Patent Application
20240001204
This disclosure relates to golf club heads, such as heads having cast components, and related methods for manufacturing such golf club heads.
With the ever-increasing popularity and competitiveness of golf, substantial effort and resources are currently being expended to improve golf clubs. Much of the recent improvement activity has involved the combination of the use of new and increasingly more sophisticated materials in concert with advanced club-head engineering. For example, modern “wood-type” golf clubs (e.g., “drivers,” “fairway woods,” “rescues,” and “utility or hybrid clubs”), with their sophisticated shafts and non-wooden club-heads, bear little resemblance to the “wood” drivers, low-loft long-irons, and higher numbered fairway woods used years ago. These modern wood-type clubs are generally called “metalwoods” or simply “woods.”
The current ability to fashion metalwood club-heads of strong, light-weight metals and other materials has allowed the club-heads to be made hollow. Use of materials of high strength and high fracture toughness has also allowed club-head walls to be made thinner, which reduces total weight and allows increases in club-head size, compared to earlier club-heads without the swing speed penalty resulting from increased weight. Larger club-heads tend to have a larger face plate area and can also be made with high club-head inertia, thereby making the club-heads more “forgiving” than smaller club-heads. Characteristics such as size of the optimum impact location (also known as the “sweet spot”) are determined by many variables including the shape, profile, size and thickness of the face plate as well as the location of the center of gravity (CG) of the club-head.
An exemplary metalwood golf club typically includes a shaft having a lower end to which the club-head is attached. Most modern versions of these club-heads are made, at least in part, of a light-weight but strong metal such as titanium alloy. In some cases, the club-head comprises a body to which a face plate (used interchangeably herein with the terms “face” or “face insert” or “striking plate” or “strike plate”) is later attached, while in other cases the body and face place are cast together as a unitary structure, such that the face plate does not have to be later attached to the body. The face plate defines a front surface or strike face that actually contacts the golf ball.
Regarding the total mass of the metalwood club-head as the club-head's mass budget, at least some of the mass budget must be dedicated to providing adequate strength and structural support for the club-head. This is termed “structural” mass. Any mass remaining in the budget is called “discretionary” or “performance” mass, which can be distributed within the metalwood club-head to address performance issues, for example. Thus, the ability to reduce the structural mass of the metalwood club-head without compromising strength and structural support provides the potential for increasing discretionary mass and hence improved club performance.
One opportunity to reduce the total mass of the club head is to lower the mass of the face plate by reducing its thickness; however, opportunities to do this are somewhat limited given that the face absorbs the initial impact of the ball and thus has quite rigorous requirements on its physical and mechanical properties. Club manufacturers have used titanium and titanium alloys for face plate manufacture as well as whole club head manufacture, given their lightness and high strength. Typically for the club head given its relatively complex 3-D structure, casting processes have been used for its manufacture. Many such face plates are made by the investment casting process wherein an appropriate metal melt is cast into a preheated ceramic investment mold formed by the lost wax process. Investment casting has also been used to prepare the face plate either as a unitary structure cast with the rest of the club head body or as separately formed face plate which is then attached to the front of the club head body, usually by welding. Although widely used, investment casting of complex shaped components of such reactive materials can be characterized by relatively high costs and low yields. Low casting yields are attributable to several factors including surface or surface-connected void type defects and/or inadequate filling of certain mold cavity regions, especially thin mold cavity regions, and associated internal void, shrinkage and like defects.
To further compound the deficiencies of investment casting the face plate, club head manufacturers often also introduce curvature onto the face of the club to help compensate for directional problems caused by shots hit other than where the center of gravity is located. Thus, rather than a planar face plate, manufacturers may wish to form the face with both a heel-to-toe convex curvature (referred to as “bulge”) and a crown-to-sole convex curvature (referred to as “roll”). In addition, manufacturers may also introduce variable face thickness profiles across the face plate. Varying the thickness of a faceplate may increase the size of a club head COR zone, commonly called the sweet spot of the golf club head, which, when striking a golf ball with the golf club head, allows a larger area of the face plate to deliver consistently high golf ball velocity and shot forgiveness. Also, varying the thickness of a faceplate can be advantageous in reducing the weight in the face region for re-allocation to another area of the club head.
In order to make up for the deficiencies of investment casting these more complex face plate structures, manufacturers have turned to alternative methods of forming the face plate including laser cutting the face plate shape from a rolled titanium sheet followed by subsequent forging to impart any desired bulge and roll followed by a machining step on a lathe to introduce any desired face thickness profile. Disadvantages of these steps include the fact that three separate forming steps are needed and the machining process on a lathe to form variable thickness profiles is not only wasteful but also limits the profiles to circular shaped areas as a result of the circular motion of the lathe.
Thus, it would be highly desirable to have club head face plates with sufficient physical properties to allow reduction in thickness to result in more available discretionary weight in a club head. It would also be desirable if the face plates were also able to exhibit any desired bulge and roll curvature in addition to any variable thickness profile having any shape-circular, oval, asymmetrical or otherwise. It would also be desirable if a simplified process for manufacture of such face plates could be employed which would result in face plate with the required thickness and physical strength properties which process would also result in a face plate with any desired bulge and roll and variable thickness profile while requiring a minimum of processing steps and minimizing any waste produced in the process. It would also be desirable if the club head body and the face could be cast at the same time from the same material as a single unitary body, rather than two pieces that must be later attached together. It would also be desirable if the cast face plate did not require chemical etching to remove or reduce the thickness of the alpha case to provide adequate durability properties for the face plate.
Golf club heads disclosed herein can comprise a cast cup component, which can include a forward portion of a golf club head, including a hosel, forward portions of a crown, sole, heel, and toe, and a face portion or an opening to receive a face insert. The club heads can also comprise a rear ring component, which can be formed separately from the cast cup and coupled to heel and toe portions of the cast cup to form a rigid club head body, such that the club head body defines a hollow interior region, a crown opening, a sole opening, and/or face opening. The cast cup and rear ring can be made of different materials, including various metals, composites, and polymers. Composite crown, sole, and/or face inserts can be coupled to the crown, sole, and/or face openings to enclose the hollow internal cavity of the club head. Various forms of adjustable or fixed weights can be coupled to the sole portion of the cast cup and to the rear end of the rear ring. In addition, the face can have a complex variable thickness geometry.
Some golf club head bodies disclosed herein can be cast of 9-1-1 titanium with the face plate being cast as a unitary part of the body along the with crown, sole, skirt and hosel. Due to the 9-1-1 titanium material, the face plate and other portions of the body acquire less oxygen from the mold and can have a reduced alpha case thickness, resulting in greater ductility and durability. This can eliminate the need to reduce the alpha case thickness after casting using hydrofluoric acid or other dangerous chemical etchants. Casting methods can include preheating the casting mold to a lower than normal temperature and/or coating an inner surface of the mold, to further reduce the amount of oxygen transferred from the mold to the 9-1-1 titanium during casting.
In some embodiments, a wood-type golf club head body comprises a crown, a sole, skirt, a face plate, and a hosel; the body defines a hollow interior region; the body is cast substantially entirely of 9-1-1 titanium; and the body is cast as a single unitary casting, with the face plate being formed integrally with the crown, sole, skirt, and hosel. The body may comprise trace fluorine atoms as alloying impurities found in the titanium alloy, but due to the absence of etching the face with hydrofluoric acid after casting, the content of fluorine present in the body can be very low. In some embodiments, the face plate can have substantially no fluorine atoms, such as less than 1000 ppm, less than 500 ppm, less than 200 ppm, and or less than 100 ppm. In some embodiments, the body can have an alpha case thickness of 0.150 mm or less, 0.100 mm or less, and/or 0.070 mm or less.
Some exemplary methods comprise preparing a mold for casting and then casting a golf club head body substantially entirely of 9-1-1 titanium using the mold, wherein the cast body includes a crown, a sole, skirt, a face plate, and a hosel, wherein the cast body defines a hollow interior region; and wherein the body is cast as a single unitary casting, with the face plate being formed integrally with the crown, sole, skirt, and hosel during the casting. Some such methods do not include etching the face plate after the casting. In some methods, preparing the mold comprises preheating the mold such that the mold is at a temperature of 800 C or less, 700 C or less, 600 C or less, and/or 500 C or less, when the casting occurs.
Also disclosed herein are golf club head embodiments comprising a metallic cast cup forming a forward portion of the club head, including a hosel, a face portion, a forward portion of a crown, and a forward portion of a sole. A metallic rear ring can be formed separately from the cast cup and coupled to heel and toe portions of the cast cup to form a club head body, such that the metallic club head body defines a hollow interior region, a crown opening, and a sole opening. A composite crown insert can then be coupled to the crown opening. A sole insert made of composite, metal, or other material can be coupled to the sole opening. In some embodiments, there is no sole opening or sole insert. The cast cup and rear ring can be cast of the same titanium alloy, or two different materials, and can be welded, brazed, bonded, or mechanically interlocked together to form the club head body. In some embodiments, the ring and cup are comprised of different metallic materials, such as two different titanium alloys, or a titanium allow and steel. The cast cup can include a face portion that has an intricate geometry to provide desirable performance properties. The face portion can have a twisted front surface and/or the rear surface of the face can have a geometry that provides an asymmetric variable thickness profile across the face. The rear surface of the face portion of the cast cup can be machined and/or otherwise modified before the rear ring is attached such that there is increased room to access the entire rear surface of the face with tools. A front weight can be attached to the heel side of the sole of the cast cup, either on the inside or the exterior. A rear weight can be attached to a rear portion of the ring, either on the inside or the exterior of the ring. Weights can be one piece screw-in or bonded/welded in, or can be multi-piece, such as using a screw to attach a separate weight to the cup/ring.
Also disclosed are methods of forming a wax cup from a wax cup frame and a separately formed wax face, using a wax welding process. Such a wax cup can then be used to create a mold for casting the metallic cup that forms the front portion of a golf club head. The two piece wax welding process can provide manufacturing, prototyping, and testing advantages.
Also disclosed are cast face plates, such as comprising titanium alloys, which have novel geometries.
Some embodiments comprise composite face inserts that can be attached to a front opening of the cast cup.
Some embodiments disclosed herein comprise a rear ring that comprises anodized aluminum, which can provide various coloring options for the ring.
Some embodiments disclosed herein comprise a rear ring that is molded of polymeric materials, rather than cast of metallic material. Such polymer based rear rings can include fibers or other additives, and can also comprise various coatings and finishes. In some embodiments, the rear weight can be co-molded with the polymeric rear ring, such that the rear weight is partially or fully enclosed by the rear ring.
In some embodiments, the club head can comprise a weight track on the sole of the cast cup, and a sliding weight assembly that can be adjustably positioned along the track.
The foregoing and other objects, features, and advantages of the disclosed technology will become more apparent from the following detailed description, which proceeds with reference to the accompanying figures.
The following describes embodiments of golf club heads for metalwood type golf clubs, including drivers, fairway woods, rescue clubs, utility clubs, hybrid clubs, and the like. However, the herein disclosed technology can be implemented for any type of golf club head, not just the examples disclosed, including drivers, fairways, rescues, hybrids, utility clubs, irons, wedges, and putters.
For reference, within this disclosure, reference to a “driver type golf club head” means any metalwood type golf club head intended to be used primarily with a tee. In general, driver type golf club heads have lofts of 15 degrees or less, and, more usually, of 12 degrees or less. Reference to a “fairway wood type golf club head” means any wood type golf club head intended to be used to strike a ball off the ground, while also being usable to strike a ball off a tee as well. In general, fairway wood type golf club heads have lofts of 15 degrees or greater, and, more usually, 16 degrees or greater. In general, fairway wood type golf club heads have a length from leading edge to trailing edge of 73-97 mm. Various definitions distinguish a fairway wood type golf club head from a hybrid type golf club head, which tends to resemble a fairway wood type golf club head but be of smaller length from leading edge to trailing edge. In general, hybrid type golf club heads are 38-73 mm in length from leading edge to trailing edge. Hybrid type golf club heads may also be distinguished from fairway wood type golf club heads by weight, by lie angle, by volume, and/or by shaft length. Driver type golf club heads of the current disclosure may be 15 degrees or less in various embodiments or 10.5 degrees or less in various embodiments. In various embodiments, fairway wood type golf club heads of the current disclosure may be from 13-26 degrees.
As illustrated in
The body may further include openings in the crown and/or sole that are overlaid or covered by inserts formed of lighter-weight material, such as composite materials. For example, the crown of the body can comprise a composite crown insert that covers a large portion of the area of the crown and has a lower density that the metal the body is made out of, thereby saving weight in the crown. Similarly, the sole can include one or more openings in the body that are covered by sole inserts. The sole insert can be made of composite material, metallic material, or other material. In embodiments where the body includes openings in the crown or sole, such openings can provide access to the inner cavity of the club head during manufacturing, especially where the face plate is formed as an integral part of the body during casting (and there is not a face opening in the body to provide access during manufacturing). The club heads disclosed herein in relation to
In some embodiments, the club head can comprise adjustable weights, such as one or more weights movable along weight tracks formed in the sole and/or perimeter of the club head. Other exemplary weights can be adjusted by rotating the weights within threaded weight ports. Various ribs, struts, mass pads, and other structures can be included inside the body to provide reinforcement, adjust mass distribution and MOI properties, adjust acoustic properties, and/or for other reasons.
Wood-type club heads, such as the club head 2, have a volume, typically measured in cubic-centimeters (cm3), equal to the volumetric displacement of the club head, assuming any apertures are sealed by a substantially planar surface. (See United States Golf Association “Procedure for Measuring the Club Head Size of Wood Clubs,” Revision 1.0, Nov. 21, 2003). In the case of a driver, the golf club head can have a volume between approximately 250 cm3 and approximately 600 cm3, such as between approximately 300 cm3 and approximately 500 cm3, and can have a total mass between approximately 145 g and approximately 260 g. In the case of a fairway wood, the golf club head can have a volume between approximately 120 cm3 and approximately 300 cm3, and can have a total mass between approximately 115 g and approximately 260 g. In the case of a utility or hybrid club, the golf club head can have a volume between approximately 80 cm3 and approximately 140 cm3, and can have a total mass between approximately 105 g and approximately 280 g.
The sole 14 is defined as a lower portion of the club head 2 extending upwards from a lowest point of the club head when the club head is ideally positioned, i.e., at a proper address position relative to a golf ball on a level surface. In some implementations, the sole 14 extends approximately 50% to 60% of the distance from the lowest point of the club head to the crown 12, which in some instances, can be approximately 15 mm for a driver and between approximately 10 mm and 12 mm for a fairway wood.
Materials which may be used to construct the body 10, including the face plate 18, can include composite materials (e.g., carbon fiber reinforced polymeric materials), titanium or titanium alloys, steels or alloys of steel, magnesium alloys, copper alloys, nickel alloys, and/or any other metals or metal alloys suitable for golf club head construction. Other materials, such as paint, polymeric materials, ceramic materials, etc., can also be included in the body. In some embodiments, the body including the face plate can be made of a metallic material such as titanium or titanium alloys (including but not limited to 9-1-1 titanium, 6-4 titanium, 3-2.5, 6-4, SP700, 15-3-3-3, 10-2-3, or other alpha/near alpha, alpha-beta, and beta/near beta titanium alloys), or aluminum and aluminum alloys (including but not limited to 3000 series alloys, 5000 series alloys, 6000 series alloys, such as 6061-T6, and 7000 series alloys, such as 7075), Ti Grade 9 (Ti-3Al-2.5V) having a chemical composition of ≤3.5-2.5% Al; ≤3.0-2.0% V; ≤0.02% N; ≤0.013% H; ≤0.12 Fe.
Injection molding is used to form sacrificial “initial” patterns (e.g., made of casting “wax”) of the desired castings. A suitable injection die can be made of aluminum, or other suitable metal or metal alloy, or other material, e.g., by a computer-controlled machining process using a casting master. CNC (computer numerical control) machining can be used to form the intricacies of the mold cavity in the die. The cavity dimensions are established so as to compensate for linear and volumetric shrinkage of the casting wax encountered during casting of the initial pattern and also to compensate for any similar shrinkage phenomena expected to be encountered during actual metal casting performed later using an investment-casting “shell” formed from the initial pattern.
