Patent Application
20230173349
During the game of golf, a golfer may often desire to hit a golf ball further. For instance, with a driver, the golfer may desire to hit the golf ball as far as possible. One factor in the distance the golf ball travels is the club head speed of the golf club as it is being swung. As a golf club is swung by a golfer, the golf club experiences significant drag effects that require greater power from the golfer to achieve higher swing speeds. Thus, a reduction in drag of the golf club head allows for higher club head speeds with the same amount of effort from the golfer.
It is with respect to these and other general considerations that the aspects disclosed herein have been made. Also, although relatively specific problems may be discussed, it should be understood that the examples should not be limited to solving the specific problems identified in the background or elsewhere in this disclosure.
Examples of the present disclosure describe improved golf club heads with improved aerodynamic properties. In an aspect, the technology relates to a metal-wood type golf club head having improved aerodynamic properties. The golf club head includes a striking face; a sole connected to a bottom side of the striking face; a crown connected to a top side of the striking face; and an asymmetric hosel extending from the crown at a heelward side of the golf club head, the hosel including a hosel opening configured to receive a golf club shaft defining a shaft axis, wherein the hosel comprises at least one tripping structure on an exterior of the hosel, an uppermost point at a height (HH), a midpoint at half the height (HH), and an exterior. At the midpoint, a frontmost point of the exterior of the hosel is a distance DHF1/2 from the shaft axis; and at the midpoint, a rearmost point of the exterior of the hosel is a distance DHR1/2 from the shaft axis, the distance DHR1/2 is 25%-70% greater than the distance DHF1/2.
In an example, at the uppermost point of the hosel, a frontmost point of the exterior of the hosel is a distance DHFMIN from the shaft axis; and at the uppermost point of the hosel, a rearmost point of the exterior of the hosel is a distance DHRMIN from the shaft axis, the distance DHRMIN being 5%-15% greater than the distance DHFMIN. In another example, at a lowest point of the hosel where the hosel meets the crown, a frontmost point of the exterior of the hosel is a distance DHFMAX from the shaft axis; and at the lowest point of the hosel, the rearmost point of the exterior of the hosel is a distance DHRMAX from the shaft axis, the distance DHRMAX being 80%-120% greater than the DHFMAX distance. In yet another example, the golf club head further includes an asymmetric ferrule coupled to the hosel, the ferrule having an uppermost point at a height (HF) above the uppermost point of the hosel and a lowermost point where the ferrule contacts the hosel, and: at the uppermost point of the ferrule, a frontmost point of the exterior of the ferrule is a distance DFFMIN from the shaft axis; and at the uppermost point of the ferrule, a rearmost point of the exterior of the ferrule is at a distance DFRMIN from the shaft axis, wherein the distance DFRMIN is less than 5% greater than the distance DFFMIN. In still another example, at the lowermost point of the ferrule, the frontmost point of the exterior of the ferrule is a distance DFFMAX from the shaft axis; and at the lowermost point of the ferrule, the rearmost point of the exterior of the ferrule is a distance DFRMAX from the shaft axis, the distance DFRMAX being 25%-70% greater than the distance DFFMAX. In still yet another example, the golf club head defines a front-to-back axis, and wherein the distance DHF1/2 and the distance DHR1/2 are measured along an extension axis, the extension axis intersecting the shaft axis and being offset from the front-to-back axis by 5-15 degrees. In a further example, a cross section of the hosel is shaped as an airfoil.
In another example, the cross section of the hosel has a distance DFOIL20 between exterior surfaces of the hosel, measured along an axis perpendicular to the extension axis, that is 50%-70% of a maximum distance DCENTER between the exterior surfaces of the hosel as measured through a center of the hosel opening along the axis perpendicular to the extension axis. In yet another example, the at least one tripping structure is formed as a ridge or a groove having a height or depth of between 0.005 inches and 0.03 inches.
In another aspect, the technology relates to a metal-wood type golf club head having improved aerodynamic properties. The golf club head includes a striking face; a sole connected to a bottom side of the striking face; a crown connected to a top side of the striking face; an asymmetric hosel extending from the crown at a heelward side of the golf club head, the hosel including a hosel opening configured to receive a golf club shaft defining a shaft axis, wherein the hosel comprises at least one tripping structure on an exterior of the hosel, an uppermost point at a height (HH), a midpoint at half the height (HH), and an exterior, wherein: at the midpoint, a frontmost point of the exterior of the hosel is a distance DHF1/2 from the shaft axis; and at the midpoint, a rearmost point of the exterior of the hosel is a distance DHR1/2 from the shaft axis, the distance DHR1/2 is 25%-70% greater than the distance DHF1/2; and an asymmetric ferrule further comprises an asymmetric ferrule coupled to the hosel, the ferrule having an uppermost point at a height (HF) above the uppermost point of the hosel and a lowermost point where the ferrule contacts the hosel, wherein: at the uppermost point of the ferrule, a frontmost point of the exterior of the ferrule is a distance DFFMIN from the shaft axis; and at the uppermost point of the ferrule, a rearmost point of the exterior of the ferrule is at a distance DFRMIN from the shaft axis, wherein the distance DFRMIN is less than 5% greater than the distance DFFMIN.
In an example, at the uppermost point of the hosel, a frontmost point of the exterior of the hosel is a distance DHFMIN from the shaft axis; and at the uppermost point of the hosel, a rearmost point of the exterior of the hosel is a distance DHRMIN from the shaft axis, the distance DHRMIN being 5%-15% greater than the distance DHFMIN. In another example, at a lowest point of the hosel where the hosel meets the crown, a frontmost point of the exterior of the hosel is a distance DHFMAX from the shaft axis; and at the lowest point of the hosel, the rearmost point of the exterior of the hosel is a distance DHRMAX from the shaft axis, the distance DHRMAX being 80%-120% greater than the DHFMAX distance. In yet another example, at the lowermost point of the ferrule, the frontmost point of the exterior of the ferrule is a distance DFFMAX from the shaft axis; and at the lowermost point of the ferrule, the rearmost point of the exterior of the ferrule is a distance DFRMAX from the shaft axis, the distance DFRMAX being 25%-70% greater than the distance DFFMAX. In still another example, the golf club head defines a front-to-back axis, and wherein the distance DHF1/2, the distance DHR1/2, the distance DFFMIN, and the distance DFRMIN are measured along an extension axis, the extension axis intersecting the shaft axis and being offset from the front-to-back axis by 5-15 degrees. In still yet another example, the at least one tripping structure is formed as a ridge or a groove having a height or depth of between 0.005 inches and 0.03 inches.
In another aspect, the technology relates to a metal-wood type golf club head having improved aerodynamic properties. The golf club head includes a striking face; a sole connected to a bottom side of the striking face; a crown connected to a top side of the striking face; and an asymmetric hosel extending from the crown at a heelward side of the golf club head, the hosel including a hosel opening configured to receive a golf club shaft defining a shaft axis, wherein the hosel comprises at least one tripping structure on an exterior of the hosel, an uppermost point at a height (HH), a midpoint at half the height (HH), and an exterior, wherein: at the midpoint, a frontmost point of the exterior of the hosel is a distance DHF1/2 from the shaft axis as measured along an extension axis that intersects the shaft axis is offset from a front-to-back axis of the golf club head by 5-15 degrees; and at the midpoint, a rearmost point of the exterior of the hosel is a distance DHR1/2 from the shaft axis as measured along the extension axis, the distance DHR1/2 is 25%-70% greater than the distance DHF1/2.
In an example, at the uppermost point of the hosel, a frontmost point of the exterior of the hosel is a distance DHFMIN from the shaft axis measured along the extension axis; and at the uppermost point of the hosel, a rearmost point of the exterior of the hosel is a distance DHRMIN from the shaft axis measured along the extension axis, the distance DHRMIN being 5%-15% greater than the distance DHFMIN. In another example, at a lowest point of the hosel where the hosel meets the crown, a frontmost point of the exterior of the hosel is a distance DHFMAX from the shaft axis measured along the extension axis; and at the lowest point of the hosel, the rearmost point of the exterior of the hosel is a distance DHRMAX from the shaft axis measured along the extension axis, the distance DHRMAX being 80%-120% greater than the DHFMAX distance. In yet another example, the golf club head further includes an asymmetric ferrule coupled to the hosel, the ferrule having an uppermost point at a height (HF) above the uppermost point of the hosel and a lowermost point where the ferrule contacts the hosel, wherein: At the uppermost point of the ferrule, a frontmost point of the exterior of the ferrule is a distance DFFMIN from the shaft axis measured along the extension axis; and at the uppermost point of the ferrule, a rearmost point of the exterior of the ferrule is at a distance DFRMIN from the shaft axis measured along the extension axis, wherein the distance DFRMIN is less than 5% greater than the distance DFFMIN. In yet another example, the at least one tripping structure is formed as a ridge or a groove having a height or depth of between 0.005 inches and 0.03 inches.
