Mixed Material Golf Club Heads

Abstract

To provide a golf club head having a mixed material structure.SOLUTION: A golf club head 10 includes a rear body 16 having a crown member 18 and a sole member coupled to the crown member. The golf club head 10 includes a front body 14 coupled to the rear body 16 to define a substantially hollow structure. The front body 16 includes a strike face 30 and a surrounding frame 32 that extends rearward from a perimeter of the strike face 30. The front body 14 includes a fabric reinforced thermoplastic composite layer and a filled thermoplastic layer each extending across the entire strike face 30. The fabric reinforced thermoplastic composite layer and the filled thermoplastic layer each comprise a common thermoplastic resin component, and are directly bonded to each other without an intermediate adhesive.SELECTED DRAWING: Figure 1

Description

[Technical field]

[0001] <CROSS REFERENCE TO RELATED APPLICATIONS> This application claims the benefit of priority from U.S. Provisional Patent Nos. 62 / 619,631, filed January 19, 2018, 62 / 644,319, filed March 16, 2018, 62 / 702,996, filed July 25, 2018, 62 / 703,305, filed July 25, 2018, 62 / 718,857, filed August 14, 2018, 62 / 770,000, filed November 20, 2018, 62 / 781,509, filed December 18, 2018, and 62 / 781,513, filed December 18, 2018. The disclosures of each of the above-referenced applications are incorporated by reference in their entirety.

[0002] SUMMARY The present disclosure relates generally to golf club heads having mixed material construction. [Background technology]

[0003] In an ideal club design for a given total swing weight, the amount of structural mass would be minimized (without sacrificing resiliency) to provide the designer with additional discretionary mass to specifically place in an effort to customize club performance. In general, the total mass of all golf club heads is the sum of the total amount of structural mass and the total amount of discretionary mass. Structural mass generally refers to the mass of material required to provide the club head with the structural resiliency required to withstand repeated impacts. Structural mass is highly design dependent and provides the designer with a relatively low amount of control over the specific mass distribution. Conversely, discretionary mass is any additional mass (beyond the minimum structural necessity) that can be added to the club head design for the sole purpose of customizing the club's performance and / or restitution tolerance. There is a need in the art for an alternative design to all metal golf club heads that provides a means to maximize discretionary weight to maximize the club head's moment of inertia (MOI) and lower / retract the center of gravity (COG).

[0004] The background provided herein seeks to clarify some club terminology, but is by way of example and not meant to be limiting. Industry practices, rules established by golf organizations such as the United States Golf Association (USGA) or the R&A, and naming conventions may augment this explanation of terminology without departing from the scope of this application. [Brief description of the drawings]

[0005] [Figure 1] 1 is a schematic perspective view of a mixed material golf club head.

[0006] [Diagram 2] FIG. 2 is a schematic bottom view of a mixed material golf club head.

[0007] [Diagram 3] 2 is a schematic exploded perspective view of an embodiment of a mixed material golf club head similar to that shown in FIG. 1.

[0008] [Figure 4] 1 is a schematic perspective view of an embodiment of a sole member of a mixed material golf club head.

[0009] [Diagram 5] 5 is a schematic, enlarged cross-sectional view of a portion of the sole member of FIG. 4 taken along section 5-5.

[0010] [Figure 6] 6 is a schematic partial cross-sectional view of the joining structure of the golf club head of FIG. 2 taken along line 6-6.

[0011] [Figure 7] 7 is a schematic partial cross-sectional view of the joining structure of the golf club head of FIG. 2 taken along line 7-7.

[0012] [Figure 8]1 is a schematic flow diagram illustrating a method of manufacturing a mixed material golf club head.

[0013] [Figure 9] FIG. 2 is a schematic top perspective view of a mixed material crown piece.

[0014] [Figure 10] FIG. 2 is a schematic bottom perspective view of a mixed material crown piece.

[0015] [Figure 11] FIG. 2 is a schematic perspective view of a thermoplastic composite front body of a golf club head.

[0016] [Figure 12] 12 is a schematic partial cross-sectional view of a first embodiment of a golf club head having a thermoplastic composite front body taken along line 12-12 of FIG. 11.

[0017] [Figure 13] 12 is a schematic partial cross-sectional view of a second embodiment of a golf club head having a thermoplastic composite front body taken along line 12-12 of FIG. 11.

[0018] [Figure 14] 1 is a schematic rear view of a thermoplastic composite front body of a golf club head having a debossed channel surrounding the striking face. FIG.

[0019] [Figure 15] FIG. 2 is a schematic top view of a front body of the golf club head.

[0020] [Figure 16] FIG. 2 is a schematic perspective view of a molded front body of a golf club head with a sprue and mold gate leading to the front body.

[0021] [Figure 17] FIG. 17 is an opposite view of the front body of FIG. 16.

[0022] [Figure 18] 1 is a schematic perspective view of a rear portion of a molded front body of a golf club head having a fabric-reinforced composite inner surface.

[0023] [Figure 19] 4 is a schematic flow chart illustrating a method for manufacturing a thermoplastic composite front body of a golf club head.

[0024] [Figure 20] FIG. 2 is a schematic exploded view of a portion of a multi-layer thermoplastic crown.

[0025] [Figure 21] FIG. 21 is a schematic top view of the multi-layer thermoplastic crown of FIG.

[0026] [Figure 22] FIG. 2 is a schematic exploded view of a portion of a multi-layer thermoplastic crown.

[0027] [Diagram 23] FIG. 23 is a schematic top view of the multi-layer thermoplastic crown of FIG.

[0028] [Figure 24] FIG. 2 is a schematic top view of layers of a multi-layer thermoplastic crown or sole having a plurality of openings.

[0029] [Diagram 25] 1 is a schematic top view of an embodiment of a layer of a multi-layer thermoplastic crown or sole having a plurality of openings.

[0030] [Figure 26] 1 is a schematic top view of an embodiment of a layer of a multi-layer thermoplastic crown or sole having a plurality of openings.

[0031] [Figure 27] 1 is a schematic top view of an embodiment of a layer of a multi-layer thermoplastic crown or sole having multiple openings and weights. FIG.

[0032] [Figure 28] 1 is a schematic top view of an embodiment of a layer of a multi-layer thermoplastic crown or sole having an opening and a plurality of weights.

[0033] [Figure 29] 1 is a schematic top view of an embodiment of a layer of a multi-layer thermoplastic crown or sole having a plurality of openings.

[0034] [Diagram 30] 1 is a schematic top view of an embodiment of a layer of a multi-layer thermoplastic crown or sole having a plurality of openings.

[0035] [Diagram 31] 1 is a schematic top view of an embodiment of a layer of a multi-layer thermoplastic crown or sole having multiple openings and weights. FIG.

[0036] [Diagram 32] 1 is a schematic, partially exploded view of a thermoplastic composite striking face having multiple unidirectional woven reinforced composite layers and a filled or unfilled thermoplastic layer;

[0037] [Diagram 33] 1 is a schematic graph illustrating the coefficient of restitution and relative weight savings versus titanium for several different polymers and methods of manufacturing the polymer striking face.

[0038] [Diagram 34] 1 is a schematic exploded perspective view of an embodiment of a mixed material club head.

[0039] [Diagram 35] 35 is a schematic cross-sectional view of an embodiment of a mixed material club head as shown in FIG. 34 taken along the midplane of the club head.

[0040] [Diagram 36]1 is a schematic perspective view of one embodiment of a thermoplastic composite front body of a golf club head with an integrated weight;

[0041] [Figure 37] 1 is a schematic perspective view of one embodiment of a thermoplastic composite front body of a golf club head with an integrated weight;

[0042] [Figure 38] FIG. 2 is a schematic perspective view of one embodiment of a thermoplastic composite front body of a golf club head with an attached weight.

[0043] [Figure 39] FIG. 1 is a schematic exploded perspective view of a thermoplastic composite rear body of a golf club head having a weight integrated into a forward portion of a laminated fabric reinforced composite sole member.

[0044] [Diagram 40] FIG. 2 is a schematic cross-sectional view of a weight member integrated between two textile reinforced composite sheets.

[0045] [Diagram 41] FIG. 2 is a schematic exploded perspective view of a thermoplastic composite rear body of a golf club head having an internal weight skeleton.

[0046] [Diagram 42] FIG. 42 is a schematic cross-sectional view of a thermoplastic composite rear body of a golf club head having an internal weight skeleton as shown in FIG. 41.

[0047] [Diagram 43] FIG. 43 is a schematic plan view of a lower cage and peripheral band of a weight framework such as may be used in the golf club head of FIG. 41 or FIG. 42.

[0048] [Diagram 44] FIG. 2 is a schematic exploded perspective view of a thermoplastic composite rear body of a golf club head having a weight member disposed between laminated sheets of a fabric-reinforced composite sole member;

[0049] [Diagram 45] FIG. 2 is a schematic top view of a fabric reinforced composite sole member having an embodiment of an integrated weight member.

[0050] [Diagram 46] FIG. 2 is a schematic top view of a fabric reinforced composite sole member having an embodiment of an integrated weight member.

[0051] [Figure 47] FIG. 2 is a schematic top view of a fabric reinforced composite sole member having an embodiment of an integrated weight member.

[0052] [Figure 48] 1 is a schematic front view of a golf club head showing the center of gravity of the club head.

[0053] [Figure 49] 49 is a schematic cross-sectional view of the golf club head of FIG. 48 taken along line 49-49.

[0054] [Figure 50] 1 is a plot of center of gravity height and depth for various golf club head constructions. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0055] In the embodiments described below, at least a portion of the club head may be formed from a thermoplastic composite, such as, for example, a woven fabric reinforced thermoplastic composite or a fiber-filled thermoplastic composite. In some embodiments, one or more layers of a woven fabric reinforced thermoplastic composite may be joined with one or more layers of a molded fiber-filled thermoplastic composite. For the purposes of easy distinction within this specification, a "woven fabric reinforced composite" is intended to refer to a composite having a reinforcing fabric embedded within a thermoplastic matrix. The fabric may be formed from a plurality of unidirectional or multidirectional constituent fibers aligned, layered, or woven in a fabric-like pattern. Conversely, a "fiber-filled thermoplastic composite" (or "filled thermoplastic" (FT) for short) is one in which discontinuous chopped fibers are mixed with a liquid / flowable polymer before being injected into a mold to create the final part.

[0056] During molding of filled thermoplastics, the thermoplastics are heated to a temperature above the melting point of the polymer at which they are free to flow. To promote flow characteristics despite having dispersed filler material embedded within the resin, the filler material generally comprises discrete particles having a maximum dimension of less than about 25 mm, or more commonly less than about 12 mm. For example, the filler material may comprise discrete particles having a maximum dimension of 4 mm, 5 mm, 6 mm, 7 mm, 8 mm, 9 mm, or 10 mm. Filler materials useful in the present design may include, for example, glass beads or discontinuous reinforcing fibers formed from carbon, glass, or aramid polymers.

[0057] In contrast to the separate nature of the fibers / fillers in filled thermoplastics, the fibers in a fabric-reinforced composite (FRC) may be substantially larger / longer and have sufficient size and properties such that they may be provided as a continuous fabric separate from the polymer. When integrated with a thermoplastic, the included continuous fibers are generally not flowable, even if the polymer is freely flowable when melted.

[0058] FRC materials are generally formed by arranging fibers in a desired configuration and then impregnating the fiber material with a sufficient amount of polymeric material to provide stiffness. In this manner, FT materials can have a resin content of more than about 45% by volume, or more preferably more than about 55% by volume, while FRC materials desirably have a resin content of less than about 45% by volume, or more preferably less than about 35% by volume. FRC materials traditionally use two-part thermosetting epoxies as the polymer matrix, but the design of the present invention generally uses a thermoplastic polymer instead as the matrix. In many cases, FRC materials are pre-prepared before final manufacturing. Such intermediate materials are often called prepregs. When a thermosetting polymer is used, the prepreg is partially cured in an intermediate form, and the final cure occurs when the prepreg is formed into the final shape. When a thermoplastic polymer is used, the prepreg can include a cooled thermoplastic matrix. The cooled thermoplastic matrix can then be heated and molded into the final shape.

[0059] As explained below, woven reinforced composites are best suited for portions of a design where strength is desired over a continuous surface, while filled thermoplastics are best suited where more complex and / or variable geometries are desired, or for junctions where walls or features come together at angles. Similarly, each will have a different dynamic response during impact, which may further dictate their placement within a design.

[0060] In the present design, one or both of the front body 14 and the rear body 16 may be substantially formed from a thermoplastic composite material including at least one of a textile reinforced composite material or a filled thermoplastic material. In some implementations, the striking face 30 and / or the front body 14 may include a metal (e.g., titanium alloy, steel alloy). However, in other embodiments, the striking face 30 and / or the front body 14 may include a thermoplastic polymer and / or be formed entirely from a thermoplastic composite material. Similarly, in some configurations, a portion of the rear body 16 may be constructed from a textile reinforced composite resilient layer and a filled thermoplastic structural layer. Additionally, one or more portions of the rear body 16 may include or be substantially formed from a metal.

