The present application concerns golf clubs and golf club heads, and more particularly, golf clubs and golf club heads that incorporate features to provide increased forgiveness for off-center hits, reduced weight and/or increased head speed during a swing, among other advantages. Unique combinations of moments of inertia, inverted cone technology, club head face characteristics and golf club component characteristics are described.
Golf club head manufacturers and designers are constantly looking for ways to improve golf club head performance, which includes the forgiveness of the golf club head, while having an aesthetic appearance. Generally, “forgiveness” can be defined as the ability of a golf club head to reduce the effects of mishits, i.e., hits resulting from striking the golf ball at a less than an ideal impact location on the golf club head, on the shot shape and distance of a golf ball struck the by club.
Golf club head performance can be directly affected by the moments of inertia of the club head. A moment of inertia is the measure of a club head's resistance to twisting about the golf club head's center of gravity upon impact with a golf ball. Generally, the higher the moments of inertia of a golf club head, the less the golf club head twists at impact with a golf ball, particularly during “off-center” impacts with a golf ball, the greater the forgiveness of the golf club head and probability of hitting a straight golf shot. Further, higher moments of inertia typically result in greater ball speed upon impact with the golf club head, which can translate into increased golf shot distance.
In general, the moment of inertia of a mass about a given axis is proportional to the square of the distance of the mass away from the axis. In other words, the greater the distance of a mass away from a given axis, the greater the moment of inertia of the mass about the given axis. Accordingly, golf club head designers and manufacturers have sought to increase the moment of inertia about one or more golf club head axes, which are typically axes extending through the golf club head center of gravity, by increasing the distance of the head mass away from the axes of interest.
In an effort to increase the forgiveness of a golf club head, some golf club head manufacturers have focused on the size of the golf club head striking surface. Generally, the larger the striking surface, the greater the forgiveness of the golf club head. However, to maintain the durability of the striking surface, increasing the size of the striking surface typically requires increasing the thickness of the face, e.g., face plate, defining the striking surface, which has a direct effect on the Coefficient of Restitution (COR) of the striking surface, or the measurement of the ability of the striking surface to rebound the ball, e.g., the spring-like effect of the surface. In a simplified form, the COR may be expressed as a percentage of the speed of a golf ball immediately after being struck by the club head divided by the speed of the club head upon impact with the golf ball, with the measurement of the golf ball speed and club head speed governed by United States Golf Association guidelines
United States Golf Association (USGA) regulations and constraints on golf club head shapes, sizes and other characteristics tend to limit the moments of inertia and COR achievable by a golf club head. According to the most recent version of the USGA regulations, golf club heads must, inter alia, be generally plain in shape, have envelope dimensions at or below maximum envelope dimensions (maximum height of 2.8 inches, maximum width of 5.0 inches and a maximum depth of 5.0 inches), and have a volume at or below a maximum head volume of 470 cm3. It should be noted that this maximum volume constraint of 470 cm3 is well below the volume of the maximum envelope dimensions. Note that the 470 cm3 USGA limit includes a 10 cm3 tolerance (i.e., 460 cm3+10 cm3). Further, the USGA regulations require the COR value to be less than 0.830, or have a Pendulum Characteristic Time (PCT) of less than 257 microseconds. The COR and PCT limits just identified each include a tolerance.
Often, golf club manufacturers are faced with the choice of increasing one performance characteristic at the expense of another. For example, to promote forgiveness, some conventional golf club heads focus on increasing the moments of inertia at the expense of increased striking surface size. In these golf club heads, as much of the golf club head mass as possible is moved away from the center of gravity. However, due to mass constraints resulting from attempting to achieve the desired swing weight (e.g., driver club head mass typically ranges from about 185 g to about 215 g), the more mass that is distributed away from the center of gravity, the less mass available for the face. With less mass available for the face, to remain within the USGA constraints governing COR and PCT, the golf club head face thickness, and thus the club head striking surface size, is limited. Accordingly, with these conventional golf club heads, the forgiveness of the heads can be increased by the increased moments of inertia, but limited by the resulting constraints on the size of the golf club head striking surface.
Conversely, to promote forgiveness, some conventional golf club heads focus on increasing the size of the golf club head striking surface at the expense of increased moments of inertia, potentially also sacrificing desired center-of-gravity (“CG”) properties. As described above, with conventional face designs, the larger the size of the striking surface, the thicker and more massive the face must be to comply with USGA constraints. With more mass dedicated to the face, there is typically more mass closer to the center of gravity, and less mass, e.g., discretionary mass, available for moving away from the center of gravity. Accordingly, with these conventional golf club heads, the forgiveness of the heads can be increased by the increased striking surface sizes, but limited by the resulting constraints on the achievable moments of inertia.
As described above, golf club designers and manufacturers have struggled to design USGA-conforming golf club heads that have both high moments of inertia and large striking surface sizes for improved forgiveness.
This application addresses at least the foregoing and discloses, inter alia, golf club heads that provide improved forgiveness as well as golf clubs that may have particular dimensional and/or weight properties to promote increased performance.
This application describes golf club heads that include a body defining an interior cavity. The golf club heads also include a sole positioned at a bottom portion of the golf club head, a crown positioned at a top portion, and a skirt positioned around a periphery between the sole and crown. The body has a forward portion and a rearward portion. Additionally, the golf club heads include a face positioned at the forward portion of the body, and the face defines a striking surface having an ideal impact location at a golf club head origin. The head origin includes an x-axis tangential to the face and generally parallel to the ground when the head is ideally positioned, a y-axis generally perpendicular to the x-axis and generally parallel to the ground when the head is ideally positioned, and a z-axis perpendicular to both the x-axis and y-axis. The positive direction for the axis is toe-to-heel, for the y-axis is front-to-back, and for the z-axis is sole-to-crown.
According to a first aspect, this application describes golf club heads that have a moment of inertia about a golf club head center of gravity z-axis generally parallel to the head origin z-axis greater than approximately 490 kg·mm2. The face has a thickness along the head origin x-axis between tmin and tmax for at least 50% of the x-axis coordinates x within a first range between approximately −10 mm and approximately −50 mm, and a second range between approximately 10 mm and approximately 50 mm, where
tmin=1.6+0.002378(40−|x|)2, (1)
and
tmax=2.5+0.002854(40−|x|)2. (2)
The thickness of a first portion of the face within at respective one of the first and second ranges can be at least approximately 2 mm greater than a second portion of the face within the respective one of the first and second ranges.
In some instances, the thickness of the face can be between tmin and tmax for at least 80% of the x-axis coordinates x within the first and second ranges.