Usually, a group of initial patterns is assembled together and attached to a central wax sprue to form a casting “cluster.” Each initial pattern in the cluster forms a respective mold cavity in the casting shell formed later around the cluster. The central wax sprue defines the locations and configurations of runner channels and gates for routing molten metal, introduced into the sprue, to the mold cavities in the casting shell. The runner channels can include one or more filters (made, e.g., of ceramic) for enhancing smooth laminar flow of molten metal into and in the casting shell and for preventing entry of any dross, that may be trapped in the mold, into the shell cavities.
The casting shell is constructed by immersing the casting cluster into a liquid ceramic slurry, followed by immersion in a bed of refractory particles. This immersion sequence is repeated as required to build up a sufficient wall thickness of ceramic material around the casting cluster, thereby forming an investment-casting shell. An exemplary immersion sequence includes six dips of the casting cluster in liquid ceramic slurry and five dips in the bed of refractory particles, yielding an investment-casting shell comprising alternating layers of ceramic slurry and refractory material. The first two layers of refractory material desirably comprise fine (300 mesh) zirconium oxide particles, and the third to fifth layers of refractory material can comprise coarser (200 mesh to 35 mesh) aluminum oxide particles. Each layer is dried under controlled temperature (25±5° C.) and relative humidity (50±5%) before applying the subsequent layer.
The investment-casting shell is placed in a sealed steam autoclave in which the pressure is rapidly increased to 7-10 kg/cm2. Under such a condition, the wax in the shell is melted out using injected steam. The shell is then baked in an oven in which the temperature is ramped up to 1000-1300° C. to remove residual wax and to increase the strength of the shell. The shell is now ready for use in investment casting.
After the club-head is designed and the initial pattern is made, the manufacturing effort is shifted to a metal caster. To make the investment-casting shell, the metal caster first configures the cluster comprising multiple initial patterns for individual club-heads. Configuring the cluster also involves configuring the metal-delivery system (gates and runners for later delivery of molten metal). After completing these tasks, the caster tools up to fabricate the casting shells.
An important aspect of configuring the cluster is determining the locations at which to place the gates. A mold cavity for an individual club-head usually has one main gate, through which molten metal flows into the mold cavity. Additional auxiliary (“assistant”) gates can be connected to the main gate by flow channels. During investment casting using such a shell, the molten metal flows into each of the mold cavities through the respective main gates, through the flow channels, and through the auxiliary gates. This manner of flow requires that the mold for forming the initial pattern of a club-head also define the main gate and any assistant gates. After molding the wax initial pattern of the club-head, the initial pattern is removed from the mold, and the locations of flow channels are defined by “gluing” (using the same wax) pieces of wax between the gates. Reference is made to
Multiple initial patterns for respective club-heads are then assembled into the cluster, which includes attaching the individual main gates to “ligaments.” The ligaments include the sprue and runners of the cluster. A “receptor,” usually made of graphite or the like, is placed at the center of the cluster where it later will be used to receive the molten metal and direct the metal to the runners. The receptor desirably has a “funnel” configuration to aid entry-flow of molten metal. Additional braces (made of, e.g., graphite) may be added to reinforce the cluster structure.
Usually, the overall wax-cluster is sufficiently large (especially if the furnace chamber that will be used for forming the shell is large) to allow pieces of wax to be “glued” to individual branches of the cluster first, followed by ceramic coating of the individual branches separately before the branches are assembled together into the cluster. Then, after assembling together the branches, the cluster is transferred to the shell-casting chamber.
Two exemplary clusters are shown in
The reinforced wax cluster is then coated with multiple layers of slurry and ceramic powders, with drying being performed between coats. After forming all the layers, the resulting investment-casting shell is autoclaved to melt the wax inside it (the ceramic and graphite portions are not melted). After removing the wax from the shell, the shell is sintered (fired), which substantially increases its mechanical strength. If the shell will be used in a relatively small metalcasting furnace (e.g., capable of holding a cluster of only one branch), the shell can now be used for investment casting. If the shell will be used in a relatively large metal-casting furnace, the shell can be assembled with other shell branches to form a large, multi-branched cluster.
Modern investment casting of metal alloys is usually performed while rotating the casting shell in a centrifugal manner to harness and exploit the force generated by the ω2r acceleration of the shell undergoing such motion, where ω is the angular velocity of the shell and r is the radius of the angular motion. This rotation is performed using a turntable situated inside a casting chamber under a sub atmospheric pressure. The force generated by the ω2r acceleration of the shell urges flow of the molten metal into the mold cavities without leaving voids. The investment-casting shell (including its constituent clusters and runners) is generally assembled outside the casting chamber and heated to a pre-set temperature before being placed as an integral unit on the turntable in the chamber. After mounting the shell to the turntable, the casting chamber is sealed and evacuated to a pre-set sub atmospheric-pressure (“vacuum”) level. As the chamber is being evacuated, the molten alloy for casting is prepared, and the turntable commences rotating. When the molten metal is ready for pouring into the shell, the casting chamber is at the proper vacuum level, the casting shell is at a suitable temperature, and the turntable is spinning at the desired angular velocity. Thus, the molten metal is poured into the receptor of the casting shell and flows throughout the shell to fill the mold cavities in the shell.
As molten metal flows into the shell cavity and makes contact with the cavity surface, the high temperature environment (from both the molten metal and the preheated shell) encourages diffusion of elements, such as oxygen, in the shell material. Although titanium casting is always carried out under the sub atmospheric-pressure (vacuum) and oxygen is not available in the ambient environment, oxygen can still be found in the shell (as the shell consists of multiple layers of “oxides”). Introducing oxygen to the molten titanium causes the formation of an oxygen-rich layer, the alpha-case, on the surface of the titanium object to be cast. Typically, the thickness of the alpha-case is on the order of 1-4% of the thickness of the object.
As the alpha-case is “enriched” with oxygen, it is brittle (oxygen is one of the most effective elements of increasing the strength of titanium alloys, but while the strength is increased the ductility is greatly reduced) and can easily crack upon loading. To reduce the propensity of forming alpha-case the diffusion rate of oxygen needs to be reduced, and to reduce the diffusion rate the temperature needs to be reduced. However, it is impossible to reduce the temperature of the molten titanium. Therefore, reducing the temperature of the pre-heated shell is one way of reducing the diffusion rate of oxygen, thus reducing the formation of the alpha-case.
Typically, before transferring to the casting furnace a casting shell will be heated (called pre-heating) to aid the flow of molten titanium. The higher the pre-heat temperature of the shell, the easier the flow of titanium. This is essential for thin-wall titanium casting and the pre-heat temperature can be as high as 1100-1200 C. On the other hand, such high temperatures tend to produce thick alpha-case layers (towards the higher end of the 1-4% wall thickness range). Therefore, the pre-heat temperature of a casting shell can be lowered if the formation of alpha-case is a concern. Typically, the pre-heat temperature of a casting shell is lower than 1000 C or, preferably, lower than 900 C for non-flow-critical titanium castings where formation of alpha-case is undesirable.
As seen with reference to
In some embodiments, step 363 includes heating metal to molten state. In various embodiments, heating temperatures may be higher or lower depending on application. In some embodiments, step 362 includes accelerating the cluster angularly to an angular velocity, e.g., about 360 revolutions per minute. In various embodiments, angular speeds may range from 250-450 revolutions per minute. In various embodiments, angular speeds as low as 150 rpm and as high as 600 rpm may be suitable.
Because of lower casting temperatures, the step of allowing molten metal to cool in the mold cluster includes a reduced waiting time as compared to traditional investment-casting processes. The result is improved yield and better cycle times. In various traditional investment casting methods that rely on gravity, casting of only 6-8 maximum parts was possible. Using centrifugal casting, 18-25 parts or more may be cast in one cycle, thereby increasing production capacity for a single casting cycle. Additionally, yield per gram of pour is also increased. For traditional investment casting methods, a certain mass of metal is used to cast a certain number golf club heads. With spin casting techniques of the current disclosure, the same mass of metal can be used to produce more golf club heads. Improvements and honing of the techniques in the current disclosure can reduce this mass of metal/per head even further. Reduced cycle times can also be present depending on particular methodology. Additionally, the methods described herein lead to reduced tooling and capital expenditure required for the same production demand. As such, methods described herein reduce cost and improve production quality.
Additionally, casting according to the method described herein leads to a savings in material and achieve greater throughput because material can be more easily flowed to a greater number of heads given the increased acceleration and, thereby, force applied to the casting. Finally, alloys that typically are manufactured using other methods may be more easily cast to similar geometries.
Configuring the gates and the cluster(s) involves consideration of multiple factors. These include (but are not necessarily limited to): (a) the dimensional limitations of the casting chamber of the metal-casting furnace, (b) handling requirements, particularly during the slurry-dipping steps that form the investment-casting shell, (c) achieving an optimal flow pattern of the molten metal in the investment-casting shell, (d) providing the cluster(s) of the investment-casting shell with at least minimum strength required for them to withstand rotational motion during metal casting, (e) achieving a balance of minimum resistance to flow of molten metal into the mold cavities (by providing the runners with sufficiently large cross-sections) versus achieving minimum waste of metal (e.g., by providing the runners with small cross-sections), and (f) achieving a mechanical balance of the cluster(s) about a central axis of the casting shell. Item (e) can be important because, after casting, any metal remaining in the runners does not form product but rather may be “contaminated” (a portion of which is usually recycled). These configurational factors are coupled with metal-casting parameters such as shell-preheat temperature and time, vacuum level in the metal-casting chamber, and the angular velocity of the turntable to produce actual casting results. As club-head walls are made increasingly thinner, careful selection and balance of these parameters are essential to produce adequate investment-casting results.
Details of investment casting as performed at metal casters tend to be proprietary. But, experiments at various titanium casters have in the past revealed some consistencies and some general trends. For example, a particular club-head (having a volume of 460 cm3, a crown thickness of 0.6 mm, and a sole thickness of 0.8 mm) was fabricated at each of six titanium casters (having respective metal-casting furnaces ranging from 10 kg to 80 kg capacity), producing the data tabulated in
From the minimum-force requirement can be derived a lower threshold of the amount of molten metal necessary for pouring into the shell. Excluding unavoidable pouring losses, the best metal usage (as achieved by caster 1) was 386 g (0.386 kg) for club-heads each having a mass of approximately 200 g (including gate and some runner). This is equivalent to a material-usage ratio of 200/386=52 percent. The accelerations (max) applied to the investment-casting shell by the casters 2-6 were all higher than the acceleration applied by caster 1, but more molten metal was needed by each of casters 2-6 to produce respective casting yields that were equivalent to that achieved by caster 1.
Some process loss (splashing, cooled metal adhering to side walls of the crucible and coup supplying the liquid titanium alloy, revert cleaning loss, and the like) is unavoidable. Process loss imposes an upper limit to the efficiency that can be achieved by smaller casting furnaces. i.e., the percentage of process loss increases rapidly with decreases in furnace size, as illustrated in
On the other hand, smaller casting furnaces advantageously have simpler operation and maintenance requirements. Other advantages of smaller furnaces are: (a) they tend to process smaller and simpler clusters of mold cavities, (b) smaller clusters tend to have separate respective runners feeding each mold cavity, which provides better interface-gating ratios for entry of molten metal into the mold cavities, (c) the furnaces are more easily and more rapidly preheated prior to casting, (d) the furnaces offer a potentially higher achievable shell-preheat temperature, and (e) smaller clusters tend to have shorter runners, which have lower Reynolds numbers and thus pose reduced potentials for disruptive turbulent flow. While larger casting furnaces tend not to have these advantages, smaller casting furnaces tend to have more unavoidable process loss of molten metal per mold cavity than do larger furnaces.
In view of the above, the cost-effective casting systems (furnaces, clusters, yields, net material costs) appear to include medium-sized systems, so long as appropriate cluster- and gate-design considerations are incorporated into configurations of the investment-casting shells used in such furnaces. This can be seen from comparing casters 1, 4, and 5. The overall usages of material (without considering process losses) by these three casters are very close (664-667 g/cavity). Material usage (considering process loss) by caster 1 is 386 g, while that of casters 4 and 5 is 510 g. Thus, whereas casters 4 and 5 could still improve, it appears that caster 1 has reached its limit in this regard.
At least the minimum threshold force applied to molten metal entering the investment-casting shell can be achieved by either changing the mass or increasing the velocity of the molten metal entering the shell, typically by decreasing one and increasing the other. There is a realistic limit to the degree to which the mass of “pour material” (molten metal) can be reduced. As the mass of pour material is reduced, correspondingly more acceleration is necessary to generate sufficient force to move the molten metal effectively into the investment-casting shell. But, increasing the acceleration increases the probability of creating turbulent flow of the molten metal entering the shell. Turbulent flow is undesirable because it disrupts the flow pattern of the molten metal. A disrupted flow pattern can require even greater force to “push” the metal though the main gate into the mold cavities.
The Reynolds number can be easily modified by changing the shape and/or dimensions of the runner(s). For example, changing R (flow radius) will affect the Reynolds number directly. The smaller R (flow radius) will result in less minimum force (the two almost having a reciprocal relationship). Hence, an advantageous consideration is first to reduce the Reynolds number to maintain a steady flow field of the molten metal, and then satisfy the requirement of minimum force by adjusting the amount of pour material.
One additional factors is preheating the investment-casting shell before introducing the molten metal to it. Caster 1 achieved 94% yield with the smallest Reynolds number and the minimum amount of pour material (and thus the lowest force) in part because caster 1 had the highest shell-preheat temperature. Another factor is the complexity of the cluster(s). Evaluating a complex cluster is very difficult, and the high Reynolds numbers usually exhibited by such clusters are not the only variable to be controlled to reduce disruptive turbulent flow of molten metal in such clusters. For example, the number of “sharp” turns (90-degree turns or greater) in runners and mold cavities of the cluster is also a factor. In regard to
Another factor is matching the runner and gates. The interface gating ratio for caster 1 is the closest to 100% (indicating optimal gating), compared to the substantially inferior data from the other casters. The “worst” was caster 3, whose investment-casting shell had a Reynolds number almost as low as that of caster 1, but caster 3 achieved a yield of only 78%, due to a poor interface gating ratio (approximately 23%). The low interface gating ratio exhibited by the shell of caster 3 increased the difficulty of determining whether the cause of caster 3's low yield was insufficient pour material to fill the gates or the occurrence of “two-phase flow-liquid and vacancy.” In any event, the overall cross-sectional areas of runners and gates may be kept as nearly equal (and constant) to each other as possible to achieve constant flow velocity of liquid metal throughout the shell at any moment during pouring. For thin-walled titanium alloy castings, this principle applies especially to the interfaces between the runner and the main gates, where the interface gating ratio should be no less than unity (1.0).
Yet another factor is the cross-sectional shape of the runner. Comparing casters 4 and 5, and casters 2 and 5, triangular-section runners appeared to produce lower Reynolds numbers than rounded or rectangular runners. Although using triangular-section runners can cause problems with interface gating ratio (as metal flows from such a runner into a rectilinear-section or round-section gate), the significant reduction in Reynolds numbers achieved using triangular-section runners is worth pursuing as the difference in pour material used by casters 2 and 5 indicates (39 kg versus 32 kg).
A flow-chart for configuring a cluster of an investment-casting shell is shown in
More information regarding investment casting methods and devices for casting thin-walled club heads using titanium alloys and other materials can be found in U.S. Pat. No. 7,513,296, issued Apr. 7, 2009, and in U.S. Publication No. 2016/0175666, published Jun. 23, 2016, both of which are incorporated by reference herein in their entireties. While these incorporated references disclose methods and systems for casting club head bodies without the face plate included (face plate is later attached to body), the same or similar methods and systems can be used, with the same or similar benefits and advantages, to cast the herein disclosed club head bodies where the face in an integrally cast part of the body, not formed separately and later attached to the body.
More information regarding coatings on molds for casting titanium alloys, and methods for producing molds having a calcium oxide face coat for use in casting titanium alloys, can be found in U.S. Pat. No. 5,766,329, issued Jun. 16, 1998, which is incorporated by reference herein in its entirety.
Compared to titanium golf club faces formed for sheet machining or forging processes, cast faces can have the advantage of lower cost and complete freedom of design. However, golf club faces cast from conventional titanium alloys, such as 6-4 Ti, need to be chemically etched to remove the alpha case on one or both sides so that the faces are durable. Such etching requires application of hydrofluoric (HF) acid, a chemical etchant that is difficult to handle, extremely harmful to humans and other materials, an environmental contaminant, and expensive.