In an aspect, the technology relates to a metal-wood type golf club head having improved aerodynamic properties. The golf club head includes a striking face; a sole; a crown; and a plurality of vortex generators positioned in at least one of: an aft half of the sole or an aft half of the crown.
In an example, the plurality of vortex generators are positioned along an arc defined by an offset distance from an outer perimeter of the crown, the offset distance being between 0.2 inches and 1.2 inches. In another example, the plurality of vortex generators include between 12-22 vortex generators. In still another example, a first subset of the vortex generators have a first extension angle, and a second subset of vortex generators have a second extension angle that is different than the first extension angle. In a further example, the first extension angle is a positive angle and the second extension angle is a negative extension angle. In yet another example, at least one of the vortex generators includes a top surface; a bottom surface; a heel side surface; and a leading edge, wherein the leading edge is curved as is extends from a frontmost point of the vortex generator to the top surface of the vortex generator. In still yet another example, the at least one of the vortex generators has a height between 0.05-0.09 inches.
In another example, the plurality of vortex generators are formed on an aft vortex generator inlay. In yet another example, the crown is made from a first material and the aft vortex generator inlay is made from a second material that is different than the first material.
In another aspect, the technology relates to a metal-wood type golf club head having improved aerodynamic properties. The golf club head includes a striking face; a sole; a crown, the crown defining an aft recess in an aft half of the crown; and an aft vortex generator inlay positioned in the aft recess, the aft vortex generator inlay including a base and vortex generators protruding therefrom.
In an example, the aft recess has a depth; the base of the aft vortex generator inlay has a thickness; and the depth is substantially the same as the thickness. In another example, the vortex generators are positioned along an arc defined by an offset distance from an outer perimeter of the crown, the offset distance being between 0.2 inches and 1.2 inches. In yet another example, the vortex generators protrude from an upper side of the base, and the aft vortex generator inlay further includes at least one attachment extension protruding from a lower surface of the base. In a further example, the aft recess includes at least one receiving hole through which the at least one attachment extension is inserted. In yet another example, the crown is made from a first material, and the aft vortex generator inlay is made from a second material that is different than the first material. In still another example, the crown further defines a forward recess, and the club head further comprises a forward inlay that includes an alignment indicator.
In another aspect, the technology relates to a method for manufacturing a golf club head with improved aerodynamic properties. The method includes forming from a first material, by a first manufacturing process, a crown of the golf club head, the crown including an aft recess; forming from a second material, by a second manufacturing process, an aft vortex generator inlay, the aft vortex generator inlay including a base and vortex generators protruding from an upper surface of the base; and inserting the aft vortex generator inlay into the aft recess.
In an example, the first material is a metallic material and the second material is a non-metallic material. In another example, the first manufacturing process is a casting process and the second manufacturing process is an injection molding process. In still another example, forming the aft vortex generator inlay includes forming at least one attachment extension; forming the crown includes forming at least one receiving hole in the aft recess; and inserting the aft vortex generator inlay into the aft recess includes pushing the at least one attachment extension through the at least one receiving hole.
In an aspect, the technology relates to a metal-wood type golf club head having improved aerodynamic properties, the golf club head having a club head frontmost point and a club head rearmost point. The golf club head includes a striking face, the striking face defining the frontmost point; a sole connected to a bottom side of the striking face, the sole having a rearmost point and a closing ascent angle of less than about 35 degrees, wherein the closing ascent angle is: an angle between (1) a line from the rearmost point of the sole to a sole point, of a projected silhouette of the golf club head from a toe-side viewpoint, located one third a front-to-back length from the club head rearmost point, as measured along a ground plane, and (2) a plane intersecting the sole point and parallel to the ground plane; and a crown connected to a topside of the striking face, the crown including a rearmost point and a closing descent angle of less than about 35 degrees. The closing descent angle is: an angle between (1) a line from the rearmost point of the crown to a crown point, of the projected silhouette of the golf club head from the toe-side viewpoint, located one third a front-to-back length from the club head rearmost point, as measured along a ground plane, and (2) a plane intersecting the crown point and parallel to the ground plane; and within 85%-115% of the closing ascent angle of the sole.
In an example, a club head height of the golf club head is at least 2 inches, and a club head length is greater than 4.0 inches. In another example, the golf club head further includes a skirt, wherein rearmost point on the sole is an intersection point of the sole and a lower boundary of the skirt, and the rearmost point on the crown is an intersection point of the crown and an upper boundary of the skirt. In still another example, the lower boundary is a skirt height above the ground plane, and the skirt height satisfies a head-length-to-skirt-height ratio between 3:1 and 8:1. In a further example, the skirt height is between 12-35 mm. In yet another example, the skirt has a skirt thickness that satisfies a head-length-to-skirt-thickness ratio of 6:1 and 11:1.
In another example, the skirt thickness is between 8-20 mm. In a further example, the closing ascent angle is less than 30 degrees and the closing descent angle is less than 30 degrees. In still another example, the closing ascent angle is within 95%-105% of the closing ascent angle of the sole.
In another aspect, the present technology relates to a metal-wood type golf club head having improved aerodynamic properties. The golf club head includes a striking face, the striking face defining a frontmost point of the golf club head; a sole connected to a bottom side of the striking face; a crown connected to a topside of the striking face; a hosel at a heelward side of the golf club head, the hosel including a hosel opening configured to receive a golf club shaft defining a shaft axis. The hosel includes a first tripping structure extending in a direction from the hosel opening towards the sole, the first tripping structure having a height or depth of between 0.005 inches and 0.03 inches; and a second tripping structure extending a direction from the hosel opening towards the sole, the second tripping structure having a height or depth of between 0.005 inches and 0.03 inches and the second tripping structure located apart from the first tripping structure by angular position of 70-170 degrees, as measured around the shaft axis. The golf club head further includes a skirt connected to, and located in between, the crown and the sole, wherein the skirt includes an aft skirt portion at a rear of the golf club head, wherein the aft skirt portion has: a rearmost point that is a head length from the frontmost point of the striking face; a lower boundary located at an intersection of the skirt and sole, wherein the lower boundary is a skirt height above ground plane, the skirt height satisfies a head-length-to-skirt-height ratio between 3:1 and 8:1; and a skirt thickness that satisfies a head-length-to-skirt-thickness ratio of 5:1 and 14:1. In an example, the skirt thickness is between 8-20 mm. In another example, the skirt height is between 12-35 mm.
In another aspect, the present technology relates to a metal-wood type golf club head having improved aerodynamic properties. The golf club head includes a striking face; a sole connected to a bottom side of the striking face; a crown connected to a topside of the striking face; and a hosel at a heelward side of the golf club head, the hosel including a hosel opening configured to receive a golf club shaft defining a shaft axis. The hosel includes a toeward tripping structure extending in a direction from the hosel opening towards the sole, the toeward tripping structure having a height or depth of between 0.005 inches and 0.03 inches, the toeward tripping structure being positioned at a shaft-axis angular position of 0-80 degrees measured around the shaft axis, wherein a zero-degree shaft-axis angular position corresponds to a direction forward of the golf club head and perpendicular to a plane defined by the striking face; and a heelward tripping structure extending a direction from the hosel opening towards the sole, the heelward tripping structure having a height or depth of between 0.005 inches and 0.03 inches, the heelward tripping structure being positioned at a shaft-axis angular position of 260-340 degrees measured around the shaft axis.
In an example, a position of the toeward tripping structure and a position of the heelward tripping structure are substantially symmetric about a line extending along a 350 degree shaft-axis angle, wherein a zero-degree shaft-axis angular position corresponds to a direction forward of the golf club head and perpendicular to a plane defined by the striking face. In another example, the toeward tripping structure is located at a shaft-axis angular position of 30-60 degrees and the heelward tripping structure is located at a shaft-axis angular position of 280-310 degrees. In yet another example, the heelward tripping structure is located apart from the toeward tripping structure by angular position of less than 100 degrees, as measured around the shaft axis. In still another example, the golf club head further includes a second toeward tripping structure and a third toeward tripping structure, the second toeward tripping structure and the third toeward tripping structure located within 30 degrees of the toeward tripping structure, as measured around the shaft axis.
In another example, the toeward tripping structure is one of a ridge or a groove; and the heelward tripping structure is one of a ridge or a groove. In yet another example, the toeward tripping structure has a length of at least 40 mm, and wherein the hosel is configured to cause tripping from laminar flow to turbulent flow around the hosel at a Reynolds number characteristic of flow conditions experienced by golfers. In still another example, the hosel is adjustable and includes an adjustable component having multiple setting positions, wherein the adjustable component includes a portion of a tripping structure for each setting position such that, at each setting position, one of the tripping structure portions aligns with remaining tripping structure portions on the hosel.