Golf club heads according to the first aspect can have a moment of inertia about a golf club head center of gravity x-axis generally parallel to the head origin x-axis greater than approximately 280 kg·mm2.
Golf club heads of the first aspect can have a center of gravity with an x-axis coordinate between approximately 0.0 mm and approximately 6.0 mm, and a z-axis coordinate between approximately 0.0 mm and approximately −6.0 mm.
In some embodiments, the striking surface has an area between approximately 3,500 mm2 and approximately 4,500 mm2. In other embodiments, the striking surface may have an area greater than approximately 4,500 mm2, and may be up to and including approximately 5,500 mm2, for example.
The face can also have a thickness along the head origin z-axis, between tmin and tmax for at least 50% of the z-axis coordinates z within a third range between approximately −10 mm and approximately −30 mm, and a fourth range between approximately 10 mm and approximately 30 mm, where
tmin=1.6+0.002378(40−|z|)2, (1)
and
tmax=2.5+0.002854(40−|z|)2. (2)
According to a second aspect, this application describes golf club heads that have a moment of inertia about a golf club head center of gravity x-axis generally parallel to the head origin x-axis greater than approximately 280 kg·mm2. The face has a thickness along the head origin z-axis between tmin and tmax for at least 50% of the z-axis coordinates z within a first range between approximately −10 mm and approximately −30 mm, and a second range between approximately 10 mm and approximately 30 mm, where
tmin=1.6+0.002378(40−|z|)2, (1)
and
tmax=2.5+0.002854(40−|z|)2. (2)
The thickness of a first portion of the face within at respective one of the first and second ranges can be at least approximately 2 mm greater than a second portion of the face within the respective one of the first and second ranges for golf clubs according to the second aspect.
The thickness of the face can be between tmin and tmax for at least 80% of the z-axis coordinates z within the first and second ranges.
The striking surface of golf clubs according to the second aspect can have an area between approximately 3,500 mm2 and approximately 4,500 mm2. In other embodiments, the striking surface may have an area greater than approximately 4,500 mm2, and may be up to and including approximately 5,500 mm2, for example.
The face of golf clubs according to the second aspect can have a thickness along the head origin x-axis, the thickness being between tmin and tmax for at least 50% of the x-axis coordinates x within a third range between approximately −10 mm and approximately −50 mm, and a fourth range between approximately 10 mm and approximately 50 mm, where
tmin=1.6+0.002378(40−|x|)2, (1)
and
tmax=2.5+0.002854(40−|x|)2. (2)
Some embodiments according to the second aspect have a moment of inertia about a golf club head center of gravity z-axis generally parallel to the head origin z-axis greater than approximately 490 kg·mm2. Some embodiments have a center of gravity with an x-axis coordinate between approximately 0.0 mm and approximately 6.0 mm, and a z-axis coordinate between approximately 0.0 mm and approximately −6.0 mm.
According to a third aspect, this application describes golf club heads that have a moment of inertia about a golf club head center of gravity z-axis generally parallel to the head origin z-axis greater than approximately 490 kg·mm2, and a moment of inertia about a golf club head center of gravity x-axis generally parallel to the head origin x-axis greater than approximately 280 kg·mm2. The face has a thickness along a radial axis extending tangential to and radially outwardly away from the golf club head origin between tmin and tmax along at least 50% of the distances r away from the golf club head origin along the radial axis equal to or greater than approximately 10 mm and equal to or less than approximately 50 mm, where
tmin=1.6+0.002378(40−r)2, (1)
and
tmax=2.5+0.002854(40−r)2. (2)
Golf club heads according to the third aspect can have a striking surface area between approximately 3,500 mm2 and approximately 5,500 mm2. Golf club heads of the third aspect can have a center of gravity with an x-axis coordinate between approximately 0.0 mm and approximately 6.0 mm, and a z-axis coordinate between approximately 0.0 mm and approximately −6.0 mm.
According to a fourth aspect, golf club heads having a moment of inertia about a golf club head center of gravity z-axis generally parallel to the head origin z-axis greater than approximately 500 kg·mm2 are disclosed. The face of golf clubs heads according to the fourth aspect has a bending stiffness along the head origin x-axis, the bending stiffness being between BSmin and BSmax for at least 50% of the x-axis coordinates x within a first range between approximately −10 mm and approximately −50 mm, and a second range between approximately 10 mm and approximately 50 mm, where
BSmin=1.1·105[1.6+0.002378(40−|x|)2]3, (1)
and
BSmax=1.1·105[2.5+0.002854(40−|x|)2]3. (2)
In some instances according to the fourth aspect, the face has a thickness along the head origin x-axis, the thickness being between tmin and tmax for at least 50% of the x-axis coordinates x within a third range between approximately −10 mm and approximately −50 mm, and a fourth range between approximately 10 mm and approximately 50 mm, where
tmin=1.6+0.002378(40−|x|)2, (1)
and
tmax=2.5+0.002854(40−|x|)2. (2)
The face can have a thickness along the head origin z-axis, the thickness being between tmin and tmax for at least 50% of the z-axis coordinates z within a third range between approximately −10 mm and approximately −30 mm, and a fourth range between approximately 10 mm and approximately 30 mm, where
tmin=1.6+0.002378(40−|z|)2, (1)
and
tmax=2.5+0.002854(40−|z|)2. (2)
The striking surface can have an area between approximately 3,500 mm2 and approximately 4,500 mm2. In other embodiments, the striking surface may have an area greater than approximately 4,500 mm2, and may be up to and including approximately 5,500 mm2, for example.
Golf club heads can have a center of gravity with an x-axis coordinate between approximately 0.0 mm and approximately 6.0 mm, and a z-axis coordinate between approximately 0.0 mm and approximately −6.0 mm.
Golf club heads according to a fifth aspect have a moment of inertia about a golf club head center of gravity x-axis generally parallel to the head origin x-axis greater than approximately 280 kg·mm2. The face has a bending stiffness along the head origin z-axis, the bending stiffness being between BSmin and BSmax for at least 50% of the z-axis coordinates z within a first range between approximately −10 mm and approximately −30 mm, and a second range between approximately 10 mm and approximately 30 mm, where
BSmin=1.1·105[1.6+0.002378(40−|z|)2]3, (1)
and
BSmax=1.1·105[2.5+0.002854(40−|z|)2]3. (2)
Golf club heads according to the fifth aspect can have a thickness along the head origin x-axis, the thickness being between tmin and tmax for at least 50% of the x-axis coordinates x within a third range between approximately −10 mm and approximately −50 mm, and a fourth range between approximately 10 mm and approximately 50 mm, where
tmin=1.6+0.002378(40−|x|)2, (1)
and
tmax=2.5+0.002854(40−|x|)2. (2)
The face in some embodiments has a thickness along the head origin z-axis, the thickness being between tmin and tmax for at least 50% of the z-axis coordinates z within a third range between approximately −10 mm and approximately −30 mm, and a fourth range between approximately 10 mm and approximately 30 mm, where
tmin=1.6+0.002378(40−|z|)2, (1)
and
tmax=2.5+0.002854(40−|z|)2. (2)
The striking surface can have an area between approximately 3,500 mm2 and approximately 4,500 mm2. In other embodiments, the striking surface may have an area greater than approximately 4,500 mm2, and may be up to and including approximately 5,500 mm2, for example.