[0061] In configurations in which both the front body 14 and the rear body 16 include a thermoplastic composite, the front body 14 may include a thermoplastic composite that is the same as or different from the thermoplastic composite of the rear body 16. If compatible / miscible thermoplastic resins are used for both the front body 14 and the rear body 16, in some configurations the front body 14 may be secured and / or bonded to at least a portion of the rear body 16 without the need for intermediate adhesives or fasteners. Instead, the polymers of adjacent bodies may be heat fused / welded together.

[0062] Additionally, in embodiments including directly adjacent FRC and FT layers / portions, the use of miscible thermoplastic resins in these respective layers provides the unique ability to co-mold the layers together, which provides unique geometric club head designs to reduce weight via filled thermoplastic layers, but also provides the manufacturing capability to merge layers of stiffness strength via composite elastomeric layers.

[0063] Finally, in some embodiments, the use of certain thermoplastic resins may provide acoustic advantages not possible with other materials. The use of thermoplastic polymers in the present construction can allow the assembled golf club head to respond acoustically closer to that of an all-metal design.

[0064] "A," "an," "the," "at least one," and "one or more" are used interchangeably to indicate the presence of at least one item, and a plurality of such items may be present unless the context clearly indicates otherwise. All values ​​of parameters (e.g., amounts or conditions) in this specification, including the appended claims, are to be understood in all instances to be modified by the term "about," regardless of whether "about" is actually present before the value. "About" indicates that the stated value allows for some slight imprecision (some proximity to the precision of the value, approximately, or reasonably close to, the value). When the imprecision provided by "about" is not otherwise understood in the art in this ordinary sense, as used herein, "about" indicates at least the variation that may result from ordinary methods of measuring and using such parameters. In addition, the disclosure of a range includes the disclosure of all values ​​and sub-divided ranges contained throughout the range. Each value within a range, and the endpoints of the range, are all disclosed herein as separate embodiments. The terms "comprises," "comprising," "including," and "having" are inclusive and thus specify the presence of stated items but do not exclude the presence of other items. As used herein, the term "or" includes any and all combinations of one or more of the listed items. When terms first, second, third, etc. are used to distinguish various items from one another, these designations are merely for convenience and do not limit the items.

[0065] The terms "loft" or "loft angle" of a golf club, as described herein, refer to the angle formed between the club face and the shaft as measured by any suitable loft and lie machine.

[0066] Terms such as "first," "second," "third," and "fourth" in the detailed description and claims, when present, are used to distinguish between similar elements and are not necessarily used to describe a particular sequential or chronological order. It should be understood that such terms used are interchangeable under appropriate circumstances, and that the embodiments described herein are capable of, for example, sequences of operation other than those illustrated or otherwise described herein. Moreover, the terms "comprise" and "have," as well as any variations thereof, are intended to cover a non-exclusive inclusion, such that a process, method, system, article, device, or apparatus that includes a list of elements is not necessarily limited to those elements, but can include other elements not expressly recited or inherent in such process, method, system, article, device, or apparatus.

[0067] In this description and in the claims, terms such as "left," "right," "front," "back," "top," "bottom," "upper," "lower," and similar terms are used for descriptive purposes, if any, with general reference to a golf club addressed on a horizontal ground plane and held at a given loft and lie angle, but are not necessarily intended to describe permanent relative positions. Terms so used are interchangeable under appropriate circumstances. Thus, it should be understood that the apparatus, method, and / or article embodiments described herein can operate in orientations other than those shown or otherwise described herein, for example.

[0068] Terms such as "couple," "coupled," "connection," and "coupled" should be understood broadly and refer to connecting two or more elements, mechanically or otherwise. The connection (mechanical or otherwise) can be for any length of time, for example, permanently or semi-permanently, or only momentarily.

[0069] Other features and aspects will become apparent upon consideration of the following detailed description and the accompanying drawings. Before any embodiment of the present disclosure is described in detail, it should be understood that the present disclosure is not limited in its application to the details or construction and arrangement of components as set forth in the following description or illustrated in the drawings. The present disclosure is capable of supporting other embodiments and may be practiced or carried out in various ways. It should be understood that the description of a specific embodiment is not intended to limit the present disclosure, since it covers all modifications, equivalents, and alternatives falling within the spirit and scope of the present disclosure. It should also be understood that the phraseology and terminology used herein are for the purpose of description and should not be regarded as limiting.

[0070] Like reference numerals are used in the various views to identify similar or identical components. Referring to the drawings, Figure 1 generally illustrates a perspective view of a golf club head 10. In particular, the present technology relates to wood-style head designs, such as drivers, fairway woods, or hybrid irons.

[0071] The golf club head 10 includes a front body portion 14 (front body 14) and a rear body portion 16 (rear body 16) secured together to define a substantially closed / hollow interior volume. As is conventional for wood-style heads, the golf club head 10 includes a crown 18 and a sole 20, which may be generally divided into a heel portion 22, a toe portion 24, and a central portion 26 located between the heel portion 22 and the toe portion 24.

[0072] The front body 14 generally includes a striking face 30 intended for impacting a golf ball, a frame 32 that surrounds a perimeter 34 of the striking face 30 and extends rearwardly therefrom to provide the front body 14 with a cup-shaped appearance, and a hosel 36 for receiving a golf club shaft or shaft adapter.

[0073] To reduce the structural mass of the club head beyond that possible with conventional metal forming techniques, some or all of the front body 14 and / or rear body 16 may be formed substantially from one or more thermoplastic composite materials, such as textile reinforced composites and / or filled thermoplastics. The structural weight reduction achieved by this design may be used to reduce the overall weight of the club head 10 (which may provide higher club head speeds and / or longer distances) or to increase the amount of discretionary mass available for placement in the club head 10 (i.e., for a constant club head weight). In a preferred embodiment, the additional discretionary mass is again included in the final club head design via one or more metal weights 40 (as shown in FIG. 2) coupled to the sole 20, frame 32, and / or rearmost portion of the club head 10.

[0074] 3, in some configurations, rear body 16 may be generally formed by joining a crown member 50 to a sole member 52. In a preferred embodiment, crown member 50 forms part of crown 18 and sole member 52 forms part of sole 20, which meet at an outer join line generally at or slightly below where a tangent to the club head surface lies in a vertical plane (i.e., when club head 10 is held in a neutral striking position according to a given loft and lie angle).

[0075] 3, in embodiments, the crown member 50 may be formed substantially from a formed fiber reinforced composite material comprising a woven glass or carbon fiber reinforcement layer embedded in a polymer matrix. In such embodiments, the polymer matrix is ​​preferably a thermoplastic material, such as, for example, polyphenylene sulfide (PPS), polyether ether ketone (PEEK), polyetherimide (PEI), or a polyamide, such as PA6 or PA66. In other embodiments, the crown member 50 may instead be formed from a filled thermoplastic material, such as, for example, polyphenylene sulfide (PPS), polyether ether ketone (PEEK), polyetherimide (PEI), or a polyamide, including glass beads or discontinuous glass, carbon, or aramid polymer fiber fillers embedded throughout the thermoplastic material. Additionally, in other embodiments, the crown member 50 may have a mixed material construction including both filled thermoplastic materials and formed fiber reinforced composite materials, such as those described below with respect to Figures 9, 10 and 20-31.

[0076] In the embodiment shown in FIG. 3, the sole member 52 comprises a mixed material / multi-layer structure including both a fiber reinforced thermoplastic composite elastic layer 54 and a molded thermoplastic structural layer 56. In a preferred embodiment, the molded thermoplastic structural layer 56 may be formed from a filled thermoplastic material including, for example, glass beads or discontinuous glass, carbon, or aramid polymer fiber fillers embedded throughout a thermoplastic material such as polyphenylene sulfide (PPS), polyether ether ketone (PEEK), polyetherimide (PEI), or a polyamide such as PA6 or PA66. The elastic layer 54 may then include a woven glass, carbon fiber, or aramid polymer fiber reinforcement layer embedded in a thermoplastic polymer matrix including, for example, polyphenylene sulfide (PPS), polyether ether ketone (PEEK), polyetherimide (PEI), or a polyamide such as PA6 or PA66. In one particular embodiment, the crown member 50 and the resilient layer 54 each comprise a woven carbon fiber fabric embedded in polyphenylene sulfide (PPS), and the structural layer 56 may include a filled polyphenylene sulfide (PPS) polymer.

[0077] With regard to the polymeric construction of both the crown member 50 and the sole member 52, any filled thermoplastics and fiber reinforced thermoplastic composites should preferably incorporate one or more engineering polymers that have sufficiently high material strength and / or strength / weight ratio properties to withstand typical use while providing weight saving benefits to the design. Specifically, it is important for the design and materials to efficiently withstand the stresses imparted during impact between the striking face 30 and the golf ball, but not contribute substantially to the total weight of the golf club head 10. In general, preferred polymers can be characterized by a tensile strength at yield of greater than about 60 MPa (net). Also, if filled, they may have a tensile strength at yield of greater than about 110 MPa, or more preferably, greater than about 180 MPa, and even more preferably, greater than about 220 MPa. In some embodiments, suitable filled thermoplastic polymers may have a tensile strength at yield of about 60 MPa to about 350 MPa. In some embodiments, these polymers can have a density ranging from about 1.15 to about 2.02 in either the filled or unfilled state, and can preferably have a melting temperature greater than about 210° C., or more preferably greater than about 250° C.

[0078] PPS and PEEK are two exemplary thermoplastic polymers that meet the strength and weight requirements of the present design. However, unlike many other polymers, the use of PPS or PEEK is further advantageous due to their unique acoustic properties. Specifically, in many situations, PPS and PEEK generally emit a metallic sounding acoustic response upon impact. Thus, by using PPS or PEEK polymers, the present design can take advantage of the strength / weight benefits of the polymer without compromising the desirable metallic club head sound upon impact.

[0079] With continued reference to FIG. 3, the present design utilizes a mixed material sole construction to take advantage of the strength-to-weight ratio benefits of FRC, and also the design flexibility and dimensional stability / consistency offered by FT. More specifically, FRC is typically stronger and less dense than FT of the same polymer, but its strength is typically dependent on smooth and continuous geometries. Conversely, FT is slightly denser than FRC, but can form much more complex geometries, and is generally stronger than FRC in intricate or discontinuous designs. These differences are believed to be due in large part to FRC relying heavily on continuous fibers to provide strength, while FT relies more on the structure of the polymer itself.

[0080] 3 utilizes FRC material to locally enhance the flexibility and / or strength of the design, with FT material to maximize the strength of the design at the lowest possible structural weight, to form the majority of the resilient outer shell of the sole 20. More specifically, the FT material is utilized to provide optimized selective structural reinforcement (i.e., voids / openings that would otherwise compromise the strength of the FRC), to add one or more metal swingweights 40 (i.e., FT makes attachment of discretionary metal swingweights easier than molding complex receiving cavities or overmolding weights), and / or to provide a continuous outer club head surface while providing a dimensionally consistent joint structure that facilitates structural attachment between the crown member 50 and the sole member 52.

[0081] 4 more clearly illustrates an embodiment of the sole member 52 with the FRC resilient layer 54 bonded to the FT structural layer 56. As shown, the structural layer 56 may generally include a forward portion 60 and a rear peripheral portion 62 that defines an outer perimeter 64 of the sole member 52. In the assembled club head 10, the forward portion 60 is bonded to the front body 14 and the rear peripheral portion 62 is bonded to the crown member 50. The structural layer 56 defines a plurality of openings 66 each located inwardly of the perimeter 64 and extending through the thickness of the layer 56. Finally, the structural layer 56 may include one or more structural members 68 extending from the forward portion 60 between at least two of the plurality of openings 66.

[0082] 4, and more clearly in FIGS. 5-7, the resilient layer 54 may be bonded to an outer surface 70 of the structural layer 56 such that it directly abuts and / or overlaps the forward portion 60, the rear peripheral portion 62, and at least a portion of the one or more structural members 68. In doing so, the resilient layer 54 may completely cover each of the plurality of openings 66 when viewed from the outside of the club head 10. Similarly, the one or more structural members 68 may act as selective reinforcement to an inner portion of the resilient layer 54, similar to a reinforcing rib or gusset.

[0083] 2-4, in some embodiments, the structural layer 56 may include a weight portion 72 adapted to receive one or more of a plurality of metallic weights 40 (e.g., tungsten-based swing weights, etc.) by directly adhering or incorporating the weights into a molded cavity or by providing a recess 74 operable to receive a removable metallic mass. The weight portion 72 is generally located toward the rearmost point on the club head 10. Thus, the weight portion 72 may be integral with and / or directly bonded to the rear peripheral portion 62 of the structural layer 56 and spaced from the forward portion 60. As noted above, the filled thermoplastic construction of the structural layer 56 is particularly well suited to receive one or more weights 40 due to its ability to form complex geometric shapes in a structurally stable manner. More specifically, the filled thermoplastic construction of structural layer 56 allows for the inclusion of one or more dimensional recesses in the design that are not typically possible with all-FRC constructions (i.e., because the strength benefits of FRC are usually only available over a continuous surface geometry). For example, as shown in FIG. 3, weighted portion 72 may be molded to define grooves or recesses that receive one or more weights that have a non-uniform thickness, extend around corners, and / or join other surfaces at acute angles, all of which would be difficult or impossible to precisely form using fiber-reinforced composites.

