Co-forged golf club head and method of manufacture
09616304 ยท 2017-04-11
Assignee
Inventors
- Uday V. Deshmukh (Carlsbad, CA, US)
- Ronald K. Hettinger (Oceanside, CA, US)
- Jonathan Hebreo (San Diego, CA, US)
Cpc classification
B21K17/00
PERFORMING OPERATIONS; TRANSPORTING
International classification
Abstract
A co-forged iron type golf club is disclosed. More specifically, the present invention discloses a co-forged iron type golf club with the body portion made out of a first material and at least one weight adjustment portion monolithically encased within the body portion of the co-forged iron type golf club head without the need for secondary attachment or machining operations. The present invention creates of an iron type golf club head from a pre-form billet that already contains two or more materials before the actual forging process resulting in a multi-material golf club head that doesn't require any post manufacturing operations such as machining, welding, swaging, gluing, and the like.
Claims
1. A forged golf club head comprising: a body portion having a striking surface made out of a first material; and at least one weight adjustment portion made out of a second material encased within said body portion; wherein said at least one weight adjustment portion is encased monolithically within said body portion without any secondary attachment operations, and wherein said first material has a first flow stress at a first forging temperature, and said second material has a second flow stress at a second forging temperature; said first flow stress and said second flow stress are substantially the same with one another.
2. The forged golf club head of claim 1, wherein said first forging temperature and said second forging temperature are substantially the same with one another.
3. The forged golf club head of claim 2, wherein said first forging temperature is about 1,200 C., and said second forging temperature is about 1,100 C.
4. The forged golf club head of claim 1, wherein said first flow stress and said second flow stress are different from one another.
5. The forged golf club head of claim 4, wherein said first flow stress is about 10 ksi and said second flow stress is about 12 ksi.
6. The forged golf club head of claim 1, wherein said first material has a first thermal expansion coefficient, and the second material has a second thermal expansion coefficient; wherein said first thermal expansion coefficient is greater than or equal to said second thermal expansion coefficient.
7. The forged golf club head of claim 6, wherein said first thermal expansion coefficient is about 8.0 in/in F., and said second thermal expansion coefficient is about 6.1 in/in F.
8. A forged golf club head comprising: a body portion having a striking surface made out of a first material; and at least one weight adjustment portion made out of a second material encased within said body portion; wherein said at least one weight adjustment portion is encased monolithically within said body portion without any secondary attachment operations, wherein said first material has a first thermal expansion coefficient, and the second material has a second thermal expansion coefficient; said first thermal expansion coefficient is greater than or equal to said second thermal expansion coefficient wherein said first material has a first flow stress at a first forging temperature, and said second material has a second flow stress at a second forging temperature, and wherein said first flow stress and said second flow stress are different from one another.
9. The forged golf club head of claim 8, wherein said first thermal expansion coefficient is about 8.0 in/in F., and said second thermal expansion coefficient is about 6.1 in/in F.
10. The forged golf club head of claim 8, wherein said first flow stress is about 10 ksi and said flow stress is about 12 ksi.
11. The forged golf club head of claim 10, wherein said at least one weight adjustment portion is located near a sole of said golf club head.
12. The forged golf club head of claim 11, wherein said at least one weight adjustment portion is located near a heel portion of said sole of said golf club head.
13. The forged golf club head of claim 12, wherein said at least one weight adjustment portion is located near a toe portion of said sole of said golf club head.
14. The forged golf club head of claim 13, wherein an interface between said body portion and said at least one weight adjustment portion creates an irregular interface.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The foregoing and other features and advantages of the invention will be apparent from the following description of the invention as illustrated in the accompanying drawings. The accompanying drawings, which are incorporated herein and form a part of the specification, further serve to explain the principles of the invention and to enable a person skilled in the pertinent art to make and use the invention.
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DETAILED DESCRIPTION OF THE INVENTION
(7) The following detailed description is of the best currently contemplated modes of carrying out the invention. The description is not to be taken in a limiting sense, but is made merely for the purpose of illustrating the general principles of the invention, since the scope of the invention is best defined by the appended claims.
(8) Various inventive features are described below that can each be used independently of one another or in combination with other features. However, any single inventive feature may not address any or all of the problems discussed above or may only address one of the problems discussed above. Further, one or more of the problems discussed above may not be fully addressed by any of the features described below.