Golf club heads of the fifth aspect can have a center of gravity with an x-axis coordinate between approximately 0.0 mm and approximately 6.0 mm, and a z-axis coordinate between approximately 0.0 mm and approximately −6.0 mm.
Golf clubs according to a sixth aspect may include a golf club head, golf club shaft, and golf club grip. The golf club may include one or more reduced weight portions as compared to a conventional club, as will be explained in more detail later.
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.
In the following description, 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. These 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.
As illustrated in
The crown 12 is defined as an upper portion of the club head (1) above a peripheral outline 34 of the club head as viewed from a top-down direction; and (2) rearwards of the topmost portion of a ball striking surface 22 of the striking face 18 (see
The sole 14 is defined as a lower portion of the club head 2 extending upwards from a lowest point of the club head when the club head is ideally positioned, i.e., at a proper address position relative to a golf ball on a level surface. In some implementations, the sole 14 extends approximately 50% to 60% of the distance from the lowest point of the club head to the crown 12, which in some instances, can be approximately 15 mm for a driver and between approximately 10 mm and 12 mm for a fairway wood.
A golf club head, such as the club head 2, is at its proper address position when the longitudinal axis 21 of the hosel 20 or shaft is substantially normal to the target direction and at the proper lie angle such that the scorelines are substantially horizontal (e.g., approximately parallel to the ground plane 17) and the face angle relative to target line is substantially square (e.g., the horizontal component of a vector normal to the geometric center of the striking surface 22 substantially points towards the target line). If the faceplate 18 does not have horizontal scorelines, then the proper lie angle is set at an approximately 60-degrees. The loft angle 15 is the angle defined between a face plane 27, defined as the plane tangent to an ideal impact location 23 on the striking surface 22, and a vertical plane 29 relative to the ground 17 when the club head 2 is at proper address position. Lie angle 19 is the angle defined between a longitudinal axis 21 of the hosel 20 or shaft and the ground 17 when the club head 2 is at proper address position. The ground, as used herein, is assumed to be a level plane.
The skirt 16 includes 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 striking surface 22, from the toe portion 28, around the rear portion 32, to the heel portion 26.
In the illustrated embodiment, the ideal impact location 23 of the golf club head 2 is disposed at the geometric center of the striking surface 22 (see
In some embodiments, the striking face 18 is made of a composite material such as described in U.S. Patent Application Publication Nos. 2005/0239575 and 2004/0235584, U.S. patent application Ser. No. 11/642,310, and U.S. Provisional Patent Application No. 60/877,336, which are incorporated herein by reference. In other embodiments, the striking face 18 is made from a metal alloy (e.g., titanium, steel, aluminum, and/or magnesium), ceramic material, or a combination of composite, metal alloy, and/or ceramic materials.
The striking face 18 can be a striking plate having a variable thickness such as described in U.S. Pat. No. 6,997,820, which is incorporated herein by reference. For example, as shown in
In some embodiments, the cross-sectional profile of the striking face 18 along any axes extending perpendicular to the striking surface at the ideal impact location 23 is substantially similar as in
In other embodiments, the cross-sectional profile can vary, e.g., is non-symmetric. For example, in certain implementations, the cross-sectional profile of the striking face 18 along the head origin z-axis might include central, transition, diverging and converging portions as described above (see
Variation in thickness of the striking face 18 with distance from the geometric center of the striking face along an axis can be determined. According to one representative embodiment, a minimum thickness tmin, maximum thickness tmax, and nominal thickness tnom of the striking face 18 along the head origin x-axis within the effective range 10 mm≦|x|≦50 mm can be determined from the following equations:
tmin(x)=1.6+0.002378(40−x)2 (1)
tmax(x)=2.5+0.002854(40−x)2 (2)
tnom(x)=2.05+0.002616(40−x)2 (3)
Referring to
Similar to that described above, a minimum thickness tmin, maximum thickness tmax, and nominal thickness tnom of the striking face 18 along the head origin z-axis within the effective range of about 10 mm≦|z|≦30 mm can be determined according to the following equations:
tmin(z)=1.6+0.002378(40−z)2 (4)
tmax(z)=2.5+0.002854(40−z)2 (5)
tnom(z)=2.05+0.002616(40−z)2 (6)
Referring to
In some implementations, the above equations and constraints can be defined in terms of the radial distance away from the golf club head origin. For example, a minimum thickness tmin, maximum thickness tmax, and nominal thickness tnom of the striking face 18 in terms of the distance r away from the golf club head origin can be determined according to the following equations:
tmin(r)=1.6+0.002378(40−r)2 (7)
tmax(r)=2.5+0.002854(40−r)2 (8)
tnom(r)=2.05+0.002616(40−r)2 (9)
where r is a distance equal to or greater than approximately 10 mm away from the golf club head origin.
Compared to constant thickness faces, the nominal thickness profiles along the x-axis and z-axis represent preferred thickness profiles for reducing the weight of the face 18, increasing the COR zone of the face and providing larger, more forgiving faces that meet the USGA COR constraints. The same or similar advantages can be achieved, however, by a face having thickness profiles along the x-axis and z-axis that are bounded by the minimum and maximum thickness profiles for the respective x-axis and z-axis along a predetermined portion of the effective range. For example, according to certain implementations, the striking face 18 can have a thickness profile along the origin x-axis that is bounded by the minimum and maximum thickness profiles along at least 50% of the effective x-axis range. Similarly, the striking face 18 can have a thickness profile along the origin z-axis that is bounded by the minimum and maximum thickness profiles along at least 50% of the effective z-axis range. In more specific implementations, the thickness profile of the striking face 18 is bounded by the minimum and maximum thickness profiles along at least 60%, 70%, 80% or 90% of the effective axis range.
In the illustrated implementation, the face 18 of golf club head 2 has a thickness profile along the x-axis (see
In one exemplary embodiment, the face 18 is made of an isotropic monolithic material, such as titanium. The bending stiffness (BS) for an isotropic monolithic material is proportional to the modulus of elasticity (E) and thickness of the material, and can be determined according to the following equation:
BS=Et3 (10)
where t is the thickness of the face 18.