[0084] Attaching one or more weights 40 to the structural layer 56 at the rear portion of the club head 10 may desirably shift the center of gravity of the club head 10 rearward and downward, creating a cantilevered mass spaced apart from the more structural metal front body 14 while also increasing the rotational moment of the club head. Thus, in some embodiments, one or more structural members 68 may span between the weight portion 72 and the front portion 60 to provide an enhanced load path between the one or more weights 40 and the metal front body 14. In this manner, the one or more reinforcing members 68 may act to help transfer dynamic loads between the weight portion 72 and the front body 14 during impact between the striking face 30 and the golf ball. At the same time, these same ribbed reinforcing members 68 may act to strengthen the resilient layer 54 and increase the modal frequencies of the club head at impact. Thus, the natural frequency is above about 3500 Hz at impact and exists without substantial damping from the polymer. When this surface enhancement is combined with the desirable metal-like acoustic impact properties of a polymer such as PPS or PEEK, a user will find the club head 10 to be acoustically similar to an all-metal club head, and the design can provide significantly improved mass properties (CG location and / or moment of inertia).

[0085] In a preferred embodiment, the elastic layer 54 and the structural layer 56 may be integrally bonded to one another without the use of an intermediate adhesive. Such a configuration may simplify manufacturing, reduce problems with component tolerances, and provide a better bond between the constituent layers than can be achieved with adhesives or other bonding methods. To achieve an integral bond, the elastic layer 54 and the structural layer 56 may each comprise a compatible thermoplastic polymer that can be thermally bonded to the polymer of the mating layer.

[0086] 8 illustrates an embodiment of a method 80 for manufacturing a golf club head 10 having an integrally bonded resilient layer 54 and structural layer 56 of a sole member 52. The method 80 includes, at step 82, thermoforming a fiber reinforced thermoplastic composite into a shell portion of the club head 10. The thermoforming process may include, for example, preheating a thermoplastic prepreg to a molding temperature at least above the glass transition temperature of the thermoplastic polymer, molding the prepreg into the shape of the shell portion, and then trimming the molded portion to size.

[0087] After the composite shell portion is in the proper shape, at step 84, a filled polymer support structure may be injection molded into direct contact with the shell. Such a process is commonly referred to as insert molding. In this process, the shell is placed directly into a heated mold having a gated cavity exposed to a portion of the shell. Molten polymer is forced into the cavity and then either directly mixed with the molten polymer of the heated composite shell or locally bonded with the softened shell. When the mold cools, the polymer of the composite shell and the support structure harden together in a fused relationship. Bonding is improved if the polymer of the shell portion and the polymer of the support structure are compatible, and is further improved if the two components comprise a common (or compatible) thermoplastic resin composition. Insert molding is the preferred technique for forming the structure, although other molding techniques such as compression molding may be used.

[0088] Continuing with reference to FIG. 8, once the sole member 52 has been formed through steps 82 and 84, the FRC crown member 50 is bonded to the sole member 52 to substantially complete the construction of the rear body 16 (step 86). In a preferred embodiment, the crown member 50 may be formed from a thermoplastic FRC material that is formed into a shape using thermoforming techniques similar to those described with respect to step 82. Forming the crown member 50 from a thermoplastic composite material allows the crown member 50 to be bonded to the sole member 52 using localized welding techniques. Such welding techniques may include, for example, laser welding, ultrasonic welding, or potentially electrical resistance welding if the polymer is conductive. If the crown member 50 is formed using a thermosetting polymer, the crown member 50 may be bonded to the sole member 52 using, for example, adhesives or mechanical fastening techniques (such as studs, screws, posts, mechanical interference fit engagements, etc.).

[0089] 6 illustrates generally an embodiment of an interface 90 that serves to join the crown member 50 and the sole member 52. As illustrated, the structural layer 56 receives the resilient layer 54 and the crown member 50 separately and forms a continuous outer surface 92 (i.e., the outer surface 92 of the rear body 16 includes the outer surface 94 of the crown member 50, the outer surface 70 of the structural layer 56, and the outer surface 96 of the resilient layer 54).

[0090] Referring again to FIG. 8 , the rear body 16, including the attached crown and sole members 50 and 52, is then attached to the front body structure 14 at step 88. In embodiments in which both the frame 32 of the front body 14 and the forward portion of the rear body 16 comprise a common or miscible thermoplastic resin, the bonding step 88 may be performed via heat fusion and without the use of an intermediate adhesive. If the front body 14 is formed substantially from metal, bonding may require the use of an adhesive to facilitate bonding. While adhesives adhere easily to most metals, the process of bonding polymers may require the use of one or more adhesion promoters or surface treatments to enhance the bond between the adhesive and the polymer of the rear body 16.

[0091] FIG. 7 shows a schematic example of a joint interface 100 between the sole member 52 and a metal embodiment of the frame 32 of the front body 14. As shown, the joint interface 100 resembles a lap joint in which the structural layer 56 and / or the elastic layer 54 overlap a joint flange 102 recessed inwardly from the outer surface 104 of the frame 32. In the illustrated embodiment, the structural layer 56 may be adhesively bonded directly to the joint flange 102 via an intermediately disposed adhesive 106. Alternatively, the elastic layer 54 may extend across the entire forward portion 60 of the structural layer 56 such that the outer surface 96 of the elastic layer 54 is flush with the outer surface 104 of the frame 32. By recessing the joint flange 102 as shown, the structural layer 56 and / or the elastic layer 54 may directly abut an extension wall 108 joining the frame 32 and the flange 102, further facilitating the transfer of dynamic impact loads from the weight 40 / weight portion 72 to the frame 32.

[0092] In some embodiments, the elastic layer 54 may have a substantially uniform thickness in the range of about 0.5 mm to about 0.7 mm, about 0.5 mm to about 1.0 mm, about 0.6 mm to about 0.9 mm, or about 0.7 mm to about 0.8 mm. In some embodiments, the elastic layer 54 may have a non-uniform thickness of 0.5 mm, 0.55 mm, 0.60 mm, 0.65 mm, or 0.70 mm. In the region of the structural layer 56 that directly contacts the elastic layer 54 (i.e., the region where the elastic layer 54 is located outside the structural layer 56), the structural layer 56 of some embodiments may have a substantially uniform thickness of about 0.5 mm to about 0.7 mm, about 0.5 mm to about 1.0 mm, about 0.6 mm to about 0.9 mm, or about 0.7 mm to about 0.8 mm. In some embodiments, the structural layer 56 may have a non-uniform thickness of 0.5 mm, 0.55 mm, 0.60 mm, 0.65 mm, or 0.70 mm. Substantially uniform structures of both the elastic layer 54 and the structural layer 56 are shown in Figures 4-7 and 11. In these embodiments, the combined thickness of the elastic layer 54 and the structural layer 56 may be, for example, about 1.0 mm to about 1.5 mm, about 1.0 mm to about 2.0 mm, about 1.25 mm to about 1.75 mm, or about 1.4 mm to about 1.6 mm. In some embodiments, the combined thickness of the elastic layer 54 and the structural layer 56 may be 1.0 mm, 1.1 mm, 1.2 mm, 1.3 mm, 1.4 mm, or 1.5 mm.

[0093] 3 and 6, in embodiments, the recessed interface flange 102 may completely surround the striking face 30 and / or extend from the frame 32 across all portions of the crown 18 and sole 20. In this manner, the rear body 16 may be further secured to the front body 14 by adhering the crown member 50 to the interface flange 102, as shown in FIG.

[0094] While the method 80 described in FIG. 8 is primarily focused on forming a club head similar to that shown in FIG. 3 (i.e., step 82 forms the resilient layer 54 of the sole member 52 and step 84 forms the structural layer 56 of the sole member 52), the processes described with respect to steps 82 and 84 may alternatively be used to form the crown member 50. For example, as shown in FIGS. 9 and 10, the crown member 50 may include one or both of an outer structural layer 110 and an inner structural layer 112 bonded to a thermoplastic FRC resilient crown layer 114. The inner structural layer 112 may generally function similarly to the structural layer 56 of the sole member 52, while the outer structural layer 110 may provide further weight reduction benefits by concentrating reinforcing structures in areas that provide the most structural benefits, and also allowing for thinner component thickness in the interstitial spaces. This concept of structural ribs will generally create weight reduction zones between the ribs. These weight reduction zones can be present in the sole or crown and are further described in US Pat. Nos. 7,361,100 and 7,686,708, which are incorporated by reference in their entireties.

[0095] Specific to the construction of the mixed material crown member 50, formation similar to that described above with respect to the sole member 52 may begin by thermoforming a fiber reinforced thermoplastic composite into the shell portion of the club head 10. The thermoforming process may include, for example, preheating a thermoplastic prepreg to a molding temperature at least above the glass transition temperature of the thermoplastic polymer, molding the prepreg into the shape of the shell portion, and then trimming the molded portion to size.

[0096] After the composite shell portion is in the proper shape, a filled thermoplastic support structure (i.e., one or both of the inner structural layer 112 and the outer structural layer 110) may then be injection molded (e.g., by insert molding as described above) into direct contact with the shell.

[0097] While FIGS. 4-10 generally focus on the structure of the rear body 16, these same co-molding techniques can be used to form the thermoplastic composite front body 14 as generally shown in FIGS. 11-13. More specifically, FIG. 12 illustrates a first front body configuration 200 including a filled thermoplastic outer layer 202 bonded to an outer surface 204 of a textile reinforced composite layer 206. In this embodiment, the filled thermoplastic outer layer 202 defines the ball striking surface. Meanwhile, the textile reinforced composite layer 206 provides a high strength backing for the face 30. In some embodiments, the textile reinforced composite layer and the filled thermoplastic layer may each extend across the entire striking face to provide resiliency and strength to withstand repeated high speed impacts with a golf ball. Additionally, in some embodiments, the textile reinforced composite layer 206 can extend rearward to form at least a portion of the frame 32. As shown, in one embodiment, the textile reinforced composite layer 206 may have a generally uniform thickness 208 formed from one or more layers of unidirectional and / or multidirectional plies that extend continuously across a substantial majority of the striking face 30.

[0098] As further shown, the filled thermoplastic outer layer 202 may have a variable thickness 210 extending between the textile reinforced composite layer 206 and the ball striking surface. In embodiments in which the textile reinforced composite layer 206 has a substantially uniform thickness, the filled thermoplastic outer layer 202 may primarily contribute to the variable thickness 212 across the striking face 30.

[0099] 13 next illustrates a second front body configuration 220 including a filled thermoplastic inner layer 222 bonded to an inner surface 224 of a textile reinforced composite layer 226. In this embodiment, the textile reinforced composite layer 226 defines the striking face 30 and extends rearward to form at least a portion of the frame 32. The filled thermoplastic inner layer 212 then serves as a structural backing for the composite layer 226. Similar to FIG. 12, in one embodiment, the textile reinforced composite layer 226 may have a uniform thickness 228 generally formed from one or more layers of unidirectional and / or multidirectional plies that extend continuously across a substantial majority of the striking face 30. The filled thermoplastic inner layer 222 may then have a variable thickness 230, which may be designed to tailor the dynamic response of the face 30 to an impact.

[0100] As shown in Figures 12-13, each front body configuration 200, 220 can include a variable face thickness substantially provided by the filled thermoplastic layer 202, 222. In many embodiments, the face thickness may vary such that the minimum face thickness is in the range of 0.114 inches and 0.179 inches and the maximum face thickness is in the range of 0.160 inches and 0.301 inches. The minimum face thickness may be 0.110 inches, 0.114 inches, 0.115 inches, 0.120 inches, 0.125 inches, 0.130 inches, 0.135 inches, 0.140 inches, 0.145 inches, 0.150 inches, 0.155 inches, 0.160 inches, 0.165 inches, 0.170 inches, 0.175 inches, 0.179 inches, or 0.180 inches. The maximum face thickness can be 0.160 inches, 0.165 inches, 0.175 inches, 0.180 inches, 0.190 inches, 0.195 inches, 0.200 inches, 0.210 inches, 0.215 inches, 0.225 inches, 0.230 inches, 0.235 inches, 0.245 inches, 0.250 inches, 0.260 inches, 0.270 inches, 0.280 inches, 0.285 inches, 0.290 inches, 0.301 inches, 0.305 inches, or 0.310 inches.

[0101] With reference to FIG. 14, in some embodiments, the filled thermoplastic inner layer 222 can include one or more discontinuities, voids, debossed geometries, or other irregular surface features. In some configurations, the textile reinforced composite layer 226 can be seen through one or more molded holes or channels in the filled thermoplastic inner layer 222. In the embodiment shown in FIG. 14, the filled thermoplastic inner layer 222 can define a channel 232 that extends around the periphery of the striking face 30 to increase bending of the face and increase energy transfer to the golf ball during impact. The embodiment shown in FIG. 14 shows the channel 232 extending continuously around the periphery of the striking face 30. However, in other embodiments, the channel 232 can extend discontinuously around one or more portions of the periphery of the striking face 30. Additionally, in other embodiments, the channel 232 can extend along any portion of the back surface of the striking face 30.

