Patent Application
20150133233
The present invention relates to an improved golf club head. More particularly, the present invention relates to a golf club head having a compliant portion.
The complexities of golf club design are well known. The specifications for each component of the club (i.e., the club head, shaft, grip, and subcomponents thereof) directly impact the performance of the club. Thus, by varying the design specifications, a golf club can be tailored to have specific performance characteristics.
The design of club heads has long been studied. Among the more prominent considerations in club head design are loft, lie, face angle, horizontal face bulge, vertical face roll, center of gravity, inertia, material selection, and overall head weight. While this basic set of criteria is generally the focus of golf club engineering, several other design aspects must also be addressed. The interior design of the club head may be tailored to achieve particular characteristics, such as the inclusion of hosel or shaft attachment means, perimeter weights on the club head, and fillers within hollow club heads.
Golf club heads must also be strong to withstand the repeated impacts that occur during collisions between the golf club and the golf ball. The loading that occurs during this transient event can create a peak force of over 2,000 lbs. Thus, a major challenge is designing the club face and body to resist permanent deformation or failure by material yield or fracture. Conventional hollow metal wood drivers made from titanium typically have a face thickness exceeding 2.5 mm to ensure structural integrity of the club head.
Players generally seek a metal wood driver and golf ball combination that delivers maximum distance and landing accuracy. The distance a ball travels after impact is dictated by the magnitude and direction of the ball's translational velocity and the ball's rotational velocity or spin. Environmental conditions, including atmospheric pressure, humidity, temperature, and wind speed, further influence the ball's flight. However, these environmental effects are beyond the control of the golf equipment manufacturer. Golf ball landing accuracy is driven by a number of factors as well. Some of these factors are attributed to club head design, such as center of gravity and club face flexibility.
The United States Golf Association (USGA), the governing body for the rules of golf in the United States, has specifications for the performance of golf balls. These performance specifications dictate the size and weight of a conforming golf ball. One USGA rule limits the golf ball's initial velocity after a prescribed impact to 250 feet per second+2% (or 255 feet per second maximum initial velocity). To achieve greater golf ball travel distance, ball velocity after impact and the coefficient of restitution of the ball-club impact must be maximized while remaining within this rule.
Generally, golf ball travel distance is a function of the total kinetic energy imparted to the ball during impact with the club head, neglecting environmental effects. During impact, kinetic energy is transferred from the club and stored as elastic strain energy in the club head and as viscoelastic strain energy in the ball. After impact, the stored energy in the ball and in the club is transformed back into kinetic energy in the form of translational and rotational velocity of the ball, as well as the club. Since the collision is not perfectly elastic, a portion of energy is dissipated in club head vibration and in viscoelastic relaxation of the ball. Viscoelastic relaxation is a material property of the polymeric materials used in all manufactured golf balls.
Viscoelastic relaxation of the ball is a parasitic energy source, which is dependent upon the rate of deformation. To minimize this effect, the rate of deformation must be reduced. This may be accomplished by allowing more club face deformation during impact. Since metallic deformation may be purely elastic, the strain energy stored in the club face is returned to the ball after impact thereby increasing the ball's outbound velocity after impact.
A variety of techniques may be utilized to vary the deformation of the club face, including uniform face thinning, thinned faces with ribbed stiffeners and varying thickness, among others. These designs should have sufficient structural integrity to withstand repeated impacts without permanently deforming the club face. In general, conventional club heads also exhibit wide variations in initial ball speed after impact, depending on the impact location on the face of the club. Hence, there remains a need in the art for a club head that has a larger “sweet zone” or zone of substantially uniform high initial ball speed.
Technological breakthroughs in recent years provide the average golfer with more distance, such as making larger head clubs while keeping the weight constant or even lighter, by casting consistently thinner shell thickness and going to lighter materials such as titanium. Also, the faces of clubs have been steadily becoming extremely thin. The thinner face maximizes the coefficient of restitution (COR). The more a face rebounds upon impact, the more energy that may be imparted to the ball, thereby increasing distance. In order to make the faces thinner, manufacturers have moved to forged, stamped or machined metal faces which are generally stronger than cast faces. Common practice is to attach the forged or stamped metal face by welding them to the body or sole. The thinner faces are more vulnerable to failure. The present invention provides a novel manner for providing the face of the club with the desired flex and rebound at impact thereby maximizing COR.
The present invention relates to a golf club head including a flexure that alters the compliance characteristics as compared to known golf club heads.
In an embodiment, a golf club head comprises a crown, a sole, a side wall, a hosel, a face and a flexure. The crown defines an upper surface of the golf club head, the sole defines a lower surface of the golf club head and the side wall extends between the crown and sole. The hosel extends from the crown and includes a shaft bore. The face defines a ball-striking surface and intersects the lower surface at a leading edge. The flexure is a tubular member interposed between a face portion and a rear body portion of the golf club head so that it forms an intermediate ring that is spaced aftward of the ball-striking surface. The sole is constructed of a first material having a first Young's modulus and the flexure is constructed of a second material having a second Young's modulus that is lower than the first Young's modulus, and at least a portion of the flexure is constructed of a β-Ti alloy.
In another embodiment, a golf club head comprises a crown, a sole, a side wall, a hosel, a face, and a flexure component. The crown defines an upper surface of the golf club head, the sole defines a lower surface of the golf club head, and the side wall extends between the crown and sole. The hosel extends from the crown and includes a shaft bore. The face defines a ball-striking surface and intersects the lower surface at a leading edge. The flexure component is spaced aftward of the ball-striking surface, and extends in a generally heel-to-toe direction and parallel to the leading edge of the golf club head. The flexure component is coupled to a forward flange and an aft flange of the golf club head. The sole is constructed of a first material having a first Young's modulus and the flexure is constructed of a second material having a second Young's modulus that is lower than the first Young's modulus. At least a portion of the flexure component is constructed of a β-Ti alloy, and the flexure component extends across the body in a generally heel-to-toe direction and within between about 5.0 mm and about 20.0 mm from the leading edge of the golf club head.