Assuming the modulus of elasticity of titanium is about 1.1·105 (N/mm2), the minimum, maximum and nominal bending stiffness BS of the face 18 along the head origin x-axis within the effective range of about 10 mm≦|x|≦50 mm can be determined according to the following equations:
BSmin(x)=1.1·105[1.6+0.002378(40−x)2]3 (11)
BSmax(x)=1.1·105[2.5+0.002854(40−x)2]3 (12)
BSnom(x)=1.1·105[2.05+0.002616(40−x)2]3 (13)
Referring to
Similarly, the minimum, maximum and nominal bending stiffness BS of the face 18 along the head origin z-axis within the effective range of about 10 mm≦|x|≦30 mm can be determined according to the following equations (again assuming titanium with a Young's modulus of about 1.1·105 N/mm2:
BSmin(z)=1.1·105[1.6+0.002378(40−z)2]3 (14)
BSmax(z)=1.1·105[2.5+0.002854(40−z)2]3 (15)
BSnom(z)=1.1·105[2.05+0.002616(40−z)2]3 (16)
Referring to
Compared to constant thickness faces, the bending stiffness profiles along the x-axis and z-axis represent preferred bending stiffness profiles for increasing the stiffness distribution for a more forgiving face. The same or similar advantages can be achieved, however, by a face having bending stiffness profiles along the x-axis and z-axis that are bounded by the minimum and maximum thickness profiles for the respective x-axis and z-axis along a predetermined portion of the effective range. For example, according to certain implementations, the striking face 18 can have a bending stiffness profile along the origin x-axis that is bounded by the minimum and maximum bending stiffness profiles along at least 50% of the effective x-axis range. Similarly, the striking face 18 can have a bending stiffness profile along the origin z-axis that is bounded by the minimum and maximum bending stiffness profiles along at least 50% of the effective z-axis range. In more specific implementations, the bending stiffness profile of the striking face 18 is bounded by the minimum and maximum bending stiffness profiles along at least 60%, 70%, 80% or 90% of the effective axis range.
As the bending stiffness profiles vary according to the thickness profiles, the face 18 of golf club head 2 has a bending stiffness profile along the x-axis that is bounded by the minimum and maximum bending stiffness profiles also along approximately 71% of the effective x-axis range. Likewise, the bending stiffness profile along the z-axis of face 18 is bounded by the minimum and maximum bending stiffness profiles also along approximately 65% of the effective z-axis range.
As described above, the bending stiffness profiles shown in
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 means known in the art. For example, the striking face 18 can be attached to the body 10 as described in U.S. Patent Application Publication Nos. 2005/0239575 and 2004/0235584. The body 10 can be made from a metal alloy (e.g., titanium, steel, aluminum, and/or magnesium), composite material, ceramic material, or any combination thereof. The wall 72 of the golf club head 2 can be made of a thin-walled construction, such as described in U.S. application Ser. No. 11/067,475, filed Feb. 25, 2005, which is incorporated herein by reference. For example, in some implementations, the wall can have a thickness between approximately 0.65 mm and approximately 0.8 mm. In one specific implementation, the wall 72 of the crown 12 and skirt 16 has a thickness of approximately 0.65 mm, and the wall of the sole 14 has a thickness of approximately 0.8 mm.
A club head origin coordinate system may be defined such that the location of various features of the club head (including, e.g., a club head center-of-gravity (CG) 50 (see
Referring to
In one embodiment, the golf club head can have a CG with an x-axis coordinate between approximately 0.0 mm and approximately 6.0 mm, a y-axis coordinate between approximately 30 mm and approximately 50 mm, and a z-axis coordinate between approximately 0.0 mm and approximately −6.0 mm. Referring to
Referring to
Referring to
A moment of inertia about the golf club head CG x-axis 90 is calculated by the following equation (17)
Ixx=∫(y2+z2)dm (17)
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.
A moment of inertia about the golf club head CG z-axis 85 is calculated by the following equation
Izz=∫(x2+y2)dm (18)
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.
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. The higher the moment of inertia about the CG x-axis (Ixx), the greater the forgiveness of the golf club head on high and low off-center impacts with a golf ball. In other words, a golf ball hit by a golf club head on a location of the striking surface 18 above the ideal impact location 23 causes the golf club head to twist upwardly and the golf ball to have a higher trajectory than desired. Similarly, a golf ball hit by a golf club head on a location of the striking surface 18 below the ideal impact location 23 causes the golf club head 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 to reduce the negative effects of high and low off-center impacts.
Compared to relatively constant thickness face designs, the variable thickness of the striking face 18 described above facilitates (1) a reduction in the mass, e.g., weight, of the face without exceeding the USGA COR constraints to allow more discretionary weight to be positioned away from the center of gravity for increased moments of inertia or strategically positioned for achieving a desired center of gravity location; (2) an increase in the size of the striking surface to promote forgiveness; and (3) an increase in the size of a club head COR zone, e.g., the sweet spot of the golf club head face that provides the better golf shot forgiveness compared to other portions of the face.
Because of the weight savings resulting from the variable thickness striking face 18, more discretionary weight is available to increase the moments of inertia of the golf club head 2. For example, in some implementations, the moment of inertia about the CG z-axis (Izz) of golf club head 2 is between approximately 490 kg·mm2 and 600 kg·mm2, and the moment of inertia about the CG x-axis (Ixx) of golf club head 2 is between approximately 280 kg·mm2 and approximately 420 kg·mm2. In one specific exemplary implementation, as shown in
As described above, a variable thickness striking face, such as striking face 18, allows the area of the striking face 20 to be increased, while maintaining the durability of the face and keeping the COR of the face within the USGA limitations. The larger the face, the more surface area available to contact a golf ball, and thus the more forgiving the golf club head. A larger striking face is one of the most important features of a golf club, because it is the only part of the club that makes contact with the ball. Providing a larger face minimizes the chance to hit the ball off the edge of the face (resulting in, for example, a “pop up” ball trajectory). Accordingly, a larger striking face gives golfers more confidence to swing more aggressively at the ball.
Variable thickness striking faces, such as striking face 18, increases the COR zone of the face to increase the forgiveness of the golf club head. For example, referring to
This is not to say that club heads with a variable thickness face plate and an Izz of 600 kg·mm2 has an actual moment of inertia about the z-axis in excess of 600 kg·mm2 Instead, the “feel” of the club head compares favorably to a golf club head having the higher moment of inertia about the z-axis. It can thus be said that a club head with a variable thickness face plate and an Izz of 600 kg·mm2 has an “effective MOI” in excess of 800 kg·mm2 when considering ball speed resulting from off-center hits. Club heads with actual MOI less than 600 kg·mm2 (e.g., 590 kg·mm2+10 kg·mm2 measurement tolerance) would actually be considered conforming to USGA MOI rules even though the effective MOI (compared to constant face plate thickness designs) appears to be greater than 600 kg·mm2.
