This present technology generally relates to systems, devices, and methods related to golf clubs, and more specifically to new and improved metalwood golf clubs having a stiffening member.
The complexities of golf club design are well known. The specifications for each component of the club (i.e., the club head, shaft, grip, and subcomponents thereof) directly impact the performance of the club. Thus, by varying the design specifications, a golf club can be tailored to have specific performance characteristics.
The design of club heads has long been studied. Among the more prominent considerations in club head design are loft, lie, face angle, horizontal face bulge, vertical face roll, center of gravity (CG), inertia, material selection, and overall head weight. While this basic set of criteria is generally the focus of golf club engineering, several other design aspects must also be addressed. The interior design of the club head may be tailored to achieve particular characteristics, such as the inclusion of hosel or shaft attachment means, perimeter weights on the club head, and fillers within hollow club heads.
Golf club heads must also be strong to withstand the repeated impacts that occur during collisions between the golf club and the golf ball. The loading that occurs during this transient event can create a peak force of over 2,000 lbs. Thus, a major challenge is designing the club face and body to resist permanent deformation or failure by material yield or fracture.
Players generally seek a metal wood driver and golf ball combination that delivers maximum distance and landing accuracy. The distance a ball travels after impact is dictated by the magnitude and direction of the ball's translational velocity and the ball's rotational velocity or spin. Environmental conditions, including atmospheric pressure, humidity, temperature, and wind speed, further influence the ball's flight. However, these environmental effects are beyond the control of the golf equipment manufacturer. Golf ball landing accuracy is driven by a number of factors as well. Some of these factors are attributed to club head design, such as center of gravity and club face flexibility.
Technological breakthroughs in recent years provide the average golfer with more distance, such as making larger head clubs while keeping the weight constant or even lighter, by casting consistently thinner shell thickness and going to lighter materials such as titanium or composites.
However, despite the potential gains in the discretionary mass gained by the utilization of thinner constructions and lightweight materials, they usually comes with some drawbacks. More specifically, they may generally come with an undesirable acoustic characteristic at impact, making the golf club undesirable to a golfer irrespective of performance. U.S. Pat. No. 6,612,938 to Murphy et al. illustrates one of the earlier attempts to use exotic materials in a golf club head such as plies of pre-preg material. One method of improving the acoustic signature of the golf club head is to stiffen the club head using stiffening members, such as those disclosed in U.S. Pat. No. 9,498,688 to Galvan et al. U.S. Pat. No. 8,651,975 to Soracco provided another example of an attempt to address the acoustic characteristics associated with golf clubs that utilizes exotic material. More specifically, Soracco provided a golf club head with sound tuning composite members forming at least a portion of the surface of the golf club head. Finally, U.S. Pat. No. 8,849,635 to Hayase et al. went above and beyond the mere basic design of a golf club head for acoustic characteristics and even made an attempt to predict modal damping ratio of composite golf club heads.
Despite the above, none of the references provide a method to improve the performance of a golf club head by providing a way to improve the performance of a golf club head utilizing advanced materials all while providing a clean way to address the degradation of the acoustic characteristics of the golf club head. Hence, it can be seen from the above that a golf club design that is capable of achieving both of the goal of incorporating lightweight constructions in order to increase discretionary mass as well as achieving a desirable acoustic characteristic while minimizing the undesirable sound and feel of the golf club head. The present invention provides novel solutions for improving the stiffness and acoustic characteristics of a golf club head at impact.
The systems, methods, and devices described herein have innovative aspects, no single one of which is indispensable or solely responsible for their desirable attributes. Without limiting the scope of the claims, some of the advantageous features will now be summarized.
The present invention relates to a golf club head including a stiffening member that alters the compliance characteristics as compared to known golf club heads.