[0102] In the embodiment shown in FIG. 14, the channel 232 has a rounded concave cross-sectional shape. In other embodiments, the channel 232 may include any cross-sectional shape, including but not limited to, a circle, an oval, a square, a rectangle, a triangle, or any other polygon or shape having at least one curved side. The channel 232 further includes a depth. The depth is measured as the maximum depth of the channel 232 in a direction extending substantially perpendicular to the back side of the striking face 30. In many embodiments, the channel depth may range from about 0.1 mm to about 3 mm. In other embodiments, the channel depth may range from about 0.125 mm to about 2 mm.

[0103] In the illustrated embodiment, the channels 232 allow the striking face 30 to absorb more than 0.9% of the impact energy that can be transferred to the golf ball, increasing the ball's velocity and distance traveled. In many embodiments, the channels 232 allow the striking face 30 to absorb more than 0.75% to 1.5% of the impact energy that can be transferred to the golf ball, increasing the ball's velocity and distance traveled.

[0104] In embodiments in which the filled thermoplastic outer layer 202 is disposed outside the woven reinforced composite layer 206, as shown in FIG. 11, the filled thermoplastic material can form one or more aerodynamic features. The aerodynamic features can effectively reduce club head drag and increase club speed. Such features can include repeating patterns of debossed geometric shapes (e.g., hemispherical indentations, hexagonal indentations, pyramidal indentations, grooves, etc.) and repeating patterns of embossed geometric shapes (e.g., hemispherical protrusions, hexagonal protrusions, pyramidal protrusions, ribs, etc.). Similarly, these aerodynamic features may include individual indentations or protrusions such as the multiple turbulators 240 shown in FIG. 11. These aerodynamic features can be used to modify boundary layer airflow and are further described in U.S. Pat. No. 9,555,294 (the '294 patent), which is incorporated by reference in its entirety. It will be appreciated that due to the nature of polymer molding, where the surface contour of the mold determines the surface geometry of the finished part, molded thermoplastic materials may be particularly well suited to creating these aerodynamic features (i.e., when compared to woven reinforced composites).

[0105] Because filled thermoplastics have anisotropic structural qualities that depend on the typical or average orientation of the embedded discontinuous fibers, special care must be taken in forming the filled thermoplastic (FT) layer 202, 222 to ensure that it has sufficient strength to withstand repeated impacts. More specifically, filled polymer components generally have greater strength for loads that are aligned with the longitudinal axis of the embedded fibers and relatively less strength for loads applied laterally. Fiber orientation in filled polymers is highly dependent on mold flow during initial part formation. Thus, embodiments of the polymer front body 14 can utilize mold and part designs that help orient the embedded fibers along the most likely force / stress propagation paths.

[0106] As will be appreciated, during a molding process such as injection molding, embedded fibers tend to align with the direction of the flowing polymer. With some fibers (i.e., particularly short fiber reinforced thermoplastics) and resins, the alignment tends to occur more completely near the walls of the mold or the edges of the part. These layers are called shear layers or skin layers. Conversely, within the central core layer, the fibers can sometimes be more randomized and / or perpendicular to the flowing polymer. The thickness of the core layer can generally be altered by various molding parameters, including molding speed (i.e., slower molding speeds can result in thinner core layers) and mold design. In the design of the present invention, it is desirable to minimize the thickness of any randomized core layer to allow for better control of fiber orientation.

[0107] During impact, stresses tend to radiate outward from the impact location while propagating toward the rear of the club head 10. In addition, a bending moment is imparted about the shaft, which induces material stresses between the impact location and the hosel 36, and along the hosel 36 parallel to the hosel axis 240, as shown in FIG. 15. Thus, where applicable, embedded fibers are preferably generally oriented in the same direction: parallel to the hosel axis 240 within the hosel 36; at least across the center of the face 30 (represented by the horizontal face axis 242); and in a direction generally outwardly from the face center, with the fibers making a large rearward turn within frame 32 (ie, parallel to front-to-back axis 244).

[0108] Because the discontinuous fibers are mixed in the flowable polymer before forming the part, perfect alignment cannot be guaranteed. However, with it, the design of the front body 14 and the injection molding method (e.g., fill rate, gating / venting, and temperature) may be controlled to align as many of the embedded fibers as possible with these axes. For example, within the hosel, it is preferred that about 50% or more of the fibers are aligned within 30 degrees of the hosel axis 240. Between the center of the face and the hosel 36, it is preferred that about 50% or more of the fibers are aligned within 30 degrees of the horizontal face axis 242 and / or aligned within the frame 32. It is preferred that about 50% or more of the fibers are aligned within 30 degrees of the front-to-rear axis 244. In another embodiment, greater than about 60% of the fibers in the hosel 36 are aligned within 25 degrees of the hosel axis 240, greater than about 60% of the fibers between the center of the face and the hosel 36 are aligned within 25 degrees of the horizontal face axis 242, and / or greater than about 60% of the fibers in the frame 32 are aligned within 25 degrees of the front-to-back axis 244. In yet another embodiment, greater than about 70% of the fibers in the hosel 36 are aligned within 20 degrees of the hosel axis 240, greater than about 70% of the fibers between the center of the face and the hosel 36 are aligned within 20 degrees of the horizontal face axis 242, and / or greater than about 70% of the fibers in the frame 32 are aligned within 20 degrees of the front-to-back axis 244.

[0109] 16-17 show the FT layers 202, 222 which generally achieve the fiber alignment described above. In these figures, the FRC layers 206, 226 have been removed to better show the contours of the face 30. Although FIGS. 16-17 show the FT layers 202, 222 forming at least a portion of the frame 32, this layer need not form or complete the frame 32. It should be noted that in some embodiments, the FT layers 202, 222 are constrained only to the striking face 30, while the FRC layers 206, 226 form the entirety of the frame 32.

[0110] FIG. 16 illustrates a schematic of the flow and fiber alignment within one embodiment of the FT layer 202, 222. As shown in these figures, the flowable polymer enters the toe portion 24 of the front body 14 directly from the sprue 250 and connected gate 252. From there, the polymer can flow across the face 30 and then up through the hosel 36. By flowing across the face 30 and up through the hosel 36, the FT can form the somewhat complex geometry of the hosel 36 while elevating and forcing the weld line into the heel side of the hosel 36. The heel side of the hosel 36 is generally the least stressed area of ​​the hosel 36. If one were to attempt to gate the front body 14 at the hosel 36 (rather than the toe), there would be a greater likelihood of introducing a weld line at or near the face 30 or of the toe side of the hosel 36 being relatively more stressed than the heel side. Because weld lines have a lower ultimate strength than typical polymers, it is important to ensure that weld lines do not form in areas that are typically subject to higher stresses.

[0111] To encourage the polymer to fill the hosel 36 from the bottom to the top, it may be desirable to fill the face from a location near the toe 24, preferably at a horizontal centerline 254 of the face 30 (i.e., between the crown 18 and a line drawn through the center 256 of the face and parallel to the ground when the club is held at address). This may encourage the flow 258 and corresponding fiber alignment to follow a generally downward slope from above the horizontal centerline 254 at the toe 24 toward the center 256 of the face. Following this, at the center 256, the flow 260 and corresponding fiber alignment may be generally parallel to the horizontal centerline 254 at or immediately around the center 256 of the face. Finally, the flow 262 may arc upward, filling the hosel 36 primarily from the bottom toward the neck. 16 illustrates the gate 252 attached directly to the frame 32, however, in the absence of a FT frame, the gate 252 can be directly coupled to a portion of the striking face 30 closest to the toe 24. The general directional references indicated at 258, 260, and 262 are intended to indicate that generally, greater than about 50% of the fibers in the polymer are aligned within about 30 degrees of the indicated direction, or more preferably, greater than about 60% of the fibers are aligned within about 25 degrees of the indicated direction, or even more preferably, greater than about 70% of the fibers are aligned within about 20 degrees of the indicated direction.

[0112] As shown in FIGS. 17-18, flow leaders 264 may protrude from the rear surface 266 of the FT layers 202, 222 to promote flow 258, 260 across the face 30 while encouraging a slight downward arc at 258. As shown, the flow leaders 264 may be embossed channels that extend from the edge of the FT layers 202, 222 at or near the gate and propagate inwardly away from the gate toward the central region of the face 30. The flow leaders 264 may act as a relatively low resistance path for material to flow during molding, thus ensuring the primary flow direction. In some embodiments, the flow leaders 264 may be elevated above the peripheral surface 266 by a height of about 0.5 mm to about 1.5 mm, or about 0.7 mm to about 1.0 mm. Additionally, the flow leaders 264 may have a lateral width of about 5 mm to about 15 mm, or about 7 mm to about 12 mm. The lateral width is measured perpendicular to the height and perpendicular to a line from the origin of the flow leader at the toe 24 to the face center 256 .

[0113] As further shown in Figs. 17-18, in one embodiment, the flow leader 264 can lead to a thickened central region 268 of the face 30. This thickened central portion 268 can be used primarily to reinforce the central region of the face against impacts. As a result, the face moves more as a single unit while avoiding localized deformation. From a molding standpoint, this thickened region 268 can function as a type of well or manifold. The well or manifold can feed polymer radially outward to fill the frame from front to back (or at least steer the polymer flowing through the thinner region toward the trailing edge 270 of the frame). The convergence of the flow from the thicker region 268 to the surrounding thinner regions also aids in the alignment of the embedded fibers. Fig. 18 further shows an FRC backing 206 provided on the inner surface of the front body 14, similar to Figs. 11-12.

[0114] 16-18 specifically illustrate fiber alignment in the front body 14 and striking face 30, these techniques should be considered exemplary and applicable to the rear body 16 as well. For example, in some embodiments, any injection molded structure in the rear body (e.g., structural layer 56 shown in FIG. 3) may be gated / molded to align embedded discontinuous fibers along the primary load path axis while minimizing knit lines or pushing knit lines to a position that experiences relatively low stress. To accomplish this, for example, in one embodiment, the rear body 16 may be gated at the rearmost point of the structural layer 56 to ensure that the fiber-laden resin flows uniformly from rear to front. The structure may be optimized to promote uniform forward flow, for example, by minimizing the amount of structure that diverts the resin flow or prevents the flow from continuing forward. In other embodiments, the structure may include one or more flow leaders operable to direct the resin flow back and forth. In both the front body 14 and rear body 16, it is preferable to utilize only one gate since the flows from multiple gates would ultimately converge to form structurally inharmonious knit lines.

[0115] FIG. 19 illustrates an embodiment of a method 280 for manufacturing a front body 14 having integrally bonded FRC resilient layers 206, 226 and FT structural layers 202, 222. The method 280 generally begins in step 282 by thermoforming a woven fabric reinforced thermoplastic composite material into a shell portion of the front body 14. The thermoforming process may include, for example, preheating one or more thermoplastic prepregs to a molding temperature at least above the glass transition temperature of the thermoplastic polymer, forming the prepregs into a desired shape, and then trimming the molded part to size. In one configuration, the one or more prepregs are compression molded into a shape that can form the exterior surfaces of the striking face 30 and the frame 32, as shown in FIG. 13. Such a configuration may generally involve a final shape having a plurality of flat and / or rounded surfaces. In another configuration, the one or more prepregs are compression molded into a shape that can form at least a portion of the interior surface of the front body 14 or striking face 30. In such an embodiment, the compression molded prepreg can follow the outer contours of any variable face thickness, flow leaders, or other interior surface features to direct the flow of material, so that the exterior surface 204 can create surface depressions that are ultimately filled with the flowable polymer.

[0116] Once the composite shell portion is in the proper shape, it is placed in a mold at step 284. The filled thermoplastic is then injection molded in direct contact with the FRC at step 286. As previously mentioned, such a process is commonly referred to as insert molding. In this process, a preformed shell is placed directly into a heated mold having a gated cavity / void that directly abuts the exposed portion of the shell. Molten polymer is forced into the cavity and then either mixes directly with the molten polymer of the heated composite shell or bonds locally with the softened shell. When the mold cools, the polymers of the composite shell and the support structure harden together in a fused relationship. Bonding is enhanced when the polymer of the shell portion and the polymer of the support structure are compatible, and is further enhanced when the two components include a common or otherwise miscible thermoplastic component. While insert molding is the preferred technique for forming the structure, other molding techniques such as compression molding may also be used (e.g., when the FT layer is produced as a distinct, separate layer and then fused with the other layers via compression molding).

[0117] In a further design, multiple inserts are provided in the mold prior to injecting the filled thermoplastic resin. For example, a first insert may form the exterior surface of the front body 14, a second insert may form the reinforced rear surface, and the filled thermoplastic resin may be injected between them. In another embodiment, one or more reinforcing meshes, including metal meshes or screens, may be embedded within the FT layer to provide additional reinforcement and strength. In such an embodiment, to facilitate solid integration between the mesh and the FT layer, the mesh may include multiple openings through which the thermoplastic resin may flow during the generation of the FT layer.

[0118] While the above disclosure generally describes the use of thermoplastic composites having at least one woven reinforced composite layer and at least one filled thermoplastic layer, it should be understood that the technique is not limited to just two layers within a given component. In many embodiments, the thermoplastic composites can include laminates having two or more, three or more, four or more, five or more, six or more, seven or more, eight or more, nine or more, ten or more layers of mixed materials. By forming each layer with a thermoplastic base resin, there is almost no limit to the number of times any one or more layers can be modified if the design so requires. This unique attribute can allow the formation of intricate and / or complex three-dimensional material structures by preforming layers with different grain patterns, internal fiber orientations, and / or aperture sizes, shapes, and / or spacings. This technique then allows the strength-to-weight ratio to be optimized by engineering the material's structure itself.