Referring to
Unless otherwise noted, the general details and features of the body 110 of golf club head 100 can be understood with reference to the same or similar features of the body 10 of golf club head 2.
In the illustrated implementation, the face 118 of golf club head 100 has a thickness profile along the x-axis (see
As the bending stiffness profiles vary according to the thickness profiles, the face 118 of golf club head 100 has a bending stiffness profile along the x-axis that is bounded by the minimum and maximum bending stiffness profiles also along approximately 100% of the effective x-axis range. Likewise, the bending stiffness profile along the z-axis of face 118 is bounded by the minimum and maximum bending stiffness profiles also along approximately 100% of the effective z-axis range.
The sole 114 extends upwardly from the lowest point of the golf club head 100 a shorter distance than the sole 14 of golf club head 2. For example, in some implementations, the sole 114 extends upwardly approximately 50% to 60% of the distance from the lowest point of the club head 100 to the crown 112, which in some instances, can be approximately 15 mm for a driver and between approximately 10 mm and approximately 12 mm for a fairway wood. Further, the sole 114 comprises a substantially flat portion 119 extending horizontal to the ground 117 when in proper address position. In some implementations, the bottommost portion of the sole 114 extends substantially parallel to the ground 117 between approximately 5% and approximately 70% of the depth (Dch) of the golf club head 100.
Because the sole 114 of golf club head 100 is shorter than the sole 12 of golf club head 2, the skirt 116 is taller, i.e., extends a greater approximately vertical distance, than the skirt 16 of golf club head 2.
In at least one implementation, the golf club head 100 includes a weight port 140 formed in the skirt 116 proximate the rear portion 132 of the club head (see
In some implementations, the striking surface 122 golf club head 100 has a height (Hss) between approximately 45 mm and approximately 65 mm, and a width (Wss) between approximately 75 mm and approximately 105 mm. In one specific implementation, the striking face 122 has a height (Hss) of approximately 54.4 mm, width (Wss) of approximately 90.6 mm, and total striking surface area of approximately 4,098 mm2.
In one embodiment, the golf club head 100 has a CG with an x-axis coordinate between approximately 0.0 mm and approximately 6.0 mm, a y-axis coordinate between approximately 30 mm and approximately 50 mm, and a z-axis coordinate between approximately 0.0 mm and approximately −6.0 mm. In one specific implementation, the CG x-axis coordinate is approximately 2.0 mm, the CG y-axis coordinate is approximately 37.9 mm, and the CG z-axis coordinate is approximately −4.67 mm.
In some implementations, the golf club head 100 has a height (Hch) between approximately 48 mm and approximately 72 mm, a width (Wch) between approximately 100 mm and approximately 130 mm, and a depth (Dch) between approximately 100 mm and approximately 130 mm. In one specific implementation, the golf club head 100 has a height (Hch) of approximately 62.2 mm, width (Wch) of approximately 119.3 mm, and depth (Dch) of approximately 103.9 mm.
According to certain exemplary embodiments, the golf club head 100 has a moment of inertia about the CG z-axis (Izz) between about 490 kg·mm2 and about 600 kg·mm2, and a moment of inertia about the CG x-axis (Ixx) between about 280 kg·mm2 and about 420 kg·mm2. In one specific implementation, the club head 100 has a moment of inertia about the CG z-axis (Izz) of approximately 500 kg·mm2 and a moment of inertia about the CG x-axis (Ixx) of approximately 337 kg·mm2.
Referring to
Unless otherwise noted, the general details and features of the body 210 of golf club head 200 can be understood with reference to the same or similar features of the body 10 of golf club head 2 and body 110 of golf club head 100.
In the illustrated implementation, the face 218 of golf club head 200 has a thickness profile along the x-axis (see
As the bending stiffness profiles vary according to the thickness profiles, the face 218 of golf club head 200 has a bending stiffness profile along the x-axis that is bounded by the minimum and maximum bending stiffness profiles also along approximately 100% of the effective x-axis range. Likewise, the bending stiffness profile along the z-axis of face 218 is bounded by the minimum and maximum bending stiffness profiles also along approximately 100% of the effective z-axis range.
Like sole 114 of golf club head 100, the sole 214 extends upwardly approximately 50% to 60% of the distance from the lowest point of the club head 200 to the crown 212. Therefore, the skirt 216 is taller, i.e., extends a greater approximately vertical distance, than the skirt 16 of golf club head 2.
In at least one implementation, and shown in
In some implementations, the striking surface 222 golf club head 200 has a height (Hss) between approximately 45 mm and approximately 65 mm, and a width (Wss) between approximately 75 mm and approximately 105 mm. In one specific implementation, the striking surface 222 has a height (Hss) of approximately 53.5 mm, width (Wss) of approximately 92.3 mm, and total striking surface area of approximately 4,013 mm2. In another specific implementation, the striking surface 222 has a height (Hss) of approximately 54.7 mm, width (Wss) of approximately 92.3 mm, and total striking surface area of approximately 4,115 mm2.
In one embodiment, the golf club head 200 has a CG with an x-axis coordinate between approximately 0.0 mm and approximately 6.0 mm, a y-axis coordinate between approximately 30 mm and approximately 50 mm, and a z-axis coordinate between approximately 0.0 mm and approximately −6.0 mm. In one specific implementation, the CG x-axis coordinate is approximately 2.2 mm, the CG y-axis coordinate is approximately 37.9 mm, and the CG z-axis coordinate is approximately −4.3 mm. In another specific implementation, the CG x-axis coordinate is approximately 2.8 mm, the CG y-axis coordinate is approximately 35.8 mm, and the CG z-axis coordinate is approximately −3.4 mm.
In some implementations, the golf club head 200 has a height (Hch) between approximately 48 mm and approximately 72 mm, a width (Wch) between approximately 100 mm and approximately 130 mm, and a depth (Dch) between approximately 100 mm and approximately 130 mm. In one specific implementation, the golf club head 200 has a height (Hch) of approximately 62.3 mm, width (Wch) of approximately 120.0 mm, and depth (Dch) of approximately 111.6 mm. In another specific implementation, the golf club head 200 has a height (Hch) of approximately 62.6 mm, width (Wch) of approximately 121.0 mm, and depth (Dch) of approximately 107.4 mm.