One non-limiting embodiment of the present technology includes a golf club head, including a metallic body including a striking face, an aft portion extending aft from the striking face; the aft portion including: a sole defining a lower surface of the golf club head and extending aft from the striking face; a crown defining an upper surface of the golf club head and extending aft from the striking face; a skirt extending between the sole and the crown; a hosel extending from the crown; an interior cavity defined by the striking face, the sole, the crown, and the skirt; a composite panel affixed to the metallic body, the composite panel having a substantially constant thickness; and a composite stiffening member affixed to the composite panel, the composite stiffening member extending into the interior cavity; wherein the composite stiffening member comprises a composite stiffening member length measured along the major axis of the composite stiffening member, a composite stiffening member height measured perpendicularly to the composite stiffening member length and extending into the interior cavity, and a composite stiffening member width measured perpendicularly to the composite stiffening member length and the composite stiffening member height, wherein the composite stiffening member height is at least twice the composite stiffening member width and wherein the composite stiffening member length is at least five times the composite stiffening member height; wherein the composite panel comprises a thermoplastic composite.
In an additional non-limiting embodiment of the present technology the composite stiffening member comprises continuous carbon fibers running along its entire length.
In an additional non-limiting embodiment of the present technology the composite stiffening member is affixed to the metallic body.
In an additional non-limiting embodiment of the present technology the length of the composite stiffening member extends beyond the composite panel and the composite stiffening member is affixed to the metallic body at both a first end of the composite stiffening member and a second end of the composite stiffening member.
In an additional non-limiting embodiment of the present technology the metallic body comprises a shelf configured to receive the composite panel, and wherein the shelf comprises a shelf aperture, wherein the composite stiffening member resides within the shelf aperture.
In an additional non-limiting embodiment of the present technology the composite stiffening member is affixed to the metallic body.
An additional non-limiting embodiment of the present technology includes a method of constructing a golf club head, including: forming a substantially constant thickness composite body panel out of thermoplastic carbon composite; forming a composite stiffening member including a composite stiffening member length measured along the major axis of the composite stiffening member, a composite stiffening member height measured perpendicularly to the composite stiffening member length, and a composite stiffening member width measured perpendicularly to the composite stiffening member length and the composite stiffening member height, wherein the composite stiffening member height is at least twice the composite stiffening member width and wherein the composite stiffening member length is at least five times the composite stiffening member height; affixing the composite stiffening member to the composite body panel; affixing the composite body panel to a metallic body; wherein the metallic body comprises: a striking face, an aft portion extending aft from the striking face; the aft portion including: a sole defining a lower surface of the golf club head and extending aft from the striking face; a crown defining an upper surface of the golf club head and extending aft from the striking face; a skirt extending between the sole and the crown; a hosel extending from the crown; and an interior cavity defined by the striking face, the sole, the crown, and the skirt.
An additional non-limiting embodiment of the present technology includes affixing the composite stiffening member to the metallic body.
In an additional non-limiting embodiment of the present technology the metallic body comprises a shelf configure to receive the composite body panel, wherein the shelf comprises a shelf aperture configured to receive the composite stiffening member, and wherein the method of constructing a golf club head further comprises installing the composite stiffening member into the shelf aperture.
In an additional non-limiting embodiment of the present technology the composite stiffening member extends beyond the composite panel and the composite stiffening member is affixed to the metallic body at both a first end of the composite stiffening member and a second end of the composite stiffening member
In an additional non-limiting embodiment of the present technology affixing the composite stiffening member to the composite body panel comprises diffusion bonding process the composite stiffening member to the composite body panel.
In an additional non-limiting embodiment of the present technology affixing the composite stiffening member to the composite body panel comprises a compression thermoforming process.
In an additional non-limiting embodiment of the present technology forming a composite stiffening member comprises laying continuous carbon fibers along the length of the composite stiffening member.
In an additional non-limiting embodiment of the present technology the composite body panel covers an aperture formed in the sole of the metallic body.
