Transient liquid phase bonding of golf club components
12515110 ยท 2026-01-06
Assignee
Inventors
- Alex Power (Carlsbad, CA, US)
- Danielle Reyes (Carlsbad, CA, US)
- Scott Manwaring (Carlsbad, CA, US)
- William Mellor (San Diego, CA, US)
Cpc classification
A63B53/042
HUMAN NECESSITIES
B23K35/007
PERFORMING OPERATIONS; TRANSPORTING
A63B2053/0491
HUMAN NECESSITIES
International classification
Abstract
A method for transient liquid phase bonding golf club head components is disclosed herein. Golf club components composed of dissimilar materials are joined using transient liquid phase bonding. One embodiment of the transient liquid phase bonding process joins a steel component to titanium component using a pure copper interlayer heated between the temperature of 870 C. to 1085 C. The interaction between the titanium and the copper forms a eutectic below the melt temperature of pure copper, transitions to a liquid phase, and joins the titanium component to the steel component upon cooling.
Claims
1. A method for joining golf club head components comprising: placing in a heating apparatus a golf club head face component composed of a titanium alloy, a golf club head body component composed of an iron alloy, and an interlayer component in a joint between the golf club head face component and the golf club head body component, the interlayer component comprising a first layer directly contacting the golf club head face component and composed of a zirconium material and a second layer directly contacting the golf club head body component and composed of a copper material; applying a temperature below a melt temperature of the interlayer component to form a transient liquid at the joint during a transient liquid phase, wherein the temperature of the transient liquid phase ranges from 893 C. to 1085 C.; diffusing the transient liquid into at least one of the golf club head face component or the golf club head body component; and solidifying at least a portion of the transient liquid to join the golf club head face component to the golf club head body component.
2. The method according to claim 1 wherein the golf club head face component is a wood-type golf club face component and the golf club head body component is a wood-type golf club body component.
3. The method according to claim 1 wherein the golf club head face component is an iron-type golf club face component and the golf club head body component is an iron-type golf club body component.
4. The method according to claim 1 further comprising applying a vacuum with a maximum vacuum level ranging from 10.sup.2 Torr to 10.sup.7 Torr.
5. A method for joining golf club head components comprising: placing in a heating apparatus a golf club head body component composed of a steel, a weight component composed of tungsten or a tungsten alloy, and an interlayer component in a joint between the golf club head body component and the weight component, the interlayer component comprising a first layer directly contacting the golf club head body component and composed of a zirconium material and a second layer directly contacting the weight component and composed of a copper material; applying a temperature below a melt temperature of the interlayer component to form a transient liquid at the joint during a transient liquid phase, wherein the temperature of the transient liquid phase ranges from 893 C. to 1085 C.; diffusing the transient liquid into at least one of the golf club head body component or the weight component; and solidifying at least a portion of the transient liquid to join the golf club head body component to the weight component.
6. The method according to claim 5 wherein the golf club head body component is a wood-type golf club body component.
7. The method according to claim 5 wherein the golf club head body component is an iron-type golf club body component.
8. The method according to claim 5 further comprising applying a vacuum with a maximum vacuum level ranging from 10.sup.2 Torr to 10.sup.7 Torr.
Description
BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS
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DETAILED DESCRIPTION OF THE INVENTION
(24) Transient Liquid Phase Diffusion Bonding/Eutectic Brazing/eutectic bonding: utilizing eutectics to form a liquid phase that creates a joint between two dissimilar base metals through the use of one or more interlayers. The process differs from brazing since the process temperature used to create the liquid phase is below the melt temperature of the interlayer or interlayers used, and new phases are formed that act as the joint.
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(26) A first embodiment of the transient liquid phase bonding process is to join a component of steel (and its alloys) or tungsten (and its alloys), to a component composed of a titanium (and its alloys) using a substantially pure copper interlayer heated between a temperature 870 C. to 1085 C. The interaction between titanium and copper forms a eutectic below the melt temperature of pure copper, transitions to a liquid phase, and joins the titanium component to the steel component upon cooling below a temperature of 870 C. The primary result is a titanium-copper intermetallic that acts as the joint (with some amounts of elements from the steel sidedepending on the alloy). Depending on the temperature used and the interlayer thickness used, the composition of the intermetallic formed can be adjusted as well as the joint thickness.