Preferred features of the present invention are disclosed in the accompanying drawings, wherein similar reference characters denote similar elements throughout the several views, and wherein:
Other than in the operating examples, or unless otherwise expressly specified, all of the numerical ranges, amounts, values and percentages such as those for amounts of materials, moments of inertias, center of gravity locations, loft and draft angles, and others in the following portion of the specification may be read as if prefaced by the word “about” even though the term “about” may not expressly appear with the value, amount, or range. Accordingly, unless indicated to the contrary, the numerical parameters set forth in the following specification and attached claims are approximations that may vary depending upon the desired properties sought to be obtained by the present invention. At the very least, and not as an attempt to limit the application of the doctrine of equivalents to the scope of the claims, each numerical parameter should at least be construed in light of the number of reported significant digits and by applying ordinary rounding techniques.
Notwithstanding that the numerical ranges and parameters setting forth the broad scope of the invention are approximations, the numerical values set forth in the specific examples are reported as precisely as possible. Any numerical value, however, inherently contains certain errors necessarily resulting from the standard deviation found in their respective testing measurements. Furthermore, when numerical ranges of varying scope are set forth herein, it is contemplated that any combination of these values inclusive of the recited values may be used.
Coefficient of restitution, or “COR”, is a measure of collision efficiency. COR is the ratio of the velocity of separation to the velocity of approach. As an example, such as for a golf ball struck off of a golf tee, COR may be determined using the following formula:
(Mball(Vball-post−Vball-pre)+Mclub(Vball-post−Vclub-pre))/Mclub(Vclub-pre−Vball-pre)
where,
(MballVball-post+Mclub(Vball-post−Vclub-pre))/Mclub(Vclub-pre)
COR, in general, depends on the shape and material properties of the colliding bodies. A perfectly elastic impact has a COR of one (1.0), indicating that no energy is lost, while a perfectly inelastic or perfectly plastic impact has a COR of zero (0.0), indicating that the colliding bodies did not separate after impact resulting in a maximum loss of energy. Consequently, high COR values are indicative of greater ball velocity and distance.
Referring to
When club head 10 is in the address position, crown 12 provides an upper surface and sole 14 provides a lower surface of the golf club head. Skirt 16 extends between crown 12 and sole 14 and forms a perimeter of the club head. Face 18 provides a forward-most ball-striking surface 20 and includes a perimeter that is coupled to crown 12, sole 14 and skirt 16 to enclose cavity 24. Face 18 includes a toe portion 26 and a heel portion 28 on opposite sides of a geometric center of face 18. Hosel 22 extends outward from crown 12 and skirt 16 adjacent heel portion 28 of face 18 and provides an attachment structure for a golf club shaft (not shown).
Hosel 22 may have a through-bore or a blind hosel construction. In particular, hosel 22 is generally a tubular member and it may extend through cavity 24 from crown 12 to the bottom of the club head 10 at sole 14 or it may terminate at a location between crown 12 and sole 14. Furthermore, a proximal end of hosel 22 may terminate flush with crown 12, rather than extending outward from the club head away from crown 12 as shown in
Inner cavity 24 may have any volume, but is preferably greater than 100 cubic centimeters, and the golf club head may have a hybrid, fairway or driver type constructions. Preferably, the mass of the inventive club head 10 is greater than about 150 grams, but less than about 220 grams, although the club head may have any suitable weight for a given length to provide a desired overall weight and swing weight. The body may be formed of stamped, forged, cast and/or molded components that are welded, brazed and/or adhered together. Golf club head 10 may be constructed from a titanium alloy, any other suitable material or combinations of different materials. Further, weight members constructed of high density mater, such as tungsten, may be coupled to any portion of the golf club head, such as the sole.
Face 18 may include a face insert 30 that is coupled to a face perimeter 32, such as a face flange. The face perimeter 32 defines an opening for receiving the face insert 30. The face insert 30 is preferably connected to the perimeter 32 by welding. For example, a plurality of chads or tabs (not shown) may be provided to form supports for locating the face insert 30 or a face insert may be tack welded into position, and then the face insert 30 and perimeter 32 may be integrally connected by laser or plasma welding. The face insert 30 may be made by milling, casting, forging or stamping and forming from any suitable material, such as, for example, titanium, titanium alloy, carbon steel, stainless steel, beryllium copper, and carbon fiber composites and combinations thereof. Additionally, crown 12 or sole 14 may be formed separately and coupled to the remainder of the body.
The thickness of the face insert 30 is preferably between about 0.5 mm and about 4.0 mm. Additionally, the insert 30 may be of a uniform thickness or a variable thickness. For example, the face insert 30 may have a thicker center section and thinner outer section. In another embodiment, the face insert 30 may have two or more different thicknesses and the transition between thicknesses may be radiused or stepped. Alternatively, the face insert 30 may increase or decrease in thickness towards toe portion 26, heel portion 28, crown 12 and/or sole 14. It will be appreciated that one or both of the ball-striking surface or the rear surface of face 18 may have at least a portion that is curved, stepped or flat to vary the thickness of the face insert 30.
As mentioned above, club head 10 includes a construction that improves behavior of the club when it strikes a golf ball, particularly when a lower portion of the face impacts a golf ball. A flexure 36 is formed in a forward portion of the crown, sole and/or skirt. Flexure 36 is an elongate corrugation that extends in a generally heel to toe direction and that is formed in a forward portion of sole 14.