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(10) Before moving onto subsequent figures, it is worthwhile here to emphasize that the current golf club head 100 is created using a forging process and the weights are incorporated without any post finish machining operations. This is an important distinction to establish because the same result of a monolithically encasing a weight adjustment portion is extremely difficult to achieve using alternative manufacturing processes such as casting. Monolithically encased, as referred to in the current patent application, may generally be defined as a having a specific internal component placed inside a separate external component without joints or seams in the finished product. With respect to the current invention, having weight adjustment portions monolithically encased within the body portion 102 of the golf club head 100 may generally refer to the ability to have weight adjustment portions placed inside the body portion 102 of the golf club head without joints or seams that are generally required by post manufacturing processes such as milling, welding, brazing, gluing, or swaging.
(11) It should also be noted here that a weight that is monolithically encased within the current definition of the present invention could potentially have certain aspect of the internal weights exposed in the finish product to illustrate the existence of a weight adjustment portion without departing from the scope and content of the present invention. More specifically, monolithically encased refers to the methodology used to create the ultimate product as described above, and may not necessarily be limited to visually concealing the weight adjustment member.
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(14) Moving onto
(15) Finally,
(16) Although the above discussion regarding the forging of a golf clubs incorporated by reference do a good job describing the actual forging process, it fails to address the additional concerns with the co-forging process of the current invention wherein two different materials are involved in this forging process. More specifically, because a weight adjustment portion 215 is made out of a second material that could be different from the first material used to create remainder of the pre-form billet 201, special care must be taken to ensure that the different materials can be forged together to form a golf club head 200. Hence, in order to select two cohesive materials that are capable of being co-forged together, the first material and the second material may generally have to have very specific material properties requirements with respect to their flow stress and their thermal expansion coefficient. Although it is most preferential for the two materials to have identical material properties yielding in consistency in forging, the usage of identical materials may not offer any weight adjustment benefits required for the basis of the current invention.
(17) First of, in order for metallic materials to have the capabilities of being co-forged together, the respective flow stress' of each of the materials needs to be properly considered. Flow stress of a material, may generally be defined as the instantaneous value of stress require for continued deforming the material (i.e. to keep the metal flowing); and the creation of a cohesive forged component from two different materials will require them to flow at relatively the same speed when subjected to the stresses of the forging process. It is commonly known that the flow stress of a material is generally a function of the yield strength, the flow stress of a material may generally be summed up by Eq. (1) below.
Y.sub.f=Ke.sup.nEq. (1)
wherein
(18) Y.sub.f=Flow Stress (MPa)
(19) K=Strain Coefficient (MPa)
(20) N=Strain Hardening Exponent
(21) In addition to the above equation, it is worthwhile to mention here that the flow stress of a material may not be construed in vacuum, but rather, it is a function of the forging temperature of the material as well. Hence, in a current exemplary embodiment of the present invention, a first flow stress of the first material at its first forging temperate is substantially similar but not identical to the second flow stress of the second material at its second forging temperature; with the first forging temperature and the second forging temperature being substantially similar. More specifically, in a more detailed embodiment, the first material may be 1025 steel having a first flow stress of about 10 ksi (kilo-pound per square inch) at a forging temperature of about 1,200 C., while the second material may a Niobium material having a second flow stress of also about 12 ksi at a forging temperature of about 1,100 C.
(22) Although in the exemplary embodiment of the present invention described above, the first material may be a 1025 steel and the second material may be a Niobium material, various other materials may also be used without departing from the scope and content of the present invention so long as their flow stresses are similar at a similar forging temperature. Alternatively speaking, any two materials may be used in the current co-forging process so long as the second flow stress is no more than 20% greater or no less than 20% lesser than the first flow stress.
(23) As mentioned before, other than flow stress, the thermal expansion coefficient of the first and second materials are also important to the proper co-forging of two distinct materials. More specifically, a first thermal expansion coefficient of the first material may generally need to be greater than or at least equal to the second thermal expansion coefficient of the second material. Because the thermal expansion coefficient also relate to the shrinkage of the material after forging, it is important that the first material that monolithically encases the second material have a higher thermal expansion coefficient to prevent gaps from forming at the interface portion of the materials. In a more detailed embodiment of the present invention, the first material may be 1025 steel having a thermal expansion coefficient of about 8.0 in/in F., while the second material may be Niobium having a second thermal expansion coefficient of about 3.94 in/in F.