The golf club head 200 can, in some implementations, have a moment of inertia about the CG z-axis (Izz) between about 490 kg·mm2 and about 600 kg·mm2, and a moment of inertia about the CG x-axis (Ixx) between about 280 kg·mm2 and about 420 kg·mm2. In one specific implementation, the club head 200 has a moment of inertia about the CG z-axis (Izz) of approximately 516 kg·mm2 and a moment of inertia about the CG x-axis (Ixx) of approximately 354 kg·mm2. In another specific implementation, the club head 200 has a moment of inertia about the CG z-axis (Izz) of approximately 496 kg·mm2 and a moment of inertia about the CG x-axis (Ixx) of approximately 329 kg·mm2.
Referring to
The club head grip 280 may comprise a reduced weight grip as compared to a typical grip. For example, the grip 280 may have a total mass between about 15 grams and about 50 grams. In this embodiment, the golf club grip may preferably have a total mass less than about 40 grams, or more preferably less than about 30 grams. Similarly, the shaft 278 may have a reduced weight as compared to a typical shaft. In this embodiment, the shaft 278 may have a total mass than about 60 grams, preferably less than about 50 grams and more preferably less than about 45 grams. As noted previously, the golf club head may have a total mass between about 185 grams and 215 grams. When assembled, golf club 282 may have a reduced weight as compared to a typical club, and may have a total mass between about 245 grams and about 300 grams, and more preferably between about 270 grams and about 300 grams. This weight may be less than a weight of a club of equal club length or less than or equal to a weight of a club of lesser club length.
The shaft 278 may be formed from one or more materials or combinations of materials, such as carbon fiber or epoxy, as just a few examples. The shaft 278 may have a relatively low fiber areal weight, such as a fiber areal weight less than about 75 g/mm2 if the shaft is formed from carbon fiber, for example. Furthermore, the resin content may be relatively low, such as less than about 33%, if the shaft 278 incorporates resin. The grip 280 may be formed from one or more materials or combinations of materials, such as low density foam, polyurethane and/or rubber, for example. As noted previously, this may result in a relatively light weight shaft and grip, which, in combination with a golf club head may result in a golf club having a relatively low weight.
The above golf club illustrated in
In view of the many possible embodiments to which the principles of the disclosed golf club head may be applied, it should be recognized that the illustrated embodiments are only preferred examples of the golf club head and should not be taken as limiting the scope of the golf club head. Rather, the scope of the invention is defined by the following claims. We therefore claim as our invention all that comes within the scope and spirit of these claims.
This application is a continuation of U.S. patent application Ser. No. 12/813,442, filed Jun. 10, 2010, which is a continuation-in-part of U.S. patent application Ser. No. 12/006,060, filed Dec. 28, 2007, now U.S. Pat. No. 8,353,786, which is a continuation-in-part of U.S. patent application Ser. No. 11/863,198, filed Sep. 27, 2007, now U.S. Pat. No. 7,731,603, all of which are incorporated herein by reference. Other applications and patents concerning golf club heads include U.S. patent application Ser. No. 11/871,933, filed Oct. 12, 2007, U.S. patent application Ser. No. 11/669,891, U.S. patent application Ser. No. 11/669,894, U.S. patent application Ser. No. 11/669,900, U.S. patent application Ser. No. 11/669,907, U.S. patent application Ser. No. 11/669,910, U.S. patent application Ser. No. 11/669,916, U.S. patent application Ser. No. 11/669,920, U.S. patent application Ser. No. 11/669,925, and U.S. patent application Ser. No. 11/669,927, all filed on Jan. 31, 2007, which are continuations of U.S. patent application Ser. No. 11/067,475, filed Feb. 25, 2005, now U.S. Pat. No. 7,186,190, which is a continuation-in-part of U.S. patent application Ser. No. 10/785,692, filed Feb. 23, 2004, now U.S. Pat. No. 7,166,040, which is a continuation-in-part of U.S. patent application Ser. No. 10/290,817, now U.S. Pat. No. 6,773,360. These applications are incorporated herein by reference.
Number | Name | Date | Kind |
---|---|---|---|
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 |
1704119 | Buhrke | Mar 1929 | A |
1970409 | Wiedemann | Aug 1934 | A |
D107007 | Cashmore | Nov 1937 | S |
2214356 | Wettlaufer | Sep 1940 | A |
2225930 | Sexton | Dec 1940 | A |
2360364 | Reach | Oct 1944 | A |
2460435 | Schaffer | Feb 1949 | A |
2681523 | Sellers | Jun 1954 | A |
3064980 | Steiner | Nov 1962 | 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 |
3692306 | Glover | Sep 1972 | A |
3743297 | Dennis | Jul 1973 | A |
3897066 | Belmont | Jul 1975 | A |
3976299 | Lawrence et al. | Aug 1976 | A |
3979122 | Belmont | Sep 1976 | A |
3979123 | Belmont | Sep 1976 | A |
3984103 | Nix | Oct 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 |
4165874 | Lezatte et al. | Aug 1979 | A |
4214754 | Zebelean | Jul 1980 | A |
4240631 | MacDougall | Dec 1980 | A |
4261566 | MacDougall | Apr 1981 | A |
4262562 | MacNeill | Apr 1981 | A |
D259698 | MacNeill | Jun 1981 | S |