An additional non-limiting embodiment of the present technology includes a method of constructing a golf club head, including: forming a substantially constant thickness composite body panel; forming a composite stiffening member including a composite stiffening member length measured along the major axis of the composite stiffening member, a composite stiffening member height measured perpendicularly to the composite stiffening member length, and a composite stiffening member width measured perpendicularly to the composite stiffening member length and the composite stiffening member height, wherein the composite stiffening member height is at least twice the composite stiffening member width and wherein the composite stiffening member length is at least five times the composite stiffening member height; affixing the composite stiffening member to the composite body panel; affixing the composite body panel to a metallic body; wherein the metallic body comprises: a striking face, an aft portion extending aft from the striking face; the aft portion including: a sole defining a lower surface of the golf club head and extending aft from the striking face; a crown defining an upper surface of the golf club head and extending aft from the striking face; a skirt extending between the sole and the crown; a hosel extending from the crown; an interior cavity defined by the striking face, the sole, the crown, and the skirt; and a shelf configure to receive the composite body panel, wherein the shelf comprises a shelf aperture configured to receive the composite stiffening member; installing and affixing the composite stiffening member into the shelf aperture.
In an additional non-limiting embodiment of the present technology the composite body panel comprises a thermoplastic carbon composite
In an additional non-limiting embodiment of the present technology affixing the composite stiffening member to the composite body panel comprises a diffusion bonding process.
In an additional non-limiting embodiment of the present technology affixing the composite stiffening member to the composite body panel comprises a compression thermoforming process.
In an additional non-limiting embodiment of the present technology forming a composite stiffening member comprises laying continuous carbon fibers along the length of the composite stiffening member.
In an additional non-limiting embodiment of the present technology wherein the composite body panel covers an aperture formed in the sole of the metallic body.
This summary is provided to introduce a selection of concepts in a simplified form that are further described below in the Detailed Description. This summary is not intended to identify key features or essential features of the claimed subject matter, nor is it intended to be used to limit the scope of the claimed subject matter.
The accompanying drawings form a part of the specification and are to be read in conjunction therewith. The illustrated embodiments, however, are merely examples and are not intended to be limiting. Like reference numbers and designations in the various drawings indicate like elements.
In the following detailed description, reference is made to the accompanying drawings, which form a part of the present disclosure. The illustrative embodiments described in the detailed description, drawings, and claims are not meant to be limiting. Other embodiments may be utilized, and other changes may be made, without departing from the spirit or scope of the subject matter presented herein. It will be readily understood that the aspects of the present disclosure, as generally described herein, and illustrated in the Figures, can be arranged, substituted, combined, and designed in a wide variety of different configurations, all of which are explicitly contemplated and form part of this disclosure. For example, a system or device may be implemented or a method may be practiced using any number of the aspects set forth herein. In addition, such a system or device may be implemented or such a method may be practiced using other structure, functionality, or structure and functionality in addition to or other than one or more of the aspects set forth herein. Alterations and further modifications of inventive features illustrated herein, and additional applications of the principles of the inventions as illustrated herein, which would occur to one skilled in the relevant art and having possession of this disclosure, are to be considered within the scope of the invention.
Other than in the operating examples, or unless otherwise expressly specified, all of the numerical ranges, amounts, values and percentages such as those for amounts of materials, moments of inertias, center of gravity locations, loft and draft angles, and others in the following portion of the specification may be read as if prefaced by the word “about” even though the term “about” may not expressly appear with the value, amount, or range. Accordingly, unless indicated to the contrary, the numerical parameters set forth in the following specification and attached claims are approximations that may vary depending upon the desired properties sought to be obtained by the present invention. At the very least, and not as an attempt to limit the application of the doctrine of equivalents to the scope of the claims, each numerical parameter should at least be construed in light of the number of reported significant digits and by applying ordinary rounding techniques.
Notwithstanding that the numerical ranges and parameters setting forth the broad scope of the invention are approximations, the numerical values set forth in the specific examples are reported as precisely as possible. Any numerical value, however, inherently contains certain errors necessarily resulting from the standard deviation found in their respective testing measurements. Furthermore, when numerical ranges of varying scope are set forth herein, it is contemplated that any combination of these values inclusive of the recited values may be used.