In another aspect, the technology relates to a golf club head that includes a striking face, the striking face defining a frontmost point of the golf club head; a sole connected to a bottom side of the striking face; a crown connected to a top side of the striking face, wherein an aft slice of the golf club head has a centroid height (HCentroid) that is at least 95% of a height of a geometric center of the striking face above a ground plane and a height (HLow) of a lowest point of the aft slice is at least 40% of the height of the geometric center of the striking face above the ground plane, the aft slice being a portion of the golf club head to a rear of a slice line and between an outer perimeter of the golf club head and an offset perimeter slice curve. The slice line extends in a heel-to-toe direction and is located a slice depth rearward from the frontmost point and the slice depth is equal to 70% of a front-to-back length of the golf club head. The offset perimeter slice curve is offset from the outer perimeter of the golf club head by a perimeter offset distance of 0.5 inches.
In an example, the centroid height is equal to at least 50% of a club head height of the golf club head. In another example, the centroid height is at least 28 mm. In still another example, a club head height of the golf club head is at least 2 inches, and a club head length greater than 4.0 inches. In a further example, the centroid height (HCentroid) is less than 35 mm. In yet another example, the height (HLow) of the lowest point of the aft slice is at least 10 mm and less than 15 mm above the ground plane.
In another example, a second aft slice of the golf club head has a centroid height (HCentroid) of at least 28 mm and a height (HLow) of a lowest point of the second aft slice is greater than 6 mm above the ground plane, the second aft slice being a portion of the golf club head to the rear of a second slice line and between the outer perimeter of the golf club head and a second perimeter slice curve. The second slice line extends in the heel-to-toe direction and is located a second slice depth rearward from the frontmost point, the second slice depth being equal to 60% of the front-to-back length of the golf club head; and the second perimeter slice curve is offset from the outer perimeter of the golf club head by a second perimeter offset distance of 1.0 inches.
This Summary is provided to introduce a selection of concepts in a simplified form that are further described below in the Detailed Description. This Summary is not intended to identify key features or essential features of the claimed subject matter, nor is it intended to be used to limit the scope of the claimed subject matter. Additional aspects, features, and/or advantages of examples will be set forth in part in the description which follows and, in part, will be apparent from the description, or may be learned by practice of the disclosure.
Non-limiting and non-exhaustive examples are described with reference to the following figures.
Due to the swing speeds and the shape of golf club heads, many golf clubs, or parts thereof, operate in a Reynolds number regime in which the state of the viscous boundary layer is typically laminar unless forced to a turbulent state by a tripping structure. On bluff bodies, such as the hosel of a golf club, the laminar boundary layer will separate creating a large wake with a relatively low-pressure region. This low pressure acting on the aft facing surface area results in a drag force that retards the speed of the clubhead at impact. In particular, hosels on golf clubs are often constructed having a circular (or nearly so) cross section. Circular cylinders at subcritical (prior to natural transition) Reynolds numbers have a relatively high drag coefficient as compared to those operating with a turbulent boundary layer. By forcing the transition to occur with a tripping structure the drag can be reduced with a resultant increase in clubhead speed. Due to the rotation of the golf club head, the location and dimensions of the tripping structures become important to create the transition from the laminar flow to the turbulent flow.
In addition to tripping structures on the hosel of the golf club head, the shape of the golf club head may also be altered to improve its aerodynamic properties. For instance, changing the shape of the golf club head, such as the striking face, crown, and sole, causes changes in drag experienced by the golf club head during a swing of the golf club head. As an example, what is commonly perceived as an improved aerodynamic shape to the golf club head is to have the crown and the sole meet a singular point at the aft of the golf club head, such as to form a teardrop shape of the golf club head that has a sharper trailing edge. The present technology, however, goes against that traditional perception of the teardrop shape while still lowering drag and improving the overall aerodynamic properties of the golf club head. For instance, the traditional teardrop shape causes a high closure angle of the crown and/or the sole. This high closure angle causes an earlier, or more forward, separation of the turbulent flow over the crown and the sole, which increases the pressure drag experienced by the golf club head during a swing. The present technology changes, and reduces, the closure angles of the crown and/or the sole to move the separation of the turbulent flow further towards the aft the golf club. These reduced closure angles result in a golf club head that may look less aerodynamic but actually results in a golf club that experiences less pressure drag forces and has overall improved aerodynamic properties. The changes to the closure angles of the crown and/or the sole may be accomplished, for example, by raising an aft portion of the skirt further above the ground plane and/or increasing the thickness of the aft portion of the skirt.
The golf club head 100 also includes a hosel 112. The hosel 112 is used to attach a shaft (not depicted) to the golf club head 100. The hosel 112 may be formed into at least a portion of the crown 104 and the heel portion 108. The hosel 112 may also include a ferrule or components of an interchangeable shaft system.
The hosel 112 also includes a plurality of tripping structures 114. In the example depicted, the tripping structures 114 are formed as elongate ridges extending from the top of the hosel towards the sole. This particular pattern has three substantially parallel ridges on both the heelward and toeward side of the hosel. The height of the ridges (e.g., the distance the ridges protrude from the surface of the hosel) may be between 0.005 inches and 0.03 inches. In some examples, the height of the ridges is between 0.009 inches and 0.015 inches.
The length (L1) of the tripping structures 114 may be between 30-70 mm. In some examples, the length (L2) of the tripping structures 114 may be greater than 40 mm. The length of the tripping structures 114 may also be considered as two components, a first length component that extends through a ferrule and any additional hosel components (e.g., adjustable shaft components, rings, sleeves, etc.) and a second length component extending across the body of the club head 100, such as the heel region 108 of the club head 100. The second length component is represented as L2 in
The locations or positions of the tripping structures 114 account for the rotational movement of the club head during a swing of a golf club head. For instance, during the downswing of golf club, the heelward tripping structures 114D-F are more exposed to the airflow, whereas at impact and during the follow through, the toeward tripping structures 114A-C are more exposed to the airflow. Due to the toeward tripping structures 114A-C being located more towards the striking face 102, the toeward tripping structures 114A-C also provide tripping effects during the downswing of the golf club head 100.
The location or position of each of the tripping structures 114 may be described as an angular position around the shaft axis. The angular positions may be described as relative to a toe-to-heel axis 120 or a front-to-back axis 122. The front-to-back axis 122 is an axis that runs from the front of the golf club head 100 to the back of the golf club head, and the toe-to-heel axis 120 is an axis that runs from the toe to heel of the golf club head 100 and is substantially perpendicular to the front-to-back axis 122. For instance, the front-to-back axis 122 may be perpendicular to a plane defined by the striking face 102. In the examples used herein, the front-to-back axis 122 has a zero-degree position pointing forward of the golf club head 100. For instance, the zero-degree shaft-axis angular position may correspond to a direction forward of the golf club head 100 and perpendicular to the plane defined by the striking face 102. The origin of the front-to-back axis 122 and the toe-to-heel axis 120 may be located at the center of the hosel (e.g., at the shaft axis).
The tripping structures 114 on the toeward side of the front-to-back axis 122 are referred to as the toeward tripping structures 114, and the tripping structures 114 that are on the heelward side of the front-to-back axis 122 are referred to as the heelward tripping structures 114. As measured from the front-to-back axis 122, the first toeward tripping structure 114A is located 30 degrees around the shaft axis, as represented by angle α1, as measured in a clockwise direction. The second toeward tripping structure 114B is offset by 15 degrees around the shaft axis from the first toeward tripping structure 114A. The third toeward tripping structure 114C is offset by 15 degrees from the third toeward tripping structure 114C. In other words, the second toeward tripping structure 114B is located 45 degrees around the shaft axis, as represented by angle α2, and the third toeward tripping structure 114C is located 60 degrees around the shaft axis, as represented by angle α3.
Of note, the toeward tripping structures 114A-C are located towards the front of the golf club head 100 from the toe-to-heel axis 120. In other words, the toeward tripping structures are located between 0-90 degrees around the shaft axis as measured from the front-to-back axis 122. By positioning the toeward tripping structures 114A-C towards the front of the golf club head 100, the toeward tripping structures 114A-C are able to provide the tripping effect for more of the downswing of the golf club as the golf club rotates from an open position to a closed position.
As also measured from the front-to-back axis 122, the first heelward tripping structure 114D is located −60 degrees around the shaft axis, as represented by the angle β1. The second heelward tripping structure 114E is offset by 15 degrees around the shaft axis from the first heelward tripping structure 114D. The third heelward tripping structure 114F is offset by 15 degrees around the shaft axis from the second heelward tripping structure 114E. In other words, the second heelward tripping structure 114E is located −75 degrees around the shaft axis, as represented by angle β2, and the third heelward tripping structure 114F is located −90 degrees around the shaft axis, as represented by angle β3. In some examples, the heelward tripping structures may be more easily measured from the toe-to-heel axis 120. For instance, the third heelward tripping structure 114F is aligned with, or parallel to, the heel-to-toe axis 120.
The first toeward tripping structure 114A may be referred to as the frontmost toeward tripping structure 114A, and the first heelward tripping structure 114A may be referred to as the frontmost heelward tripping structure 114D. The frontmost toeward tripping structure 114A and the frontmost heelward tripping structure 114D in the example depicted are positioned 90 degrees apart from one another.