Flexure 36 is generally flexible in a fore/aft direction and provides a flexible portion in the club head 10 away from face 18 so that it allows at least a portion of face 18 to translate and rotate as a unit, in addition to flexing locally, when face 18 impacts a golf ball. The golf club head is designed to have two distinct vibration modes of the face between about 3000 Hz and about 6000 Hz, and the flexure is generally constructed to add the second distinct vibration mode of the face. The first face vibration mode primarily includes the local deflection of the face during center face impacts with a golf ball. The deflection profile of the second face vibration mode generally includes the entire face deflecting similar to an accordion and provides improved performance for off-center impacts between the face and a golf ball.
Flexure 36 is also configured to generally maintain the stiffness of sole 14 in a crown/sole direction so that the sound of the golf club head is not significantly affected. A lower stiffness of the sole in the crown/sole direction will generally lower the pitch of the sound that the club head produces, and the lower pitch is generally undesirable.
Flexure 36 allows the front portion of the club, including face 18, to flex differently than would otherwise be possible without altering the size and/or shape of face 18. In particular, a portion of the golf club head body adjacent the face is designed to elastically flex during impact. That flexibility reduces the reduction in ball speed, and reduces the backspin, that would otherwise be experienced for ball impacts located below the ideal impact location. The ideal impact location is a location on the ball-striking surface that intersects an axis that is normal to the ball-striking surface and that extends through the center of gravity of the golf club head, and as a result the ideal impact location is generally located above the geometric face center by a distance between about 0.5 mm and 5.0 mm. By providing flexure 36 in sole 14, close to face 18, the club head provides less of a reduction in ball speed, and lower back spin, when face 18 impacts a golf ball at a location below the ideal impact location. Thus, ball impacts at the ideal impact location and lower on the club face of the inventive club head will go farther than the same impact location on a conventional club head for the same swing characteristics. Locating flexure 36 in sole 14 is especially beneficial because the ideal impact location is generally located higher than the geometric face center in metal wood-type golf clubs. Therefore, a large portion of the face area is generally located below the ideal impact location. Additionally, there is a general tendency of golfers to experience golf ball impacts low on the face. Similar results, however, may be found for a club head 10 with flexures provided on other portions of the club head 10 for impacts located toward the flexure from the geometric face center. For example, a club having a flexure disposed in the crown may improve performance for ball impacts that are between the crown and the geometric face center.
In an embodiment, flexure 36 is provided such that it is substantially parallel to at least a portion of a leading edge 38 of the club head 10, so that it is generally curved with the leading edge, and is provided within a selected distance D from ball-striking surface 20. Preferably, flexure 36 is provided a distance D within 30 mm of ball-striking surface 20, more preferably within 20 mm of ball-striking surface 20, and more preferably between about 5.0 mm and 20.0 mm. For smaller golf club heads, such as those with fairway wood or hybrid constructions, it is preferable that the flexure 36 is provided within 10 mm of ball striking surface 20.
Flexure 36 is constructed from a first member 40 and a second member 42. First member 40 is coupled to a rearward edge of a forward transmittal portion 46 of sole 14 and curves into inner cavity 24 from sole 14. Second member 42 is coupled to a forward edge of a rearward portion of sole 14 and also curves into inner cavity 24 from sole 14. The ends of first member 40 and second member 42 that are spaced away from sole 14 are coupled to each other at an apex 44. Preferably, the flexure is elongate and extends in a generally heel to toe direction.
The dimensions of flexure 36 are selected to provide a desired flexibility during a ball impact. Flexure 36 has a height H, a width W, and a curl length C, as shown in
The inventive examples described above were analyzed using finite element analysis to determine the effect on COR and vibration response of the golf club head. In particular, a club head lacking a flexure (i.e., Baseline) was compared to the inventive examples. Table 2 summarizes the comparison.
In the above table, “extra mode” refers to a mode shape, or a natural mode of vibration that does not exist unless a flexure is present. The extra mode generally presents itself as a the face portion rotating and flexing relative to the remainder of the golf club body. In particular, the inventive examples include a flexure that extends across a portion of the sole and the extra mode includes the face rotating about the interface between the face and crown so that the flexure flexes. The flexure is tuned so that that extra mode takes place in a range of frequencies from about 2900 Hz to about 4000 Hz, and more preferably at approximately 3600 Hz, which has been analyzed to be most effective in increasing the ball speed after impact. Practically speaking, that tuning results in the width W of the flexure varying sinusoidally, immediately after impact, at a frequency of about 2900 Hz to about 4000 Hz. If the extra mode takes place at a frequency that is higher or lower than that range, the ball speed can actually be lower compared to the baseline example that does not include a flexure. It has been determined using FEA analysis of inventive example 1 that a flexure that is tuned to provide an extra mode with a frequency below 2900 Hz, particularly approximately 2157 Hz, the ball speed is reduced below the baseline golf club head that does not include a flexure. Additionally, including a flexure that is too rigid provides a golf club head that does not include the extra mode, as shown by inventive example 5, and only provides minimal increase in ball speed after impact.
Transmittal portion 46 of sole 14 extends between flexure 36 and leading edge 38. Transmittal portion 46 is preferably constructed so that the force of a golf ball impact is transmitted to flexure 18 without transmittal portion 46 flexing significantly. For example, transmittal portion is oriented so that it is less inclined to bend. In particular, a transmittal plane that is tangent to the center of transmittal portion 46 (in both fore/aft and heel/toe directions) of sole 14 is angled relative to the ground plane by an angle α. Angle α is preferably less than, or equal to, the loft angle of the golf club head at address, so that the angle between the transmittal plane and the ball striking surface is generally equal to, or less than, 90° so that transmittal portion 46 is less likely to bend during a ball impact.