(24) It should be noted that although in the above exemplary embodiment the second thermal expansion coefficient is smaller than the first thermal expansion coefficient, the numbers can be identical to achieve perfect mating of the two materials without departing from the scope and content of the present invention. In fact, in one exemplary embodiment of the present invention, it may be preferred for the first material and the second material to have the same thermal expansion coefficient, as excessive shrinkage of the outer material upon the inner material could potentially create additional stresses at the interface portions of the two materials.
(25) Alternatively, in an attempt to provide different weighting characteristics, the second material could be made out of a 6-4 Titanium material to reduce the weight of the weight adjustment portion 215. The Titanium material may generally have a flow stress of about 10 ksi at a forging temperature of about 1,100 C. and a thermal expansion coefficient of about 6.1 in/in F.
(26) Now that the forging process, and the specific concerns involving the co-forging of different materials have been discussed,
(27) Before moving onto a discussion regarding different embodiments of the present invention, it is worthwhile here to note that the exact placement of the weight adjustment portion 215 within the body portion 202 of the golf club head 200 is slightly different in every single different club head, this is the outcome of the current inventive co-forging process involves different materials. More specifically, the exact placement of the weight adjustment portion 215 may differ with each single golf club 200, as the flow stress of the first material and the second material will help determine the final location of the weight adjustment portion 215. In addition to the above, it should be noted that the interface between the weight adjustment portion 215 and the body portion 202 of the golf club head 200 may generally be an irregular interface, with the boundaries jagged to indicate that the entire golf club head 200 has been co-forged. This is dramatically different from a cavity created via a post machining secondary operations such as milling and drilling; which generally have clean bifurcation lines of the two different materials.
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(32) Similar to the methodology described above, the co-forging of the third material within the cavity created within the first material, the third material may generally need to have a third flow stress that is similar with the first flow stress of the first material and a third thermal expansion coefficient less than the first thermal expansion coefficient of the first material. More specifically, in one exemplary embodiment of the present invention, the third material may be a 6-4 Titanium material having a third flow stress of about 10 ksi at a forging temperature of about 1,100 C. and a third thermal expansion coefficient of about 6.1 in/in F.
(33) Although
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(35) More specifically
(36) It is worth noting here that in this current exemplary embodiment, the hosel portion 504 of the golf club head 500 is deliberately made from the conventional first material, as the bending characteristics of the second material used to form the weight adjustment portion 514 may generally not be suitable for the bending requirements of an iron type golf club head 500. More specifically, the third material used to form the weight adjustment portion 514 could be a lightweight iron-aluminum material having a density of less than about 7.10 g/cc, more preferably less than about 7.05 g/cc, and most preferably less than about 7.00 g/cc, all without departing from the scope and content of the present invention. However, numerous other materials can also be used as the third material used to form the weight adjustment portion 514 without departing from the scope and content of the present invention so long as the third material has a density within the range described above.
(37) Other than in the operating example, or unless otherwise expressly specified, all of the numerical ranges, amounts, values and percentages such as those for amounts of materials, moment of inertias, center of gravity locations, loft, draft angles, various performance ratios, and others in the aforementioned portions of the specification may be read as if prefaced by the word about even though the term about may not expressly appear in the value, amount, or range. Accordingly, unless indicated to the contrary, the numerical parameters set forth in the following specification and attached claims are approximations that may vary depending upon the desired properties sought to be obtained by the present invention. At the very least, and not as an attempt to limit the application of the doctrine of equivalents to the scope of the claims, each numerical parameter should at least be construed in light of the number of reported significant digits and by applying ordinary rounding techniques.
(38) Notwithstanding that the numerical ranges and parameters setting forth the broad scope of the invention are approximations, the numerical values set forth in the specific examples are reported as precisely as possible. Any numerical value, however, inherently contains certain errors necessarily resulting form the standard deviation found in their respective testing measurements. Furthermore, when numerical ranges of varying scope are set forth herein, it is contemplated that any combination of these values inclusive of the recited values may be used.
(39) It should be understood, of course, that the foregoing relates to exemplary embodiments of the present invention and that modifications may be made without departing from the spirit and scope of the invention as set forth in the following claims.