The angular positions of the tripping structures 114 described above are for a particular example, and some variations on the angular positions may also be implemented to achieve the tripping effects described herein. For example, the toeward tripping structures 114 may be located within 0-80 degrees, 10-80 degrees, 10-70 degrees, and/or 30-70 degrees around the shaft axis as measured from the front-to-back axis 122. The heelward tripping structures 114 may be located between −30 to −90, −50 to −90, −60 to −90, and/or −40 to −110 degrees around the shaft axis as measured from the front-to-back axis 122.
The toeward tripping structures 114 and/or the heelward tripping structures 114 may be spaced from one another by an angular amount of 5-25 degrees and/or 10-20 degrees. In some examples, such as the one depicted in
One or more of the toeward tripping structures 114A-C may be symmetrically positioned about radial line of 350 degree (i.e., −10 degree) shaft-axis angle from one or more of the heelward tripping structures 114D-F. For instance, a position of the toeward tripping structure and a position of the heelward tripping structure may be substantially symmetric about a line extending along a 350 degree shaft-axis angle. Such symmetry may improve the overall aerodynamic properties of the hosel 112. As an example, a toeward tripping structure being positioned at a shaft-axis angular position of 0-80 degrees measured around the shaft axis, and a heelward tripping structure may be positioned, symmetrically about the 350 degree line, at a shaft-axis angular position of 260-340 degrees measured around the shaft axis. the toeward tripping structure is located at a shaft-axis angular position of 30-60 degrees and the heelward tripping structure is located at a shaft-axis angular position of 280-310 degrees.
The heights, lengths, and locations of the tripping structures 114 discussed herein are able to trigger a transition from a laminar flow to a turbulent flow around the hosel at the Reynolds numbers and swing speeds typically associated with the swinging of a golf club head. For instance, the tripping structures 114 may be configured to cause tripping from laminar flow to turbulent flow around the hosel at a Reynolds number characteristic of flow conditions experienced by golfers (such as less than 30,000), as the hosel 112 of the golf club head 100 usually is within a 20,000 to 50,000 Reynolds number regime. In addition, the dimensions and locations of the tripping structures 114 are important for causing the transition from the laminar flow to turbulent flow in the proper location. For example, if the tripping occurs too early, the flows will fully separate and not reattach, or if there is a very strong favorable gradient, the flows will relaminarize and then separate—both of which may actually increase drag. The present dimensions and locations of the tripping structures 114 prevent such adverse phenomenon even when the golf club head rotates during a golf swing.
While the tripping structures 114 shown in
The tripping structures 114 may also be formed from tooling marks, that have adequate roughness to transition the boundary layer, positioned in similar locations and orientations as the ridges discussed above. Additional patterns, such as three-dimensional sine waves that are roughly axisymmetric with respect to the shaft or hosel axis, may also be used. The sine waves may also be a function of both position along the shaft or hosel axis and the circumferential position around the hosel. A three-dimensional pattern of interconnect ridges, such as a hexagonal pattern, may also be used as tripping structures 114. Dimples or pimples (e.g., the opposite of dimples) may also be used as tripping structures 114 in some examples.
The example configurable hosel 212 depicted in
The configurable hosel 212 also includes tripping structures 214. The tripping structures 214 may be divided into separate pieces or portions corresponding to the number of different components in the configurable hosel 212. In the example depicted, there are four components of the adjustable hosel 212—the fixed portion 230, the rotatable ring 232, the rotatable sleeve 234, and the ferrule 236. The tripping structures 214 extend across each of the four components. To allow for adjustment of the adjustable hosel 212, each of the tripping structures are separated into four pieces corresponding to the four different components of the adjustable hosel 212. For instance, each tripping structure 214 may have a first piece on the ferrule 236, a second piece on the sleeve 234, a third piece on the ring 232, and a fourth piece on the fixed portion 230. Each of the pieces of the tripping structure 214 may be separated from one another, such as by a cut, or the pieces of the tripping structures 214 may be separately formed as part of the respective components, such as the ring 232 and the sleeve 234. Accordingly, as the adjustable components of the hosel 212 (e.g., the ring 232 and the sleeve 234) are rotated, the corresponding piece of the tripping structure 214 move with the respective adjustable component. For example, the pieces of tripping structures 214 located on the ring 232 move with the ring 232 as the ring 232 is rotated.
The number and/or positions of the tripping structures 214 may be based on the number of different settings available from the adjustable components of the hosel 212. In the example depicted, the ring 232 and the sleeve 234 each have four possible settings (e.g., settings A-D and settings 1-4). Accordingly, four tripping structures 214 may be incorporated into the hosel 212. Each of the four setting positions on the ring 232 and the sleeve 234 are offset by 90 degrees (e.g., 360 degrees divided by four). Thus, the four tripping structures 214 are also offset from one another by 90 degrees. As a result, in any setting combination of the ring 232 and the sleeve 234, the respective pieces of the tripping structures 214 align with other pieces of the tripping structures 214 to form the full-length tripping structures 214. With the offsets of 90 degrees, the tripping structures 214 may be located in the angular positions discussed above with respect to
As another example, if the adjustable components have only three settings, three tripping structures 214 may be included and may be offset by 120 degrees, whereas if the adjustable components have five settings, five tripping structures 214 may be incorporated and may be offset by 72 degrees. The number of tripping structures 214 may be equal to the number of settings, and the offset angle of the tripping structures 214 may be based on the offset angles of the different settings of the adjustable components. In some examples, multiple tripping structures 214 may be included on each of the different settings (such as the tangs of the ring 232). In such examples, the number of tripping structures 214 may be equal to a multiple of the number of settings. For instance, for an adjustable component with four settings, 4, 8, 12, or 16 tripping structures 214 may be included on the hosel 212.
Testing of prototype golf club heads have also demonstrated improvements due to the incorporation of the above tripping structures. For example, testing was performed using a control club (e.g., a club with no hosel tripping structures) and a test golf club head with tripping structures added to the hosel of the control club. Testing was performed by applying the same force to the golf clubs via a robotic swinging system in substantially the same aerodynamic conditions (e.g., location, air temperature, etc.) The results of the testing indicated that the control club had an average swing speed of 105.21-105.59 miles per hour (mph), and the testing club had an average swing speed of 106.07 mph. Thus, with the same force applied, a swing speed increase of 0.48-0.86 mph was observed based on the inclusion of the hosel tripping structures. For the testing, the tripping structures of the test club had a configuration similar to the configuration shown in
Like the golf club heads described above, the golf club head 500 includes a striking face 502, a crown 504, a sole 510, and a hosel 512. The golf club head 500 also has a frontmost point 518 and a rearmost point 516. The frontmost point 518 may also be referred to as a leading edge, and the club head rearmost point 516 may also be referred to as the trailing edge.
The golf club head 500 also includes a skirt 520 or “boat tail” portion that connects the crown 504 and the sole 510. The skirt 520 may be defined as a portion of the club head 500 that is between the crown 504 and the sole 510, and defines a plane having an angle that is substantially different from the planes formed by either the crown 504 or the sole. For instance, the skirt 520 may define a plane that is within 80-120 percent of a loft angle of the golf club head 500. The angle of the plane formed by the skirt 520 may be referred to as the skirt angle. In other examples, the skirt 520 defines a plane that is within 20 degrees of being perpendicular to a ground plane defined by the ground.
The dimensions of the golf club head 500 result in the golf club head 500 experiencing lower drag during a swing of the golf club head 500. The dimensions of the golf club head 500 include a front-to-back length (LFB), a ½ front-to-back length (LFB1/2), and a ⅓ front-to-back length (LFB1/3). The front-to-back length (LFB) is the length between the club head frontmost point 518 and the club head rearmost point 516 as measured along the ground plane. The front-to-back length (LFB) may also be referred to as the head length. The golf club head 500 also has a club head height that is measured from the lowest point on the sole to the highest point on the crown in a direction perpendicular to the ground plane.
Closing descent angles (Φ) and closing ascent angles (θ) are also defined by the golf club head 500. The closing descent angles (Φ) indicate how steeply the crown 504 is closing towards the rear of the golf club head 500. The closing ascent angles (θ) indicate how steeply the sole 510 is closing towards the rear of the golf club head 500.
The closing descent angle (Φ) is defined as an angle between (1) a line from a point on the crown 504, of the projected silhouette of the golf club from the toe-side viewpoint, to the rearmost point 516 of the crown 504 and (2) a plane intersecting the crown point and parallel to the ground plane. The rearmost point 516 of the crown 504 may be an intersection point of the crown 504 and an upper boundary of the skirt 520. The closing descent angles (Φ) may be measured from different points on the golf club head 500. For instance, a half-point closing descent angle (Φ1/2) may be measured from a point on the crown 504 that is halfway between the frontmost point 518 and the rearmost point 516 of the club head 500 (e.g., from a point located the ½ front-to-back length (LFB1/2) from the rearmost point 516 as measured along the ground plane.) A third-point closing descent angle (Φ1/3) may be measured from a point on the crown 504 that is located the ⅓ front-to-back length (LFB1/3) from the rearmost point 516 of the golf club as measured along the ground plane. In the example depicted, the rearmost point 516 of the golf club happens to also be the rearmost point 516 of the crown 504.