Faces cast from titanium alloys comprising aluminum (e.g., 8.5-9.5% Al), vanadium (e.g., 0.9-1.3% V), and molybdenum (e.g., 0.8-1.1% Mo), optionally with other minor alloying elements and impurities, herein collectively referred to a “9-1-1 Ti”, can have less significant alpha case, which renders HF acid etching unnecessary or at least less necessary compared to faces made from conventional 6-4 Ti and other titanium alloys.
Further, 9-1-1 Ti can have minimum mechanical properties of 820 MPa yield strength, 958 MPa tensile strength, and 10.2% elongation. These minimum properties can be significantly superior to typical cast titanium alloys, such as 6-4 Ti, which can have minimum mechanical properties of 812 MPa yield strength, 936 MPa tensile strength, and ˜6% elongation.
Golf club heads that are cast including the face as an integral part of the body (e.g., cast at the same time as a single cast object) can provide superior structural properties compared to club heads where the face is formed separately and later attached (e.g., welded or bolted) to a front opening in the club head body. However, the advantages of having an integrally cast Ti face are mitigated by the need to remove the alpha case on the surface of cast Ti faces.
With the herein disclosed club heads comprising an integrally cast 9-1-1 Ti face and body unit, the drawback of having to remove the alpha case can be eliminated, or at least substantially reduced. For a cast 9-1-1 Ti face, using a conventional mold pre-heat temperature of 1000 C or more, the thickness of the alpha case can be about 0.15 mm or less, or about 0.20 mm or less, or about 0.30 mm or less, such as between 0.10 mm and 0.30 mm in some embodiments, whereas for a cast 6-4 Ti face the thickness of the alpha case can be greater than 0.15 mm, or greater than 0.20 mm, or greater than 0.30 mm, such as from about 0.25 mm to about 0.30 mm in some examples.
In some cases, the reduced thickness of the alpha case for 9-1-1 Ti face plates (e.g., 0.15 mm or less) may not be thin enough to provide sufficient durability needed for a face plate and to avoid needing to etch away some of the alpha case with a harsh chemical etchant, such as HF acid. In such cases, the pre-heat temperature of the mold can be lowered (such as to less than 800 C, less than 700 C, less than 600 C, and/or less than or equal to 500 C) prior to pouring the molten titanium alloy into the mold. This can further reduce the amount of oxygen transferred from the mold to the cast titanium alloy, resulting in a thinner alpha case (e.g., less than 0.15 mm, less than 0.10 mm, and/or less than 0.07 mm). This provides better ductility and durability for the cast body/face unit, which is especially important for the face plate.
The thinner alpha case in cast 9-1-1 Ti faces helps provide enhanced durability, such that the face is durable enough that the removal of part of the alpha case from the face via chemical etching is not needed. Thus, hydrofluoric acid etching can be eliminated from the manufacturing process when the body and face are unitarily cast using 9-1-1 Ti, especially when using molds with lower pre-heat temperatures. This can simplify the manufacturing process, reduce cost, reduce safety risks and operation hazards, and eliminate the possibility of environmental contamination by HF acid. Further, because HF acid is not introduced to the metal, the body/face, or even the whole club head, can comprise very little or substantially no fluorine atoms, which can be defined as less than 1000 ppm, less than 500 ppm, less than 200 ppm, and or less than 100 ppm, wherein the fluorine atoms present are due to impurities in the metal material used to cast the body.
In certain embodiments, a variable thickness face profile may be implemented on the face plate, for example as is described in U.S. patent application Ser. No. 12/006,060 and U.S. Pat. Nos. 6,997,820; 6,800,038; 6,824,475; 7,731,603; and 8,801,541; the entire contents of each of which are incorporated herein by reference. Varying the thickness of a face plate may increase the size of a club head COR zone, commonly called the sweet spot of the golf club head, which, when striking a golf ball with the golf club head, allows a larger area of the face plate to deliver consistently high golf ball velocity and shot forgiveness. Also, varying the thickness of a faceplate can be advantageous in reducing the weight in the face region for re-allocation to another area of the club head. For example, as shown in
In some embodiments, the cross-sectional profile of the face plate 18 along any axes extending perpendicular to the face plate at the ideal impact location 23 is substantially similar as in
In some embodiments of a golf club head having a face plate with a protrusion, the maximum face plate thickness is greater than about 4.8 mm, and the minimum face plate thickness is less than about 2.3 mm. In certain embodiments, the maximum face plate thickness is between about 5 mm and about 5.4 mm and the minimum face plate thickness is between about 1.8 mm and about 2.2 mm. In yet more particular embodiments, the maximum face plate thickness is about 5.2 mm and the minimum face plate thickness is about 2 mm. The face thickness should have a thickness change of at least 25% over the face (thickest portion compared to thinnest) in order to save weight and achieve a higher ball speed on off-center hits.
In some embodiments of a golf club head having a face plate with a protrusion and a thin sole construction or a thin skirt construction, the maximum face plate thickness is greater than about 3.0 mm and the minimum face plate thickness is less than about 3.0 mm. In certain embodiments, the maximum face plate thickness is between about 3.0 mm and about 4.0 mm, between about 4.0 mm and about 5.0 mm, between about 5.0 mm and about 6.0 mm or greater than about 6.0 mm, and the minimum face plate thickness is between about 2.5 mm and about 3.0 mm, between about 2.0 mm and about 2.5 mm, between about 1.5 mm and about 2.0 mm or less than about 1.5 mm.
As shown in
The method used to obtain the values in the present disclosure is the optical comparator method. Referring back to
To measure the roll, the club head 4 is rotated by 90 degrees such that the Z-axis Z of the club head is generally parallel to the X-axis of the machine. Measurements are taken at the geometric center point 5a of the club face. Further measurements are then taken 15 millimeters away from the geometric center point 5a and along the Z-axis Z of the club face 6 on either side of the center point 5a, and 20 millimeters away from the geometric center point and along the Z-axis of the club face on either side of the center point. An arc is fit through these five measurement points. This arc corresponds to the circumference of a circle with a given radius. This measurement of radius is what is meant by the roll radius.
Curvature is defined as 1/R wherein R is the radius of the circle which corresponds to the measurement arc of the bulge or the roll. As an example, a bulge with a curvature of 0.020 cm−1 corresponds to a bulge measured by a bulge measurement arc which is part of a circle with a radius of 50 cm. A roll with a curvature of 0.050 cm−1 corresponds to a roll measured by a roll measurement arc which is part of a circle with a radius of 20 cm.
In some embodiments, the face plates of the disclosed club heads can have the following properties:
Use of vacuum die casting to produce the club heads described herein results in improved quality and reduced scrap. In addition, rejections due to high porosity are virtually eliminated as are rejections after any secondary processing. An excellent surface quality is produced while increasing product density and strength are increased and thus making possible larger, thinner, and more complex, castings. From a processing standpoint, less casting pressure is required, and tool life and mold life are extended. Also waste of the metal or alloy due to flash is reduced or eliminated.
By utilizing a vacuum die casting process, it has been surprisingly found that the titanium bodies and face plates of the disclosed club heads exhibit much smaller grain size than is typically observed for analogous titanium objects made by investment casting, with grains of about 100 μm (micrometers) in size versus about 750 μm grain size for investment cast titanium face plates. More specifically, the titanium bodies/face plates disclosed herein can have a grain size of less than about 400 μm, preferably less than about 300 μm, more preferably less than about 200 μm and even more preferably less than about 150 μm, and most preferably less than about 120 μm.
The titanium bodies/face plates disclosed herein can also exhibit much lower porosity than is typically observed for an analogous separately formed titanium face plate made by investment casting. More specifically, the titanium face plates disclosed herein can have a porosity of less than 1% preferably less than 0.5% more preferably less than 0.1%.
The titanium bodies/face plates disclosed herein can also exhibit much higher yield strength, as measured by ASTM E8, than is typically observed for an analogous titanium face plate made by investment casting.
The titanium face plates disclosed here can also exhibit similar fracture toughness to that typically observed for an analogous titanium face plates made by investment casting, and higher than an analogous face plate made from a wrought mill-annealed product.
The titanium face plates disclosed herein can also exhibit ductility as measured by the percent elongation reported in a tensile test which is defined as the maximum elongation of the gage length divided by the original gage length of from about 10% to about 15%.
The titanium face plates disclosed herein can also exhibit a Young's Modulus of 100 GPa+/−10%, preferably +/−5% and more preferably +/−2% as measured by ASTM E-111.
The titanium face plates disclosed herein can also exhibit an Ultimate Tensile Strength of 970 MPa+/−10%, preferably +/−5% and more preferably +/−2% as measured by ASTM E8.
Combination of the various properties described above allows fabrication of metalwood titanium club heads having titanium face plates that can be 10% thinner than the analogous face plates made by conventional investment casting while maintaining as good if not better strength properties.
In addition to the strength properties of the golf club heads of the present invention, in certain embodiments, the shape and dimensions of the golf club head may be formed so as to produce an aerodynamic shape as according to U.S. Patent Publication No. 2013/0123040 A1, filed on Dec. 18, 2012 to Willett et al., the entire contents of which are incorporated by reference herein. The aerodynamics of golf club heads are also discussed in detail in U.S. Pat. Nos. 8,777,773; 8,088,021; 8,540,586; 8,858,359; 8,597,137; 8,771,101; 8,083,609; 8,550,936; 8,602,909; and 8,734,269; the teachings of which are incorporated by reference herein in their entirety.
In addition to the strength properties of the aft body, and the aerodynamic properties of the club head, another set of properties of the club head which must be controlled are the acoustical properties or the sound that a golf club head emits when it strikes a golf ball. At club head/golf ball impact, a club striking face is deformed so that vibrational modes of the club head associated with the club crown, sole, or striking face are excited. The geometry of most golf clubs is complex, consisting of surfaces having a variety of curvatures, thicknesses, and materials, and precise calculation of club head modes may be difficult. Club head modes can be calculated using computer-aided simulation tools. For the club heads of the present invention the acoustic signal produced with ball/club impact can be evaluated as described in in copending U.S. application Ser. No. 13/842,011 filed on Mar. 15, 2013, the entire contents of which are incorporated by reference herein.
In certain embodiments of the present invention the golf club head may be attached to the shaft via a removable head-shaft connection assembly as described in more detail in U.S. Pat. No. 8,303,431 issued on Nov. 6, 2012, the entire contents of which are incorporated by reference herein. Further in certain embodiments, the golf club head may also incorporate features that provide the golf club heads and/or golf clubs with the ability not only to replaceably connect the shaft to the head but also to adjust the loft and/or the lie angle of the club by employing a removable head-shaft connection assembly. Such an adjustable lie/loft connection assembly is described in more detail in U.S. Pat. No. 8,025,587 issuing on Sep. 27, 2011, U.S. Pat. No. 8,235,831 issued on Aug. 7, 2012, U.S. Pat. No. 8,337,319 issued on Dec. 25, 2012, as well as copending US Publication No. 2011/0312437A1 filed on Jun. 22, 2011, US Publication No. 2012/0258818 A1 filed on Jun. 20, 2012, US Publication No. 2012/0122601A1 filed on Dec. 29, 2011, US Publication No. 2012/0071264 A1 filed on Mar. 22, 2011 as well as copending U.S. application Ser. No. 13/686,677 filed on Nov. 27, 2012, the entire contents of which patents, publications and applications are incorporated in their entirety by reference herein.
In certain embodiments the golf club head may feature an adjustable mechanism provided on the sole portion to “decouple” the relationship between face angle and hosel/shaft loft, to allow for separate adjustment of square loft and face angle of a golf club. For example, some embodiments of the golf club head may include an adjustable sole portion that can be adjusted relative to the club head body to raise and lower the rear end of the club head relative to the ground. Further detail concerning the adjustable sole portion is provided in U.S. Pat. No. 8,337,319 issued on Dec. 25, 2012, U.S. Patent Publication Nos. US2011/0152000 A1 filed on Dec. 23, 2009, US2011/0312437 filed on Jun. 22, 2011, US2012/0122601A1 filed on Dec. 29, 2011 and copending U.S. application Ser. No. 13/686,677 filed on Nov. 27, 2012, the entire contents of each of which are incorporated herein by reference.
In some embodiments movable weights can be adjusted by the manufacturer and/or the user to adjust the position of the center of gravity of the club to give the desired performance characteristics can be used in the golf club head. This feature is described in more detail in the following U.S. Pat. Nos. 6,773,360; 7,166,040; 7,452,285; 7,628,707; 7,186,190; 7,591,738; 7,963,861; 7,621,823; 7,448,963; 7,568,985; 7,578,753; 7,717,804; 7,717,805; 7,530,904; 7,540,811; 7,407,447; 7,632,194; 7,846,041; 7,419,441; 7,713,142; 7,744,484; 7,223,180; and 7,410,425; the entire contents of each of which are incorporated by reference in their entirety herein.
According to some embodiments of the golf club heads described herein, the golf club head may also include a slidably repositionable weight positioned in the sole and/or skirt portion of the club head. Among other advantages, a slidably repositionable weight facilitates the ability of the end user of the golf club to adjust the location of the CG of the club head over a range of locations relating to the position of the repositionable weight. Further detail concerning the slidably repositionable weight feature is provided in more detail in U.S. Pat. Nos. 7,775,905 and 8,444,505 and U.S. patent application Ser. No. 13/898,313 filed on May 20, 2013 and U.S. patent application Ser. No. 14/047,880 filed on Oct. 7, 2013, the entire contents of each of which are hereby incorporated by reference herein as well the contents of paragraphs [430] to [470] and FIGS. 93-101 of US Patent Publication No. 2014/0080622 corresponding to U.S. patent application Ser. No. 13/956,046 filed on Jul. 31, 2013 as well as copending U.S. Patent Application Nos. 62/020,972 filed on Jul. 3, 2014 and 62/065,552 filed on Oct. 17, 2014, the contents of each of which are hereby incorporated by reference herein.
According to some embodiments of the golf club heads described herein, the golf club head may also include a coefficient of restitution feature which defines a gap in the body of the club, for example located on the sole portion and proximate the face. Such coefficient of restitution features are described more fully in U.S. patent application Ser. No. 12/791,025, filed Jun. 1, 2010, and Ser. No. 13/338,197, filed Dec. 27, 2011 and Ser. No. 13/839,727, filed Mar. 15, 2013 (US Publication No. 2014/0274457A1) and Ser. No. 14/457,883 filed Aug. 12, 2014 and Ser. No. 14/573,701 filed Dec. 17, 2014, the entire contents of each of which are incorporated by reference herein in their entirety.
The head 200 comprises a body 202, an adjustable head-shaft connection assembly 204, the crown insert 206 attached to the upper portion of the body, the sole insert 208 mounted inside the body on top of the lower portion of the body, the front weight assembly 210 slidably mounted in the front weight track 214, and the rear weight assembly 212 slidably mounted in the rear weight track 216. The head 200 includes a front sit pad, or ground contact surface, 226 between the front track 214 and the face 270, and a rear sit pad, or ground contact surface, 224 at the rear of the body to the heel side of the rear track 216, with the rest of the sole elevated above the ground when in the normal address position.
The head 200 has a raised sole that is defined by a combination of the body 202 and the sole insert 208. As shown in
The head 200 also includes a toe-side cantilevered ledge 232 extending around the perimeter from the rear weight track 216 or rear sit pad 224 around to toe region adjacent the face, where the ledge 232 joins with a toe portion 230 of the body that extends toeward from the front sit pad 226. One or more optional ribs 236 can join the toe portion 230 to the raised sole adjacent a forward end of the toe-side opening 240 in the body. Three such triangular ribs are illustrated in
The head 200 also includes a heel-side cantilevered ledge 234 that extends from near the hosel region rearward to the rear sit pad 224 or to the rear end of the rear weight track 216. In some embodiments, the two cantilevered ledges 232 and 234 can meet and/or form a continuous ledge that extends around the rear of the head. The rear sit pad 224 can optionally include a recessed rear portion 222 (as shown in
The lower portion of the body 202 that forms part of the sole can include various features, thickness variations, ribs, etc, to provide enhanced rigidity where desired and weight saving when rigidity is less desired. The body can include thicker regions 238, for example, near the intersection of the two weight tracks 214, 216. The body can also include thin ledges or seats 260 around the openings 240, 242, with the ledges 260 configured to receive and mate with sole insert 208. The lower surfaces of the body can also include various internal ribs to enhance rigidity and acoustics, such as ribs 262, 263, 265, and 267 shown in
The upper portion of the body can also include various features, thickness variations, ribs, etc, to provide enhanced rigidity where desired and weight saving when rigidity is less desired. For example, the body includes a thinner seat region 250 around the upper opening to receive the crown insert 206. As shown in
The sole insert 208 has a geometry and size selected to at least cover the openings 240, 242, 244 in the bottom of the body, and can be secured to the frame by adhesion or other secure fastening technique. In some embodiments, the ledges 260 may be provided with indentations to receive matching protrusions or bumps on the underside of the sole insert to further secure and align the sole insert on the frame.