(27) A second embodiment of the transient liquid phase bonding process is to join steel (and its alloys) to tungsten (and its alloys) using a dual interlayer (pure copper and pure titanium) between 870 C. to 1085 C. (same explanation as above).
(28) A third embodiment of the transient liquid phase bonding process is to join a component composed of a steel (and its alloys) or tungsten (and its alloys), to a component composed of a titanium (and its alloys) using a substantially pure copper interlayer and a substantially pure zirconium interlayer, heated between the temperatures 893 C. to 1085 C. The location of interlayer is important for this application so that the zirconium and copper form the main eutectic and not the titanium and copper. The stack is titanium.fwdarw.zirconium.fwdarw.copper.fwdarw.steel. The interaction between copper and zirconium forms a eutectic below the melt temperature of pure copper, transitions to a liquid phase, and joins the component of titanium to the component of steel upon cooling below a temperature of 893 C. The primary result is a zirconium-copper intermetallic (with some amounts of elements from the steel and titanium sidedepends on the alloys) that acts as the joint. Depending on the temperature used and the interlayer thickness used, the composition of the intermetallic formed can be adjusted as well as the joint thickness.
(29) A fourth embodiment of the transient liquid phase bonding process is to join a component of steel (and its alloys) to a component of tungsten (and its alloys) using a dual interlayer (substantially pure copper and substantially pure zirconium) between 893 C. to 1085 C. (same explanation as above).
(30) For all these embodiments of transient liquid phase bonding, it is also possible to nickel plate the steel side. At certain temperatures, the diffusion of iron into the joint is controlled for the bonding process.
(31) Further embodiments include a co-transient liquid phase diffusion bonding process. These co-transient liquid phase diffusion bonding embodiments include using a combination of eutectics to join the titanium face to the body at the same time as a tungsten weight to the body using a single or dual interlayer.
(32) Combinations of dissimilar metal materials include, for example, stainless steel to titanium, steel to titanium, stainless steel to aluminum, steel to aluminum, aluminum to titanium, tungsten to titanium, tungsten to stainless steel, and tungsten to steel. In these combinations, the stainless steel may be 17-4, 304, 304L, 321, 303, 316, 316L, 420, 425, 425M, 450, 455, 475, or HSR300; the aluminum may be 6061, 6063, or 7075; the titanium may be 6-4, 811, FS2S, FS2S+, SP700, Ti 17, Ti 21, 15-3-3-3; the steel may be C300 maraging steel, 1020, 1025, 1045, 4130, 4140, 4340; and the tungsten may have a density of 10 g/cc to 18 g/cc.
(33) An exemplary golf club head 40 made up of components 51, 53 made of dissimilar materials and assembled using the method described above is illustrated in
(34) In another embodiment of the present invention, a golf club is assembled using the preferred method 100 described above. In this embodiment, the component 51 is a tungsten or tungsten alloy weight piece that is affixed as described above to the body 53 of a golf club head 40.
(35) As shown in
(36) As shown in
(37) Ambient pressure is approximately 760 Torr. A low vacuum has a pressure ranging 760-25 Torr. A medium vacuum has a pressure ranging from 25 to 10.sup.3 Torr. A high vacuum has a pressure ranging from 10.sup.3 to 10.sup.9 Torr. In one embodiment, during a transient liquid phase bonding cycle within a heating apparatus, a reducing environment is created by generating a high vacuum preferably ranging from 10.sup.3 Torr to 10.sup.5 Torr. The reducing environment is created to reduce any oxides created by heating the interlayer material applied to the golf club components.
(38) In one embodiment, the first component is a wood-type golf club face component and the second component is a wood-type golf club body component. The wood-type golf club head has a volume ranging from 200 cubic centimeters to 475 cubic centimeters.
(39) In another embodiment, the first component is an iron-type golf club face component and the second component is an iron-type golf club body component.
(40) In another embodiment, the first component is a face component composed of a titanium alloy, and the second component is a body component composed of a steel material.
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(49) Typical loft angles for irons are set forth in Table One.
(50) TABLE-US-00001 TABLE ONE #1 15 #2 18 #3 21 #4 24 #5 27 #6 30 #7 34 #8 38 #9 42 PW 46 AW 50 SW 55 LW 60
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(52) A method 1900 for joining golf club head components is shown in
(53) A method 2000 for joining golf club head components is shown in
(54) A method 2100 for joining golf club head components is shown in
(55) Aplin et al., U.S. Pat. No. 10,946,255 for Methods Of Manufacturing Golf Club Heads, is hereby incorporated by reference in its entirety.
