dec 2010 A1
20110021284 Stites et al. Jan 2011 A1
20110098127 Yamamoto Apr 2011 A1
20110151989 Golden et al. Jun 2011 A1
20110151997 Shear Jun 2011 A1
20110195798 Sander et al. Aug 2011 A1
20110218053 Tang et al. Sep 2011 A1
20110294599 Albertsen et al. Dec 2011 A1
20120083362 Albertsen et al. Apr 2012 A1
20120083363 Albertsen et al. Apr 2012 A1
20120122601 Beach et al. May 2012 A1
20120142447 Boyd et al. Jun 2012 A1
20120142452 Burnett et al. Jun 2012 A1
20120149491 Beach et al. Jun 2012 A1
20120165110 Cheng Jun 2012 A1
20120165111 Cheng Jun 2012 A1
20120196701 Stites et al. Aug 2012 A1
20120202615 Beach et al. Aug 2012 A1
20120220387 Beach et al. Aug 2012 A1
20120244960 Tang et al. Sep 2012 A1
20120270676 Burnett et al. Oct 2012 A1
20120277029 Albertsen et al. Nov 2012 A1
20120277030 Albertsen et al. Nov 2012 A1
20120289361 Beach et al. Nov 2012 A1
20120302366 Murphy Nov 2012 A1
20130065705 Morales et al. Mar 2013 A1
20130102410 Stites et al. Apr 2013 A1
20130165254 Rice et al. Jun 2013 A1
20130210542 Harbert et al. Aug 2013 A1
20130324284 Stites et al. Dec 2013 A1
20140080629 Sargent et al. Mar 2014 A1
20150011328 Harbert et al. Jan 2015 A1
20150065265 Motokawa et al. Mar 2015 A1
20150105177 Beach et al. Apr 2015 A1
20150217167 Frame et al. Aug 2015 A1
20150231453 Harbert et al. Aug 2015 A1
20150297961 Voshall Oct 2015 A1
20150306475 Curtis et al. Oct 2015 A1
20160023060 Harbert et al. Jan 2016 A1
20160250525 Motokawa et al. Sep 2016 A1
20160271464 Murphy et al. Sep 2016 A1
Foreign Referenced Citations (67)
Number Date Country
2436182 Jun 2001 CN
201353407 Dec 2009 CN
9012884 Sep 1990 DE
0470488 Mar 1995 EP
0617987 Nov 1997 EP
1001175 May 2000 EP
2377586 Oct 2011 EP
194823 Dec 1921 GB
57-157374 Oct 1982 JP
4180778 Jun 1992 JP
05-317465 Dec 1993 JP
06-126004 May 1994 JP
6190088 Jul 1994 JP
06-238022 Aug 1994 JP
6-304271 Nov 1994 JP
09-028844 Feb 1997 JP
03035480 Mar 1997 JP
09-308717 Dec 1997 JP
09-327534 Dec 1997 JP
10-234902 Aug 1998 JP
10-277187 Oct 1998 JP
11114102 Oct 1998 JP
2000014841 Jan 2000 JP
2000197718 Jul 2000 JP
2001054595 Feb 2001 JP
2001-129130 May 2001 JP
2001170225 Jun 2001 JP
2001204856 Jul 2001 JP
2001346918 Dec 2001 JP
2002003969 Jan 2002 JP
2002017910 Jan 2002 JP
2002052099 Feb 2002 JP
2002248183 Sep 2002 JP
2002253706 Sep 2002 JP
2003038691 Feb 2003 JP
2003093554 Apr 2003 JP
2003126311 May 2003 JP
2003226952 Aug 2003 JP
2004174224 Jun 2004 JP
2004183058 Jul 2004 JP
2004222911 Aug 2004 JP
2004-261451 Sep 2004 JP
2004267438 Sep 2004 JP
2004313762 Nov 2004 JP
2004351054 Dec 2004 JP
2004351173 Dec 2004 JP
2005028170 Feb 2005 JP
05-296582 Oct 2005 JP
2005-296458 Oct 2005 JP
05-323978 Nov 2005 JP
2006231063 Sep 2006 JP
2006-320493 Nov 2006 JP
2008515560 May 2008 JP
4128970 Jul 2008 JP
2008200118 Sep 2008 JP
2009000281 Jan 2009 JP
2010279847 Dec 2010 JP
2011024999 Feb 2011 JP
WO8802642 Apr 1988 WO
WO1999020358 Apr 1999 WO
WO2001049376 Jul 2001 WO
WO0166199 Sep 2001 WO
WO02062501 Aug 2002 WO
WO03061773 Jul 2003 WO
WO2004043549 May 2004 WO
WO2006044631 Apr 2006 WO
WO2014070343 May 2014 WO
Non-Patent Literature Citations (21)
Entry
Adams Golf Speedline F11 Ti 14.5 degree fairway wood (www.bombsquadgolf.com, posted Oct. 18, 2010).
Callaway Golf, World's Straightest Driver: FT-i Driver downloaded from www.callawaygolf.com/ft%2Di/driver.aspx?lang=en on Apr. 5, 2007.
Declaration of Tim Reed, VP of R&D, Adams Golf, Inc., dated Dec. 7, 2012.
Jackson, Jeff, The Modern Guide to Golf Clubmaking, Ohio: Dynacraft Golf Products, Inc., copyright 1994, p. 237.
Nike Golf, Sasquatch 460, downloaded from www.nike.com/nikegolf/index.htm on Apr. 5, 2007.
Nike Golf, Sasquatch Sumo Squared Driver, downloaded from www.nike.com/nikegolf/index.htm on Apr. 5, 2007.
Office action from the Japanese Patent Office in Patent Application No. 2008-264880, dated Nov. 21, 2012.
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 12/781,727, dated Aug. 5, 2010.
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 13/338,197, dated Jun. 5, 2014.
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 13/401,690, dated May 23, 2012.
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 13/401,690, dated Feb. 6, 2013.
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 13/469,023, dated Jul. 31, 2012.
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 13/469,031, dated Oct. 9, 2014.
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 13/469,031, dated May 20, 2015.
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 13/975,106, dated Feb. 24, 2014.
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 13/828,675, dated Jun. 30, 2014.
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 14/495,795, dated Jun. 15, 2015.
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 14/701,476, dated Jun. 15, 2015.
Taylor Made Golf Company, Inc. Press Release, Burner Fairway Wood, www.tmag.com/media/pressreleases/2007/011807_burner_fairway_rescue.html, Jan. 26, 2007.
Taylor Made Golf Company Inc., R7 460 Drivers, downloaded from www.taylormadegolf.com/product_detail.asp?pID=14section=overview on Apr. 5, 2007.
Titleist 907D1, downloaded from www.tees2greens.com/forum/Uploads/Images/7ade3521-192b-4611-870b-395d.jpg on Feb. 1, 2007.
Related Publications (1)
Number Date Country
20170304693 A1 Oct 2017 US
Provisional Applications (1)
Number Date Country
61427772 Dec 2010 US
Continuations (4)
Number Date Country
Parent 14939648 Nov 2015 US
Child 15645587 US
Parent 14701476 Apr 2015 US
Child 14871789 US
Parent 14495795 Sep 2014 US
Child 14701476 US
Parent 13828675 Mar 2013 US
Child 14495795 US
Continuation in Parts (3)
Number Date Country
Parent 14871789 Sep 2015 US
Child 14939648 US
Parent 13469031 May 2012 US
Child 13828675 US
Parent 13338197 Dec 2011 US
Child 13469031 US