Like the sole, the crown also has an opening 246 that reduces the mass of the body 202, and more significantly, reduces the mass of the crown, a region of the head where increased mass has the greatest impact on raising (undesirably) the CG of the head. Along the periphery of the opening 246, the frame includes a recessed ledge 250 to seat and support the crown insert 206. The crown insert 206 (see
In various embodiments, the ledges of the body that receive the crown and sole inserts (e.g. ledges 250 and 260) may be made from the same metal material (e.g., titanium alloy) as the body and, therefore, can add significant mass to the golf club head. In some embodiments, in order to control the mass contribution of the ledge to the golf club head, the width of the ledges can be adjusted to achieve a desired mass contribution. In some embodiments, if the ledges add too much mass to the golf club head, it can take away from the decreased weight benefits of a sole and crown inserts, which can be made from a lighter materials (e.g., carbon fiber or graphite composites and/or polymeric materials). In some embodiments, the width of the ledges may range from about 3 mm to about 8 mm, preferably from about 4 mm to about 7 mm, and more preferably from about 4.5 mm to about 5.5 mm. In some embodiments, the width of the ledges may be at least four times as wide as a thickness of the respective insert. In some embodiments, the thickness of the ledges may range from about 0.4 mm to about 1 mm, preferably from about 0.5 mm to about 0.8 mm, and more preferably from about 0.6 mm to about 0.7 mm. In some embodiments, the thickness of the ledges may range from about 0.5 mm to about 1.75 mm, preferably from about 0.7 mm to about 1.2 mm, and more preferably from about 0.8 mm to about 1.1 mm. Although the ledges may extend or run along the entire interface boundary between the respective insert and the body, in alternative embodiments, the ledges may extend only partially along the interface boundaries.
The periphery of crown opening 246 can be proximate to and closely track the periphery of the crown on the toe-, rear-, and heel-sides of the head 200. In contrast, the face-side of the crown opening 246 can be spaced farther from the face 270 region of the head. In this way, the head can have additional frame mass and reinforcement in the crown area 252 just rearward of the face 270. This area and other areas adjacent to the face along the toe, heel and sole support the face and are subject to the relatively higher impact loads and stresses due to ball strikes on the face. As described elsewhere herein, the frame may be made of a wide range of materials, including high strength titanium, titanium alloys, and/or other metals. The opening 246 can have a notch at the front side which matingly corresponds to the crown insert projection 207 to help align and seat the crown insert on the body.
The front and rear weight tracks 214, 216 are located in the sole of the club head and define tracks for mounting two-piece slidable weight assemblies 210, 212, respectively, which may be fastened to the weight tracks by fastening means such as screws. The weight assemblies can take forms other than as shown in
The sole of the body 202 preferably is integrally formed with the front weight track 214 extending generally parallel to and near the face of the club head and generally perpendicular to the rear weight track 216, which extends rearward from near the middle of the front track toward the rear of the head.
In the illustrated embodiments, the weight tracks each only include one weight assembly. In other embodiments, two or more weight assemblies can be mounted in either or both of the weight tracks to provide alternative mass distribution capabilities for the club head.
By adjusting the CG heelward or toeward via the front weight track 214, the performance characteristics of the club head can be modified to affect the flight of the ball, especially the ball's tendency to draw or fade and/or to counter the ball's tendency to slice or hook. By adjusting the CG forward or rearward via the rear weight track 216, the performance characteristics of the club head can be modified to affect the flight of the ball, especially the ball's tendency to move upwardly or resist falling during flight due to backspin. The use of two weights assemblies in wither track can allow for alternative adjustment and interplay between the two weights. For example, with respect to the front track 214, two independently adjustable weight assemblies can be positioned fully on the toe side, fully on the heel side, spaced apart a maximum distance with one weight fully on the toe side and the other fully on the heel side, positioned together in the middle of the weight track, or in other weight location patterns. With a single weight assembly in a track, as illustrated, the weight adjustment options are more limited but the effective CG of the head still can be adjusted along a continuum, such as heelward or toeward or in a neutral position with the weight centered in the front weight track.
As shown in
The weight assemblies can be adjusted by loosening the screws and moving the weights to a desired location along the tracks, then the screws can be tightened to secure them in place. The weights assemblies can also be swapped out and replaced by other weight assemblies having different masses to provide further mass adjustment options. If a second or third weight is added to the weight track, many additional weight location and distribution options are available for additional fine tuning of the head's effective CG location in the heel-toe direction and the front-rear direction, and combinations thereof. This also provides great range of adjust of the club head's MOI properties.
Either or both of the weight assemblies 210, 212 can comprise a three piece assembly including an inner weight member, an outer weight member, and a fastener coupling the two weight members together. The assemblies can clamp onto front, back, or side ledges of the weight tracks by tightening the fastener such that the inner member contacts the inner side the ledge and the outer weight member contacts the outer side of the ledge, with enough clamping force to hold the assembly stationary relative to the body throughout a round of golf. The weight members and the assemblies can be shaped and/or configured to be inserted into the weight track by inserting the inner weight member into the inner channel past the ledge(s) at a usable portion of the weight track, as opposed to inserting the inner weight at an enlarged opening at one end of the weight track where the weight assembly is not configured to be secured in place. This can allow for elimination of such a wider, non-functional opening at the end of the track, and allow the track to be shorter or to have a longer functional ledge width over which the weight assembly can be secured. To allow the inner weight member to be inserted into the track in the middle of the track (for example) past the ledge, the inner weight member can be inserted at an angle that is not perpendicular to the ledge, e.g., an angled insertion. The weight member can be inserted at an angle and gradually rotated into the inner channel to allow insertion past the clamping ledge. In some embodiments, the inner weight member can have a rounded, oval, oblong, arcuate, curved, or otherwise specifically shaped structure to better allow the weight member to insert into the channel past the ledge at a useable portion of the track.
In the golf club heads of the present disclosure, the ability to adjust the relative positions and masses of the slidably adjusted weights and/or threadably adjustable weights, coupled with the weight saving achieved by titanium alloys material use and incorporation of the light-weight crown insert and/or sole insert, further coupled with the discretionary mass provided by the raised sole configurations, can allow for a large range of variation of a number properties of the club-head all of which affect the ultimate club-head performance including the position of the CG of the club-head, MOI values of the club head, acoustic properties of the club head, aesthetic appearance and subjective feel properties of the club head, and/or other properties.
In certain embodiments, the front weight track and the rear weight track have certain track widths. The track widths may be measured, for example, as the horizontal distance between a first track wall and a second track wall that are generally parallel to each other on opposite sides of the inner portion of the track that receives the inner weight member of the weight assembly. With reference to
Additionally, both the front track and rear track have a certain track length. Track length may be measured as the horizontal distance between the opposing longitudinal end walls of the track. For both the front track and the rear track, their track lengths may be between about 30 mm and about 120 mm, such as between about 50 mm and about 100 mm, or such as between about 60 mm and about 90 mm. Additionally, or alternatively, the length of the front track may be represented as a percentage of the striking face length. For example, the front track may be between about 30% and about 100% of the striking face length, such as between about 50% and about 90%, or such as between about 60% and about 80% mm of the striking face length.
The track depth, width, and length properties described above can also analogously also be applied to the front channel 36 of the club head 10.
In
Referring to
In one embodiment, the vertical distance between the level of the ground contact surfaces of the sit pads and the adjacent surfaces of the raised sole portions may be in the range of about 2-12 mm, preferably about 3-9 mm, more preferably about 4-7 mm, and most preferably about 4.5-6.5 mm. In one example, the vertical distance is about 5.5 mm.
In some embodiments, it the joints 420 can be located a sufficient distance from the strike face to avoid potential failures due to the severe impacts undergone by the golf club when striking a golf ball. For example, in some embodiments, the joints 420 can be spaced at least 20 mm, at least 30 mm, at least 40 mm, at least 50 mm, at least 60 mm, and/or from 20 mm to 70 mm rearward of a center face of the club head as measured along a y-axis (front-to-back direction).
In some embodiments, the ring 404 can include a mass pad having increased thickness, such as in the projections 430 or elsewhere, to provide rear weighting for the golf club and move the center of mass rearward and increase MOI about the z and x axes. Such rear weighting can also be accomplished with an added weight member coupled to the rear ring, such as a removable, swappable, and/or adjustable weight member coupled to the rear part of the ring. For example, the projection 430 or other part of the ring 404 can include an opening, such as a threaded opening, a track, or other weight member receiving feature.
In some embodiments, the cup 402 can include a mass pad, such as the mass pad 432 shown in the drawings, at the bottom sole region to lower the center or mass and/or move the center of mass forward. In some embodiments, the cup 402 can include one or more added weight members coupled to the sole portion of the cup, such as in or near the mass pad 432 and/or rearward of the slot 418, such as one or more removable, swappable, and/or adjustable weight members coupled to the cup. For example, the mass pad 432 or other part of the cup 402 can include one or more openings, such as a threaded opening, a track, or other weight member receiving feature. Two or more weight members can also be coupled to the cup at the same time. The weight member(s) can comprise a relatively more dense material that the cast cup material, such as tungsten or steel. In some embodiments, the cup and the ring can have matching weight ports that can allow for swapping weight members between the rear ring locations and the lower cup locations, providing adjustability options to change the mass properties of the club head. In some such examples, a group of swappable weights can be provided with the club head, such as including a 1-3 g weight and a 8-15 g weight, which can be coupled to a weight port in the rear ring or to a weight port in the sole portion of the cup, which can allow for a higher MOI (heavier weight in rear) or lower spin (heavier weight in the low-forward location), or other combinations and mass properties.
The cup 402 is illustrated in more detail in
Forming the wax cup from two separate wax pieces (as in
Starting with two separate wax pieces also allows for efficiencies in forming large numbers of the wax pieces, as each wax piece is smaller and can be produced in greater numbers per batch on the same tree.
Once the wax cup (e.g., 500 or 510) is created, the wax cup can be used to form a mold for casting a metal cup (e.g., cup 402). The mold can comprise ceramic material and/or any other suitable material for casting a metal cup. Once the mold is formed around the wax cup, the wax can be melted and drained out of the mold. Various subsequent steps can then be applied to prepare the mold for casting, including adding gating and/or surface treatments to the mold. In addition, several cup molds can be combined into one mold tree for casting several metallic cups at the same time. After the mold is prepared, molten metal can then be introduced into the mold to cast the metal cup. The mold can then be opened/removed to access the cast metal cup. The cast metal cup can be formed of any suitable metal or metal alloy, including titanium alloys (any suitable metallic material disclosed herein can be used for the cast cup).
After the metal cup is cast, portions of the cast cup can be machined or modified to remove parts of the cast cup as desired. For one example, the front surface of the face portion of the cup can be machined to add horizontal score lines and/or to create a more precise texture, curvature, and twist. For another example, the rear surface of the face portion of the cup can be machined to modify the thickness profile across the height and width of the face portion, producing a desired variable thickness profile across the face portion. The front and/or rear surface of the face portion of the cast cup can also be machined or chemically etched (e.g., using hydrofluoric acid) to remove part or all of the alpha case layer formed during the casting process (e.g., for titanium alloys), such as to make the face portion less brittle and to increase durability of the face portion.
In anticipation of post-casting removal of material from the face portion of the cup, the face portion of the cup can be cast with extra thickness of material, such that a desired amount of material and a desired thickness profile is left after post-casting material removal.
As shown in
Another advantage of casting the cup and the ring separately is that it allows for efficiencies in casting large numbers of each of the ring and cup pieces, as each cast piece is smaller than the combined body and can be produced in greater numbers per batch on the same tree. Also, the same ring piece can be used with various differently shaped cup pieces, so only the tooling for the cup piece need be changed to accommodate a change to the club head body or making several different variations of the club head with different cup/face geometries.
In a sheet-based process, the face plate is formed from a flat sheet of metal having a uniform thickness. Such a sheet of metal is typically rolled along one axis to reduce the thickness to a certain uniform thickness across the sheet. This rolling process can impart a grain direction in the sheet that creates a different material properties in the rolling axis direction compared to the direction perpendicular to the rolling direction. This variation in material properties can be undesirable and can be avoided by using the disclosed casting methods instead to create face portion.
Furthermore, because a conventional face plate starts off as a flat sheet of uniform thickness, the thickness of the whole sheet has to be at least as great as the maximum thickness of the desired end product face plate, meaning much of the starting sheet material has to be removed and wasted, increasing material cost. By contrast, in the disclosed casting methods, the face portion is initially formed much closer to the final shape and mass, and much less material has to be removed and wasted. This saves time and cost.
Still further, in a conventional process, the initial flat sheet of metal has to be bent in a special process to impart a desired bulge and roll curvature to the face plate. Such a bending process is not needed when using the disclosed casting methods.
The unique thickness profiles illustrated in
By using the herein disclosed casting methods, large numbers of the disclosed club heads can be manufacture faster and more efficiently. For example, 50 or more of the cups 402 can be cast at the same time on a single casting tree, whereas it would take much longer and require more resources to create the novel face thickness profiles on face plates using a conventional milling methods using a lathe, one at a time.
In
The second ring 608 can itself have a variable thickness profile, such that the thickness of the second ring 608 varies as a function of the circumferential position around the center 602. Similarly, the variable blend zone 606 can have a thickness profile that varies as a function of the circumferential position around the center 602 and provides a transition in thickness from the maximum thickness ring 604 to the variable and less thicknesses of the second ring 608. For example, the variable blend zone 606 to a second ring 608 can be divided into eight sectors that are labeled A-H in
One example of the cast cup 600 can have the following thicknesses: 3.1 mm at center 602, 3.3 mm at ring 604, the second ring 608 can vary from 2.8 mm in zone A to 2.2 mm in zone C to 2.4 mm in zone E to 2.0 mm in zone G, and 1.8 mm in the heel and toe zones 610.
One example of the face portion 700 can have the following thicknesses: 3.9 mm at center 702, 4.05 mm at ring 704, 3.6 mm in zone A, 3.2 mm in zone B, 3.25 mm in zone C, 2.05 mm in zone D, 3.35 mm in zone E, 2.05 mm in zone F, 3.00 mm in zone G, 2.65 mm in zone H, and 1.9 mm at perimeter ring 710.
To the heel side, the thicknesses are offset by set amount (e.g., 0.15 mm) to be slightly thicker relative to their counterpart areas on the toe side. A thickening zone 820 (dashed lines) provides a transition where all thicknesses gradually step up toward the thicker offset zone 822 (dashed lines) at the heel side. In the offset zone 822, the ring 823 is thicker than the ring 806 on the heel side by a set amount (e.g., 0.15 mm), and the ring 825 is thicker that the ring 808 by the same set amount. Blend zones 824 and 826 gradually decrease in thickness moving radially outwardly, and are each thicker than their counterpart blend zones 807 and 810 on the toe side. In the thickening zone 820, the inner ring 804 gradually increases in thickness moving toward the heel.
One example of the face portion 800 can have the following thicknesses: 3.8 mm at the center 802, 4.0 mm at the inner ring 804 and thickening to 4.15 mm across the thickening zone 820, 3.5 mm at the second ring 806 and 3.65 mm at the ring 823, 2.4 mm at the third ring 808 and 2.55 mm at the ring 825, 2.0 mm at the fourth ring 811, and 1.8 mm at the perimeter ring 814.