[0119] In some embodiments, one or more of the striking face 30, crown 18, or sole 20 may include multiple separate layers of thermoplastic composite material. Each layer is fused to at least one immediately adjacent / abutting thermoplastic composite layer without the use of an intermediate adhesive. Each layer may be comprised of a woven reinforced thermoplastic composite material, a filled thermoplastic material (preferably filled with long and / or short fiber fillers), or an unfilled thermoplastic material. The base thermoplastic resin of each layer may be the same as or otherwise miscible with the base thermoplastic resin of one or more immediately adjacent layers. In this manner, in one configuration, at least multiple layers may be formed separately and then collectively fused together by application of heat and pressure, such as using a compression molding process.

[0120] FIG. 20 shows an example of such a laminated structure that may be used with the crown 18 (although such a design may be used in the sole as well). As shown in an exploded view 300, the crown 18 includes three layers. A first layer 302 forms a portion of an exterior surface 304. A second layer 306 forms a portion of an interior surface 308. A third layer 310 is disposed between the first layer 302 and the second layer 306. In this embodiment, the first layer 302 is solid throughout and does not include any openings. The second layer 306 includes a first plurality of hexagonal shaped openings 312 that span a majority of the crown 18. The third layer 310 includes a second plurality of hexagonal shaped openings 314 that span a majority of the crown 18. When the second layer 306 and the third layer 310 are nested together as shown in FIG. 21, A second plurality of hexagonal Opening 31 4 is offset from the location of the first plurality of hexagonal openings 312. One or both of the second layer 306 and the third layer 310 may include a filled thermoplastic resin. Similarly, one or both of the second layer 306 and the third layer 310 may include a woven reinforced composite. When FRC is used, each reinforcing fiber preferably extends around the openings 312, 314 rather than terminating at the openings as if the openings were cut into a preformed sheet. To further illustrate the advantages of thermoplastics, each layer shown in FIG. 20 may be individually formed and fully cured in a dimensionally stable manner before stacking in a compression mold. The compression mold essentially bonds the layers together over the entire surface by heating each layer to a temperature above its respective glass transition temperature. Complex 3D material structures can be engineered by forming and modifying each layer individually and / or collectively multiple times.

[0121] Further expanding on the concept of engineered material construction, Figures 22 and 23 show an embodiment similar to that shown in Figures 20-21, but with the different layer designs made to serve different specific purposes. As shown, Figure 22 shows an exploded (or pre-assembled) view of a crown member 320 including a first outer layer 322, a second middle layer 324, and a third bottom layer 326. The first layer 322 is substantially solid, as in the design of Figure 20. The second layer 324 includes a plurality of struts 328 extending between a front portion 330 of the crown member and a rear portion 332 of the crown member 320. These struts 328 act to reinforce the crown in the anterior-posterior dimensions. The third layer 326 then includes at least one strut 334 extending laterally across the crown member 320 to reinforce the crown in the heel-toe direction.

[0122] While FIG. 22 illustrates one embodiment that uses individual layer structures to achieve different structural design objectives, in some embodiments, layers may be used to strategically alter weight performance. For example, different layers may have different densities (e.g., by using fillers or fabric reinforcements of different densities) and may be included only to affect the location of the center of gravity or moment of inertia. To this effect, each layer may have a layer-specific center of gravity that is different from the other layer-specific centers of gravity, which are located at different locations within the layer. Similarly, some layers may function as "structural layers" that can provide optimized structural designs, while other layers may function as "mass layers" that can be used to alter the placement of the center of gravity of the club head. In some implementations, the mass layers may be doped with metal fillers such as tungsten. Mass layers may be particularly suited for use in soles where the additional mass can serve the functional purpose of moving the center of gravity of the club head rearward and downward. One example of a mass layer structure may include a layer with openings concentrated in the forward portion of the layer, but no openings in the rearward portion.

[0123] Each of Figures 24-31 illustrates a different laminate layer design embodiment. Each embodiment can have functional properties and can be used alone or in combination with others of the illustrated designs or solid layers to form the crown 18 or sole 20. When solid layers are used, they may include woven fabric reinforced composite materials, filled thermoplastic materials, or unfilled thermoplastic materials. In some embodiments, a laminate may include multiple unidirectional woven fabric reinforced composite layers, each provided with a different relative orientation (i.e., when viewed from a plan view, the longitudinal axes of the fibers are rotated with respect to adjacent layers).

[0124] 24 illustrates one embodiment of a fiber reinforced laminate layer 350 that may be used to form a portion of the crown 18 or sole 20. As illustrated, the layer 350 may include a plurality of openings 352. The openings 352 each have a circular shape. The openings 352 may be disposed across the entire surface of the layer 350. Such openings 352 may be similar to those described in U.S. Patent No. 9,776,052, which is incorporated by reference in its entirety.

[0125] 25 is another embodiment of a fiber reinforced laminate layer 360 that may be used to form a portion of the crown 18 or sole 20. As shown, the layer 360 may include a plurality of openings 362, including four openings 362 extending from near the striking face 30 toward a trailing edge 364. The openings include a first opening positioned near a heel end 366, a second opening positioned near a toe end 368, a third opening positioned between the first and second openings, and a fourth opening positioned between the third and second openings. The first and second openings include a triangular shape and the third and fourth openings include a trapezoidal shape.

[0126] 26 is another embodiment of a fiber reinforced laminate layer 370 that may be used to form a portion of the crown 18 or sole 20. As shown, the layer 370 may include a plurality of openings 372 including first, second, third, and fourth openings positioned in a heel-toe direction near the striking face 30, fifth, sixth, seventh, and eighth openings positioned in a heel-toe direction near a trailing edge 374, and ninth and tenth openings positioned between the first through eighth openings.

[0127] FIG. 27 is another embodiment of a fiber reinforced laminate layer 380 that may be used to form a portion of the crown 18 or sole 20. As shown, the layer 380 includes a plurality of openings 382, ​​including four openings 382 extending from near the striking face 30 toward a trailing edge 384. A first opening is located near a heel end 386, a second opening is located near a toe end 388, a third opening is located between the first and second openings, and a fourth opening is located between the third and second openings. The material between the first, second, third, and fourth openings includes circular shapes such that the first, second, third, and fourth openings include distorted polygons. In some embodiments, these circular portions may be used to modify one or more mass properties of the layer and / or the club head in general.

[0128] 28 illustrates another embodiment of a fiber reinforced laminate layer 390 that may be used to form a portion of the crown 18 or sole 20. As shown, the layer 390 may include an aperture 392 having a plurality of material portions 394 extending from a perimeter 396 toward a center of the layer 390. The material portions 394 may include an enlarged mass portion 398 at a distal end of the material portions 394 to modify one or more mass properties of the layer 390 and / or the club head generally.

[0129] 29 is another embodiment of a fiber reinforced laminate layer 400 that may be used to form a portion of the crown 18 or sole 20. As shown, the layer 400 may include a plurality of openings 402, including six openings, with a first opening closest to the striking face, and each successive opening (i.e., the second, third, fourth, fifth and sixth openings) disposed adjacent one another in a direction toward the rear of the golf club head 10. Each opening 402 includes a striped arc extending in an arc from a heel end 404 to a toe end 406.

[0130] 30 is another embodiment of a fiber reinforced laminate layer 410 that may be used to form a portion of the crown 18 or sole 20. As shown, the layer 410 may include a plurality of apertures 412, including three apertures. A first aperture is positioned near the running plane on the toe end 404. A second aperture is positioned near the running plane on the heel end 406. A third aperture is positioned near the rear portion 408 between the heel end 406 and the toe end 404. And, the material separating the three apertures may form a Y-shape.

[0131] Figure 31 illustrates an embodiment similar to Figure 30. A mass 420 is included in the center of the layer (at the intersection of each arm of the "Y" shape). As such, masses can be included in any layer of the examples shown in Figures 24-30. Such masses are not limited to circular sections, but rather can be any shape.

[0132] Similar to the crown / sole shown in Figures 20-31, the striking face 30 can include multiple laminar layers. At least two of the layers are fused together by a compression molding operation. In one configuration, as shown in Figure 32, the striking face 30 can include multiple unidirectional woven reinforced thermoplastic composite layers 450, each layer rotated relative to adjacent layers. Each layer can include a common base thermoplastic resin. The common base thermoplastic resin fuses with the polymer of the adjacent layers when collectively heated above the glass transition temperature of the polymer. In some embodiments, the striking face 30 can further include a filled or unfilled thermoplastic layer 452. The thermoplastic layer 452 can be preformed and compression molded with the FRC layer 450 or can be injection molded into contact with the molten FRC layer, for example, by an insert injection molding process. Forming such layups / laminates with a thermoplastic used as the resin matrix has been proven to provide a more repeatable layup while providing desirable weight reduction and coefficient of restitution. Three examples of stacking sequences that have proven to have suitable strength properties are shown in Table 1 below. [Table 1]

[0133] FIG. 33 illustrates how different injection molded composite materials perform both in terms of relative coefficient of restitution (COR) 460 and relative weight savings 462 when compared to a titanium metal face. As can be seen, compression molded fabric reinforced composites 464 tend to be lighter and can have a higher COR than pure injection molded variants 466 of similar polymers. However, due to the lower percentage of resin in the compression molded layers, compression molded composites tend to be relatively more brittle than the injection molded variants shown. Thus, in some design embodiments, a combination of the two can ultimately provide the most desirable results with the best balance of strength and resilience.

[0134] As mentioned above, different blended materials or compounds / elements can form each of these lamina layers in the crown 18, sole 20, and / or striking face 30. The different lamina layers can share a common matrix polymer (i.e., the same thermoplastic polymer in each lamina layer) and the same or different reinforcing elements or reinforcing compounds per lamina layer. The different lamina layers can share a common derivative matrix polymer that is not chemically the same but is miscible with each other. For example, one lamina layer can be a thermoplastic polymer that is one chemical compound, and the next lamina layer is another thermoplastic compound that is a different chemical formula from the thermoplastic compound of the lamina layer above, but shares sufficient chemical structure, 3D shape, and chemical properties to be miscible with the thermoplastic layer above. In these "miscible" thermoplastic lamina layers, each of the reinforcing elements or reinforcing compounds can be the same or different. The different lamina layers can also share a common thermoplastic resin with each layer, but each lamina layer can have the same or different matrix polymer and / or reinforcing elements / reinforcing compounds.

[0135] The combination of matrix polymer and reinforcing elements (woven or fiber filled) allows the final product to include the benefits of both the matrix polymer and the reinforcing elements. Also, the matrix polymer with reinforcing elements shrinks less than unfilled resin / polymer when subjected to any form of thermoforming, thereby improving dimensional control of the molded part and reducing the cost of the composite. In many embodiments, the matrix polymer of the crown / sole portion 24 / 26 can be polycarbonate (PC), polyphenylene sulfide (PPS), polypropylene (PP), nylon-6 (PA6), nylon 6-6 (PA66), nylon-12 (PA12), polymethylpentene (TPX), polyvinylidene fluoride (PVDF), polymethyl macyl (PMMA), polyetherketone (PEEK), polyetherimide (PEI), or polyetherketone (PEK).

[0136] For example, the material of the matrix polymer of the crown 18, sole 20, and / or striking face 30 can each be selected and / or formed to achieve one or more material properties, such as tensile strength, tensile modulus, and density. The matrix polymer of the crown, sole, and / or striking face can include a tensile strength in the range of 30 MPa to 3000 MPa. In some embodiments, the tensile strength of the matrix polymer can be in the range of 30 MPa to 500 MPa, 500 MPa to 1000 MPa, 1000 MPa to 1500 MPa, 1500 MPa to 2000 MPa, 2000 MPa to 2500 MPa, 2500 MPa to 3000 MPa, 30 MPa to 1500 MPa, 1500 MPa to 3000 MPa, 500 MPa to 2500 MPa, 30 MPa to 1000 MPa, 1000 MPa to 2000 MPa, or 2000 MPa to 3000 MPa. In some embodiments, the tensile strength of the matrix polymer of the crown, sole, and / or striking face may be 30 MPa, 200 MPa, 400 MPa, 800 MPa, 1200 MPa, 1600 MPa, 2000 MPa, 2400 MPa, 2800 MPa, or 3000 MPa.

[0137] The matrix polymer of the crown, sole, and / or striking face can include a tensile modulus in the range of 1.5 GPa to 12 GPa. In some embodiments, the tensile modulus can be in the range of 1.5 GPa to 6 GPa, 6 GPa to 12 GPa, 1.5 GPa to 3 GPa, 3 GPa to 6 GPa, 6 GPa to 9 GPa, or 9 GPa to 12 GPa. In some embodiments, the matrix polymer of the crown, sole, and / or striking face can have a tensile modulus of 1.5 GPa, 2 GPa, 3 GPa, 4 GPa, 5 GPa, 6 GPa, 7 GPa, 8 GPa, 9 GPa, 10 GPa, 11 GPa, or 12 GPa.