4340229 | Stuff, Jr. | Jul 1982 | A |
4411430 | Dian | Oct 1983 | A |
4423874 | Stuff, Jr. | Jan 1984 | A |
4432549 | Zebelean | Feb 1984 | A |
4438931 | Motomiya | Mar 1984 | A |
4530505 | Stuff | Jul 1985 | A |
D284346 | Masters | Jun 1986 | S |
4602787 | Sugioka et al. | Jul 1986 | A |
4607846 | Perkins | Aug 1986 | A |
4679791 | Hull | Jul 1987 | A |
4712798 | Preato | Dec 1987 | A |
4730830 | Tilley | Mar 1988 | A |
4736093 | Braly | Apr 1988 | A |
4754977 | Sahm | Jul 1988 | A |
4795159 | Nagamoto | Jan 1989 | A |
4819939 | Kobayashi | Apr 1989 | A |
4867457 | Lowe | Sep 1989 | A |
4867458 | Sumikawa et al. | Sep 1989 | A |
4869507 | Sahm | Sep 1989 | A |
4895371 | Bushner | Jan 1990 | A |
4957294 | Long | Sep 1990 | A |
4962932 | Anderson | Oct 1990 | A |
4994515 | Washiyama et al. | Feb 1991 | A |
5039267 | Wollar | Aug 1991 | A |
5050879 | Sun et al. | Sep 1991 | A |
5058895 | Igarashi | Oct 1991 | A |
RE33735 | Rumble et al. | Nov 1991 | E |
5244210 | Au | Sep 1993 | A |
5253869 | Dingle et al. | Oct 1993 | A |
D343558 | Latraverse et al. | Jan 1994 | S |
5316305 | McCabe | May 1994 | A |
5320005 | Hsiao | Jun 1994 | A |
5328176 | Lo | Jul 1994 | A |
5385348 | Wargo | Jan 1995 | A |
5410798 | Lo | 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 |
D365615 | Shimatani | Dec 1995 | S |
5482280 | Yamawaki | Jan 1996 | A |
5518243 | Redman | May 1996 | A |
5533730 | Ruvang | Jul 1996 | A |
5571053 | Lane | Nov 1996 | A |
5620379 | Borys | Apr 1997 | A |
5624331 | Lo et al. | Apr 1997 | A |
5629475 | Chastonay | May 1997 | A |
5632694 | Lee | May 1997 | A |
5669827 | Nagamoto | Sep 1997 | A |
5683309 | Reimers | Nov 1997 | A |
5709613 | Sheraw | Jan 1998 | A |
5718641 | Lin | Feb 1998 | A |
D392526 | Nicely | Mar 1998 | S |
5746664 | Reynolds, Jr. | May 1998 | A |
5755627 | Yamazaki et al. | May 1998 | A |
5769737 | Holladay et al. | Jun 1998 | A |
5776011 | Su et al. | Jul 1998 | A |
RE35955 | Lu | Nov 1998 | E |
5873791 | Allen | Feb 1999 | A |
D409463 | McMullin | May 1999 | S |
5908356 | Nagamoto | Jun 1999 | A |
5911638 | Parente et al. | Jun 1999 | A |
D412547 | Fong | Aug 1999 | S |
5935019 | Yamamoto | Aug 1999 | A |
5941782 | Cook | Aug 1999 | A |
5947840 | Ryan | Sep 1999 | A |
5954596 | Noble et al. | Sep 1999 | A |
5967905 | Nakahara et al. | Oct 1999 | A |
5997415 | Wood | Dec 1999 | A |
6015354 | Ahn et al. | Jan 2000 | A |
6019686 | Gray | Feb 2000 | A |
6023891 | Robertson et al. | Feb 2000 | A |
6032677 | Blechman et al. | Mar 2000 | A |
6056649 | Imai | May 2000 | A |
6089994 | Sun | Jul 2000 | A |
6149533 | Finn | Nov 2000 | A |
6162133 | Peterson | Dec 2000 | A |
6238303 | Fite | May 2001 | B1 |
6244974 | Hanberry, Jr. | Jun 2001 | B1 |
6270422 | Fisher | Aug 2001 | B1 |
6277032 | Smith | Aug 2001 | B1 |
6296579 | Robinson | Oct 2001 | B1 |
6299547 | Kosmatka | Oct 2001 | B1 |
6332848 | Long et al. | Dec 2001 | B1 |
6334817 | Ezawa et al. | Jan 2002 | B1 |
6338683 | Kosmatka | Jan 2002 | B1 |
6348014 | Chiu | Feb 2002 | B1 |
6354962 | Galloway et al. | Mar 2002 | B1 |
6379265 | Hirakawa et al. | Apr 2002 | B1 |
6383090 | O'Doherty et al. | May 2002 | B1 |
6390933 | Galloway | May 2002 | B1 |
6398666 | Evans et al. | Jun 2002 | B1 |
6409612 | Evans et al. | Jun 2002 | B1 |
6425832 | Cackett et al. | Jul 2002 | B2 |
6428425 | Naruo et al. | Aug 2002 | B1 |
6436142 | Paes et al. | Aug 2002 | B1 |
6440009 | Guibaud et al. | Aug 2002 | B1 |
6471604 | Hocknell et al. | Oct 2002 | B2 |
6491592 | Cackett et al. | Dec 2002 | B2 |
6514154 | Finn | Feb 2003 | B1 |
6524197 | Boone | Feb 2003 | B2 |
6527649 | Neher et al. | Mar 2003 | B1 |
6530848 | Gillig | Mar 2003 | B2 |
6547676 | Cackett et al. | Apr 2003 | B2 |
6565448 | Cameron et al. | May 2003 | B2 |
6565452 | Helmstetter et al. | May 2003 | B2 |
6569040 | Bradstock | May 2003 | B2 |
6572489 | Miyamoto et al. | Jun 2003 | B2 |
6575845 | Galloway et al. | Jun 2003 | B2 |
6582323 | Soracco et al. | Jun 2003 | B2 |
6602149 | Jacobson | Aug 2003 | B1 |
6605007 | Bissonnette et al. | Aug 2003 | B1 |
6607452 | Helmstetter et al. | Aug 2003 | B2 |
6612938 | Murphy et al. | Sep 2003 | B2 |
6641487 | Hamburger | Nov 2003 | B1 |
6648773 | Evans | Nov 2003 | B1 |
6669571 | Cameron et al. | Dec 2003 | B1 |
6669578 | Evans | Dec 2003 | B1 |
6669580 | Cackett et al. | Dec 2003 | B1 |
6676536 | Jacobson | Jan 2004 | B1 |
6739982 | Murphy et al. | May 2004 | B2 |
6739983 | Helmstetter et al. | May 2004 | B2 |
6743118 | Soracco | Jun 2004 | B1 |
6757572 | Forest | Jun 2004 | B1 |
6758763 | Murphy et al. | Jul 2004 | B2 |
6773360 | Willett et al. | Aug 2004 | B2 |
6800038 | Willett et al. | Oct 2004 | B2 |
6824475 | Burnett et al. | Nov 2004 | B2 |
6860818 | Mahaffey et al. | Mar 2005 | B2 |
6860823 | Lee | Mar 2005 | B2 |
6860824 | Evans | Mar 2005 | B2 |
6875129 | Erickson et al. | Apr 2005 | B2 |
6878073 | Takeda | Apr 2005 | B2 |
6881159 | Galloway et al. | Apr 2005 | B2 |
6904663 | Willett et al. | Jun 2005 | B2 |
6926619 | Helmstetter et al. | Aug 2005 | B2 |
6960142 | Bissonnette et al. | Nov 2005 | B2 |
6964617 | Williams | Nov 2005 | B2 |
6974393 | Caldwell et al. | Dec 2005 | B2 |
6979270 | Allen | Dec 2005 | B1 |
6988960 | Mahaffey et al. | Jan 2006 | B2 |
6991558 | Beach et al. | Jan 2006 | B2 |
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 |
7056228 | Beach et al. | Jun 2006 | B2 |
7140974 | Chao et al. | Nov 2006 | B2 |