The targeted offset thickness profile shown in
Various other varying face thickness profiles can be produced using the disclosed methods, including those disclosed in U.S. patent application Ser. No. 12/006,060 and U.S. Pat. Nos. 6,997,820; 6,800,038; 6,824,475; 7,731,603; 8,801,541; 9,943,743; and 9,975,018; the entire contents of each of which are incorporated herein by reference in their entireties. For example, U.S. Pat. No. 9,975,018 discloses examples of striking faces that include a localized stiffened region, such as an inverted cone or ‘donut’ shaped thickness profile that is offset from the center of the face, which alters the launch conditions of golf balls struck by the club head in a way that wholly or partially compensates for, overcomes, or prevents the occurrence of a rightward/leftward deviation. In particular, the localized stiffened region is located on the striking face such that a golf ball struck under typical conditions will not impart a left-tending and/or right-tending sidespin to the golf ball.
All of the disclosed face thickness profiles can be made possible by the casting methods disclosed herein. Such configurations would not be possible using a conventional turning process of removing material in concentric circle patterns from the rear of an originally flat face plate.
In some golf club head embodiments, the face plate can be cast individually, and then welded into a front opening in the frame of the club head. When a face plate is welded to the front opening of frame, extra material is typically produced around the weld zone, and this extra material has to be removed after the welding process to smooth out the transition between the face plate and the frame. This process can be avoided by casting the entire cup, including the face and the frontal frame, as a single cast unit, as disclosed herein.
However, casting the face plate separately can provide advantages over casting the entire cup as a unit. For example, post-processing of the cast face plate is much easier compared to post-processing the face surfaces when it is part of a cup.
Golf club heads that are cast including the face as an integral part of the body (e.g., cast at the same time as a single cast object) can provide superior structural properties compared to club heads where the face is formed separately and later attached (e.g., welded or bolted) to a front opening in the club head body. However, the advantages of having an integrally cast Ti face are mitigated by the need to remove the alpha case on the surface of cast Ti faces.
With the herein disclosed club heads comprising an integrally cast titanium alloy face and body unit (e.g., cast cup), the drawback of having to remove the alpha case can be eliminated, or at least substantially reduced. For a cast 9-1-1 Ti face, using a mold pre-heat temperature of 1000 C or more, the thickness of the alpha case can be about 0.10 mm or less, 0.15 mm or less, or about 0.20 mm or less, or about 0.30 mm or less, such as between 0.10 mm and 0.30 mm in some embodiments, whereas for a cast 6-4 Ti face the thickness of the alpha case can be greater than 0.10 mm, greater than 0.15 mm, or greater than 0.20 mm, or greater than 0.30 mm, such as from about 0.25 mm to about 0.30 mm in some examples. In some embodiments, the alpha case thickness can be as low as 0.1 mm and up to 0.15 mm while providing sufficiently durable products that have a desirably high CT time across the face. In some embodiments, the alpha case on the rear of the face at the geometric center of the face can have a thickness less than 0.30 mm and/or less than 0.20 mm, and this can be accomplished without chemically etching the surface after formation.
Other titanium alloys that can be used to form any of the striking faces and/or club heads described herein can comprise titanium, aluminum, molybdenum, chromium, vanadium, and/or iron. For example, in one representative embodiment the alloy may be an alpha-beta titanium alloy comprising 6.5% to 10% Al by weight, 0.5% to 3.25% Mo by weight, 1.0% to 3.0% Cr by weight, 0.25% to 1.75% V by weight, and/or 0.25% to 1% Fe by weight, with the balance comprising Ti (one example is sometimes referred to as “1300” titanium alloy).
In another representative embodiment, the alloy may comprise 6.75% to 9.75% Al by weight, 0.75% to 3.25% or 2.75% Mo by weight, 1.0% to 3.0% Cr by weight, 0.25% to 1.75% V by weight, and/or 0.25% to 1% Fe by weight, with the balance comprising Ti.
In another representative embodiment, the alloy may comprise 7% to 9% Al by weight, 1.75% to 3.25% Mo by weight, 1.25% to 2.75% Cr by weight, 0.5% to 1.5% V by weight, and/or 0.25% to 0.75% Fe by weight, with the balance comprising Ti.
In another representative embodiment, the alloy may comprise 7.5% to 8.5% Al by weight, 2.0% to 3.0% Mo by weight, 1.5% to 2.5% Cr by weight, 0.75% to 1.25% V by weight, and/or 0.375% to 0.625% Fe by weight, with the balance comprising Ti.
In another representative embodiment, the alloy may comprise 8% Al by weight, 2.5% Mo by weight, 2% Cr by weight, 1% V by weight, and/or 0.5% Fe by weight, with the balance comprising Ti. Such titanium alloys can have the formula Ti-8Al-2.5Mo-2Cr-1V-0.5Fe. As used herein, reference to “Ti-8Al-2.5Mo-2Cr-1V-0.5Fe” refers to a titanium alloy including the referenced elements in any of the proportions given above. Certain embodiments may also comprise trace quantities of K, Mn, and/or Zr, and/or various impurities.
Ti-8Al-2.5Mo-2Cr-1V-0.5Fe can have minimum mechanical properties of 1150 MPa yield strength, 1180 MPa ultimate tensile strength, and 8% elongation. These minimum properties can be significantly superior to other cast titanium alloys, including 6-4 Ti and 9-1-1 Ti, which can have the minimum mechanical properties noted above. In some embodiments, Ti-8Al-2.5Mo-2Cr-1V-0.5Fe can have a tensile strength of from about 1180 MPa to about 1460 MPa, a yield strength of from about 1150 MPa to about 1415 MPa, an elongation of from about 8% to about 12%, a modulus of elasticity of about 110 GPa, a density of about 4.45 g/cm3, and a hardness of about 43 on the Rockwell C scale (43 HRC). In particular embodiments, the Ti-8Al-2.5Mo-2Cr-1V-0.5Fe alloy can have a tensile strength of about 1320 MPa, a yield strength of about 1284 MPa, and an elongation of about 10%.
In some embodiments, striking faces and/or cups with a face portion can be cast from Ti-8Al-2.5Mo-2Cr-1V-0.5Fe. In some embodiments, striking surfaces and club head bodies can be integrally formed or cast together from Ti-8Al-2.5Mo-2Cr-1V-0.5Fe, depending upon the particular characteristics desired.
The mechanical parameters of Ti-8Al-2.5Mo-2Cr-1V-0.5Fe given above can provide surprisingly superior performance compared to other existing titanium alloys. For example, due to the relatively high tensile strength of Ti-8Al-2.5Mo-2Cr-1V-0.5Fe, cast striking faces comprising this alloy can exhibit less deflection per unit thickness compared to other alloys when striking a golf ball. This can be especially beneficial for metalwood-type clubs configured for striking a ball at high speed, as the higher tensile strength of Ti-8Al-2.5Mo-2Cr-1V-0.5Fe results in less deflection of the striking face, and reduces the tendency of the striking face to flatten with repeated use. This allows the striking face to retain its original bulge, roll, and “twist” dimensions over prolonged use, including by advanced and/or professional golfers who tend to strike the ball at particularly high club velocities.
Any of the herein disclosed embodiments can include a face portion that has a striking surface that is twisted such that an upper toe portion of the striking surface is more open than a lower toe portion of the striking surface, and such that a lower heel portion of the striking surface is more closed than an upper heel portion of the striking surface. More information regarding golf club heads with twisted striking surfaces can be found in U.S. Pat. No. 9,814,944; U.S. Provisional Patent Application No. 62/687,143 filed Jun. 19, 2018; U.S. patent application Ser. No. 16/160,884 filed Oct. 15, 2018; all of which are herein incorporated by reference in their entireties. Any of these twisted face technologies disclosed in these incorporated references can be implemented in the herein disclosed club heads, in any combination with the herein disclosed technologies.
As shown in
In some embodiments, a weight can simply be a screw that is screwed into an opening in the club head. In other embodiments, the weights can be secured via discrete screws or by other means such as welding or adhesive. In some embodiments, the weight can comprise a thickened mass pad that is integrated with another part of the club head. By casting the front cup portion of the club head from lighter, stronger material such as titanium alloy, by employing a rear ring, and by employing lightweight crown and sole inserts, among other things, a significant amount of discretionary mass can be saved and added back in the form of weight members in desired locations and configurations.
The club head 1800 also comprises an adjustable head-shaft connection assembly including elements 1824 and 1826 secured in hosel 1822 via a screw 1828 that is inserted via a sole recess 1834 below the hosel. The cup 1802 includes a front striking face 1852, a front sole portion 1836, a rear sole portion 1838, and a sole channel 1832 positioned between the front and rear sole portions of the cup and toward of the sole recess 1834. At the top, the cup 1802 include a forward crown portion 1848.
The cup 1802 also includes ring engagement portions 1820 that project rearwardly from the toe and from the heel for coupling to the rear ring 1804. The rear ring includes cup engagement portions 1818 at the front ends of the heel and toe sides of the ring, and together the cup engagement portions and the ring engagement portions form joints 1844 at the toe side and heel side of the club head. The joints can be secured in various manners, include with welds, adhesives, mechanical interlocking features, frictions fits, fasteners, and/or other means. In some embodiments, the two cup engagement portions of the ring can be elastically compressed or squeeze toward each other to engage with the ring engagement portions of the cup, and then released such that they resiliently expand apart to form an interlocking or friction based joint.
In some embodiments, the ring can engage with the cup via a snap-fit or friction fit engagement. In some embodiments, the ring can be detachable from the cup, and reattachable. In some embodiments, different types of rings can be selected to match with a given cup. For example, ring made of steel, titanium, or aluminum can be selected from. Rings can also be selected based on the type of rear weight system they include (e.g., integral mass pad, screw weight, bolt-on weight, etc.).
The top of the cup 1802 can have a recessed lip 1850 and the top of the ring 1804 can have a recessed lip 1860 (e.g.,
Also shown in
As shown in
At the lower side of
For any of the club heads disclosed herein, any of the front and/or rear weights, as well as any of the screws or other additional elements used to attach a weight to the club head, can be formed form dense material (e.g., tungsten, steel, nickel, cobalt, lead, gold, silver, titanium, platinum, etc.), which can be relatively more dense than the material of the club head part to which they are attached (e.g., the cup or ring), and can have any mass. The weight member and its screw can be comprised of the same or different materials, and can be combined to provide a desired total mass. Each of the front and rear weights, for example, can have a mass of from 0.5 gram to 50 grams, from 1 gram to 40 grams, from 1 gram to 30 grams, from 1 gram to 25 grams, less than 50 grams, less than 40 grams, less than 30 grams, less than 25 grams, from 2 grams to 7 grams, from 2 grams to 15 grams, from 2 grams to 25 grams, from 5 grams to 10 grams, from 5 grams to 15 grams, from 5 grams to 20 grams, from 5 grams to 25 grams, from 5 grams to 30 grams, from 7 grams to 10 grams, from 7 grams to 30 grams, from 10 grams to 20 grams, from 10 grams to 30 grams, from 15 grams to 25 grams, or from 15 grams to 50 grams. In one particular example of the club head 1800, the front weight comprises tungsten and has a mass of 18.7 grams and the rear weight comprises steel and has a mass of 8.62 grams, while the overall club head has a mass of 200.5 grams, the cup comprises 9-1-1 titanium and has a mass of 110.01 grams, and the ring comprises aluminum 7075 and has a mass of 22.36 grams. Additional mass can be added via hot melt adhesive or other similar material to any part of the body, such as behind the face and in the rear part of the ring, which can be less than 10 grams for example.
For any of the club heads disclosed herein, the entire rear ring assembly, include the rear weight and any screw and hot melt added, can have any mass, such as a mass of from 1 gram to 60 grams, from 5 grams to 50 grams, from 10 grams to 45 grams, from 10 grams to 40 grams, and/or from 15 grams to 35 grams. The ring itself can have a mass of from 1 gram to 50 grams, from 5 grams to 40 grams, from 8 grams to 30 grams, from 10 grams to 28 grams, and/or from 12 grams to 25 grams. Rings made of aluminum can have less mass, for example, compared to rings made of steel or titanium.
For any of the club heads disclosed herein, the front cup can have any mass, such as from 75 grams to 150 grams, from 80 grams to 140 grams, from 90 grams to 130 grams, and/or from 100 grams to 120 grams.
For any of the club heads disclosed herein, a ratio of the mass of the cup to the mass of the ring (without any added weights or other objects) can be greater than 1:1, greater than 2:1, greater than 3:1, greater than 4:1, greater than 5:1, greater than 6:1, and/or greater than 8:1.
By moving the mass of the club head further toward the front and rear ends of the club head, and toward the sole, the club head can achieve unique mass distribution and inertial properties. For example, the constriction of club head 1800 can free up a very high mass of discretion weight, and that discretionary weight be reapplied to desired locations primarily via the front and rear weights, and to a lesser extent via other added materials such as hot melt adhesive additions. In a given example of the club head 1800, where 30 grams of mass are freed up and redistributed via the front and rear weights, that discretionary mass can be divided in any desired way between the two weights, such as evenly (15 gram front weight and 15 gram rear weight), more in the front (e.g., 20 gram front weight and 10 gram rear weight), more in the rear (10 gram front weight and 10 gram rear weight), and even more extreme distributions like 5 g/25 g or 1 g/29 g.
Some embodiments of the club heads disclosed herein (including the club head 1800 and the other club heads disclosed herein) can have an Izz greater than 450 kg/mm2, greater than 475 kg/mm2, greater than 500 kg/mm2, greater than 510 kg/mm2, and/or greater than 525 kg/mm2. Some embodiments can have an Ixx greater than 300 kg/mm2, greater than 350 kg/mm2, greater than 375 kg/mm2, greater than 400 kg/mm2, and/or greater than 425 kg/mm2. Some embodiments of the club heads can have a combined Izz+Ixx of greater than 750 kg/mm2, greater than 800 kg/mm2, greater than 850 kg/mm2, greater than 875 kg/mm2, and/or greater than 900 kg/mm2. Some embodiments of the club heads can have an Iyy greater than 250 kg/mm2, greater than 275 kg/mm2, greater than 300 kg/mm2, greater than 310 kg/mm2, and/or greater than 325 kg/mm2.
The center of gravity is also affected by the configuration of the weights. Some embodiments of the club heads described herein (including the club head 1800 and any of the other club heads described herein) can have a CGx greater than 0, less than 0, from −1 mm to 1 mm, from −1 mm to 0, from −2 mm to 0, from −3 mm to −1 mm, from −3 mm to −2 mm. Some embodiments of the club heads described herein can have a CGz less than −2 mm, less than −2.5 mm, less than −3 mm, less than −3.5 mm, less than −4 mm, less than −4.5 mm, and/or less than −5 mm.
The golf club heads described herein can have a Delta 1, which is a measure of how far rearward in the golf club head the CG is located. More specifically, Delta 1 is the distance between the CG and the hosel axis along the y axis. Some embodiments of the club heads described herein can have a Delta 1 of at least 15 mm, at least 17 mm, at least 18 mm, at least 19 mm, at least 20 mm, at least 21 mm, at least 22 mm, at least 23 mm, at least 24 mm, at least 25 mm, and/or at least 26 mm. Some club heads can have a Delta 1 between about 15 mm and about 30 mm and/or between 21 mm and 26 mm.
These mass distribution and inertia properties can provide advantages and benefits over other club heads, such as more forgiveness on mishit shots, less back spin, more distance, higher launch angle, better acoustic properties when striking a ball, more adjustability for a user, etc. In some embodiments, the club head 1800 can have a desirable first mode frequency above 3000 Hz when striking a ball. Part of this is due to shapes and constructions of the lightweight crown and sole inserts. In some embodiments, for example, the inserts can comprise strong carbon fiber reinforces composites built up with at least 5 layers, such as 5-10 layers of composite carbon layers. The increased curvature in the sole around the transition between the sole insert 1808 and the rear sole surface 1840 can also help with strength and acoustics.
A ratio of the mass of the crown insert 1806 to the mass of the sole insert 1808 can be about even, less than 1:1, or greater than 1:1. In some embodiments, the crown insert can be thinner and/or have a lower average areal weight than the sole insert.
For any of the embodiments disclosed herein that include a cast cup and a rear ring attached to the cup, with a front weight element coupled to the cup and a rear weight element coupled to the ring, the location of each mass element on the golf club head can be defined as the location of the center of gravity of the mass element relative to the club head origin coordinate system. For example, in some implementations, the front mass element has an origin x-axis coordinate between approximately 15 mm and approximately 35 mm, an origin y-axis coordinate between approximately 10 mm and approximately 30 mm, and an origin z-axis coordinate between approximately −20 mm −30 mm and approximately −10 mm. In one specific implementation, the front mass element has an origin x-axis coordinate of approximately 22 mm, an origin y-axis coordinate of approximately 23 mm, and an origin z-axis coordinate of approximately −21 mm.