[0138] The matrix polymer of the crown, sole, and / or striking face is 0.80 g / cm 3 ~1.80g / cm 3In some embodiments, the density can range from 0.80 g / cm 3 ~1.3g / cm3, 1.3g / cm 3 ~1.8g / cm 3 , 1.0g / cm 3 ~1.6g / cm 3 , 0.8g / cm 3 ~1.1g / cm3, 1.1g / cm 3 ~1.5g / cm 3 , 1.5g / cm 3 ~1.8g / cm 3 , 0.8g / cm 3 ~1.0g / cm 3 , 1.0g / cm 3 ~1.2g / cm 3 , 1.2g / cm 3 ~1.4g / cm 3 , 1.4g / cm 3 ~1.6g / cm 3 , or 1.6 g / cm 3 ~1.8g / cm 3 In some embodiments, the matrix polymer of the crown / sole may range from 0.8 g / cm 3 , 0.9g / cm 3 , 1.0g / cm 3 , 1.1g / cm 3 , 1.2g / cm 3 , 1.3g / cm 3 , 1.4g / cm 3 , 1.5g / cm 3 , 1.6g / cm 3 , 1.7g / cm 3 , or 1.8 g / cm 3 The density can range from 0.01 to 0.01.

[0139] The reinforcing fabric / fiber embedded in one or more of the crown, sole, and / or striking face may be carbon fiber, aramid fiber (e.g., Nomex, Vectran, Kevlar, Twaron), bamboo fiber, natural fiber (e.g., cotton, hemp, flax), glass fiber, glass beads, metal fiber (e.g., Ti, Al), ceramic fiber (e.g., TiO2), and granite, SiC. The material of such reinforcing fabric / fiber in the crown, sole, and / or striking face includes material properties such as tensile strength, tensile modulus, and density. In some embodiments, the tensile strength of the reinforcing elements of the crown, sole, and / or striking face ranges from 300 MPa to 7000 MPa. In some embodiments, the tensile strength of the reinforcing element can be in the range of 300MPa to 4000MPa, 4000MPa to 7000MPa, 2000MPa to 5500MPa, 300MPa to 2000MPa, 2000MPa to 3500MPa, 3500MPa to 5000MPa, 5000MPa to 7000MPa, 300MPa to 1500MPa, 1500MPa to 2500MPa, 2500MPa to 3500MPa, 3500MPa to 4500MPa, 4500MPa to 5500MPa, or 5500MPa to 7000MPa. In some embodiments, the reinforcement elements of the crown, sole, and / or striking face can have a tensile strength of 300 MPa, 1000 MPa, 1500 MPa, 2000 MPa, 2500 MPa, 3000 MPa, 3500 MPa, 4000 MPa, 4500 MPa, 5000 MPa, 5500 MPa, 6000 MPa, 6500 MPa, or 7000 MPa.

[0140] In some embodiments, the tensile modulus of the reinforcing elements of the crown, sole, and / or striking face is in the range of 30 GPa to 700 GPa. In some embodiments, the tensile modulus of the reinforcing elements can be in the range of 30 GPa to 400 GPa, 400 GPa to 700 GPa, 200 GPa to 550 GPa, 30 GPa to 200 GPa, 200 GPa to 350 GPa, 350 GPa to 500 GPa, 500 GPa to 700 GPa, 30 GPa to 150 GPa, 150 GPa to 250 GPa, 250 GPa to 350 GPa, 350 GPa to 450 GPa, 450 GPa to 550 GPa, or 550 GPa to 700 GPa. In some embodiments, the reinforcing elements of the crown, sole, and / or striking face can have a tensile modulus of 30 GPa, 100 GPa, 150 GPa, 200 GPa, 250 GPa, 300 GPa, 350 GPa, 400 GPa, 450 GPa, 500 GPa, 550 GPa, 600 GPa, 650 GPa, or 700 GPa.

[0141] In some embodiments, the density of the reinforcing elements of the crown, sole, and / or striking face is less than or equal to 0.75 g / cm 3 ~10g / cm 3 In some embodiments, the density of the reinforcing elements ranges from 1 g / cm 3 From 5g / cm 3 In some embodiments, the reinforcing elements of the crown, sole, and / or striking face may range from 1.8 kg / mm 2 , 200kg / mm 2 , 400kg / mm 2 , 600kg / mm 2 , 800kg / mm 2 , 1000kg / mm 2 , 1200kg / mm 2 , 1400kg / mm 2 , 1600kg / mm 2 , 1800kg / mm 2 , 2000kg / mm 2 , or 2200 kg / mm 2 It could be.

[0142] 34-35 illustrate additional embodiments of a club head 10 that may be at least partially constructed in accordance with the above teachings. As illustrated, the golf club head 10 includes a front body 14 and a rear body 16 that are secured together to define a substantially closed / hollow interior volume. In some embodiments, the front body 14 may be formed from a metal (e.g., a titanium alloy or a steel alloy). However, in other embodiments, at least a portion of the front body 14, including the striking face 30, may be formed from a filled thermoplastic material and / or a fiber reinforced composite material. In some embodiments, the front body 14 may be configured as described above and / or as shown in any of FIGS. 11-18.

[0143] The rear body 16 may generally be formed from a textile reinforced thermoplastic composite crown member 500 forming at least a portion of the crown 18, a textile reinforced thermoplastic composite sole member 502 forming at least a portion of the sole 20, and a filled or unfilled thermoplastic support structure 504 supporting one or both of the FRC crown member 500 or the FRC sole member 502. In some embodiments, the thermoplastic support structure 504 may include a plurality of discontinuous reinforcing fibers and / or metal fillers (e.g., powders) embedded within a thermoplastic resin. In a preferred embodiment, the thermoplastic resin of the support structure 504 is the same as or is otherwise miscible with the thermoplastic resin used to form both the FRC crown member 500 and the FRC sole member 502. In this manner, the crown member 500 and the sole member 502 may be bonded to the support structure 504 using direct bonding, without the need for an intermediate adhesive.

[0144] 34 further illustrates weight portion 72 exploded from support structure 504. In some embodiments, weight portion 72 can comprise a metal section adapted to receive one or more removable and / or fixed weights. In one embodiment, weight portion 72 may comprise a steel alloy adapted to receive one or more fixed or removable weights 40 including tungsten. In some embodiments, at least a portion of weight portion 72 may be mechanically engaged with support structure 504, for example, by an insert injection molding process.

[0145] In embodiments in which the front body 14 and rear body 16 are formed primarily using thermoplastic composite materials, it has been found that both the moment of inertia and the total mass of the club head are significantly reduced. More specifically, the switch to this particular thermoplastic construction provides a design that is about 60 to about 100 grams lighter than conventional driver heads, which typically weigh between about 200 grams and about 210 grams. In order to maintain a constant swing weight (i.e., resistance to twisting of the club head during off-center impacts) with an improved moment of inertia, it is desirable to incorporate this mass back into the club head in the form of randomly located mass.

[0146] In some embodiments, it may be desirable to locate at least a portion of the optional mass toward a forward portion of the club head. In some embodiments, it has been found that the use of forwardly located mass provides a more stable and balanced club head. More specifically, it has been discovered that if the center of gravity is pushed rearward beyond the approximate geometric center of the club head, the club head may become unstable, especially during the deceleration phase of the swing close to impact. This concern does not arise in conventional metal constructions due to the structural mass maintained in the forward region of the club head. However, the low density of the polymer and the increased optional mass are concerns that must be considered in the design or placement of the optional mass.

[0147] 36-38 show three embodiments of a front body 14 similar to that shown in FIG. 34. Each embodiment provides a different means of placing optional mass in the toe portion 24 and / or heel portion 22 of the front body 14. FIG. 36 shows an embodiment of a thermoplastic composite front body 14 in which a mass pocket 510 is molded into the interior 512 of the front body 14. Each mass pocket 510 can include a heavy metal such as lead, tungsten, or bismuth. The heavy metal is overmolded or encapsulated into a portion of the front body 14. In one embodiment, to prevent the creation of unnecessary stress risers created at the interface between the metal and the polymer, the metal may be integrated as a filler in a thermoplastic resin that is amenable to mixing with the resin used to form the surrounding FT and / or FRC. In such an embodiment, the metal filler can form up to about 90% by volume, or up to about 80% by volume, or up to about 70% by volume, or up to about 60% by volume of the weight slug incorporated into the mass pocket 510. That way, when a metal filled polymer is overmolded, the adjacent thermoplastic can form a stronger surface bond than a pure polymer to metal interface.

[0148] FIG. 37 shows a different implementation of the design shown in FIG. 36. Finally, FIG. 38 shows a design in which the forward weight 514 in the front body 14 is at least partially mechanically secured, such as through the use of one or more screws 516. In one embodiment of such a design, the outer weight 518 can be attached to the outer surface 520 of the club head, while the inner weight 522 can cooperate with the outer weight 518 to pinch a portion of the club head wall. Both the inner weight 522 and the outer weight 518 can be formed from metal to most affect the location of the club head's center of gravity. In one embodiment, the outer weight 518 can resemble a naming badge or applique. In some embodiments, the inner weight 522 can be at least partially separated from the club head wall via a gasket 524. In one embodiment, each of the weights shown in FIGS. 36-38 can be vertically aligned with the geometric center 526 of the face. In other embodiments, the weights can be positioned below the center of the face to help pull the center of gravity lower. This will generally result in a higher ball trajectory.

[0149] FIG. 39 shows an embodiment of the design of the rear body 16. In this design, weights 530 are integrated into one or more front portions 532 of the FRC crown member 500 or the FRC sole member 502. As shown in the cross-sectional view of FIG. 40, in one embodiment, these weights 530 may be encapsulated between two adjacent fabric reinforcement lamina layers 534, 536 used to form the sole member 502. As with the above design, in one embodiment, to prevent the generation of unnecessary stress risers generated at the interface between the weights 530 and the polymer of the FRC lamina layers 534, 536, the metal may be integrated as a filler in a thermoplastic resin element having a polymer resin that is easily mixed with the resin used to form the surrounding FRC layers. In such an embodiment, the metal filler may be about 30% to about 90% by volume of the weight 530, or may be about 60% to about 80% by volume, or even about 65% to about 75% by volume of the weight element. In some embodiments, the weight 530 may have a specific gravity greater than about 8, or greater than about 9, or greater than about 10. In one particular embodiment, the weight 530 may include 70% tungsten filler (by volume) in 30% thermoplastic resin and may have a specific gravity ranging from about 12.5 to about 14.0. In these embodiments, when the metal filled polymer is overmolded, adjacent thermoplastic resin bonds with the similar resin used to form the weight, thus reducing boundary layer stresses that may form.

[0150] It has been found that in some designs, the face thickness and density can provide sufficient forward weighting to avoid the need for additional forward metal weighting. In one embodiment, it has been found that if the maximum thickness of the variable thickness striking face is about 5.0 mm to about 9.0 mm, or about 6.0 mm to about 8.0 mm, and the perimeter thickness is about 3.0 mm to about 5.0 mm, or about 3.5 mm to about 4.5 mm, no forward weighting is required. In one embodiment, if the maximum face thickness is about 7.25 mm and the perimeter face thickness is about 4.45 mm, no forward metal weighting is required.

[0151] In an embodiment that does not utilize added forward metal weights, any and all mass can be added to the club head, for example in the form of tungsten or other high density metal weights located in the rear weight portion 72 of the sole 20. Such a design helps to lower or move the center of gravity back, improving the launch characteristics of the impacted ball. Unfortunately, in some situations, concentrated loads of this nature may require strengthened support structure between the weights and the striking face so that the striking face can withstand the impact loads without catastrophically buckling. The further back, heavier and more concentrated the mass is, the more structure and / or stiffer material is required to resist buckling in the middle portion of the club head.

[0152] 41-42 show a schematic of the rear design of the club head 550. The club head 550 includes a weighted internal skeleton 552 that acts to structurally distribute weight while resisting impact buckling instead of promoting it. As shown, at least in FIG. 43, the skeleton 552 includes a lower cage 554 and a perimeter band 556. In some embodiments, the lower cage 554 is separate from the perimeter band 556, such that in the absence of an intermediate polymer, the two components are separate and distinct (as shown in FIG. 43). In some embodiments, the skeleton 552 may be formed from a metallic material that acts to alter the placement of the center of gravity. If formed from a metallic material, the skeleton 552 may be glued in place or overmolded (e.g., by insert injection molding).

[0153] In another embodiment, the scaffold 552 may be a thermoplastic composite incorporating metal fillers in a thermoplastic resin for at least one of the lower cage 554 and the perimeter band 556. This hybrid thermoplastic scaffold may then be bonded / fused to an adjacent thermoplastic structure 504, for example, on the inwardly facing surface 558 of the structure 504. In such an embodiment, the metal filler may be about 30% to about 90% by volume of the filled portion of the scaffold 552, or may be about 60% to about 80% by volume, or even about 65% to about 75% by volume of the filled portion of the scaffold 552. In some embodiments, the filled portion of the scaffold 552 may have a specific gravity of greater than about 8, or greater than about 9, or greater than about 10. In one particular embodiment, the filled portion of the scaffold 552 may include 70% by volume tungsten filler in 30% by volume thermoplastic resin and may have a specific gravity in the range of about 12.5 to about 14.0.