Flexure 36 may be formed by any suitable manner. For example, flexure 36 may be cast as an integral part of sole 14. Alternatively, flexure 36 may be stamped or forged into a sole component. Additionally, the flexure may be formed by including a thickened region and machining a recess in that thickened region to form the flexure. For example, a spin-milling process may be used to provide a desired recess, the spin-milling process is generally described in U.S. Pat. No. 8,240,021 issued Aug. 14, 2012 as applied to face grooves, but a flexure with a desired profile may be machined using that process by increasing the size of the spin mill tool and altering the profile of the cutter. In general, that process utilizes a tool having an axis of rotation that is parallel to the sole and perpendicular to the leading edge of the golf club head and a cutting end that is profiled to create the desired profile of the flexure. The tool is then moved along a cutting path that is generally parallel to the leading edge. As a further alternative described in greater detail below, a separate flexure component may be added to a flexure on the sole to further tune the flexure of the sole, as shown in
As shown in the embodiment of
In another embodiment, illustrated in
A flexure 76 is formed in a forward portion of the sole, but it may alternatively be formed in the crown and/or skirt. Preferably, flexure 76 is an elongate corrugation that extends in a generally heel to toe direction and is formed in a forward portion of sole 64 of the body of golf club head 60. Flexure 76 provides a flexible portion in the club head 60 rearward from face 68 so that it allows at least a portion of face 68 to translate or rotate as a unit, in addition to flexing locally, when face 68 impacts a golf ball.
Flexure 76 allows the front portion of the club, including face 68, to flex differently than would otherwise be possible without altering the size and/or shape of face 68. That flexibility provides less reduction in ball speed that would otherwise be experienced for mis-hits, i.e., ball impacts located away from the ideal impact location, and less spin for impacts below the ideal impact location. For example, by providing flexure 76 in sole 64, close to face 68, the club head provides less of a reduction in ball speed when ball impact is located below the ideal impact location. Thus, during use, ball impacts that occur lower on the club face of the inventive club head will go farther than when compared with the same impact location on a club face of a conventional club head, for common swing characteristics.
In an embodiment, flexure 76 is provided such that it is substantially parallel to at least a portion of a leading edge 78 of the club head 60 and is provided within a certain distance D from ball-striking surface 70. Preferably, flexure 76 is provided a distance D within 30 mm of ball-striking surface 70, more preferably within 20 mm of ball-striking surface 70, and most preferably within 10 mm.
In the present embodiment, flexure 76 is constructed from a first member 80, a second member 82 and a third member 83 and is generally constructed as a separate component that is coupled to sole 64. First member 80 is coupled to a rearward edge of a forward transmittal portion 65 of sole 64 and curves into inner cavity 74 from the transmittal portion 65. Second member 82 is coupled to a forward edge of a rearward portion of sole 64 and also curves into inner cavity 74 from sole 64. The ends of first member 80 and second member 82 that are spaced away from sole 64 are coupled to each other at an apex 84. Preferably, the flexure is elongate and extends in a generally heel to toe direction.
Similar to previous embodiments, the dimensions of flexure 76 are selected to provide a desired elastic flex in response to a ball impact. Flexure 76 defines a height H, a width W, and a curl length C. Preferably, flexure 76 has a height that is greater than 4 mm, preferably about 5 mm to about 15 mm, and a width that is greater than 4 mm, preferably about 5 mm to about 10 mm, and a wall thickness between about 0.8 mm and about 2.0 mm, and those dimensions preferably extend over a length that is at least 25% of the overall club head length along the X-axis.
Flexure 76 includes third member 83 that may be used to tune the flexibility of flexure 76. Third member 83 may be coupled to an inner surface (as shown) or an outer surface of flexure 76 and locally increases the rigidity of flexure 76. Third member 83 is preferably constructed from a material that has a lower specific gravity than the material of at least one of first member 80 and second member 82. Third member 83 may be bonded, such as by using an adhesive, or mechanically coupled, such as by fasteners, welding or brazing, to first member 80 and second member 82. The third member may be constructed from any metallic material, such as aluminum, or non-metallic material, such as a carbon fiber composite material or polyurethane.
The location, dimensions and number of flexures in a golf club head may be selected to provide desired behavior. For example, a plurality of flexures may be included as shown in golf club head 90 of
In other embodiments, flexures may be included that wrap around a portion of the golf club head body or entirely around the golf club head body. As shown in
In additional embodiments, a compliant flexure may be combined with a multi-material, light density cover member, as shown in
Cover 144 is generally a strip of material that is disposed across flexure 142 to generally enclose flexure 142. Cover 144 may be dimensioned so that it covers a portion or all of flexure 142, and it may extend into portions of golf club head 130 that do not include flexure. For example, and as shown in
The cover may be included to both assist in the control of the address position of the golf club head when the sole is placed on the playing surface and to eliminate undesirable aesthetics of the flexure. In particular, the cover may be included to tune the visual face angle of the golf club head when the head is placed on the playing surface by altering the contact surface of the golf club head. The cover may be configured to wrap around a perimeter of the golf club head to the crown and may replace a portion of the material of the perimeter to create a lower density body structure to provide additional discretionary mass, a lower and/or deeper center of gravity location and a higher moment of inertia, thus improving performance and distance potential.