The closing ascent angle (θ) is defined as an angle between (1) a line from a point on the sole 510, of the projected silhouette of the golf club from the toe-side viewpoint, to the rearmost point 517 of the sole 510 and (2) a plane intersecting the sole point and parallel to the ground plane. The rearmost point 517 of the sole 510 may be an intersection point of the sole 510 and a lower boundary of the skirt 520. The closing ascent angles (θ) may be measured from different points on the golf club head 500. For instance, a half-point closing ascent angle (θ1/2) may be measured from a point on the sole 510 that is halfway between the frontmost point 518 and the rearmost point 516 of the club head 500 (e.g., from a point located the ½ front-to-back length (LFB1/2) from the rearmost point 516 as measured along the ground plane.) A third-point closing ascent angle (θ1/3) may be measured from a point on the sole 510 that is located the ⅓ front-to-back length (LFB1/3) from the rearmost point 516 of the golf club as measured along the ground plane.
The height and thickness of the skirt 520 also have an impact on the aerodynamics of the golf club head. The height of the skirt may be represented by the height (HRS) of the rearmost point of the sole 510 above or off the ground plane. The rearmost point of the sole 510 represents the lowest point of the skirt 520. The height of the skirt 520 may also be represented by the height (HRC) of the rearmost point 516 of the crown 504 off the ground plane. The thickness (TRear) of the rear portion the skirt 520 shown in the projection may then be defined by the distance between the rearmost point 516 of the crown 504 and the rearmost point 517 of the sole 510. For instance, the thickness (TRear) may be the shortest distance between the rearmost point 516 of the crown 504 and the rearmost point 517 of the sole 510 as measured in the projection.
As discussed above, configuring these dimensions of the golf club head 500 allows for improvements to the aerodynamic properties by reducing the pressure drag forces experienced by the golf club head 500 during a swing. For instance, by raising the aft portion of the skirt 520 or boat tail and/or increasing the thickness of the aft portion of the skirt 520, the closure angles of the crown 504 and the sole may be reduced and controlled. By reducing the closure angles, the separation of the turbulent flow of air over the crown 504 and/or sole 510 may be moved further rearward on the golf club head 500. Delaying the turbulent flow separation (e.g., moving the turbulent flow separation more rearward) results in a lower pressure drag forces acting on the golf club head 500 during the golf club swing. Additional reductions to pressure drag forces may be achieved by bringing the closing ascent angle (θ) closer to the closing descent angles (Φ).
As some examples, the height (HRS) of the rearmost point of the sole 510 off the ground plane may be between 12 mm and 35 mm. The height (HRC) of the rearmost point 516 of the crown 504 off the ground plane may be between 28 and 45 mm. The thickness of the skirt 520 (TRear) may be between 8 and 20 mm. Different combinations of HRS and TRear may be utilized to achieve the aerodynamic benefits of the present technology. For example, as the skirt 520 is raised higher off the ground, the skirt 520 may not need to be as thick to achieve the shallower closure angles of the crown 504 and the sole 510. The thickness of the skirt 520 may also be adjusted based on the height of the skirt 520 to better match the closing ascent angles (θ) of the sole 510 with the closing descent angles (Φ) of the crown 504. These ranges of heights generally represent a heightened and/or thickened skirt 520 as compared to other drivers, which may have HRS values of about 9 mm, HRC values of about 22 mm, and TRear values of about 16 mm.
As will also be understood, the closing ascent angles (θ) of the sole 510 and the closing descent angles (Φ) are also dependent on the height of the golf club head 500 as well as the club length or the front-to-back length (LFB). The height of the golf club head 500 for a driver may be greater than 2 inches (50.8 mm), but may be lower for other types of metal woods, such as fairway metals. In some examples, the height of the golf club head 500 may be between 2 inches (50.8 mm) and 2.8 inches (71.12 mm). For a driver, the front-to-back length (LFB) may be between 4.13 inches (105 mm) to 4.72 inches (120 mm) or between 4 inches (101.6 mm) to 5 inches (127 mm). In some examples, the front-to-back length (LFB) may be less than 4.5 inches (114.3 mm).
Because some of the above dimensions may change as the type of metal wood changes (e.g., from drivers to fairway metals or other types of metal woods), the above dimensions may be better represented as ratios that help maintain the types closure angles of the crown 504 and the sole 510 that provide the improved aerodynamic properties discussed herein. For example, a ratio between (1) the front-to-back length (LFB) (e.g., the head length) and (2) the height (HRS) of the rearmost point of the sole 510 off the ground plane (e.g., the skirt height) may be utilized. This ratio may be referred to as the head-length-to-skirt-height ratio. The head-length-to-skirt-height ratio may be between 3:1 and 8.5:1, between 3.4:1 and 5.8:1, or less than 6:1. The value of the head-length-to-skirt-height ratio may be based on the skirt thickness (TRear) as well. For instance, for the head-length-to-skirt-height ratio may be greater where the skirt thickness (TRear) is smaller. For instance, for a skirt thickness (TRear) between 10-14 mm, the head-length-to-skirt-height ratio may be between 3.46:1 and 5.7:1. For a skirt thickness (TRear) between 16-18 mm, the head-length-to-skirt-height ratio may be between 4.3:1 and 8.5:1.
A ratio between the head length and skirt thickness (TRear) may also be utilized, and such a ratio may be referred to as a head-length-to-skirt-thickness ratio. The head-length-to-skirt-thickness ratio may be between 6:1 and 11:1, between 6.5:1 and 8.5:1, or less than 9:1. The head-length-to-skirt-thickness ratio may also depend on the skirt height similar to how the head-length-to-skirt-height ratio is dependent on the skirt thickness, as discussed above.
The closing descent angles (Φ) and the closing ascent angles (θ) of sole may be within ranges of degrees and the angles may be based on one another to more closely match the closing descent angles (Φ) to the closing ascent angles (θ). The half-point closing descent angle (Φ1/2) may be between 15 and 30 degrees, less than 30 degrees, or less than 20 degrees. The third-point closing descent angle (Φ1/3) 20 and 35 degrees, less than 35 degrees, less than 30 degrees, or less than 25 degrees. For instance, half-point closing ascent angle (θ1/2) may be between 15 and 30 degrees, less than 30 degrees, or less than 20 degrees. The third-point closing ascent angle (θ1/3) may be between 10-35 degrees, less than 35 degrees, or less than 20 degrees. As the closing descent angles (Φ) and the closing ascent angles (θ) become shallower, the golf club head 500 may incur less pressure drag effects.
In addition, as the closing descent angles (Φ) and the closing ascent angles (θ) become more closely matched, the golf club head 500 may also receive less pressure drag effects. For instance, in some examples the respective closing descent angles (Φ) and the closing ascent angles (θ) may be within 85% to 115% of one another. In another example, the respective closing descent angles (Φ) and the closing ascent angles (θ) may be within 95% to 105% of one another. For example, the half-point closing descent angle 01/2) may be within 85% to 115% or 95% to 105% of the half-point closing ascent angle (θ1/2). Similarly, the third-point closing descent angle (Φ1/3) may be within 85% to 115% or 95% to 105% of the third-point closing ascent angle (θ1/3).
Additionally or alternatively, there may be no tangent line to the aft half of the crown 504 in the projected silhouette that is greater than 45 degrees, 40 degrees, or 30 degrees. Stated another way, all tangent lines that can be drawn on the aft half of the crown 504 in the projected silhouette may have an angle relative to the ground plane that is less than or equal to 45 degrees, 40 degrees, or 30 degrees. Similarly, there may be no tangent line to the aft half of the sole 510 in the projected silhouette that is greater than 45 degrees, 40 degrees, or 30 degrees. Stated another way, all tangent lines that can be drawn on the aft half of the sole 510 in the projected silhouette may have an angle relative to the ground plane that is less than or equal to 45 degrees, 40 degrees, or 30 degrees.
The table provided in
Golf club 600a has a skirt thickness of Ta and a skirt height of Ha. Golf club 600b has a skirt thickness of Tb and a skirt height of Hb. Golf club 600c has a skirt thickness of Tc and a skirt height of Hc. Golf club 600d has a skirt thickness of Ta and a skirt height of Ha. Golf club 600e has a skirt thickness of Te and a skirt height of He. Golf club 600f has a skirt thickness of Tf and a skirt height of Hf. Golf club 600g has a skirt thickness of Tg and a skirt height of Hg. Golf club 600h has a skirt thickness of Th and a skirt height of Eh. Golf club 600i has a skirt thickness of Ti and a skirt height of Hi.
As can be seen in the first row of golf club heads 600a-c, raising the skirt height allows for a shallower closing descent angle of the crown. However, with thinner skirt thicknesses, the closing ascent angle of the sole is quite steep. As the thickness of the skirt become increasingly greater from golf club head 600a to golf club head 600c, it can be seen that the closing ascent angle of the sole becomes shallower and becomes closer to the closing descent angle of the crown.