[0154] During manufacture, scaffold 552 may be compression molded in contact with structure 504, whereby each structure is heated to a temperature above the glass transition temperature of its respective resin. Upon cooling, adjacent pieces may be fused together.

[0155] In yet another embodiment, the support structure 504 itself may include metal fillers that operate to reintroduce a portion of any available weight. In such an embodiment, at least a portion of the structure 504 may have a specific gravity greater than about 8, or greater than about 9, or greater than about 10, or in the range of about 12.5 to about 14.0.

[0156] FIG. 44 shows a schematic exploded view of an embodiment of the rear body 16 having a sole member 502 shown in an exploded view. In this embodiment, the sole member 502 can include multiple layers with at least two of the layers being thermoplastic composite materials. In particular, the embodiment shown in FIG. 44 includes an inner FRC sole layer 570, an outer FRC sole layer 572, and an intermediate weight member 574 disposed between the inner FRC sole layer 570 and the outer FRC sole layer 572. In this embodiment, the weight member 574 can be a metal plate or a FT composite having a metal filler disposed within a thermoplastic resin (as described above). Next, FIGS. 45-47 show three different embodiments of the intermediate weight member 574 that can be used with the multi-layer sole member 502.

[0157] Common to each of the presently disclosed designs is the desire to provide a golf head that maximizes the total amount of discretionary mass available to locate the center of gravity as close to the sole and rear of the club as possible while maximizing the moment of inertia to the maximum extent permitted under United States Golf Association (USGA) regulations. To accomplish this desire, one or both of the front body 14 or rear body 16 of the club head 10 are formed from reinforced thermoplastic composite materials having a lower specific gravity than the metals typically used. However, it has been found that achieving sufficient durability with polymers that are less strong than metals requires an increase in the volume of material required, thus offsetting at least a portion of the weight reduction. The presently described embodiments utilize a design-based approach to strengthen polymer structures in a manner that attempts to minimize the amount of additional material that must be added. These designs incorporate selective reinforcement to prevent buckling within the primary load paths. These designs utilize aligned reinforcing fibers embedded within the thermoplastic to match the anisotropic strength of the thermoplastic composite to the dynamics of the structure. And / or the designs utilize mixed material thermoplastic laminate constructions to leverage the design and material advantages of both filled thermoplastic and woven reinforced composites within the same structure.

[0158] The design of the present invention achieved a net weight reduction of approximately 60-100 grams. Without the reintroduction of this weight, the club head would have a dramatic reduction in both swing weight and moment of inertia. However, the reintroduction of weight presented separate challenges in terms of how to attach the weight to the structure, how to distribute the weight to avoid impact dynamics that could damage the intermediate structure, and how to position the weight to maximize the moment of inertia while pushing the center of gravity as far back and down as possible. Presently described embodiments for reweighting the club head to balance these objectives are, respectively, for example: Positioning the weight forward to minimize impact stresses and keeping the center of gravity forward of a critical point that could lead to instability; Distributing the weight in a structural manner, such as using a skeletal or metal doped reinforcement structure; or Incorporating the weight into weighted and / or doped lamina layers within the outer shell of the club head. Incorporating the weight into the structure itself is a design made possible primarily by the use of thermoplastic resins. Thermoplastic resins can be used to form separate layers with specific design properties, and then the assembly of layers is reformed into an aggregate laminate.

[0159] As will be described below, the designs described herein are successful in achieving the design objectives of a high moment of inertia club head with a depressed and rearwardly located center of gravity while maintaining stability and durability.

[0160] <General weight characteristics> As shown generally in FIGS. 48-49, the striking face 30 of the club head 10 defines a geometric center 800 and a loft plane 802 tangent to the geometric center 800 of the striking face 30. In some embodiments, the geometric center 800 can be located at the geometric center point of the striking face perimeter 804 and at the midpoint of the face height 806. In similar or other embodiments, the geometric center 800 can also be centered with respect to an engineered impact zone 808, which can be defined by an area of ​​a groove 810 on the striking face. As an alternative approach, the geometric center of the striking face can be located according to a definition of a golf governing body, such as the United States Golf Association (USGA). For example, the geometric center of the striking face can be determined according to section 6.1 of the USGA's Procedure for Measuring Flexibility of Golf Club Heads. (USGA-TPX3004, Rev. 1.0.0, May 1, 2008) (available at http: / / www.usga.org / equipment / testing / protocols / Procedure-For-Measuring-The-Flexibility-Of-A-Golf-Club-Head / ) (the “Flexibility Procedure”).

[0161] The club head 10 further comprises a head center of gravity (CG) 812 and a head depth plane 814. The head depth plane 814 extends through the geometric center 800 of the striking face 30 and perpendicular to the loft plane 802, extending in a direction from the heel 22 to the toe 24 of the club head 10. In many embodiments, the head CG 812 is located at a head CG depth 816 from the loft plane 802 measured in a direction perpendicular to the loft plane 802. The head CG 812 is further located at a head CG height 818 from the head depth plane 814 measured in a direction perpendicular to the head depth plane 814. In many embodiments, the head CG height 818 is positive when the head CG 812 is located above the head depth plane 814 (i.e., between the head depth plane 814 and the crown 18). Head CG height 818 is negative when head CG 812 is located below head depth plane 814 (ie, between head depth plane 814 and sole 20).

[0162] In many embodiments, the head CG height 818 can be less than 0.08 inches, less than 0.07 inches, less than 0.06 inches, less than 0.05 inches, less than 0.04 inches, less than 0.03 inches, less than 0.02 inches, less than 0.01 inches, or less than 0 inches (i.e., the head CG height can have a negative value such that it lies below the head depth plane). Furthermore, in many embodiments, the head CG height 818 can have an absolute value of less than about 0.08 inches, less than about 0.07 inches, less than about 0.06 inches, less than about 0.05 inches, or less than about 0.04 inches. Furthermore, in many embodiments, the head CG depth 816 can be greater than about 1.7 inches, greater than about 1.8 inches, greater than about 1.9 inches, greater than about 2.0 inches, greater than about 2.1 inches, greater than about 2.2 inches, or greater than about 2.3 inches.

[0163] In many embodiments of the present design, head CG depth 816 and head CG height 818, in units measured in inches, may be related by the following Relation 1 and / or Relation 2:

[0164] Head CG depth ≧ (head CG height + 0.115) / 0.10 ...Relationship 1

[0165] Head CG depth ≧ (head CG height + 0.14) / 0.10 ...Relationship formula 2

[0166] For purposes of determining the club head's moment of inertia, a coordinate system may be defined at the CG 812 via mutually orthogonal axes (i.e., x-axis 820, y-axis 822, and z-axis 824). The y-axis 822 extends through the head CG 812 from the crown 18 to the sole 22, perpendicular to the ground plane when the club head is in the address position. The x-axis 820 extends through the head CG 812 from the heel 22 to the toe 24 and is perpendicular to the y-axis 822. The z-axis 824 extends through the head CG 812 from the front end 830 to the back end 832 and is perpendicular to the x-axis 820 and y-axis 822.

[0167] In that case, the moments of inertia are about an x-axis Ixx (i.e., crown-to-sole moment of inertia) and about a y-axis Iyy (i.e., heel-to-toe moment of inertia). In many embodiments, the crown-sole moment of inertia Ixx is about 3000 g cm 2 Larger, approx. 3250g cm 2 Larger, approx. 3500g cm 2 Larger, approx. 3750g·cm 2 Larger, about 4000g cm 2 Larger, approx. 4250g cm 2 Larger, approx. 4500g cm 2 Larger, approx. 4750g·cm 2 Larger, about 5000g cm 2 Larger, approx. 5250g cm 2 Larger, approx. 5500g cm 2Larger, approx. 5750g·cm 2 Larger, about 6000g cm 2 Larger, approx. 6250g cm 2 Larger, approx. 6500g cm 2 Larger, approx. 6750g·cm 2 Larger or about 7000g cm 2 Further, in many embodiments, the heel-toe moment of inertia Iyy is about 5000 g cm 2 It is larger than 5250g cm 2 It is larger than 5500g cm 2 It is larger than 5750g cm 2 It is larger than 6000g cm 2 It is larger than 6250g cm 2 It is larger than 6500g cm 2 It is larger than 6750g cm 2 or approximately 7000 g cm 2 can be larger than

[0168] In many embodiments, the club head has a combined moment of inertia (i.e., the sum of the crown-sole moment of inertia Ixx and the heel-toe moment of inertia Iyy). The combined moment of inertia is greater than or equal to 8000 g cm 2 Larger: 8500g cm 2 Larger: 8750g cm 2 Larger: 9000g cm 2 Larger: 9250g cm 2 Larger: 9500g cm 2 Larger: 9750g cm 2 Larger: 10000g cm 2 Larger: 10250g cm 2 Larger: 10500g cm 2 Larger, 10750g cm 2 Larger: 11000g cm 2 Larger, 11250g cm 2 Larger: 11500g cm 2Larger, 11750g cm 2 Greater than or equal to 12000g cm 2 Larger: 12500g cm 2 Larger: 13000g cm 2 Larger: 13500g cm 2 Greater than or equal to 14000g cm 2 Greater than.

[0169] Table 1 below numerically illustrates the mass parameters of eight different club heads. Specifically, the table illustrates CG depth 816, CG height 818, moment of inertia Ixx about a horizontal x-axis 820, and moment of inertia Iyy about a y-axis 822. [Table 2]

[0170] Metal Clubs 1 to 3 are commercially available drivers having an all-metal structure design (i.e., at least the crown, sole, and face). Metal 1 is an all-titanium structure, approximately 445 cm 3 The Metal 2 is a full titanium driver head with a volume of less than 460 cm and a rear back weight. 3 Metal 3 is a metal driver head with a total titanium structure, approximately 450-457 cm 3 and a metal driver head having a movable weight system.

[0171] "Metal face;polymer body" is a driver head of similar construction as shown in Figures 1-3, having a titanium front body 14 and a rear body 16 formed substantially from a polymer composite structure. A metal weight is added to the rear weight section to provide a swing weight similar to that of commercially available all-metal driver heads. "Polymer face;metal body" is a driver head including a polymer front body 14 as shown in Figures 11-13 secured to an optimized titanium rear body 16 substantially similar to the titanium rear section of Metal 1 or Metal 2.

[0172] Finally, "All Polymer 1" is a polymer composite driver head including a polymer front body 14 (as shown in Figures 11-13) combined with a polymer rear body 16 (as shown in any or all of Figures 1-7). Weight is reintroduced in a well-distributed manner, including at least some discretionary weight located forward of the center of gravity. "All Polymer 2" is based on the "All Polymer 1" design, but moves discretionary mass rearward in the form of an 80 gram tungsten weight located at the rear of the club, as close to the sole as possible. Finally, "All Polymer 3" is a theoretical model that replaces the 80 gram weight of "All Polymer 2" with an 80 gram point mass located at the rearmost part of the club head, as close to the sole as possible.

[0173] FIG. 50 graphically depicts CG position. The vertical axis 900 represents CGy (CG height 818). The horizontal axis 902 represents CGz (CG depth 816) for each of the club head embodiments identified in Table 1. FIG. 50 further groups the various models into three categories. The first group 904 consists of commercially available all-metal drivers (i.e., Metal 1, Metal 2, and Metal 3). The second group 906 consists of designs where portions of the club head have been converted to a polymer composite (i.e., "Metal Face; Polymer Body" and "Polymer Face; Metal Body"). The third group 908 consists of designs where the entire structure has been converted to a polymer structure (i.e., All Polymer 1, All Polymer 2, and All Polymer 3). FIG. 50 further depicts two of the relationships discussed above ("Relationship 1" 910 and "Relationship 2" 912).

[0174] FIG. 50 shows that both lower and deeper center of gravity shifts (compared to commercially available all-metal designs) are only achieved by moving completely to an all-polymer construction. As shown, the use of a partial polymer construction in the present designs can actually result in a higher CG. This can work against ideal ball flight and reduce total distance. Furthermore, referring back to Table 1, these all-polymer designs (especially those with little or no forward discretionary mass, as in All-Polymers 2 and 3) can result in very substantial increases in club head moment of inertia. For example, the "All-Polymer 2" design with 80 grams of tungsten weight in the rear provides a 19% increase in Ixx over the average Ixx from the all-metal designs and a 9% increase in Iyy over the average Iyy from the all-metal designs. For comparison, note that each design provided in Table 1 has approximately the same mass (plus or minus about 3 grams).

[0175] Substitution of one or more claim elements constitutes a rearrangement, not a prosthesis. Moreover, advantages, other advantages, and solutions to a problem have been described in connection with particular embodiments. However, the advantages, other advantages, and solutions to a problem, and any one or more elements that make any advantage, advantage, or solution occur or become apparent, do not constitute a critical, essential, or essential feature or element of any or all elements of a claim, unless such advantage, advantage, solution, or element is expressly recited in such claim.