(56) Seluga et al., U.S. Pat. No. 10,569,146 for a Golf Club Head With Face Dampening And Stress-Reduction Features, is hereby incorporated by reference in its entirety.
(57) Westrum et al., U.S. Pat. No. 11,090,534 for a Golf Club Head Comprising Microscopic Bubble Material, is hereby incorporated by reference in its entirety.
(58) Seluga et al., U.S. Pat. No. 10,213,661 for a Golf Club Head With Tubes Connecting Crown To Elongated Protrusion, is hereby incorporated by reference in its entirety.
(59) Myers et al., U.S. Pat. No. 9,987,527 for an Iron-Type Golf Club Head With Stiffening Rods, is hereby incorporated by reference in its entirety.
(60) Seluga et al., U.S. Pat. No. 10,010,771 for an Iron-Type Golf Club Head With Elevated Weight Bar And Stress-Relieving Structures, is hereby incorporated by reference in its entirety.
(61) Seluga et al., U.S. Pat. No. 10,039,965 for an Iron-Type Golf Club Head With Dampening Features, is hereby incorporated by reference in its entirety.
(62) Ivanova et al., U.S. Pat. No. 9,861,863 for an Iron-Type Golf Club Head With Lightweight Hosel, is hereby incorporated by reference in its entirety.
(63) Westrum, U.S. Pat. No. 9,675,852 for an Iron-Type Golf Club Head, is hereby incorporated by reference in its entirety.
(64) Kim et al., U.S. Pat. No. 9,227,117 for an Adjustable Iron-Type Golf Club Head, is hereby incorporated by reference in its entirety.
(65) Dawson et al., U.S. Pat. No. 9,233,281 for an Iron-Type Golf Club Head, is hereby incorporated by reference in its entirety.
(66) Ivanova et al., U.S. Pat. No. 9,345,937 for an Iron-Type Golf Club Head, is hereby incorporated by reference in its entirety.
(67) Griffin et al., U.S. Pat. No. 9,381,409 for a Multiple Material Iron, is hereby incorporated by reference in its entirety.
(68) Kuhar et al., U.S. Pat. No. 9,381,408 for an Iron-Type Golf Club Head, is hereby incorporated by reference in its entirety.
(69) Dawson et al., U.S. Pat. No. 8,821,313 for an Iron-Type Golf Club Head, is hereby incorporated by reference in its entirety.
(70) Ivanova et al., U.S. Pat. No. 8,911,302 for an Iron-Type Golf Club Head, is hereby incorporated by reference in its entirety.
(71) Itokazu et al., U.S. patent application Ser. No. 18/232,979, filed on Aug. 11, 2023, for a Golf Club Head With Miter Joint For Brazing, is hereby incorporated by reference in its entirety.
(72) Itokazu et al., U.S. patent application Ser. No. 18/232,979, filed on Aug. 11, 2023, for a Golf Club Head With Miter Joint For Brazing, is hereby incorporated by reference in its entirety.
(73) Itokazu et al., U.S. patent application Ser. No. 18/732,424, filed on Jun. 3, 2024, for a Golf Club Head With Miter Joint For Brazing, is hereby incorporated by reference in its entirety.
(74) Power, U.S. patent application Ser. No. 18/240,994, filed on Aug. 31, 2023, for a Method of Co-Brazing Golf Club Components, is hereby incorporated by reference in its entirety.
(75) Power, U.S. patent application Ser. No. 18/238,304, filed on Aug. 25, 2023, for a Method of Brazing Golf Club Components, is hereby incorporated by reference in its entirety.
(76) From the foregoing it is believed that those skilled in the pertinent art will recognize the meritorious advancement of this invention and will readily understand that while the present invention has been described in association with a preferred embodiment thereof, and other embodiments illustrated in the accompanying drawings, numerous changes, modifications and substitutions of equivalents may be made therein without departing from the spirit and scope of this invention which is intended to be unlimited by the foregoing except as may appear in the following appended claims. Therefore, the embodiments of the invention in which an exclusive property or privilege is claimed are defined in the following appended claims.