Similar results are seen in the second row, which includes example golf club heads 600d-f. The skirt heights (T) of the golf club heads 600d-f is less than the skirt heights (T) of the golf club heads 600a-c in the first row. The lower skirt height (T) in golf club heads 600d-f result in a steeper closing descent angle of the crown but also results in a shallower closing ascent angle of the crown—especially as the skirt thickness increases.
In the last row, which includes example golf club heads 600g-i, the skirt heights (H) are generally lower than that of the respective golf club heads 600a-f in the first and second row. By moving the skirt height even lower, the closing ascent angle of the sole is further reduced, but the closing descent angle begins to increase more dramatically. As the skirt thickness (T) increases, the closing ascent angle of the sole further decreases to point that it is shallower than the closing descent angle of the crown.
Testing of prototype golf club heads have also shown improvements due to the incorporation of the aerodynamic shaping to modify the skirt heights and thicknesses along with the closing angles. For example, testing was performed using a control club (e.g., a club with a more traditional low skirt height) and a test golf club heads with raised skirts. Testing was performed by applying the same force to the golf clubs via a robotic swinging system in substantially the same aerodynamic conditions (e.g., location, air temperature, etc.) In testing, raising the skirt by 0.25 inches resulted in an increase in club head speed of 0.44 mph, and raising the skirt by 0.5 inches resulted in increases in club head speed of between 0.57-0.91 mph. Golf club heads that included both the raised skirt and the tripping structures discussed above resulted in a combined even greater increase in swing speed.
Raising the skirt and/or thickening the skirt also generally raises the aft portion of the club head 700 to improve the aerodynamic properties of the golf club. To identify the characteristics of the aft portion of the club head 700, an aft slice 760 of the golf club head 700 may be considered. The aft slice 760 is a portion of the golf club head 700 to the rear of a slice line 750 and between an outer perimeter of the golf club head 700 and an offset perimeter slice curve 752. The slice line 750 runs in the heel-to-toe direction (e.g., parallel with a heel-to-toe axis) and is located a slice depth D from the frontmost point of the golf club head. The offset perimeter slice curve 752 is offset from the outer perimeter of the golf club head 700 by a perimeter offset distance P. The offset perimeter slice curve 752 follows the outline or contour of the outer perimeter at the offset position. For instance, an aft portion of the golf cub head 700 to the rear of the slice line 750 may be identified. A perimeter portion that is offset by the perimeter-offset distance P from the outer perimeter of that aft portion is then extracted or identified to form or define the aft slice 760. The aft slice 760 may be formed or extracted computationally by generating a three-dimensional scan of the golf club head or other computer modelling of the golf club head. In the example depicted in
The aft slice 760 also has an aft depth A that is measured from rearmost point of the aft slice 760 to the frontmost point of the aft slice 760 (e.g., slice line 750). The aft depth A of the aft slice 760 is equal to the difference of the front-to-back length of the club head 700 and the slice depth D. In the example depicted in
Two dimensions of the aft slice 760 may be acquired or determined from the projected side-view silhouette of the aft slice 760. The first dimension is a height (HCentroid) of a centroid 762 of the aft portion 760 above a ground plane 770. A centroid of an object may be considered the center of gravity of the solid object assuming uniform density. To calculate the centroid 762 of the aft slice 760, all internal geometry of the aft slice 760 may be filled in (mathematically, computationally, etc.) to be a solid object and assumed to have the same density throughout. The center of gravity of that solid object may then be determined or calculated as the centroid 762. The second dimension is a height (HLow) of the lowest point of the aft slice 760, in the silhouette, above the ground plane 770.
In examples where the slice depth D is 60% of the front-to-back length of the golf club head 700, the aft depth A is 40% of the front-to-back length of the golf club head 700, and perimeter-offset distance P is 1.0 inches, the height (HLow) of the lowest point of the aft slice 760 may be between 5-10 mm, and the centroid height (HCentroid) may be between 28-35 mm. For example, the height (HLow) of the lowest point of the aft slice 760 may be greater than 6 mm, and the centroid height (HCentroid) may be greater than 29 mm.
In examples where the slice depth D is 70% of the front-to-back length of the golf club head 700, the aft depth A is 30% of the front-to-back length of the golf club head 700, and perimeter-offset distance P is 0.5 inches, the height (HLow) of the lowest point of the aft slice 760 may be between 10-15 mm, and the centroid height (HCentroid) may be between 28-35 mm. For example, the height (HLow) of the lowest point of the aft slice 760 may be greater than 10, 11, or 12 mm, and the centroid height (HCentroid) may be greater than 28 mm. In some examples, the centroid height (HCentroid) may be at least 50% of the club head height of the golf club head 700. In some examples, the centroid height (HCentroid) that is at least 95% of a height of a geometric center of the striking face 702 above a ground plane. For instance, the centroid height (HCentroid) may also be greater than or equal to a height of a geometric center of the striking face 702. The height (HLow) of a lowest point of the aft slice is at least 40%, 45%, or 50% of the height of the geometric center of the striking face above the ground plane.
Golf club heads having aft slices 760 with the dimensions discussed above have been shown through testing to have improved aerodynamic properties similar to those discussed above with respect to
Additional or alternative aerodynamic improvements to the golf club head may also be made by attaching vortex generators to the golf club head. As discussed above, golf clubs are bluff bodies that typically result in significant aerodynamic separation, which causes pressure drag that deters the clubhead speed. USGA limitations on fore-to-aft dimension and volume constrain the geometry and ability to eliminate this aerodynamic separation. This issue is particularly acute for driver-type golf club heads with significant face heights that are preferred for their forgiveness and a larger “sweet spot.” The current limitations on clubhead shaping do not allow the simultaneous satisfaction of desired face height, minimal base area, conforming volume, and depth (fore to aft dimension no greater than heel to toe dimensions and less than 5 inches) to eliminate the aerodynamic separation. In golf clubs with steeper closure angles that cause the aerodynamic separation (without the use of vortex generators), the addition of vortex generators can reduce or minimize the turbulent aerodynamic separation with a resulting smaller base area over which the low pressure separated flow acts. This results in a reduction in drag force with a corresponding increase in clubhead speed.
More specifically, addition of vortex generators to the crown and/or the sole of the golf club head enables the viscous boundary layer to be energized. This high energy boundary layer enables larger closure angles and reduced boat tail or aft skirt thicknesses to be used for the golf club head. The reduction in base pressure drag on the boat tail or aft skirt portion results in an increase in clubhead speed with an associated increase in distance of the struck golf ball.
The depiction of the golf club head 800 includes three possible arcs 822 on which the vortex generators 820 may be positioned. Of note, the vortex generators 820 may be placed on only one of the possible arcs 822 depicted in
The shape of the arc 822 may substantially match the aft outer perimeter of the golf club head 800 such that an offset distance remains substantially constant along the arc 822. In some examples, this results in the arc have a constant radius of curvature, and in other examples, the arc 822 may have a variable radius of curvature. For instance, the arc 822 may traverse along a constant slope line of the crown 804 (e.g., a contour line of a topographic representation of the crown 804).
The position of the arc 822, and thus the position of the vortex generators 820, may be configured based on the closure angle of the crown 804. For instance, the position of the arc 822 and the vortex generators 820 may be based on where the turbulent separation of the airflow would occur if the club head 800 did not include the vortex generators 820. More specifically, the arc 822 may be placed slightly forward (e.g., less than 0.2 inches) of where the turbulent separation would have occurred. At such a position, the vortex generators 820 provide the most beneficial effect on the reduction of drag.
As discussed above, a steeper closure angle of the crown results in an earlier, or more forward, turbulent separation. In contrast, a shallower closure angle results in later, or more aft, turbulent separation. Accordingly, for crowns 804 with a steeper closure angle, the offset distance for the arc 822 may be greater, which results in the vortex generators 820 being more forward on the crown 804. For crowns 804 with a shallower closure angle, the offset distance for the arc 822 may be smaller, which results in the vortex generators 820 being more aft on the crown 804. Regardless of the offset position of the arc 822, the vortex generators 820 (or at least 80% of the vortex generators 820) are located in the aft half of the crown 804.
The arc 822 may begin at a first boundary line 824 and end at a second boundary line 826. The first boundary line 824 extends perpendicularly to a tangent line of the perimeter of the aft, toe-side portion of the crown 804. The toe-side tangent line may be where an angle A (defined as the angle between a line parallel to the Z axis and the toe-side tangent line) is between 20-30 degrees. The second boundary line 826 extents perpendicularly to a tangent line of the perimeter of the aft, heel-side portion of the crown 804. The heel-side tangent line may be where an angle B (defined as the angle between a line parallel to the Z axis and the heel-side tangent line) is between 25-35 degrees. The Z axis is an axis that extends in a front-to-back direction of the golf club head 800. In turn, the X axis is an axis that runs in the heel-to-toe direction and is perpendicular to the Z axis.