In effect, cover provides crown compliance and the flexure provides sole compliance. As a further alternative, the cover may be removed from the flexure so that it only provides compliance in portions of the golf club head that are away from the sole. In such an example, the dimensions of the components are preferably in the ranges described with regard to
Referring now to
Golf club head 150 has a hollow body construction that is defined by a sole 152, a crown 154, a skirt 156, a face 158 and a hosel 160. Flexure 162 is formed in a forward portion of the golf club head and extends generally across the golf club head in a heel to toe direction through the sole and skirt. Flexure 162 generally includes a central portion 164, a toe portion 166 and a heel portion 168. As described above, the portions of flexure 162 are disposed at varied spatial relationships relative to the face plane so that central portion 164 is further aftward from the face plane compared to toe portion 166 and heel portion 168. Further, flexure 162 includes heel and toe extensions 170, 172 that extend from the heel and toe portions 168, 166, respectively along skirt 156 aftward. Heel and toe extensions 170, 172 may also extend aftward and meet at a location on the skirt or sole.
In additional embodiments, the flexure is provided primarily by a multi-material construction. Referring to
Flexure 192 is constructed of a material that provides a lower Young's Modulus than the adjacent portions of face portion 194 and rear body portion 196. Preferably, flexure 192, face portion 194, and rear body portion 196 are constructed from materials that can be easily coupled, such as by welding. For example, face portion 194 and rear body portion 196 are preferably constructed from a first titanium alloy and flexure 192 is constructed from a beta-titanium alloy as described in greater detail below. Flexure 192 may be constructed so that it has a thickness that is about equal to the thickness of the adjacent portions and so that the outer surface of flexure is flush with the outer surface of the adjacent portions, as shown in
Alternatively, a carbon composite ring may be incorporated for flexure 192 that provides a lower stiffness. The joint configuration, ring geometry (such as the ring width and thickness which may vary with the location in the ring), ring position, fiber orientation, resin type and percentage resin content are all parameters that are selected to optimize the flexibility of flexure 192 so that the outgoing ball speed is improved across the face of the driver while the durability of the golf club head is maintained. Preferably, a carbon composite flexure is bonded to an adjacent metallic face portion and an adjacent metallic rear body portion. As an example, the flexure may be a ring having a width in a range of about 12.0 mm to about 20.0 mm and a thickness of about 0.5 mm to about 3.0 mm and the thickness may vary depending on the location around the perimeter.
A multi-material flexure is incorporated into the golf club head of
Flexure 202 includes a front member 218, a central member 220, and an aft member 222. Preferably, the materials are chosen so that front member 218 and aft member 222 are easily coupled to face portion 204 and rear body portion 206 and so that central member 220 is thin and flexible enough to provide an extra vibration mode having a frequency in a range of about 2900 Hz to about 4000 Hz. In an embodiment, front member 218 and aft member 222 are metallic, and central member 220 is interposed between front member 218 and aft member 222 and is constructed of a carbon fiber composite. Preferably, aft member 222 is spaced from an interface between face 208 and front member 218 by at least 6.0 mm and more preferably, at least 12.0 mm. Hosel 216 may be constructed of metallic and/or non-metallic materials. In an embodiment, face portion 204 and rear body portion 206 are constructed of a titanium alloy, front member 218 and aft member 222 are constructed of a lower density, and preferably lower modulus, material than titanium, such as an aluminum or magnesium alloy, and central member 220 is constructed of a carbon fiber composite that is thin and flexible enough to provide the desired frequency response. Additionally, the front member and/or the aft member may be co-molded with the composite central member. Generally, the materials are selected to provide adequate bonding strength between the components using common practices, such as adhesive bonding.
Golf club heads of the present invention may also include a flexure that extends across the interface between the rear portion of the golf club head and the face, as shown in
The flexure has a selected stiffness to allow the face to deflect globally in concert with the deflection that occurs locally at the impact point. Similar to previous embodiments, flexure 242 is tuned so impact imparts a frequency of vibration across the flexure that is about 2900 Hz to about 4000 Hz. The properties of the ring are selected as an additional means of controlling and optimizing the COR, and corresponding characteristic time (CT), values across the face, especially for ball impacts that are away from the ideal impact location.
Flexure 242 is located generally around the perimeter of face 238 and so that it extends across the transitional curvature from the face of golf club head 230 to the rear portion of the golf club head, e.g., sole 232, crown 234 and skirt 236. Flexure 242 may be discontinuous, as shown, so that it is interrupted by the hosel portion of the golf club head. Flexure 242 terminates at flanges that provide coupling features for mounting flexure 242 in golf club head 230. It should be appreciated that coupling features may be surfaces provided to form butt joints, lap joints, tongue and groove joints, etc. Flexure 242 includes a face flange 244 and a rear flange 246. Face flange 244 is coupled to a perimeter edge 248 of face 238. Portions of rear flange 246 are coupled to portions of perimeter edges of sole 232, crown 234 and skirt 236, such as by being coupled to a crown flange 250 and a sole flange 252. Preferably, the face and rear flanges are between about 2.0 mm and about 12.0 mm.
Flexure 242 is preferably constructed of a material that provides a lower Young's modulus than the adjacent portions of the golf club head. Preferably, flexure 242, face 238, and the rear portion of golf club head 230 are constructed from materials that can be easily coupled, such as by welding. For example, face 238 and the rear portion are preferably constructed from a first titanium alloy and flexure 242 is constructed from a beta-titanium alloy as described in greater detail below.
Alternatively, flexure 242 may be constructed from a carbon fiber composite ring that provides a lower stiffness. The joint configuration, ring geometry, ring position, fiber orientation, resin type and percentage resin content are all parameters that are selected to optimize the flexibility of flexure 242 so that the outgoing ball speed is improved across the face of the driver while the durability of the golf club head is maintained. Preferably, a carbon composite flexure is bonded to an adjacent metallic face and an adjacent metallic rear body portion.