Similarly, in some implementations, the rear mass element has an origin x-axis coordinate between approximately −20 mm and approximately 10 mm, an origin y-axis coordinate between approximately 90 mm and approximately 120 mm, and an origin z-axis coordinate between approximately −30 mm and approximately 10 mm. In one specific implementation, the rear mass element has an origin x-axis coordinate of approximately −7 mm, an origin y-axis coordinate of approximately 110 mm, and an origin z-axis coordinate of approximately −11 mm.
Due to the cup and ring configuration with light-weight crown and sole inserts, and due the placement and mass of the front and rear weights, along with other structural features, the balance point (BP) of golf club heads described herein can be shifted toeward of the geometric center of the golf club head.
The configuration of the golf club head, including the locations and masses of the front and rear mass elements, can result in the club head having a moment of inertia about the CG z-axis (Izz) between about 450 kg·mm2 and about 600 kg·mm2, and a moment of inertia about the CG x-axis (Ixx) between about 280 kg mm2 and about 400 kg·mm2. In one specific implementation, the club head has a moment of inertia about the CG z-axis (Izz) of approximately 528 kg·mm2 and a moment of inertia about the CG x-axis (Ixx) of approximately 339 kg·mm2. In this implementation, then, the ratio of Ixx/Izz is approximately 0.64. However, in other implementations, the ratio of Ixx/Izz is between about 0.5 kg·mm2 and about 0.9 kg·mm2. In some embodiments, golf club heads as described herein can have a combined Izz+Ixx that is less than 1100 kg·mm2 and greater than 780 kg mm2, greater than 800 kg mm2, greater than 820 kg mm2, greater than 840 kg mm2, greater than 860 kg mm2, greater than 880 kg mm2, and/or greater than 900 kg mm2.
As described herein, the rear ring of any of the club heads disclosed herein can comprise various different materials and features, and be made of different materials and have different properties than the cast cup, which is formed separately and later coupled to the ring. In addition to or alternative to other materials described herein, the rear ring can comprise metallic materials, polymeric materials, and/or composite materials, and can include various external coatings.
Separately forming the ring not only allows for greater access to the rear portion of the face for milling operations to remove unwanted alpha case and allows for machining in various face patterns, but also allows the use of lower density materials having a density between 1 g/cc to 4 g/cc, or between 1 g/cc and 3 g/cc, or between 1 g/cc and 2 g/cc, such as aluminum or plastic or composite materials, which yields additional discretionary mass that can be redistributed throughout the club head to achieve desirable CG characteristics and a variety of launch conditions. For example, an aluminum ring may save 8 to 15 grams over a titanium ring, and a plastic ring may offer up to 3 to 7 grams of mass savings over an aluminum ring. For embodiments that include a composite crown insert and/or a composite sole insert a ledge will often be necessary to provide desirable fit and finish and sufficient bonding area to ensure the adhesive glue bond is durable and avoids premature failure. The cast cup can comprise titanium or titanium alloy and has a density greater than 4 g/cc, such as about 4.5 g/cc for example. Thus, when this ledge is formed of titanium alloy having a density of about 4.5 g/cc it reduces the amount of discretionary mas compared to an aluminum ring that has a density of about 2.7 g/cc or a plastic ring that has a density of about 1.5 g/cc. The added mass due to the bonding ledges greatly reduces the benefit of a composite crown insert because the ledges generally are a minimum of 4 mm and up to 10 mm, which diminishes any mass savings from the composite crown. Accordingly, by separately forming the ring out of a lower density material e.g. a material with a density between 1 g/cc and 4 g/cc, or between 1 g/cc and 3 g/cc, more discretionary mass can be freed up to strategically place elsewhere in the club head and the mass savings can range from 8 grams to 22 grams compared to a titanium rear ring. In some instances, the forward cup formed of a first material (e.g. titanium alloy) forms a first portion of a crown ledge having a first bond area, and the rear ring formed of a second lower density material (e.g. aluminum alloy or fiber reinforced polycarbonate) forms a second portion of the crown ledge having a second bond area, and the second bond area of the rear ring makes up between 25-60% of the total crown ledge bond area, preferably the rear ring makes up between 30-65% of the total crown ledge bond area. Similarly, in some instances, the forward cup formed of a first material (e.g. titanium alloy) forms a first portion of a sole ledge having a third bond area, and the rear ring formed of a second lower density material (e.g. aluminum alloy or fiber reinforced polycarbonate) forms a second portion of the sole ledge having a fourth bond area, and the fourth bond area of the rear ring makes up between 25-65% of the total sole ledge bond area, preferably the rear ring makes up between 40-60% of the total sole ledge bond area. Increasing the percentage of bond area made up by the lower density rear ring increases the overall discretionary mass i.e. mass savings. In some embodiments, the first bond area may be larger than the third bond area, and the fourth bond area may be larger than the second bond area, the fourth bond area may be larger than the third bond area, and the second bond area may be larger than the first bond area.
In some embodiments, the ring comprises anodized aluminum, such as 6000, 7000, and 8000 series aluminum. In one specific example, the ring comprises 7075 grade aluminum. The anodized aluminum can be colored, such as red, green, blue, gray, white, orange, purple, pink, fuchsia, black, clear, yellow, gold, silver, or metallic colors. In some embodiments, the ring can have a color that contrasts from a majority color located on other parts of the club head (e.g., the crown insert, the sole insert, the cup, the rear weight, etc.).
In some embodiments, the rear ring can comprise any combination of metals, metal alloys (e.g., Ti alloys, steel, boron infused steel, aluminum, copper, beryllium), composite materials (e.g., carbon fiber reinforced polymer, with short or long fibers), hard plastics, resilient elastomers, other polymeric materials, and/or other suitable materials. Any material selection for the ring can also be combined with any of various formation methods, such as any combination of the following: casting, injection molding, sintering, machining, milling, extruding, forging, stamping, and rolling.
A plastic ring (e.g., fiber reinforced polycarbonate ring) may offer mass savings (e.g. about 5 grams compared to an aluminum ring), cost savings, give greater design flexibility due to processes used to form the ring (e.g. injection molded thermoplastic), and/or perform similarly to an aluminum ring in abuse testing (e.g. slamming the club head into a concrete cart path (extreme abuse) or shaking it in a bag where other metal clubs can repeatedly impact it (normal abuse)).
In some embodiments, the ring can comprise a polymeric material (e.g., plastic) with a non-conductive vacuum metallizing (NCVM) coating. For example, in some embodiments, the ring can include a primer layer having an average thickness of about 5-11 micrometers (μm) or about 8.5 μm, an under coating layer on top of the primer layer having an average thickness of about 5-11 μm or about 8.5 μm, a NCVM layer on top of under coating layer having an average thickness of about 1.1-3.5 μm or about 2.5 μm, a color coating layer on top of the NCVM layer having an average thickness of about 25-35 μm or about 29 μm, and a top coating (e.g., UV protection coat) outer layer on top of the color coating layer having an average thickness of about 20-35 μm or about 26 μm. In general, for a NCVM coated part or ring the NCVM layer will be the thinnest and the color coating layer and the top coating layers will be the thickest, for example about 8-15 times thicker than NCVM layer. Generally, all the layers can combine to have a total average thickness of about 60-90 μm or about 75 μm. The described layers and NCVM coating can be applied to other parts of the club head other than the ring, such as the crown, sole, forward cup, and removable weights, and it can be applied prior to assembly.
In some embodiments, the ring can comprise a physical vapor deposition (PVD) coating or film layer. In some embodiments, the ring can include a paint layer, or other outer coloring layer. Conventionally, painting a golf club heads is all done by hand and requires masking various components to prevent unwanted spray on unwanted surfaces. Hand painting, however, can lead to great inconsistency from club to club. Separately forming the ring not only allows for greater access to the rear portion of the face for milling operations to remove unwanted alpha case and allows for machining in various face patterns, but it also eliminates the need for masking off various components. The ring can be painted in isolation prior to assembly. Or in the case of anodized aluminum, no painting may be necessary, eliminating a step in the process such that the ring can simply be bonded or attached to a cup that may also be fully finished. Similarly if the ring is coated using PVD or NCVM, this coating can be applied to the ring prior to assembly, again eliminating several steps. This also allows for attachment of various color rings that may be selectable by an end user to provide an alignment or aesthetic benefit to the user. Whether the ring is a NCVM coated ring or a PVD coated ring, it can be colored any of an array of colors, such as red, green, blue, gray, white, orange, purple, pink, fuchsia, black, clear, yellow, gold, silver, or metallic colors.
A sole insert 2014 and crown insert 2016 are coupled to the body to enclose a hollow interior cavity. The crown insert can be bonded to a crown ledge portion of the cup 2044 and a crown ledge portion of the ring 2046, which together encircle the crown opening of the body. The sole insert 2014 can be bonded to a sole ledge portion of the cup 2048 and a sole ledge portion of the ring 2050, which together encircle the sole opening of the body. The crown and sole inserts can be formed of any materials and by any methods as described elsewhere herein, and coupled to the cup/ring structure by any means.
A rear weight 2018 is coupled to the rear of the ring via fastener 2032 that secures the weight to a receiving portion of the ring 2052. A sole weight 2020 can threaded into a receptacle 2021 in the bottom of the cast cup. The rear weight 2018 and sole weight 2020 are analogous to the front and rear weight combinations described elsewhere herein, and can have any of the properties, attachment means, and locations described in connection with other front and rear weight embodiments. For example, the rear weight and sole weight can be formed of any material and have any masses as described elsewhere herein. As shown in
The cast cup 2010 includes the striking face 2030 of the club head, which can be cast integrally with the rest of the cup. Alternatively, a face plate can be formed separately and attached to an opening formed in the cast cup. The cast cup 2010 also includes a sole channel 2026 at a forward portion of the sole just behind the bottom of the striking face, and a plug 2027 can be positioned in the channel. As shown in
The cast cup also includes a hosel 2023 that receives an adjustable head-shaft connection assembly 2022, which is secured with a fastener 2024 inserted through a sole recess 2025 below the hosel. The adjustable head-shaft connection assembly 2022 can be similar to others described herein. In some embodiments, the hosel 2023 can include an opening in a wall that faces the internal cavity of the club head, as shown for example in
The cast cup can also include a port or opening 2034 at the toe end that allows for material, such as hot melt, to be injected into the interior of the club head to adjust the performance properties of the club head. A screw 2035 can fill the port 2034. The port 2034 can be functionally similar to the toe side aperture 1846 of the club head 1800. In addition, the club head 2000 can also include structures analogous to ribs 1894, walls 1895 and 1896, and area 1898. Locating the port 2034 toward the toe side of the cup avoid forming an opening in the face, which can improve the consistency and integrity of the face.
The thickness at F0 can range from 2.8 mm to 3.2 mm.
The thickness at F1 can range from 2.9 mm to 3.3 mm.
The thickness at F2 can range from 2.9 mm to 3.3 mm.
The thickness at F3 can range from 2.9 mm to 3.3 mm.
The thickness at F4 can range from 2.9 mm to 3.3 mm.
The thickness at F5 can range from 2.35 mm to 2.65 mm.
The thickness at F6 can range from 2.3 mm to 2.8 mm.
The thickness at F7 can range from 2.1 mm to 2.3 mm.
The thickness at F8 can range from 2.6 mm to 2.9 mm.
The thickness at F9 can range from 1.7 mm to 2.0 mm.
The thickness at F10 can range from 1.7 mm to 2.0 mm.
The thickness around the edges of the face can range from 1.7 mm to 2.6 mm.
These face thickness values can be applied to a face that integrally cast as part of the cast cup, or to a separately formed face that is later coupled to an opening in the cast cup. Any post-casting process as described herein can be used to modify the face after it is initially cast or otherwise formed to achieve the final desired face thickness profile. For example, the rear of the face can be machined (e.g., CNC milling) to remove material from the rear of the face after casting the face. Many methods of machining can be used. In some methods, continuous path milling can be used, where the milling tool does not leave the work piece (e.g., the face) until the final thickness profile is complete. In this method, the tool moves side to side parallel to the face in a pattern that covers the whole portion of the face that is to be machined without separating the tool from the face.
In some milling methods, a ball end mill can be used having a given diameter (e.g., ½ inch). A ball end mill has a rounded tip that leaves a curved walled groove in the face. At the mill takes each pass across the face, the mill is shifted or stepped a certain distance so that the next pass is parallel but slightly offset from the previous pass. For each adjacent pair of passes with a ball end mill, a ridge or cusp of material is left behind between the two passes, which is sometimes called a scallop. The smaller the step or offset between passes, the shorted the scallop is. Similarly, the greater the radius of curvature of the ball end mill, the shorter the scallop is. Also, the larger the diameter/radius of the ball end mill, the more material is removed with each pass. Accordingly, there can be a desirable mill diameter range that is large enough that not too many passes and steps (and precision) are needed to complete the whole process, but small enough that the scallops left behind between the passes are not too tall. For example, the mill can have a diameter between ⅛ inch and 1 inch, such as between ¼ inch and ¾ inch, for example ½ inch. Similarly, the step distance between milling passes can range from 0.5 mm to 2 mm, such as about 1 mm. Smaller step distances can produce shorter scallop heights, enabling a more precise variable face thickness profile. One benefit of the ball end mill is that it can leave a rounded edge adjacent to the passes, as opposed to a sharp 90 degree edge if the mill has a squared end. Rounded edges can be less susceptible to stress concentrations and resulting cracking and failure. In some milling processes, the mill can move in a spiral pattern around the face, such as from a center point spiraling outward, or from an edge point spiraling inward. The mill can move clockwise or counterclockwise around the face. One factor that can guide the selection of the size of the mill, the step distance, and the milling pattern, is the desired amount of material to be removed from the face and the acceptable amount of undesired material (e.g., alpha case material) that can be left on the face. Where the thickness of material to be removed is large, a larger mill and/or a larger step size may be used. Where the thickness of the material to be removed is very thin, then a smaller mill and/or smaller step size can be used.
In some embodiments, the as-cast face has the following thickness values, and the after-milling final thickness values listed above can be achieved via post-casting milling, such as with a ball end mill.
The as-cast thickness at F0 can range from 3.3 mm to 3.5 mm.
The as-cast thickness at F1 can range from 3.4 mm to 3.6 mm.
The as-cast thickness at F2 can range from 3.4 mm to 3.6 mm.
The as-cast thickness at F3 can range from 3.4 mm to 3.6 mm.
The as-cast thickness at F4 can range from 3.4 mm to 3.6 mm.
The as-cast thickness at F5 can range from 2.75 mm to 2.95 mm.
The as-cast thickness at F6 can range from 3.0 mm to 3.2 mm.
The as-cast thickness at F7 can range from 2.1 mm to 2.3 mm.
The as-cast thickness at F8 can range from 3.0 mm to 3.2 mm.
The as-cast thickness at F9 can range from 2.2 mm to 2.4 mm.
The as-cast thickness at F10 can range from 2.2 mm to 2.4 mm.
The as-cast thickness around the edges of the face can range from 1.7 mm to 3.2 mm.
The post-cast milling processes can move from 0 mm to 1 mm, such as from 0 mm to 0.5 mm, from the rear of the face, depending on the position and the desired final profile.
Variable thickness face features are described in more detail in U.S. patent application Ser. No. 12/006,060 and U.S. Pat. Nos. 6,997,820, 6,800,038, and 6,824,475, which are incorporated herein by reference in their entirety.
In some instances, a bond area for the composite face insert will range from 850 mm2 to 1800 mm2, preferably between 1,300 mm2 to 1,500 mm2. In some instances, a ratio of the composite face insert bond area to the inner surface area of the composite face insert e.g. strike plate (rear surface area of the composite face insert) will range from 21% to 45%. In some instances, a total bond area of the composite face insert will be less than a total bond area of the crown insert. Further details on composite face inserts, composite face insert support structure, bond area, and multi-material and multi-component club head construction similar to that disclosed herein can be found in U.S. patent application Ser. No. 17/124,134, filed Dec. 16, 2020 and incorporated by reference herein in its entirety.