The number of vortex generators 820 positioned along the respect arc 822 depends on the length of the arc 822, which is in turn dependent on the offset distance of the arc 822 and the position of the first boundary line 824 and the second boundary line 826. As an example, where the offset distance is D3, 10-15 vortex generators 820 may be positioned along the arc 822. Where the offset distance is D2, 14-18 vortex generators 820 may be positioned along the arc 822. Where the offset distance is D1, 17-21 vortex generators 820 may be positioned along the arc 822. In some examples, the offset distance is between 0.2-1.2 inches and there are at least 12 vortex generators placed along the corresponding an arc 822. In such an example, the number of vortex generators 820 may be between 12-22 vortex generators 820.
The vortex generators 820 may be positioned along the arc 822 such that the leading edge, or frontmost point, of each of the vortex generators 820 is positioned on the arc 822. The vortex generators 820 may also be spaced equidistant across the length of the arc or equidistant across the X axis direction.
While the vortex generators 820 are depicted as being located only on the crown 804. Additional or alternative vortex generators 820 may be included on the sole of the golf club head 800. The vortex generators 820 may be positioned on the sole in a similar manner and configuration as the vortex generations on the crown.
The vortex generators 820 may also extend in the aft direction at an angle relative to a line parallel to the Z axis. Such an angle may be referred to herein as an extension angle. Different subsets of vortex generators 820 may extend at different extension angles, as can be seen in
In
In
In an example, one subset of the vortex generators 820 may extend at the first extension angle C, and a second subset of the vortex generators 820 may extend at the second angle D. The vortex generators 820 may alternate between vortex generators 820 that extend at the first extension angle C and vortex generators 820 that extend at the second extension angle D.
Incorporating different angled vortex generators 820 allows for the vortex generators 820 to provide an affect at different points of the golf swing. For instance, during a golf swing, the golf club head 800 rotates which changes the relative direction of airflow over the golf club head 800. When the airflow is directly aligned with a vortex generator 820, the vortex generator 820 does not generate any air vortex and therefore does not provide the desired effect. Accordingly, by having multiple subsets of vortex generators 820 that extend in different extension angles, at least one subset of vortex generators 820 will generate air vortices at each point during the downswing of the golf club head 800. While only two subsets of the vortex generators 820 are shown, multiple additional subsets of vortex generators 820 with different extension angles may be included.
The leading edge 830 may be angled and/or curved as is extends from the frontmost point 837 to the top surface 836. The leading edge 830 may also come to a narrow point or edge that is radiused at a radius between 0.001-0.004 inches and may be about 0.002 inches. For instance, the heel side surface 832 and the toe side surface 834 converge together to form the edge 830.
The overall size of the example vortex generator 820 may be based on the effect of the example vortex generator 820 on the aerodynamic separation. For instance, a vortex generator 820 that has a height to energize the flow and reduce drag will likely not provide any additional benefit by having its height increased. Instead, an increase in height of the vortex generator 820 beyond what is needed to interact with the airflow may actually increase drag by introducing more energy into the airflow.
Because the vortex generators discussed herein are quite small, manufacturing processes that have high precision and tight tolerances may be needed to properly form the vortex generators. For instance, the small size of the vortex generators may effectively prevent the vortex generators from being incorporated as a standard cast metal component. Accordingly, the present technology may form a recess in the crown or sole of the golf club that is configured to receive an inlay that includes the vortex generators. The inlay may be manufactured from techniques that allow for greater precision, such as injection molding, 3D printing or the like. The inlay may then be affixed in the recess via an adhesive or other attachment mechanism. Accordingly, the club head may be manufactured using a casting process, and the inlay may be manufactured from a separate or different manufacturing process that allows for more precision. Additionally, the manufacturing process used to generate the inlays may allow for customization of the inlays while the casting process for the remainder of the club head may remain standardized.
The forward recess 966 extends across a front portion of the crown 904 in a heel-to-toe direction. The forward recess 966 may have a slight curvature to match the curvature of the front edge of the crown 904. For instance, the forward recess 966 may have a curvature that is similar to the horizontal face bulge radius of the golf club head 900. The front edge of the forward recess 966 may be positioned within 0.25 inches from the front edge of the crown 904.
The width of the aft recess 956 and the forward recess 966 may be substantially equal to the width of the respective aft vortex generator inlay 950 and the forward vortex generator inlay 960, respectively. The width of the respective inlays may be based on the lengths of the vortex generators formed thereon. For instance, the width of the aft vortex generator inlay 950 may be at least the length of the aft vortex generators 920 formed thereon. As an example, the width of the aft vortex generator inlay 950 may be between 100%-120% of the length of the aft vortex generators 920.
The depth of the aft recess 956 and the forward recess 966 may be equal to a thickness of a base of the forward vortex generator inlay 960 and the aft vortex generator inlay 950. For instance, the depth of the aft recess 956 and the forward recess 966 may be about 1 mm or between 0.5 mm to 1.5 mm. The base 951 of the aft vortex generator inlay 950 and the base 961 of the forward vortex generator inlay 960 provides a surface on which the aft vortex generators 920 and the forward vortex generators 962 may be formed, respectively. By having the depth of recesses 956, 966 be substantially the same as the thickness of the bases 951, 961, the upper surfaces of the base 951, 961 sit flush with the remainder the exterior surface of the crown 904, which provides for improved aerodynamics.
Because the aft vortex generator inlay 950 may be manufactured separately from the remainder of the golf club head 900, the alignment protrusion 964 may be customized for a particular golfer. For instance, the design, shape, size, location along the forward vortex generator inlay 960, and/or color of the alignment protrusion 964 may be configured by the golfer for custom manufacturing. In some examples, the alignment protrusion 964 may be recessed into the base 961 of the forward vortex generator inlay 960. The ability to have the alignment protrusion 964 be raised or recessed allows for additional contrast and aids in identification of the alignment protrusion 964 by the golfer.
The attachment extensions 953 protrude downward from a lower surface of the base 951 of the aft vortex generator inlay 950. In some examples, the attachment extensions 953 are configured as a pin or plug with a shaft and a flange or head portion. The aft recess 956 includes receiving holes 958 to receive the attachment extensions 953. The receiving holes 958 may be through holes in the floor of the aft recess 956 that extend into the cavity of the example golf club head 900. The position of the receiving holes 958 are aligned with the position of the attachment extensions 953 such that the attachment extensions 953 are pushed through the receiving holes 958 when the aft vortex generator inlay 950 is installed into the aft recess 956. When a plug-type attachment extension is inserted through the receiving hole 958, the head portion causes an interference with the receiving hole to provide a securing mechanism in addition to, or alternatively, an adhesive. The interference also helps with surface alignment between the upper surface of the base 951 and the exterior surface of the crown 904.
At operation 1104, one or more inlays are formed using a second manufacturing process that is different from the manufacturing process used to form the club head body in operation 1102. For example, the second manufacturing process may include an injection molding process or a 3D printing process, among others. The inlays may also be formed from a second material that is different from the material used to form the club head body. As an example, the club head body may be formed from metallic material and the inlay(s) may be formed from a non-metallic material. For instance, the material of the inlay(s) may include a plastic, composite, or polymeric material, among other types of materials. In other examples, the material of one or more of the inlays may also be metallic.
The inlay(s) formed in operation 1104 may include any of the inlays discussed herein, such as the aft vortex generator inlay, the forward vortex generator inlay, and/or the alignment inlay, among others. Forming the inlay(s) may include forming a base for the inlay and forming the vortex generators that protrude from an upper surface of the base. Forming the inlay(s) may also include forming one or more attachment extensions that protrude from a lower surface of the base.
Because the inlays may be formed from a second manufacturing process, the inlays may be formed in a customizable manner according to the needs or desires of the golfer. In addition, the inlays may be formed for particular golfer swing characteristics, such as swing speeds. For example, for higher swing speeds, the aft vortex generator inlay may have smaller (e.g., shorter) vortex generators. In contrast, for slower swing speeds, the aft vortex generator inlay may have larger (e.g., taller) vortex generators.
At operation 1106, the inlays formed in operation 1104 are inserted into the respective recesses formed in operation 1102. Inserting the inlays into the recesses may include adding an adhesive to the either the recess or the lower surface of the inlay to permanently adhere the inlay into the recess. In examples where receiving holes and attachment extensions are formed, inserting the inlays into the recesses may also include inserting the attachment extensions through the respecting receiving holes.
The aerodynamics of the golf club head may also be improved by modifying the configuration of the hosel and/or ferrule of the golf club head. Traditionally, the hosel is generally configured substantially as a cylinder and the shaft is similarly configured as a cylinder. During the golf swing, such cylinders increase drag and reduce the overall club head swing speed. Aspects of the present technology modify the hosel and/or ferrule to reduce the drag caused by such components, and in some examples, to reduce the drag caused by the shaft of the golf club.