In describing the present technology, the following terminology may have been used: The singular forms “a,” “an,” and “the” include plural referents unless the context clearly dictates otherwise. Thus, for example, reference to an item includes reference to one or more items. The term “plurality” refers to two or more of an item. The term “substantially” means that the recited characteristic, parameter, or value need not be achieved exactly, but that deviations or variations, including for example, tolerances, measurement error, measurement accuracy limitations and other factors known to those of skill in the art, may occur in amounts that do not preclude the effect the characteristic was intended to provide. A plurality of items may be presented in a common list for convenience. However, these lists should be construed as though each member of the list is individually identified as a separate and unique member. Thus, no individual member of such list should be construed as a de facto equivalent of any other member of the same lists solely based on their presentation in a common group without indications to the contrary. Furthermore, where the terms “and” and “or” are used in conjunction with a list of items, they are to be interpreted broadly, in that any one or more of the listed items may be used alone or in combination with other listed items. The term “alternatively” refers to a selection of one of two or more alternatives, and is not intended to limit the selection of only those listed alternative or to only one of the listed alternatives at a time, unless the context clearly indicated otherwise.
Features of the present disclosure will become more fully apparent from the following description and appended claims, taken in conjunction with the accompanying drawings. After considering this discussion, and particularly after reading the section entitled “Detailed Description” one will understand how the illustrated features serve to explain certain principles of the present disclosure.
The stiffening member 200 can be installed into the interior 120 in a variety of ways. In one embodiment, the golf club head 100 might have composite portions such as the crown which are affixed to the golf club head 100 after installation of the stiffening member 200, allowing the stiffening member 200 to be installed in interior of the golf club head 100 prior to final assembly of the golf club head 100.
In some embodiments, as illustrated in
The stiffening member 200 illustrated in
As illustrated in
As mentioned above, the stiffening member 200 can be adhered to the golf club head 100 utilizing adhesive. In other embodiments, the golf club head 100 and the stiffening member 200 can include complementary features such that the stiffening member 200 can snap into the golf club head 100 without the need for additional adhesives or mechanical locking features.
By manufacturing the stiffening member 200 separately from the rest of the golf club head 100 it can be made from different materials which may have higher stiffness properties and/or a lower density. The stiffening member 200 can be made from, for example, composite, carbon fiber infused polymer, thermoplastic, thermoplastic composite, titanium, steel, stainless steel, magnesium, ceramic, aluminum-boron carbide, boron carbide, aluminum, etc.
Stiffness of a material depends on its modulus of elasticity, also known as Young's modulus. It is preferable that the stiffening member 200 have a higher modulus of elasticity than the portion of the golf club head 100 it is affixed to, the sole 104 for example. It is also preferable for the stiffening member 200 to have a lower density than the portion of the golf club head 100 it is affixed to. Golf club head 100, for example, can be formed from titanium with a modulus of elasticity of approximately 113 GPa and a density of approximately 4.5 g/cm3. The stiffening member 200, for example, can be formed from carbon fiber reinforced polymer with a modulus of elasticity of approximately 181 GPa and a density of approximately 1.5 g/cm3. In one embodiment the stiffening member has a density of less than 4.0 g/cm3. In one embodiment the stiffening member has a modulus of elasticity of greater than 120 GPa.
In one embodiment the stiffening member 200 has a modulus of elasticity at least 20% greater than the modulus of elasticity of the portion of the golf club head it is affixed to. In one embodiment the stiffening member 200 has a modulus of elasticity at least 30% greater than the modulus of elasticity of the portion of the golf club head it is affixed to. In one embodiment the stiffening member 200 has a modulus of elasticity at least 40% greater than the modulus of elasticity of the portion of the golf club head it is affixed to. In one embodiment the stiffening member 200 has a modulus of elasticity at least 50% greater than the modulus of elasticity of the portion of the golf club head it is affixed to.
In one embodiment the stiffening member 200 has a density that is at least 20% less than the density of the portion of the golf club head it is affixed to. In one embodiment the stiffening member 200 has a density that is at least 30% less than the density of the portion of the golf club head it is affixed to. In one embodiment the stiffening member 200 has a density that is at least 40% less than the density of the portion of the golf club head it is affixed to. In one embodiment the stiffening member 200 has a density that is at least 50% less than the density of the portion of the golf club head it is affixed to. In one embodiment the stiffening member 200 has a density that is at least 60% less than the density of the portion of the golf club head it is affixed to.