In some embodiments, when installed to the face insert support structures 2928A, 2928B, the face insert forms a part of the transition region from the face to the crown 2120 and/or the sole 2130. For example, at least a portion of the transition region may be painted the same color or shade as at least a portion of the crown prior to installing the face insert, which when installed provides a contrasting color or shade of the face insert with respect to the painted portion of the transition region and/or crown. In other embodiments, the face insert eliminates the need for a transition region from the face to the crown 2120 and/or the sole 2130. In some embodiments, the face insert includes at least a portion of the radius of the transition from the face insert to the crown. By forming part of the radius of the transition from the face to the crown, aerodynamics of the club head may be improved by decreasing turbulence of the air passing from the face to the crown and increasing annular flow.
In some embodiments, the upper face insert support structure 2928A is provided in a shape that flexes in a similar manner as the face insert when the golf club head strikes a golf ball. For example, in some golf club head designs, the face insert material, such as a composite material, is more flexible or compliant than the golf club body material, such as an aluminum or titanium alloy. In this example, a slot or recess 3008A may be provided within the upper peripheral member 3048A to increase flexibility or compliance of the upper face insert support structure 2928A, allowing the face to flex more uniformly. Additional and different shapes may be provided to increase or decrease flexibility and compliance of one or more components of the golf club body. By flexing in a similar manner, the golf club head may be more durable, substantially preventing the face insert from decoupling, or de-bonding, from the golf club body.
In some embodiments, the lower face insert support structure 2928B is provided in a shape that flexes in a similar manner as the face insert when the golf club head strikes a golf ball. In the example discussed above, the face insert material is more flexible or compliant than the golf club body material. In this example, a slot or recess 3008B may be provided within the lower peripheral member 3048B to increase flexibility or compliance of the upper face insert support structure 2928B, allowing the face to flex more uniformly. Additional and different shapes may be provided to increase or decrease flexibility and compliance of one or more components of the golf club body. By flexing in a similar manner, the golf club head may be more durable, substantially preventing the face insert from decoupling, or de-bonding, from the golf club body.
In some embodiments, a high CFY (e.g., greater than about 15 mm, 14 mm, 13 mm, or another CFY) may produce lateral dispersion right of the intended target line. In other embodiments, a low CFY (e.g., less than about 15 mm, 14 mm, 13 mm, or another CFY) may produce lateral dispersion left of the intended target line. In some embodiments, CFY is between about 13 mm and about 15 mm.
In some embodiments, a high face progression (e.g., greater than about 20 mm, 19 mm, 18 mm, or another face progression) may produce lateral dispersion right of the intended target line. In other embodiments, a low face progression (e.g., less than about 19 mm, 18 mm, 17 mm, or another face progression) may produce lateral dispersion left of the intended target line. In some embodiments, face progression is between about 15 mm and about 20 mm.
In some embodiments, a golf club head is provided with at least one of: CFY no more than 15.5 mm; CFY no more than 15 mm; CFY no more than 14.5 mm; CFY no more than 14 mm; CFY no more than 13.5; CFY no more than 13 mm; face progression no more than 20 mm; face progression no more than 19 mm; face progression no more than 18 mm; face progression no more than 17 mm; and face progression no more than 16 mm. In some embodiments, a golf club head is provided with a CFY no more than 17.5 mm.
In other embodiments, one or more alignment features are hard tooled into the golf club head by casting one or more witness lines into the golf club head. For example, one or more positive witness lines may be cast into the hollow body 3210, such as by casting a protrusion, ridge, or other raised feature in the hollow body 3210. In another example, one or more negative witness lines may be cast into the hollow body 3210, such as an indentation, valley, or other depressed feature into the hollow body 3210. In some embodiments, a combination of positive and negative witness lines may be provided. The one or more witness line may be painted with the hollow body 3210 to provide one or more alignment features. Alternatively or additionally, the witness lines may be used as a guide for painting one or more alignment features on the golf club head. By casting the witness lines in the golf club head during manufacturing, the subsequent painting of the one or more alignment features may be more accurate from part to part.
Referring to
In some embodiments, the golf club head 3200 includes a slot 3295 and a weight track 3245. For example, the slot 3295 and/or the weight track 3245 may be cast into the hollow body 3210. As will be discussed below, the slot 3295 may increase the durability of the golf club head by allowing at least a portion of the hollow body 3210 to flex similarly to the face insert 2110, increasing performance of the golf club head and increasing the durability of the golf club head by preventing the face insert 2110 from decoupling from the hollow body 3210. In some embodiments, the golf club head 3200 includes one or more characteristic time (CT) tuning ports. Referring to
In some embodiments, the golf club head includes one or more foam inserts. For example, a foam insert 3276 is positioned within the hollow body 3210. An additional foam insert is also provided proximate to the toe portion (not depicted). The one or more foam inserts aid in CT tuning the golf club head by restraining the adhesive or other material to locations within the golf club head while the material solidifies. Additionally, a rear wall may also be provided to further restrain the material while it solidifies. Accordingly, the foam inserts and the rear wall prevent the adhesive injected into the tuning port 3275 from moving too far toeward, heelward, and backward, allowing the golf club head to be CT tuned more precisely. Additional and different structures may be provided to restrain the injected materials during CT tuning. Further information related to CT tuning is discussed is U.S. patent application Ser. No. 16/223,108 filed Dec. 17, 2018 which is hereby incorporated by reference in its entirety.
In some embodiments, the golf club head includes a multi-material inertia generator. An inertia generator, as discussed herein, may also be referred to as an aft winglet and a center of gravity (CG) lowering platform. The inertia generator 3285 moves discretionary mass rearward to increase inertia and to move the CG projection lower on the face of the golf club head. For example, the golf club head 3200 includes an inertia generator 3285 extending rearwardly and angled toewardly from the front portion of the golf club head 3200 to the rear portion of the golf club head 3200. A multi-material inertia generator may include two or more materials of different densities. For example, the inertia generator 3285 includes one or more of a low density portion 3286, a medium density portion 3287, and a high density portion 3288.
The low density portion 3286 may be a composite or another material, such as a portion of the composite sole panel 3230 or as another component. The low density portion 3286 has a density of less than about 2 g/cc, such as between about 1 g/cc and about 2 g/cc. The medium density portion 3287 may be an aluminum alloy, a titanium alloy, another alloy, another material, or a combination of multiple alloys or materials, such as a portion of the hollow body 3210 or as another component. The medium density portion 3287 has a density greater than about 2.7 g/cc, such as between about 1 g/cc and about 5 g/cc, between about 2.0 g/cc and about 5.0 g/cc, and between about 2.5 g/cc and about 4.5 g/cc. The high density portion 3288 may be a steel alloy, a tungsten alloy, another alloy, another material, or a combination of multiple alloys or materials, such as a rear weight affixed to the inertia generator 3285 or as another component. The high density portion 3288 has a density greater than about 7 g/cc. For example, an aluminum alloy is often about 2.7 g/cc, a titanium alloy is often about 4.5 g/cc, a steel alloy is often about 7.8 g/cc, and tungsten alloy a tungsten alloy is often about 19 g/cc.
In some embodiments, the golf club head 3200 includes support ribs 3296, 3297. For example, support ribs 3296 provide for additional support for the hollow body 3210, the weight track 3245 and/or slot 3295. The support ribs 3296 may be provided over the weight track 3245 and in other areas within the hollow body 3210. Support rib 3297 may be provided to support supports the hollow body 3210 and inertia generator 3285. As depicted in
In some embodiments, the golf club head 3200 includes a mass pad 3290 in the heel portion of the golf club head. Mass pad 3290 positions discretionary mass of the golf club head 3200 heelward, and may lower the CG and move CG forward to modify the CG projection onto the face. In some embodiments, a removable and/or adjustable weight may be provided in the heel portion in lieu of or in addition to the mass pad 3290.
The skirt height of golf club 3200 may also improve aerodynamic features of the golf club head. Golf club head 3200 has a skirt height S1, which may measure the lowest point above the ground plane at which the skirt meets the crown. Golf club head 4100 has a skirt height S2. In some embodiments, the skirt height S1 is at least 20 mm, and in some embodiments may be between about 25 mm and about 40 mm, such as between 30 mm and 40 mm, or between 30 mm and 35 mm. Increasing the skirt height S1 of golf club head 3200 likewise improves the aerodynamic properties of the golf club head. The golf club body has a total body height from defined from a bottom most portion of the golf club body, or the ground plane, to a top-most portion of the crown, or the peak crown height, such as vertically or along a z-axis. In some embodiments, the total body height is no less than 48 mm, no less than 42 mm, or no less than 53 mm. The golf club body also has a body length defined from a leading edge of the golf club body, or the leading-edge location, to a rearward most portion of golf club head, or the rearward most portion of the skirt, such as horizontally or along a y-axis. In some embodiments, the body length is no less than 98 mm, no less than 93 mm, or no less than 103 mm.
In some embodiments, the face insert 2110 can be machined from a composite plaque. In an example, the composite plaque can be substantially rectangular with a length between about 90 mm and about 130 mm or between about 100 mm and about 120 mm, preferably about 110 mm±1.0 mm, and a width between about 50 mm and about 90 mm or between about 6 mm and about 80 mm, preferably about 70 mm±1.0 mm plaque size and dimensions. The face insert 2110 is then machined from the plaque to create a desired face profile. For example, the face profile length 4212 can be between about 80 mm and about 120 mm or between about 90 mm and about 110 mm, preferably about 102 mm. The face profile width 4211 can be between about 40 mm and about 65 mm or between about 45 mm and about 60 mm, preferably about 53 mm. The ideal striking location width 4213 can be between about 25 mm and about 50 mm or between about 30 mm and about 40 mm, preferably about 34 mm. The ideal striking location length 4214 can be between about 40 mm and about 70 mm or between about 45 mm and about 65 mm, preferably about 55.5 mm. Alternatively, the face insert 2110 can be molded to provide the desired face dimensions and profile.
In embodiments where the face insert 2110 is machined from a composite plaque, the face insert 2110 can be machined in one or more operations, such as computer numerical control (CNC) or other operations. For example, starting with the composite plaque, a notch 4220 can be first machined from the plaque. Next, a perimeter chamfer can be machined around the perimeter of the face insert 2110. Finally, a face profile can be machined from the plaque. In some embodiments, each of the notch 4220, perimeter chamfer, and face profile can be machined in a single operation, such as a single CNC operation without removing the plaque from the CNC fixture. In other embodiments, multiple operations can be performed, such as machining one or more of the notch 4220, perimeter chamfer, or face profile being machined separately from the other features of the face. Other orders of machining features can be provided, such as machining the notch after the face profile and chamfer, as well as machining additional features into the face insert 2110, such as bond gap bumps and other features.
Additional features can be machined or molded into face the insert 2110 to create the desired face profile. 2For example, a notch 4220 can be machined or molded into the backside of a heel portion of the face insert 110. For example, the notch 4220 in the back of the face insert 2110 allows for the golf club head 2500 to utilize flight control technology (FCT) in the hosel 2150. The notch 4220 can be configured to accept at least a portion of the hosel within the face insert 2110. Alternatively or additionally, the notch 4220 can be configured to accept at least a portion of the club head body within the face insert 2110.
In some embodiments, the notch 4220, or another relief portion, defines a transition region on the face insert. For example, the notch 4220 or relief portion is proximate to a heel portion of the face and can have an area of at least about 50 mm2 and no more than about 300 mm2, preferably less than about 200 mm2, more preferably between about 75 mm2 and about 150 mm2. Preferably, the notch area is about 1.5% to about 6% of the external area of the face insert (e.g., the outward facing portion of the face configured for striking the golf ball), more preferably the notch area is about 2% to about 3% of the external face insert.
The notch may allow for the reduction of CFY by accommodating at least a portion of the hosel and/or at least a portion of the club body within the face insert, allowing the ideal striking location of the face insert to be closer to a plane passing through a center point location of the hosel. The face insert 2110 can be configured to provide a CFY no more than about 18 mm and no less than about 9 mm, preferably between about 11.0 mm and about 16.0 mm, and more preferably no more than about 15.5 mm and no less than about 11.5 mm. The face insert 2110 can be configured to provide face progression no more than about 21 mm and no less than about 12 mm, preferably no more than about 19.5 mm and no less than about 13 mm and more preferably no more than about 18 mm and no less than about 14.5 mm. In some embodiments, a difference between CFY and face progression is at least 2 mm and no more than 12 mm, preferably between at least 3 mm and 8 mm. In other embodiments, a difference between CFY and face progression is at least 2 mm and no more than 4 mm.
In another example, backside bumps 4230A, 4230B, 4230C, 4230D may be machined or molded into the backside of the face insert. The backside bumps 4230A, 4230B, 4230C, 4230D can be configured to provide for a bond gap. A bond gap is an empty space between the club head body and the face insert that is filled with adhesive during manufacturing. The backside bumps 4230A, 4230B, 4230C, 4230D protrude to separate the face from the club head body when bonding the face insert to the club head body during manufacturing. In some instances, too large or too small of a bond gap may lead to durability issues of the club head, the face insert, or both. Further, too large of a bond gap can allow too much adhesive to be used during manufacturing, adding unwanted additional mass to the club head. The backside bumps 4230A, 4230B, 4230C, 4230D can protrude between about 0.1 mm and 0.5 mm, preferably about 0.25 mm. In some embodiments, the backside bumps are configured to provide for a minimum bond gap, such as a minimum bond gap of about 0.25 mm and a maximum bond gap of about 0.45 mm.
Further, one or more of the edges of the face insert 2110 can be machined or molded with a chamfer. In an example, the face insert 2110 includes a chamfer substantially around the inside perimeter edge of the face insert, such as a chamfer between about 0.5 mm and about 1.1 mm, preferably 0.8 mm. In some embodiments, the perimeter chamfer is provided to avoid the face insert 2110 bottoming out on an internal radius of the recessed face opening of the golf club head configured to receive the face insert 2110. By providing the perimeter chamfer, the face insert 2110 can fit properly within recessed face opening despite manufacturing variances and other characteristics of the golf club head created during the casting process.
In some embodiments, the face insert 2110 is manufactured from multiple layers of composite materials. Exemplary composite materials and methods for making the same are described in U.S. patent application Ser. No. 13/452,370 (published as U.S. Pat. App. Pub. No. 2012/0199282), which is incorporated by reference. In some embodiments, an inner and outer surface of the composite face can include a scrim layer, such as to reinforce the face insert 2110 with glass fibers making up a scrim weave. Multiple quasi-isotropic panels (Q's) can also be included, with each Q panel using multiple plies of unidirectional composite panels offset from each other. In an exemplary four-ply Q panel, the unidirectional composite panels are oriented at 90°, −45°, 0°, and 45°, which provide for structural stability in each direction. Clusters of unidirectional strips (C's) can also be included, with each C using multiple unidirectional composite strips. In an exemplary four-strip C, four 27 mm strips are oriented at 0°, 125°, 90°, and 55°. C's can be provided to increase thickness of the face insert 2110 in a localized area, such as in the center face at the ideal striking location. Some Q's and C's can have additional or fewer plies (e.g., three-ply rather than four-ply), such as to fine tune the thickness, mass, localized thickness, and provide for other properties of the face insert 2110, such as to increase or decrease COR of the face insert 2110.
Additional composite materials and methods for making the same are described in U.S. Pat. Nos. 8,163,119 and 10,046,212, which is incorporated by reference. For example, the usual number of layers for a striking plate is substantial, e.g., fifty or more. However, improvements have been made in the art such that the layers may be decreased to between 30 and 50 layers.
The tables below provide examples of possible layups. These layups show possible unidirectional plies unless noted as woven plies. The construction shown is for a quasi-isotropic layup. A single layer ply has a thickness of ranging from about 0.065 mm to about 0.080 mm for a standard FAW of 70 gsm with about 36% to about 40% resin content. The thickness of each individual ply may be altered by adjusting either the FAW or the resin content, and therefore the thickness of the entire layup may be altered by adjusting these parameters.
In addition to the unidirectional composite panels oriented at 90°, −45°, 0°, and 45°, additional Q panels can be provided according to table 1.
The Area Weight (AW) is calculated by multiplying the density times the thickness. For the plies shown above made from composite material the density is about 1.5 g/cm3 and for titanium the density is about 4.5 g/cm3.