In another embodiment, shown in
Similar to previous embodiments, flexure 272 is tuned so impact imparts a frequency of vibration across the flexure that is about 2900 Hz to about 4000 Hz. Flexure 272 is located around the perimeter of face 268 and so that it extends across the transitional curvature from the face of golf club head 260 to the rear portion of the golf club head, e.g., sole 262, crown 264 and skirt 266. Flexure 272 terminates at flanges that provide examples of coupling features for mounting flexure 272 in golf club head 260. In particular, flexure 272 includes a face flange 274 and a rear flange 276. Face flange 274 is coupled to a perimeter flange 278 of face 268. Portions of rear flange 276 are coupled to portions of perimeter edges of sole 262, crown 264 and skirt 266, such as by being coupled to a crown flange 280 and a sole flange 282.
Flexure 272 is preferably constructed of a material that provides a lower Young's modulus than the adjacent portions of the golf club head. Preferably, flexure 272, face 268, and the rear portion of golf club head 260 are constructed from materials that can be easily coupled, such as by welding. For example, face 268 and the rear portion are preferably constructed from a first titanium alloy and flexure 272 is constructed from a beta-titanium alloy as described in greater detail below.
In another embodiment, shown in
In the present embodiment, front interface member 294 and aft interface member 298 are both constructed as annular members that are interposed between the adjacent components. Front interface member 294 includes a face flange 302 that is coupled to face member 296 with a lap joint, and a flexure flange 304 that is coupled to flexure 292 with a lap joint. A portion of front interface member 294 is exposed and forms a portion of the front surface of golf club head 290. Interface member 294 spaces a forward edge of flexure 292 from a perimeter edge of face member 296. Aft interface member 298 includes a rear body flange 306 that is coupled to aft body member 300 and a flexure flange 308 that is coupled to flexure 292. Aft interface member 298 space aft body member 300 and flexure 292.
Golf club head 290 has a multi-material construction. In an example, aft body member 300 and face member 296 are constructed of titanium alloys, and may be constructed of the same titanium alloy, such as Tib-4. Front interface member 294 and aft interface member 298 are constructed of a material selected to be coupled to the materials of face member 296, flexure 292 and aft body member 300. In an example, the interface members are constructed of an aluminum alloy and flexure is constructed from a carbon fiber composite. It should further be appreciated, that the interface member 298 need not be constructed with a constant cross-sectional shape.
A golf club head 320, shown in
Front interface member 324 and aft interface member 328 are both constructed as annular members that are interposed between the adjacent components. Front interface member 324 includes a face flange 332 that is coupled to face member 326 with a lap joint. Front interface member 324 also includes a flexure flange 334 that is coupled to a front flange 340 of flexure 322. A portion of front interface member 324 is exposed and forms a portion of the front surface of golf club head 320. Interface member 324 spaces a forward edge of flexure 322 from a perimeter edge of face member 326. Aft interface member 328 includes a rear body flange 336 that is coupled to aft body member 330 and a flexure flange 338 that is coupled to flexure 322. Aft interface member 328 spaces aft body member 330 and flexure 322.
Golf club head 320 has a multi-material construction. In an example, aft body member 330 and face member 326 are constructed of titanium alloys, and may be constructed of the same titanium alloy, such as Tib-4. Front interface member 324 and aft interface member 328 are constructed of a material selected to be coupled to the materials of face member 326, flexure 322 and aft body member 330. In an example, the interface members are constructed of an aluminum alloy and flexure is constructed from a carbon fiber composite.
Referring to
Flexure 352 is interposed between face 354 and a rear portion of golf club head 350. Flexure 352 is generally an annular member that has a U-shaped cross-sectional shape so that it includes a forward flange 362 and an aft flange 364. Forward flange 362 is coupled to a face flange 366 of face 354, and aft flange 364 is coupled to a flange of the rear portion of the golf club that includes a crown flange 368 and a sole flange 370.
Embodiments are illustrated in
As shown in
The configuration of the flexure of each of the embodiments may be selected from many different alternatives to provide a tuned behavior during impact with a golf ball.
In another embodiment, shown in
In additional embodiments, a flexure is formed from flanges and a generally channel-shaped flexure component. Referring to
In a similar embodiment, illustrated in
In another embodiment, illustrated in
Referring to
In another embodiment, illustrated in
Referring to
As described above, the flexure of the present invention provides lower stiffness locally in a portion of the golf club head. Generally the lower stiffness may be achieved by selecting the geometry of the flexure, such as by altering the shape and/or cross-sectional thickness, and/or by selecting the material of portions of the flexure. Materials that may be selected to provide the lower stiffness flexure include low Young's modulus beta (β), or near beta (near-β), titanium alloys.
Beta titanium alloys are preferable because they provide a material with relatively low Young's modulus. The deflection of a plate supported at its perimeter under an applied stress is a function of the stiffness of the plate. The stiffness of the plate is directly proportional to the Young's modulus and the cube of the thickness (i.e., t3). Therefore, when comparing two material samples that have the same thickness and differing Young's moduli, the material having the lower Young's modulus will deflect more under the same applied force. The energy stored in the plate is directly proportional to the deflection of the plate as long as the material is behaving elastically and that stored energy is released as soon as the applied stress is removed. Thus, it is desirable to use materials that are able to deflect more and consequently store more elastic energy.
Additionally, it is preferable to match the frequency of vibration of a golf club face with the frequency of vibration of a golf ball to maximize the golf ball speed off the face after an impact. The frequency of vibration of the face depends on the face parameters, such as the material's Young's modulus and Poisson's ratio, and the face geometry. The alpha-beta (α-β) Ti alloys typically have a modulus in the range of 105-120 GPa. In contrast, current β-Ti alloys have a Young's modulus in the range of 48-100 GPa.