[0176] Because the rules of golf change from time to time (e.g., new rules may be adopted, or old rules may be repealed or modified, by golf standards organizations and / or governing bodies such as the United States Golf Association (USGA), the Royal and American Golf Association (R&A), etc.), golf equipment related to the devices, methods and products described herein may or may not conform to the rules of golf at any particular time. Accordingly, golf equipment related to the devices, methods and products described herein may be advertised, offered for sale and / or sold as conforming or non-conforming golf equipment. The devices, methods and products described herein are not limited in this respect.

[0177] Although the above embodiments are described in the context of iron-type golf clubs, the devices, methods and products described herein may be applied to other types of golf clubs, such as driver-type golf clubs, fairwood-type golf clubs, hybrid-type golf clubs, iron-type golf clubs, wedge-type golf clubs, or putter-type golf clubs, while the devices, methods and products described herein may be applicable to other types of sporting goods, such as hockey sticks, tennis racquets, fishing rods, ski poles, etc.

[0178] Furthermore, the embodiments and limitations described in this specification are not offered to the public under the doctrine of disclosure if the embodiments and / or limitations (1) are not explicitly claimed in the claims and (2) are equivalent or potentially equivalent to the express elements and / or limitations in the claims under the doctrine of equivalents.

[0179] Various features and advantages of the disclosure are set forth in the following paragraphs.

[0180] Clause 1: A golf club head comprising: a rear body including a crown member and a sole member coupled to the crown member; and a front body connected to the rear body to define a substantially hollow structure, the front body including a striking face and a peripheral frame extending rearwardly from a periphery of the striking face, the front body comprising a woven fabric reinforced thermoplastic composite layer and a filled thermoplastic layer each extending across the striking face, the woven fabric reinforced thermoplastic composite layer and the filled thermoplastic layer each comprising a common thermoplastic resin composition, and the woven fabric reinforced thermoplastic composite layer and the filled thermoplastic layer are directly bonded to each other without an intermediate adhesive.

[0181] Clause 2: The golf club head of clause 1, wherein the filled thermoplastic layer has a non-uniform thickness across the striking face.

[0182] Clause 3: The golf club head of clause 1 or 2, wherein the striking face includes an outwardly facing ball striking face, the fabric reinforced thermoplastic composite layer forming the ball striking face.

[0183] Clause 4: The golf club head of clause 1 or 2, wherein the striking face includes an outwardly facing ball striking face and a rear surface opposite the ball striking face, the textile reinforced thermoplastic composite layer forming the rear surface.

[0184] Clause 5: The golf club head of clause 4, wherein the filled thermoplastic layer forms an outwardly facing surface of the front body, and the filled thermoplastic layer includes at least one of a functional texture or a plurality of protrusions extending outwardly from an outer surface of the golf club head, and the functional texture or the plurality of protrusions act to modify the aerodynamic characteristics of the golf club head.

[0185] Clause 6: The golf club head according to any one of clauses 1 to 5, wherein the fabric reinforced thermoplastic composite layer has a constant thickness.

[0186] Clause 7: A golf club head described in any one of clauses 1 to 6, wherein the filled thermoplastic layer includes a plurality of discontinuous fibers embedded in a thermoplastic matrix, each fiber having a respective orientation of the longitudinal axis of the fiber.

[0187] Clause 8: The golf club head of clause 7, wherein the striking face includes a toe portion, a heel portion, and a center portion, and between the center portion and the heel portion of the striking face, greater than about 50% of the embedded fiber content within the filled thermoplastic layer is aligned within 30 degrees of a face axis, the face axis extending between the toe portion and the heel portion, and the face axis is parallel to the ground surface when the golf club head is held in a neutral address position on the ground surface.

[0188] Clause 9: A golf club head as described in any one of clauses 1 to 8, wherein the filled thermoplastic layer includes a flow leader extending between a toe portion of the striking face and a center portion of the striking face, the flow leader being a thickened portion of the filled thermoplastic layer relative to an adjacent portion of the striking face.

[0189] Clause 10: A golf club head described in any one of clauses 1 to 9, wherein the front body further includes a plurality of woven fabric reinforced thermoplastic composite layers, each of the plurality of woven fabric reinforced thermoplastic composite layers having a fiber orientation different from the orientation of at least one directly adjacent woven fabric reinforced thermoplastic composite layer, and each of the plurality of woven fabric reinforced thermoplastic composite layers having a thermoplastic resin that fuses with the thermoplastic resin of each of the directly adjacent layers.

[0190] Clause 11: The golf club head according to any one of clauses 1 to 10, wherein the textile reinforced thermoplastic composite layer forms at least a portion of the frame.

[0191] Clause 12: A golf club head described in any one of clauses 1 to 11, wherein the filled thermoplastic layer includes a metal mesh embedded therein, and the resin of the filled thermoplastic layer extends into a plurality of openings defined by the mesh.

[0192] Clause 13: A golf club head described in any one of clauses 1 to 12, wherein each of the front body and the rear body comprises a thermoplastic resin, and the thermoplastic resin of the front body is fused to the thermoplastic resin of the rear body without an intermediate adhesive.

[0193] Clause 14: A golf club head as described in any one of clauses 1 to 13, wherein the fabric reinforced thermoplastic composite layer comprises a multidirectionally oriented or unidirectionally oriented fabric embedded in a first thermoplastic resin, and the filled thermoplastic layer comprises a plurality of discontinuous fibers embedded in a second thermoplastic resin.

[0194] Clause 15: The golf club head of clause 14, wherein the first thermoplastic resin and the second thermoplastic resin each comprise a common thermoplastic resin component.

[0195] Clause 16: The golf club head of clause 14, wherein the woven fabric reinforced thermoplastic composite layer comprises the first thermoplastic resin in an amount less than about 45 volume percent, and the filled thermoplastic layer comprises the second thermoplastic resin in an amount greater than about 45 volume percent.

[0196] Clause 17: A golf club head described in any one of clauses 1 to 16, wherein at least one of the crown member or sole member of the rear body has a textile reinforced thermoplastic composite layer and a filled thermoplastic layer, the textile reinforced thermoplastic composite layer of the rear body and the filled thermoplastic layer of the rear body each have a common thermoplastic resin component, and the textile reinforced thermoplastic composite layer of the rear body and the filled thermoplastic layer of the rear body are directly bonded to each other without an intermediate adhesive.

[0197] Clause 18: The golf club head of clause 17, wherein the filled thermoplastic layer of the rear body includes a weighted portion having a metal mass embedded therein.

[0198] Clause 19: The golf club head of clause 18, wherein the metal mass is a metal filler embedded within the thermoplastic resin of the filled thermoplastic layer.

[0199] Clause 20: A golf club head described in any one of clauses 17 to 19, wherein the filled thermoplastic layer of the rear body includes a plurality of openings extending in a thickness direction of the filled thermoplastic layer, and the fabric reinforced thermoplastic composite layer of the rear body extends across each of the plurality of openings.

[0200] Clause 21: A golf club head according to any one of clauses 1 to 20, comprising a center of gravity located at the depth and height of the center of gravity defined as above, the depth and height of the center of gravity satisfying at least one of the following formulas:

[0201] Head CG depth ≧ (head CG height + 0.115) / 0.10

[0202] Head CG depth ≧ (head CG height + 0.14) / 0.10

[0203] Here, head CG depth and head CG height are both measured in inches.

Claims

1. a rear body including a crown member and a sole member; a front body coupled to a rear body to define a substantially hollow structure, the front body including a striking face and a perimeter frame extending rearwardly from a perimeter of the striking face; A golf club head comprising: the front body including a woven fabric reinforced thermoplastic composite layer and a filled thermoplastic layer each extending across the striking face; The textile reinforced thermoplastic composite layer and the filled thermoplastic layer each have a common thermoplastic resin component; the textile reinforced thermoplastic composite layer and the filled thermoplastic layer are directly bonded to each other without an intermediate adhesive; The sole member is a filled thermoplastic layer of the sole member including a plurality of openings extending through a thickness of the filled thermoplastic layer of the sole member; the textile reinforced thermoplastic composite layer of the sole member being joined to an outer surface of the filled thermoplastic layer of the sole member such that the textile reinforced thermoplastic composite layer of the sole member extends across each of the plurality of openings; Equipped with the filled thermoplastic layer of the sole member and the textile reinforced thermoplastic composite layer of the sole member each comprise a common thermoplastic resin component; the filled thermoplastic layer of the sole member is directly bonded to the textile reinforced thermoplastic composite layer of the sole member without an intermediate adhesive; The crown member is a first layer that does not include any openings and that partially forms an exterior surface of the crown member; a second layer having a first plurality of openings and partially forming an interior surface of the crown member; a third layer having a second plurality of openings and disposed between the first layer and the second layer; The golf club head, wherein the second plurality of openings are offset from the location of the first plurality of openings when the second layer and the third layer are nested together.

2. The golf club head of claim 1 , wherein the filled thermoplastic layer of the front body has a non-uniform thickness across the striking face.

3. the striking face includes an outwardly facing, ball striking face and a rear surface opposite the ball striking face; The golf club head of claim 1 or 2, wherein the textile reinforced thermoplastic composite layer of the front body forms the rear surface.

4. The filled thermoplastic layer of the sole member is a front portion in contact with and joined to the metal front body; a weight portion spaced from the forward portion; a structural member extending from the forward portion to the weight portion and extending between at least two of the plurality of openings, the structural member being integrally molded with the forward portion and the weight portion; Further comprising:

4. The golf club head of claim 1, wherein the sole member further includes a metal weight at least partially embedded in the weight portion of the filled thermoplastic layer of the sole member or adhesively bonded to the weight portion of the filled thermoplastic layer of the sole member.

5. The filled thermoplastic layer of the front body forms an outwardly facing surface of the front body; 5. The golf club head of claim 4, wherein the filled thermoplastic layer of the front body includes at least one aerodynamic feature of a discrete depression or a plurality of protrusions extending outwardly from an outer surface of the golf club head.

6. The golf club head of claim 1 , wherein the textile reinforced thermoplastic composite layer of the front body has a constant thickness.

7. the filled thermoplastic layer of the front body includes a plurality of discontinuous fibers embedded in a thermoplastic matrix; 7. The golf club head of claim 1, wherein each fiber has a respective orientation of the longitudinal axis of the fiber.

8. the striking face includes a toe portion, a heel portion, and a central portion; between the center portion and the heel portion of the striking face, greater than about 50% of the embedded fiber content within the filled thermoplastic layer of the front body is aligned within 30 degrees of a face axis; the face axis extends between the toe portion and the heel portion; The golf club head of claim 7 , wherein the face axis is parallel to the ground plane when the golf club head is held in a neutral address position on the ground plane.

9. the filled thermoplastic layer of the front body includes a flow leader extending between a toe portion of the striking face and a center portion of the striking face; 9. The golf club head of claim 1, wherein the flow leader is a thickened portion of the filled thermoplastic layer relative to an adjacent portion of the striking face.

10. The front body further includes a plurality of textile reinforced thermoplastic composite layers; each of the plurality of textile reinforced thermoplastic composite plies of the front body has a fiber orientation that is different from an orientation of at least one immediately adjacent textile reinforced thermoplastic composite ply of the front body; 10. The golf club head of claim 1, wherein each of the plurality of textile reinforced thermoplastic composite layers of the front body has a thermoplastic resin that fuses with the thermoplastic resin of each of the immediately adjacent layers.

11. The golf club head of claim 1 , wherein the textile reinforced thermoplastic composite layer of the front body forms at least a portion of the perimeter frame.

12. the filled thermoplastic layer of the front body includes a metal mesh embedded therein; 12. The golf club head of claim 1, wherein the resin of the filled thermoplastic layer extends into a plurality of openings defined by the mesh.

13. A golf club head as described in any one of claims 1 to 12, wherein the filled thermoplastic material of the filled thermoplastic layer of the sole member is fused to the filled thermoplastic material of the filled thermoplastic layer of the front body without an intermediate adhesive.

14. 14. The golf club head of claim 1, wherein the common thermoplastic resin component comprises polyphenylene sulfide or polyether ether ketone.

15. The textile reinforced thermoplastic composite layer of the front body comprises a multidirectionally or unidirectionally oriented textile embedded in a first thermoplastic resin; 15. The golf club head of claim 1, wherein the filled thermoplastic layer of the front body comprises a plurality of discontinuous fibers embedded within a second thermoplastic resin.

16. the textile reinforced thermoplastic composite layer of the front body comprises the first thermoplastic resin in an amount of less than about 45 volume percent; 16. The golf club head of claim 15, wherein the filled thermoplastic layer of the front body comprises greater than about 45% by volume of the second thermoplastic resin.

17. A golf club head as claimed in any one of claims 1 to 16, wherein the filled thermoplastic layer of the sole member includes a weighted portion having an embedded metal mass.

18. 18. The golf club head of claim 17, wherein the metal mass is a metal filler embedded within the thermoplastic resin of the filled thermoplastic layer of the sole member.

19. the crown member comprises a fiber reinforced composite material; 19. The golf club head of claim 1, wherein the crown member is joined to the sole member at a joint by a means selected from the group consisting of a localized weld, an adhesive bond, and a mechanical fastener.

20. The second layer and the third layer each comprise a woven fabric reinforced composite; The golf club head of any one of claims 1 to 19, wherein reinforcing fibers of the woven fabric reinforced composite extend around the first plurality of openings and the second plurality of openings, respectively.

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