In an example, a first face insert can have a peak thickness of 4.1 mm and an edge thickness of 3.65 mm, including 12 Q's and 2 C's, resulting in a mass of 24.7 g. In another example, a second face insert can have a peak thickness of 4.25 mm and an edge thickness of 3.8 mm, including 12 Q's and 2 C's, resulting in a mass of 25.6 g. The additional thickness and mass is provided by including additional plies in one or more of the Q's or C's, such as by using two 4-ply Q's instead of two 3-ply Q's. In yet another example, a third face insert can have a peak thickness of 4.5 mm and an edge thickness of 3.9 mm, including 12 Q's and 3 C's, resulting in a mass of 26.2 g. Additional and different combinations of Q's and C's can be provided for a face insert 2110 with a mass between about 20 g and about 30 g, or between about 15 g and about 35 g.
In some embodiments, a method of assembling a golf club is provided. For example, the method includes providing a golf club head having a face opening with an internal hosel surface intruding into the face opening (e.g., forming a portion of the face opening). The golf club head can also include at least one of a crown opening and/or a sole opening. The method also includes attaching a composite face insert to the golf club body, where the face insert is machined from a composite plaque with a larger area than the finished face insert. For example, the composite face insert includes a machined perimeter chamfer and a machined in notch. The method further includes enclosing the face opening with the face insert, such as by attaching the face insert to the club head. In some embodiments, the internal hosel surface is received by the notch in the face insert. The method also includes enclosing one or more of the crown opening and/or sole opening with a crown insert and/or a sole insert. The method may further include attaching a golf club shaft having a shaft sleeve, and tightening a screw to attach the golf club shaft to the golf club head to form a golf club assembly. In some examples, the golf club head has a face progression less between 10 and 20 mm and a CFY between 9 and 18 mm, preferably less than 16 mm.
In some embodiments, the x-axis of the golf club head is tangential to the face and parallel to a ground plane, negative locations on the x-axis extend from the center face to the toe portion, and positive locations on the x-axis extend from the center face to the heel portion. In these embodiments, a center of gravity of the golf club body with respect to the x-axis (CGx) can be oriented from about 0 mm to about −10 mm.
In some embodiments, a method of counteracting a lateral dispersion tendency of a golf club head is provided. For example, the golf club head can have a face, a crown and a sole together defining an interior cavity, a body of the golf club head including a heel and a toe portion and having x, y and z axes which are orthogonal to each other and have their origin at the USGA center face (e.g., the z, y, and z origin axes as defined herein). The method can include providing a primary alignment feature comprising a line delineating a transition between at least a first portion of the crown having an area of contrasting shade or color with a shade or color of the face. The primary alignment feature can be hard tooled into the golf club head with the face of the golf club body, and the golf club head can have a first Sight Adjusted Perceived Face Angle (SAPFA) with respect to the primary alignment feature. The method also includes measuring the lateral dispersion tendency of the golf club head. The lateral dispersion tendency indicates an average dispersion from a center target line, where a positive lateral dispersion tendency is the average dispersion right of the center target line and a negative lateral dispersion tendency is the average dispersion left of the center target line. The method further includes adjusting the primary alignment feature to provide an adjusted primary alignment feature to counteract the lateral dispersion tendency of the golf club head and incorporating the adjusted primary alignment feature into the golf club head. The adjusted primary alignment feature can have a second Sight Adjusted Perceived Face Angle (SAPFA) of from about −2 to about 10 degrees and a second Radius of Curvature (circle fit) of from about 300 to about 1000 mm.
In some embodiments, the method can also include incorporating the adjusted primary alignment feature into the golf club head comprises retooling the golf club head. In some embodiments, adjusting the primary alignment feature counteracts the lateral dispersion tendency of the golf club head by providing for a positive lateral dispersion tendency for the golf club head. In some embodiments, adjusting the primary alignment feature counteracts the lateral dispersion tendency of the golf club head by providing for a negative lateral dispersion tendency for the golf club head. In some embodiments, adjusting the primary alignment feature counteracts the lateral dispersion tendency of the golf club head by reducing average dispersion from the center target line. In some embodiments, the primary alignment feature is hard tooled into the golf club head by bonding the face to the golf club body. In some embodiments, the golf club body is painted prior to bonding the face to the golf club body. In some embodiments, the adjusted primary alignment feature includes: a second Sight Adjusted Perceived Face Angle 25 mm Heelward (SAPFA25H) of from about −5 to about 2 degrees; a second Sight Adjusted Perceived Face Angle 25 mm Toeward (SAPFA25T) of from 0 to about 9 degrees; and a second Sight Adjusted Perceived Face Angle 50 mm Toeward (SAPFA50T) of from about 2 to about 9 degrees.
Composite face plate features are described in more detail in U.S. patent application Ser. Nos. 11/998,435, 11/642,310, 11/825,138, 11/823,638, 12/004,386, 12/004,387, 11/960,609, 11/960,610 and U.S. Pat. No. 7,267,620, which are herein incorporated by reference in their entirety.
The construction of the front opening 5040 of the cast cup 5010 and the face insert 5020, and how they are coupled together, can be similar to that described with regard to the embodiments described above with reference to
The rear ring 5012 can be molded using polymeric materials, composite materials, reinforcing fibers, metallic materials, coatings, or combinations of these materials. The rear ring 5012 can be injection molded, for example. Fibers or other reinforcing materials can be added to the primarily polymeric material prior to molding, and external coatings can be added after molding. The molded rear ring can have sufficient rigidity and strength to resist substantial deformation or fracturing when in use, while providing a light-weight and highly shapable and customizable structure. For example, the rear ring can comprise a carbon or glass fiber reinforced polymeric material, which can have a density between 1 g/cc and 2 g/cc. The rear ring can be made with any external colors, textures, or patterns. The molded rear ring 5012 can be coupled to the cast cup 5010 via any suitable means, such as mechanical interlocking, adhesive bonding, RF welding, and/or other manners disclosed elsewhere herein. Molding the rear ring allows for the rear weight 5028 to be co-molded with the rear ring, such that the rear weight is fully or partially enclosed within the molding material of the rear ring. As shown in
Using the cross-sectional side view of the club head 5000 in
In some instances, a ratio of the skirt height to the peak crown height ranges between about 0.45 to 0.59, preferably 0.49-0.55, and in one embodiment the skirt height is about 34 mm and the peak crown height is about 65 mm, resulting in a ratio of skirt height to peak crown height of about 0.52. A skirt height typically ranges between 28 mm and 38 mm, preferably between 31 mm and 36 mm. In some instances, the skirt height can be greater than Z-up as measured along a z-axis relative to the ground plane. Additionally, in some instances, the peak skirt height can be greater than a distance to the geometric center of the strike face as measured along a z-axis relative to the ground plane. A peak crown height typically ranges between 60 mm and 70 mm, preferably between 62 mm and 67 mm. It can be desirable to limit a difference between the peak crown height and the skirt height to no more than 40 mm, preferably between 27 mm and 35 mm. It can be desirable for the skirt height to be the same as or greater than a Z-up value for the golf club head (defined as the vertical distance along a z-axis from the ground plane to the center of gravity). It can be desirable for the peak crown height to be at least two times (2×) larger than the Z-up value for the golf club head. A greater skirt height can help with better aerodynamics and better air flow attachment, especially for faster swing speeds. Likewise, if the difference between the peak crown height and skirt height is too great there can be a greater likelihood of the flow separating early from the golf club head (i.e., increased likelihood of turbulent flow). The ratios just described are applicable to all the embodiments disclosed herein, especially those shown in
The construction and material diversity of the golf club heads described herein enables a desirable center-of-gravity (CG) location and peak crown height location (PCH location). In one example, a y-axis coordinate, on the y-axis of the club head origin coordinate system, of the PCH location is between about 26 mm and about 42 mm. In the same or a different example, a distance parallel to the z-axis of the club head origin coordinate system, from the ground plane 181, when the golf club head 100 is in the normal address position, of the PCH location ranges between 60 mm and 70 mm, preferably between 62 mm and 67 mm as described above. According to some examples, a y-axis coordinate, on the y-axis of the head origin coordinate system 185, of the center-of-gravity (CG) of the golf club head 100 ranges between 30 mm and 50 mm, preferably between 32 mm and 38 mm, more preferably between 36.5 mm and 42 mm, an x-axis coordinate, on the x-axis of the head origin coordinate system 185, of the center-of-gravity (CG) of the golf club head 100 ranges between −10 mm and 10 mm, preferably between −6 mm and 6 mm, and a z-axis coordinate, on the z-axis of the head origin coordinate system 185, of the center-of-gravity (CG) of the golf club head 100 ranges between −10 mm and 2 mm, preferably between −7 mm and −2 mm.
The weight track 6060 can be positioned in the sole of the cast cup 6010 just rearward of the sole channel 6024, as shown in
Generally, the weight track 6060 and weight assembly 6050 can be similar to the weight tracks 214, 216 and two-piece slidable weight assemblies 210, 212 described elsewhere herein. As shown in
The weight assembly can comprise two pieces, an inner piece and an outer piece, that are threadably coupled together, such that rotating the inner piece (e.g., using an wrench) relative to the outer piece moves the two pieces closer together to clamp them onto the ledge(s) of the weight track or moves the two pieces apart to loosen the weight assembly. The inner piece can have a rounded shape to allow it to rotate freely within the track, while the outer piece can have a polygonal (or otherwise non-circular) shape that fits between the walls of the track and doesn't allow the outer piece to rotate within the track. Thus, the outer piece is held stationary while the user rotates the inner piece to tighten or loosen the assembly in the track.
As shown in
Club heads having a weight track and sliding weight assembly as in the club head 6000 can have any type of rear ring and rear weight, such as any of the rear ring and rear weight combinations disclosed elsewhere herein. In the illustrated example, the club head 6000 comprises an externally attachable rear weight 6028 that is coupled to the rear ring 6012 with an external screw 6029 (see
The rear ring 6012 can comprise metallic materials (e.g., Ti alloy, steel, aluminum, etc.), polymeric materials, composite materials, and/or any other materials and coatings disclosed herein, and any method of formation and attachment disclosed herein. The face insert 6020 can comprise any materials (e.g., metallic or composite materials), have any geometry, and have any method of formation and attachment disclosed herein. The face insert 6020 can also comprise an external coating layer 6021 on the front striking surface, which can comprise polyurethane or other materials disclosed herein.
A. A wood-type golf club head comprising:
B. The club head of embodiment A, wherein the heel engagement portion of the rear ring is also adhesively bonded or welded to the heel portion of the cast cup and the toe engagement portion of the rear ring is also adhesively bonded or welded to the toe portion of the cast cup.
C. The club head of embodiment A, wherein the heel engagement portion and the toe engagement portions of the rear ring are squeezed toward each other to engage the rear ring with the cast cup.
D. The club head of embodiment A, wherein the heel engagement portion and the toe engagement portions of the rear ring include projections or notches that mechanically interlock with corresponding features on the heel and toe portions of the cast cup.
E. The club head of embodiment A, wherein the heel end of the rear ring is lower than the toe end of the rear ring along a vertical z-axis.
F. The club head of embodiment A, wherein the rear ring comprises an arcuate elongated member forming a generally U-shape between the toe end of the rear ring and the heel end of the rear ring, the arcuate elongated member defines a curved longitudinal axis extending along the arcuate elongated member between the toe end of the rear ring and the heel end of the rear ring, and the arcuate elongated member is twisted about the longitudinal axis.
G. A wood-type golf club head comprising:
H. The club head of embodiment G, wherein the first weight is positioned at a heel side of the cast cup adjacent the hosel.
I. The club head of embodiment G, wherein the first weight is detachable from the forward portion of the sole.
J. The club head of embodiment G, wherein the second weight is co-molded with the rear ring and at least partially surrounded by the rear ring.
K. The club head of embodiment G, wherein the forward portion of the sole comprises a weight track that extends in a heal-toe direction, and the first weight is positioned in the weight track and is adjustably positionable in a heal-toe direction along the weight track.
For purposes of this description, certain aspects, advantages, and novel features of the embodiments of this disclosure are described herein. The described methods, systems, and apparatus should not be construed as limiting in any way. Instead, the present disclosure is directed toward all novel and non-obvious features and aspects of the various disclosed embodiments, alone and in various combinations and sub-combinations with one another. The disclosed methods, systems, and apparatus are not limited to any specific aspect, feature, or combination thereof, nor do the disclosed methods, systems, and apparatus require that any one or more specific advantages be present, or problems be solved.
Features, properties, characteristics, materials, values, ranges, or groups described in conjunction with a particular aspect, embodiment or example of the disclosure are to be understood to be applicable to any other aspect, embodiment or example described herein unless incompatible therewith. All of the features disclosed in this specification (including any accompanying claims, abstract, and drawings), and/or all of the steps of any method or process so disclosed, may be combined in any combination, except combinations where at least some of such features and/or steps are mutually exclusive. The disclosure is not restricted to the details of any foregoing embodiments. The disclosure extends to any novel one, or any novel combination, of the features disclosed in this specification (including any accompanying claims, abstract, and drawings), or to any novel one, or any novel combination, of the steps of any method or process so disclosed.
Although the operations of some of the disclosed methods are described in a particular, sequential order for convenient presentation, this manner of description encompasses rearrangement, unless a particular ordering is required by specific language set forth below. For example, operations described sequentially may in some cases be rearranged or performed concurrently. Moreover, for the sake of simplicity, the attached figures may not show the various ways in which the disclosed methods, systems, and apparatus can be used in conjunction with other systems, methods, and apparatus.
As used herein, the terms “a,” “an,” and “at least one” encompass one or more of the specified element. That is, if two of a particular element are present, one of these elements is also present and thus “an” element is present. The terms “a plurality of” and “plural” mean two or more of the specified element. As used herein, the term “and/or” used between the last two of a list of elements means any one or more of the listed elements. For example, the phrase “A, B, and/or C” means “A,” “B,” “C,” “A and B,” “A and C,” “B and C,” or “A, B, and C.” As used herein, the term “coupled” generally means physically coupled or linked and does not exclude the presence of intermediate elements between the coupled items absent specific contrary language.
Directions and other relative references (e.g., inner, outer, upper, lower, etc.) may be used to facilitate discussion of the drawings and principles herein, but are not intended to be limiting. For example, certain terms may be used such as “inside,” “outside,”, “top,” “down,” “interior,” “exterior,” and the like. Such terms are used, where applicable, to provide some clarity of description when dealing with relative relationships, particularly with respect to the illustrated embodiments. Such terms are not, however, intended to imply absolute relationships, positions, and/or orientations. For example, with respect to an object, an “upper” part can become a “lower” part simply by turning the object over. Nevertheless, it is still the same part and the object remains the same. As used herein, “and/or” means “and” or “or,” as well as “and” and “or.”
In view of the many possible embodiments to which the principles of the disclosure may be applied, it should be recognized that the illustrated embodiments are only preferred examples and should not be taken as limiting the scope of the disclosure. Various modifications may be made thereto without departing from the broader spirit and scope of the disclosure as set forth. The specification and drawings are, accordingly, to be regarded in an illustrative sense rather than a restrictive sense. Accordingly, the scope of the disclosure is at least as broad as the following claims. We therefore claim all that comes within the scope of these claims and their equivalents.
This application is a continuation of U.S. patent application Ser. No. 17/132,645 filed Dec. 23, 2020, which is a continuation-in-part of U.S. patent application Ser. No. 16/161,337 filed Oct. 16, 2018, now U.S. Pat. No. 10,874,915, which is a continuation-in-part of U.S. patent application Ser. No. 16/059,801 filed Aug. 9, 2018, now U.S. Pat. No. 10,780,327, which claims the benefit of U.S. Provisional Patent Application No. 62/543,778, filed Aug. 10, 2017, all of which are incorporated by reference herein in their entirety. This application also claims priority, through U.S. patent application Ser. No. 17/132,645, to U.S. Provisional Patent Application No. 62/955,727 filed Dec. 31, 2019, which is incorporated by reference herein in its entirety.
| Number | Date | Country | |
|---|---|---|---|
| 62543778 | Aug 2017 | US | |
| 62955727 | Dec 2019 | US |
| Number | Date | Country | |
|---|---|---|---|
| Parent | 17132645 | Dec 2020 | US |
| Child | 18202040 | US |
| Number | Date | Country | |
|---|---|---|---|
| Parent | 16161337 | Oct 2018 | US |
| Child | 17132645 | US | |
| Parent | 16059801 | Aug 2018 | US |
| Child | 16161337 | US |