The material selection for a golf club head must also account for the durability of the golf club head through many impacts with golf balls. As a result, the fatigue life of the face must be considered, and the fatigue life is dependent on the strength of the selected material. Therefore, materials for the golf club head must be selected that provide the maximum ball speed from a face impact and adequate strength to provide an acceptable fatigue life.
The β-Ti alloys generally provide low Young's modulus, but are also usually accompanied by low material strength. The β-Ti alloys can generally be heat treated to achieve increases in strength, but the heat treatment also generally causes an increase in Young's modulus. However, β-ti alloys can be cold worked to increase the strength without significantly increasing the Young's modulus, and because the alloys generally have a body centered cubic crystal structure they can generally be cold worked extensively.
Preferably, a material having strength in a range of about 900-1200 MPa and a Young's modulus in a range of about 48-100 GPa is utilized for portions of the golf club head. For example, it would be preferably to use such a material for the face and/or flexure and/or flexure cover of the golf club head. Materials exhibiting characteristics in those ranges include titanium alloys that have generally been referred to as Gum Metals.
Although less preferable, heat treatment may be used on β-Ti to achieve an acceptable balance of strength and Young's modulus in the material. Previous applications of β-titanium alloys generally required heat treating to maximize the strength of the material without controlling Young's modulus. Titanium alloys go through a phase transition from hexagonal close packed crystal structure α phase to a body centered cubic β phase when heated. The temperature at which this transformation occurs is called the β-transus temperature. Alloying elements added to titanium generally show either a preference to stabilize the α phase or the β phase, and are therefore referred to as α stabilizers or β stabilizers. It is possible to stabilize the β phase even at room temperature by alloying titanium with a certain amount of β stabilizers. However, if such an alloy is re-heated to elevated temperature, below the β-transus temperature, the β phase decomposes and transforms into α phase as dictated by the thermodynamic rules. Those alloys are referred to as metastable βtitanium alloys.
While the thermodynamic laws only predict the formation of α phase, in reality a number of non-equilibrium phases appear on the decomposition of the β phase. These non-equilibrium phases are denoted by α′, α″, and ω. It has been reported that each of these phases has different Young's moduli and that the magnitude of the Young's modulus generally conforms with β<α″<α<ω. Thus, it is speculated that if one desires to increase the strength of β-titanium through heat treatment, it would be advantageous to do it in such a manner that the material includes α″ phase as a preferred decomposition product and we eliminate, or minimize the formation of α and ω phases. The formation of α″ phase is facilitated by quenching from the α+β region on the material phase diagram, which means the alloy should be quenched from below the β-transus temperature. Therefore, preferably a β-Ti alloy that has been heat treated to maximize the formation of α″ phase from the β phase is used for a portion of the golf club head.
The heat treatment process is selected to provide the desired phase transformation. Heat treatment variables such as maximum temperature, time of hold, heating rate, quench rate are selected to create the desired material composition. Further, the heat treatment process may be specific to the alloy selected, because the effect of different β stabilizing elements is not the same. For example, a Ti—Mo alloy would behave differently than Ti—Nb alloy, or a Ti—V alloy, or a Ti—Cr alloy; Mo, Nb, V and Cr are all β stabilizers but have an effect of varying degree. The β-transus temperature range for metastable β-Ti alloys is about 700° C. to about 800° C. Therefore, for such alloys the solution treating temperature range would be about 25-50 Celsius degrees below the β-transus temperature, in practical terms the alloys would be solution treated in the range of about 650° C. to about 750° C. Following water quenching, it is possible to age the β-Ti alloys at low temperature to further increase strength. Strength of the solution treated material was measured to be about 650 MPa, while the heat treated alloy had a strength of 1050 MPa.
Examples of suitable beta titanium alloys include: Ti-15Mo-3Al, Ti-15Mo-3Nb-0.3O, Ti-15Mo-5Zr-3Al, Ti-13Mo-7Zr-3Fe, Ti-13Mo, Ti-12Mo-6Zr-2Fe, Ti—Mo, Ti-35Nb-5Ta-7Zr, Ti-34Nb-9Zr-8Ta, Ti-29Nb-13Zr-2Cr, Ti-29Nb-15Zr-1.5Fe, Ti-29Nb-10Zr-0.5Si, Ti-29Nb-10Zr-0.5Fe-0.5Cr, Ti-29Nb-18Zr—Cr-0.5Si, Ti-29Nb-13Ta-4.6Zr, Ti—Nb, Ti-22V-4Al, Ti-15V-6Cr-4Al, Ti-15V-3Cr-3Al-3Sn, Ti-13V-11Cr, Ti-10V-2Fe-3Al, Ti-5Al-5V-5Mo-3Cr, Ti-3Al-8V-6Cr-4Mo-4-Zr, Ti-1.5Al-5.5Fe-6.8Mo, Ti-13Cr-1Fe-3Al, Ti-6.3Cr-5.5Mo-4.0Al-0.2Si, Ti—Cr, Ti—Ta alloys, the Gum Metal family of alloys represented by Ti+25 mol % (Ta, Nb, V)+(Zr, Hf, O), for example, Ti-36Nb-2Ta-3Zr-0.35O, etc (by weight percent). Near beta titanium alloys may include: SP-700, TIMET 18, etc.
In general, it is preferred that a face cup or face insert of the inventive golf club head be constructed from α-β or near-β titanium alloys due to their high strength, such as Ti-64, Ti-17, ATI425, TIMET 54, Ti-9, TIMET 639, VL-Ti, KS ELF, SP-700, etc. Further, the rear portion of the golf club body (i.e., the portion other than the face cup, face insert, flexure and flexure cover) is preferably made from α, α-β, or βtitanium alloys, such as Ti-8Al-1V-1Mo, Ti-8Al-1Fe, Ti-5Al-1Sn-1Zr-1V-0.8Mo, Ti-3Al-2.5Sn, Ti-3Al-2V, Ti-64, etc.