7153220 | Lo | Dec 2006 | B2 |
7163468 | Gibbs et al. | Jan 2007 | B2 |
7166040 | Hoffman et al. | Jan 2007 | B2 |
7169060 | Stevens et al. | Jan 2007 | B2 |
7186190 | Beach et al. | Mar 2007 | B1 |
7189169 | Billings | Mar 2007 | B2 |
7198575 | Beach et al. | Apr 2007 | B2 |
7223180 | Willett et al. | May 2007 | B2 |
7247103 | Beach et al. | Jul 2007 | B2 |
7252600 | Murphy et al. | Aug 2007 | B2 |
7255654 | Murphy et al. | Aug 2007 | B2 |
7278927 | Gibbs et al. | Oct 2007 | B2 |
7448963 | Beach et al. | Nov 2008 | B2 |
7731603 | Beach et al. | Jun 2010 | B2 |
7736245 | Hasegawa | Jun 2010 | B2 |
7798914 | Noble et al. | Sep 2010 | B2 |
7850542 | Cackett et al. | Dec 2010 | B2 |
8128508 | Sato | Mar 2012 | B2 |
8353786 | Beach | Jan 2013 | B2 |
8647216 | Beach et al. | Feb 2014 | B2 |
8801541 | Beach | Aug 2014 | B2 |
20010049310 | Cheng et al. | Dec 2001 | A1 |
20020022535 | Takeda | Feb 2002 | A1 |
20020072434 | Yabu | Jun 2002 | A1 |
20020137576 | Dammen | Sep 2002 | A1 |
20020160854 | Beach et al. | Oct 2002 | A1 |
20030130059 | Billings | Jul 2003 | A1 |
20040087388 | Beach et al. | May 2004 | A1 |
20040242343 | Chao | Dec 2004 | A1 |
20040248667 | Cackett et al. | Dec 2004 | A1 |
20050101404 | Long et al. | May 2005 | A1 |
20050239575 | Chao et al. | Oct 2005 | A1 |
20060058112 | Haralason et al. | Mar 2006 | A1 |
20060154747 | Beach | Jul 2006 | 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 |
20070129167 | Matsunaga | Jun 2007 | A1 |
20080261717 | Hoffman et al. | Oct 2008 | A1 |
20080280698 | Hoffman et al. | Nov 2008 | A1 |
20090017938 | Yokota | Jan 2009 | A1 |
20090088271 | Beach et al. | Apr 2009 | A1 |
20100216570 | Beach et al. | Aug 2010 | A1 |
20100273572 | Beach et al. | Oct 2010 | A1 |
20140155194 | Beach et al. | Jun 2014 | A1 |
Number | Date | Country |
---|---|---|
9012884 | Sep 1990 | DE |
1001175 | May 2000 | EP |
0982052 | Mar 2002 | EP |
194823 | Dec 1921 | GB |
06-304271 | Apr 1993 | JP |
05-317465 | Dec 1993 | JP |
06-126004 | May 1994 | JP |
07-275411 | Oct 1995 | JP |
08-243194 | Sep 1996 | JP |
09-028844 | Feb 1997 | JP |
09173510 | Jul 1997 | JP |
09-308717 | Dec 1997 | JP |
09-327534 | Dec 1997 | JP |
10-234902 | Aug 1998 | JP |
10-277182 | Oct 1998 | JP |
10-277187 | Oct 1998 | JP |
11299937 | Nov 1999 | JP |
2000176056 | Jun 2000 | JP |
2001238988 | Sep 2001 | JP |
2002143350 | May 2002 | JP |
2002315854 | Oct 2002 | JP |
2003102877 | Apr 2003 | JP |
2003290396 | Oct 2003 | JP |
2004135730 | May 2004 | JP |
2004222911 | Aug 2004 | JP |
2004261451 | Sep 2004 | JP |
2004267438 | Sep 2004 | JP |
2004358225 | Dec 2004 | JP |
2005160947 | Jun 2005 | JP |
2005305169 | Nov 2005 | JP |
2006149449 | Jun 2006 | JP |
2006204604 | Aug 2006 | JP |
2007500066 | Jan 2007 | JP |
2007029588 | Feb 2007 | JP |
2007151758 | Jun 2007 | JP |
2008220665 | Sep 2008 | JP |
2009018049 | Jan 2009 | JP |
2001170229 | Jun 2011 | JP |
WO8802642 | Apr 1988 | WO |
WO0166199 | Sep 2001 | WO |
WO02062501 | Aug 2002 | WO |
WO03061773 | Jul 2003 | WO |
Entry |
---|
Callaway Golf, World's Straightest Driver: FT-i Driver downloaded from www.callawaygolf.com/ft%2Di/driver.aspx?lang=en on Apr. 5, 2007. |
Final Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 11/863,198, dated Oct. 5, 2009. |
Final Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 12/006,060, dated Mar. 9, 2010. |
Final Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 12/006,060, dated Apr. 12, 2011. |
Final Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 12/006,060, dated Nov. 14, 2011. |
Final Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 12/775,359, dated Aug. 19, 2011. |
Final Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 12/775,359, dated Jan. 17, 2013. |
Final Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 12/813,442, dated Jun. 5, 2013. |
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. 2008-247526, dated Nov. 20, 2012. |
Office action from the Japanese Patent Office in Patent Application No. 2008-264852, dated Dec. 3, 2012. |
Office action from the Japanese Patent Office in Patent Application No. 2008-264852, dated Mar. 4, 2014. |
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 11/863,198, dated Mar. 13, 2009. |
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 12/006,060, dated Jul. 30, 2009. |
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 12/006,060, dated Dec. 27, 2010. |
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 12/006,060, dated Jul. 29, 2011. |
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 12/775,359, dated Jan. 28, 2011. |
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 12/775,359, dated Jun. 22, 2012. |
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 12/775,359, dated Apr. 26, 2013. |
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 12/813,442, dated Oct. 23, 2012. |
Office action from the U.S. Patent and Trademark Office in U.S. Appl. No. 12/813,442, dated Oct. 10, 2013. |
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. |
Number | Date | Country | |
---|---|---|---|
20150018115 A1 | Jan 2015 | US |
Number | Date | Country | |
---|---|---|---|
Parent | 12813442 | Jun 2010 | US |
Child | 14456927 | US |
Number | Date | Country | |
---|---|---|---|
Parent | 12006060 | Dec 2007 | US |
Child | 12813442 | US | |
Parent | 11863198 | Sep 2007 | US |
Child | 12006060 | US |