As an example, the hosel and/or ferrule may include the tripping structures discussed above, and the hosel and/or ferrule may also be elongated in a direction that is substantially parallel to a speed-weighted average flow vector that the club head encounters during a golf swing. The inclusion of both the tripping structures and the elongation results in previously unknown and unrecognized synergies for reducing the drag caused by the hosel of the golf club. For example, by introducing the tripping structures, the airflow is tripped from a laminar flow to a turbulent flow, as discussed above. By then extending the hosel and/or ferrule rearward, the turbulent flow is able to remain attached to the hosel for a longer distance, which reduces the drag caused by the hosel. In contrast, merely extending the hosel in the rearward direction, without including the tripping structures, would not provide the same reductions in drag because the flow would not be tripped to the turbulent state by the tripping structures.
The hosel and/or ferrule may also have an extended height that encompasses more the shaft to reduce the drag effects of the shaft. Due to the cylindrical shape of the shaft, the shaft results in greater drag than the improved hosel and/or ferrule disclosed herein. As such, extending the improved hosel and/or ferrule to cover more of the shaft results in an overall reduction of drag during the golf swing.
The hosel 1212 and/or the ferrule 1213 also include one or more tripping structures 1214, which may be formed and positioned similarly to the tripping structures discussed above. For example, the tripping structures 1214 may be formed as ridges, grooves, dimples, discrete bumps, roughness areas, tooling marks, etc. The roughness or tripping structures 1214 may be formed by casting, etching, chemical milling, machining, molding, forming, adhering (e.g., taping, gluing) of a separate part, spraying of a material, etc.
In some examples, the hosel 1212 and/or the ferrule 1213 may have a greater height than common hosels and ferrules. The height of the ferrule 1213 is represented by HF, and the height of the hosel 1212 is represented as HH. The combined height of the hosel 1212 and ferrule 1213 is represented by HH+F. The combined height of the hosel 1212 and ferrule 1213 (HH+F) may in some examples be between 40 mm to 80 mm or more in some examples. The distance between the uppermost point of the ferrule 1213 from the ground plane may be about 100 mm 127 mm, and that distance may be measured from the ground plane along the shaft axis.
The asymmetry of the hosel 1212 and the ferrule 1213 may be described based on the distance to the exterior portions or surfaces of the hosel 1212 and the ferrule 1213 from the shaft axis. For instance, at the uppermost point of the ferrule 1213, a frontmost point of the exterior of the ferrule 1213 is at a distance DFFMIN from the shaft axis. At the uppermost point of the ferrule 1213, a rearmost point of the exterior of the ferrule 1213 is at a distance DFRMIN from the shaft axis. At the lowest point of the 1213 (e.g., where the ferrule 1213 joins the hosel 1212), the frontmost point of the exterior of the ferrule 1213 is a distance DFFMAX from the shaft axis. At the lowest point of the ferrule 1213 (e.g., where the ferrule 1213 joins the hosel 1212), the rearmost point of the exterior of the ferrule 1213 is a distance DFRMAX from the shaft axis.
At the uppermost point of the hosel 1212 (e.g., where the hosel 1212 joins the ferrule 1213), the frontmost point of the exterior of the hosel 1212 is a distance DHFMIN from the shaft axis. Also, at the uppermost point of the hosel 1212, the rearmost point of the exterior of the hosel 1212 is a distance DHRMIN from the shaft axis. At a midpoint or halfway point on the hosel 1212 (e.g., a point equal to half HO, the frontmost point of the exterior of the hosel 1212 is a distance DHF1/2 from the shaft axis. Also, at the halfway point on the hosel 1212, the rearmost point on the exterior of the hosel 1212 is a distance DHR1/2 from the shaft axis. At the bottom or lowest point of the hosel 1212 (e.g., where the hosel 1212 meets the crown 1204), the frontmost point of the exterior of the hosel 1212 is a distance DHFMAX from the shaft axis. Also, at the bottom or lowest point of the hosel 1212, the rearmost point of the exterior of the hosel 1212 is a distance DHRMAX from the shaft axis.
The asymmetry of the hosel 1212 and/or ferrule 1213 around the shaft axis may decrease as the hosel 1212 and/or or ferrule 1213 extend away from the crown 1204. For instance, the distances DFFMIN and DFRMIN may be substantially the same or within 2%-5% of one another, with DFRMIN being greater than DFFMIN.
The DFRMAX distance is greater than the DFRMIN distance, and the DFFMAX distance is greater than the DFFMIN distance. The DFRMAX distance may be greater than the DFFMAX distance by a larger amount than the difference between the DFFMIN distance and the DFRMIN distance. For example, the DFRMAX distance may be between 5%-15% greater than the DFFMAX distance. The DHFMIN and the DHRMIN distances may be the same as the DFFMAX and the DFRMAX distances, respectively, and share the same asymmetry attributes or relationships.
The DHR1/2 distance is also progressively larger than the DHF1/2 distance. For instance, the DHR1/2 distance may be 25%-70% greater than the DHF1/2 distance. In some examples, the DHR1/2 distance may be 35%-50% greater than the DHF1/2 distance. The DHRMAX distance is also progressively larger than the DHFMAX distance. For instance, the DHRMAX distance may be 80%-120% greater than the DHFMAX distance. In some examples, the DHRMAX distance may be 90%-110% greater than the DHFMAX distance.
The distances depicted in
Each of the cross sections has a distance DEXT that is measured along the extension axis from the point of cross section that is the frontmost point along the extension axis to the rearmost point along the extension axis. The extension axis may be offset from the front-to-back axis by an angle (Ω) such that the extension axis extends along a speed-weighted average flow vector that the club head encounters during a golf swing. For example, during the golf swing, the club head twists or turns during the downswing as the club head squares to the ball at impact. As such, the air flow across the hosel is not in the front-to-back direction until just before impact of the golf ball. By extending the hosel along the extension axis, rather than along the front-to-back axis, further improved aerodynamics can be achieved throughout the downswing—resulting in higher swing speeds and further ball flight. In some examples, the angle (Ω) is between 2-20 degrees, 5-15 degrees, 7-12 degrees, or about 10 degrees. As the extension axis extends from the front to the back of the golf club head, the extension axis also extends partially in the direction from the heel towards the toe.
The distance DEXT increases for cross sections closer to the crown. For example, the distance DEXT in cross section 1260 may be 60-80% greater than the distance DEXT in the cross section 1251. In some examples, the distance DEXT increases between 2%-10% at each cross section. Stated differently, the distance DEXT may increase 2%-10% for each 10% step in height towards the crown from the end of the ferrule and/or hosel. In some examples, the maximum distance Dext or the distance DEXT in cross section 1260 may be at least twice the diameter of the hosel opening or bore.
The cross sections of the hosel and/or ferrule also form an airfoil shape, especially towards the crown. For instance, between the crown and 50% of the total height HH+F, the hosel has an airfoil shape. The airfoil shape may be partially characterized by distance DFOIL20 from the exterior surfaces of the hosel, measured along an axis that is perpendicular to the extension axis, at 20% of the DEXT from the rearmost point of the hosel along the extension axis. In some examples, the distance DFOIL20 may be between 50%-70% of the maximum distance DCENTER between the exterior surfaces of the hosel as measured through the center of the hosel bore (e.g., through the shaft axis) in a direction perpendicular to the extension axis.
Although specific devices have been recited throughout the disclosure as performing specific functions, one of skill in the art will appreciate that these devices are provided for illustrative purposes, and other devices may be employed to perform the functionality disclosed herein without departing from the scope of the disclosure. This disclosure describes some embodiments of the present technology with reference to the accompanying drawings, in which only some of the possible embodiments were shown. Other aspects may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments were provided so that this disclosure was thorough and complete and fully conveyed the scope of the possible embodiments to those skilled in the art.
Further, as used herein and in the claims, the phrase “at least one of element A, element B, or element C” is intended to convey any of: element A, element B, element C, elements A and B, elements A and C, elements B and C, and elements A, B, and C. Further, one having skill in the art will understand the degree to which terms such as “about” or “substantially” convey in light of the measurement techniques utilized herein. To the extent such terms may not be clearly defined or understood by one having skill in the art, the term “about” shall mean plus or minus ten percent.
Although specific embodiments are described herein, the scope of the technology is not limited to those specific embodiments. Moreover, while different examples and embodiments may be described separately, such embodiments and examples may be combined with one another in implementing the technology described herein. One skilled in the art will recognize other embodiments or improvements that are within the scope and spirit of the present technology. Therefore, the specific structure, acts, or media are disclosed only as illustrative embodiments. The scope of the technology is defined by the following claims and any equivalents therein.
This application is a continuation-in-part of U.S. application Ser. No. 17/727,291, filed on Apr. 22, 2022, which is a continuation-in-part of U.S. application Ser. No. 17/544,033, filed on Dec. 7, 2021, the disclosures of which is incorporated herein by reference in their entireties. To the extent appropriate, a claim of priority is made to that application.
| Number | Date | Country | |
|---|---|---|---|
| Parent | 17727291 | Apr 2022 | US |
| Child | 17977742 | US | |
| Parent | 17544033 | Dec 2021 | US |
| Child | 17727291 | US |