As described previously, the flexure may be constructed as a separate component and attached to the remainder of a golf club head body. For example, the flexure component may be stamped and formed from wrought sheet material and the remainder of the body constructed as one or more cast components. Stamping a flexure component may be preferable over casting the flexure because casting can introduce mechanical shortcomings. For example, cast materials often suffer from lower mechanical properties as compared to the same material in a wrought form. As an example, Ti-64 in cast form has mechanical properties about 10%-20% lower as compared to wrought Ti-64. This is because the grain size in castings is significantly larger as compared to the wrought forms, and generally finer grain size results in higher mechanical properties in metallic materials.
Further, titanium castings also develop a surface layer called “alpha case”, a region at the surface that has predominantly alpha phase of titanium that results from titanium that is enriched with interstitial oxygen. The alpha phase in and of itself is not detrimental, but it tends to be very hard and brittle so in fatigue applications, such as repeated golf ball impacts that cause repeated flexing, the alpha case can compromise the durability of the component.
Most titanium alloys are almost impossible to form at room temperature. Thus, the titanium alloys have to be heated to an elevated temperature to form them. The temperature necessary to form the alloy will depend on the alloy's composition, and alloys that have higher beta transus temperature typically require higher forming temperatures. Exposure to elevated temperature results in lowered mechanical properties when the material is cooled down to ambient temperature. Additionally, the exposure to elevated temperature results in the formation of an oxide layer at the surface. This oxide layer is almost like the “alpha case” discussed above except that it typically does not extend as deep into the material. Thus, it is beneficial if the forming temperature can be lowered.
Generally, if using Ti-64 as a baseline since it is commonly used in the construction of metal wood type golf club heads, alloys that have beta transus temperatures that are lower than that of Ti-64 can provide a significant benefit. For example, one such alloy is ATI 425, which has a beta transus temperature in the range of about 957°-971° C., while Ti-64 has a beta transus temperature of about 995° C. Thus, it can be expected that ATI 425 can be formed at a lower temperature as compared to Ti-64. Since ATI 425 has mechanical properties comparable to Ti-64 at room temperature, it is expected that a sole fabricated from ATI 425 alloy will be stronger as compared to a sole made from Ti-64. In addition, ATI 425 generally has better formability as compared to Ti-64, so in an example, a flexure is formed of ATI 425 sheet material and will experience less cross-sectional thinning than a flexure formed of a Ti-64 sheet material. Further, ATI 425 may be cold formable which would further result in a stronger component.
In an example, a multi-material golf club head is constructed from components constructed of Ti-64 and ATI 425. A body including a crown, a sole or partial sole, a skirt, a hosel and a face flange may be cast of Ti-64. Then a portion of the sole may be formed by a flexure component that is constructed from ATI 425 sheet material and welded to the cast Ti-64 body, such as in a slot or recess, such as in the configuration shown in
Various manufacturing methods may be used to construct the various components of the golf club head of the present invention. Preferably all of the components are joined by welding. The welding processes may be manual, such as TIG or MIG welding, or they may be automated, such as laser, plasma, e-beam, ion beam, or combinations thereof. Other joining processes may also be utilized if desired or required due to the material selections, such as brazing and adhesive bonding.
The components may be created using stamping and forming processes, casting processes, molding processes and/or forging processes. As used herein, forging is a process that causes a substantial change to the shape of a specimen, such as starting with a bar and transforming it into a sheet, that characteristically includes both dimensional and shape changes. Additionally, forging generally is performed at higher temperature and may include a change in the microstructure of the material, such as a change in the grain shape. Forming is generally used to describe a process in which a material is shaped while generally retaining the dimension of the material, such as by starting with a sheet material and shaping the sheet without significantly changing the thickness. The following are examples of material selections for the portions of the golf club head utilizing stamping and forming processes:
The density of βalloys is generally greater than the density of α-β or a alloys. As a result, the use of βalloys in various portions of the golf club head will result in those portions having a greater mass. Light weight alloys may be used in the rear portion of the body so that the overall golf club head mass may be maintained in a desired range, such as between about 170 g and 210 g for driver-type golf club heads. Materials such as aluminum alloys, magnesium alloys, carbon fiber composites, carbon nano-tube composites, glass fiber composites, reinforced plastics and combinations of those materials may be utilized.
While various descriptions of the present invention are described above, it should be understood that the various features of each embodiment could be used alone or in any combination thereof. Therefore, this invention is not to be limited to only the specifically preferred embodiments depicted herein. Further, it should be understood that variations and modifications within the spirit and scope of the invention might occur to those skilled in the art to which the invention pertains. For example, the face insert may have thickness variations in a step-wise continuous fashion. In addition, the shapes and locations of the slots are not limited to those disclosed herein. Accordingly, all expedient modifications readily attainable by one versed in the art from the disclosure set forth herein that are within the scope and spirit of the present invention are to be included as further embodiments of the present invention. The scope of the present invention is accordingly defined as set forth in the appended claims.
This application is a continuation of U.S. patent application Ser. No. 13/720,885, filed on Dec. 19, 2012, currently pending, which is a continuation-in-part of U.S. patent application Ser. No. 13/618,963, filed on Sep. 14, 2012, currently pending, the disclosures of which are hereby incorporated by reference in their entireties.
| Number | Date | Country | |
|---|---|---|---|
| Parent | 13720885 | Dec 2012 | US |
| Child | 14485571 | US |
| Number | Date | Country | |
|---|---|---|---|
| Parent | 13618963 | Sep 2012 | US |
| Child | 13720885 | US |