It is preferable for a composite stiffening member 200 to have the fibers aligned primarily in a lengthwise direction along its length to resist bending and provide stiffness to the golf club head. The modulus of the stiffening member 200 material should be taken of a sample with fibers oriented and loaded in a similar manner as it is in the golf club head 100.
In some embodiments, golf club heads can include both metallic portions and composite portions. The composite portions may replace portions of the golf club head such as the crown and/or the sole. The composite portions are generally lighter than a metallic portion and allow for more discretionary mass for the golf club head designer to optimize center of gravity properties and moments of inertia. The composite portions can be formed from a variety of materials, which may include for example, pre-preg carbon composite, injection molded carbon composite, traditionally laid carbon composite, thermoplastic carbon composite, thermoset material, injection molded carbon composite, a polymer, polyphenylene sulfide (PPS), a polyether ether ketone (PEEK), a polyamide (PA). The composite portions can be formed from a variety of processes, which may include for example, wet layups, pre-preg layup cured in an autoclave, resin infusion, compression molding, injection molding, thermoforming, etc., or any combination thereof.
In a preferred embodiment, the composite portions are thermoformed thermoplastics which offer superior strength and durability performance as compared with injection molded thermoplastics and chopped fiber constructions allowing for panels to be very thin. One limitation to thermoforming composite portions of the golf club head is that you cannot vary the thickness of the panel. Thus if a feature with height is required on one side of a panel, a corresponding depression on the opposite side of the panel is required. Often, golf club heads with composite portions require stiffening members to improve the acoustic signature of the golf club head, which offers a unique challenge when utilizing thermoformed thermoplastic composite portions. The golf club head 500 described below, which incorporates a metallic body 560 with thermoformed composite panels, offers a unique solution to that challenge.
As illustrated in
As illustrated in
As illustrated in
In a preferred embodiment, the composite sole panel 700 is a thermoformed thermoplastic and the stiffening member 800 is affixed to the composite sole panel 700. In one embodiment, the stiffening member 800 is diffusion bonded to the composite sole panel 700. In another embodiment, the stiffening member 800 is compression thermoformed to the composite sole panel 700. The composite sole panel 700 and the stiffening member 800 can be formed from materials which are thermally compatible with one-another. The components may be heated in a variety of techniques which may include, an oven, infrared heating, ultrasonic heating, etc, before they are joined together. In another embodiment, the stiffening member 800 is affixed to the composite sole panel 700 via ultrasonic welding. In another embodiment, the stiffening member 800 is affixed to the composite sole panel 700 with an adhesive. In another embodiment, the stiffening member 800 is can be co-molded to the composite sole panel 700. The stiffening member 800 can be formed from a variety of materials, which may include for example, pre-preg carbon composite, injection molded carbon composite, traditionally laid carbon composite, thermoplastic carbon composite, thermoset material, injection molded carbon composite, a polymer, polyphenylene sulfide (PPS), a polyether ether ketone (PEEK), a polyamide (PA), titanium, steel, aluminum, magnesium, etc. In one embodiment, the composite stiffening member includes continuous carbon fibers running along its entire length. In another embodiment, the stiffening member could be affixed to another composite panel such as the composite crown panel.
As illustrated in
In describing the present technology herein, certain features that are described in the context of separate implementations also can be implemented in combination in a single implementation. Conversely, various features that are described in the context of a single implementation also can be implemented in multiple implementations separately or in any suitable sub combination. Moreover, although features may be described above as acting in certain combinations and even initially claimed as such, one or more features from a claimed combination can in some cases be excised from the combination, and the claimed combination may be directed to a sub combination or variation of a sub combination.
Various modifications to the implementations described in this disclosure may be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other implementations without departing from the spirit or scope of this disclosure. Thus, the claims are not intended to be limited to the implementations shown herein, but are to be accorded the widest scope consistent with this disclosure as well as the principle and novel features disclosed herein.
This application is a continuation-in-part of U.S. patent application Ser. No. 17/484,141, filed on Sep. 24, 2021, currently pending, which is hereby incorporated by reference in its entirety. To the extent appropriate, the present application claims priority to the above-referenced application.
Number | Date | Country | |
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Parent | 17484141 | Sep 2021 | US |
Child | 17522607 | US |