Patent Application
20110039636
Not Applicable
1. Field of the Invention
The present invention relates to a wood-type golf club head. More specifically, the present invention relates to a wood-type golf club head with components that have been selectively lightened to reduce mass of the components.
2. Description of the Related Art
The prior art discloses various golf club heads.
Existing wood designs, particularly drivers, generally seek to achieve a reduced structural weight fraction in the shell portion (i.e., sole, crown, ribbon) of the head so additional weight can be available for other design aspects (weighting, styling, etc). Reduced thickness can be achieved by forming and welding high strength titanium sheet stock, but it's difficult to locally and purposefully vary thickness to minimize weight using this construction. Local and purposeful thickness variation is readily achieved using the casting method of construction, but cast titanium is generally lower strength and requires increased overall shell thickness for adequate durability.
Further, the shell portion of the head significantly influences the sound (when struck by a ball). The formed sheet construction method is very limited in affecting sound since features such as local thickening and local webbing (which would influence sound) are not practical with this construction. Such features are readily added to shells made using cast construction, but again, minimum weight is difficult to achieve with this method.
Current wood heads struggle to achieve both minimum structural weight and pleasing sound at impact.
The present invention provides a solution to the problem.
The present invention seeks to achieve a reduced structural weight fraction while also providing a means for affecting sound radiating from the sole and/or crown portions of the shell.
The present invention preferably includes of the introduction of a plurality of small diameter partial holes to the inside surface (IML) of a shell constructed using the sheet formed/welded construction. The holes are partial in that they originate on the IML surface and proceed into, but not thru the thickness of the shell. In other words, these are not “thru-holes.” Being non-thru holes avoids adding complexity to finishing (polishing, painting, etc) of the exterior surface. Also, placing the holes on the interior surface avoids a likely undesirable cosmetic appearance. Also, use of non-thru holes avoids the need to seal the holes for prevention of moisture ingression.
The holes may be patterned in such a manner as to uniformly or locally reduce the effective density of the shell for purposes of achieving minimum structural weight fraction for the shell.
Further, the holes may be patterned in such a way as to uniformly or locally affect the stiffness/mass ration (√k/m) which in turn affects the resonant frequency and sound during impact.
A wood head having a body fabricated using formed sheets of metal which are subsequently welded together. Sole and/or crown and/or ribbon portions of the body contain a plurality on non-thru holes originating from the interior surface of the body.
The wood-type golf club head also preferably includes non-thru holes have a diameter between 0.030″ and 10 microns. The wood-type golf club head also preferably includes non-thru holes penetrate between 50-90% of the local thickness of the shell. The wood-type golf club head also preferably includes non-thru holes are spaced in a pattern such that between 5/25% of the weight of the shell is removed. The wood-type golf club head also preferably includes the method of manufacture of the holes may include drilling, milling, punching, forming, forging, chemical etching, photo etching, water jet and laser.
The wood-type golf club head also preferably includes a secondary machining operation is required to re-flatten the side of the sheet w/o holes (ie fly cut). The wood-type golf club head also preferably includes the non-thru holes are applied to the sheet material in the flat state prior to forming in the general shape of the shell.
A pattern of holes are applied to the interior surface of the crown and/or sole portion of the head. The holes are non-thru holes and are not noticeable from the exterior surface of the head. The holes may be located and patterned (spaced) such that they result in reduced shell weight such that they positively affect the resonant response of the shell during impact and thus affect sound.
A wood with a selectively lightened shell by means of addition of a plurality of non-thru holes added to the interior surface of the body for purpose of weight reduction and/or sound refinement.
A driver head having a body fabricated using formed sheets of titanium which are subsequently welded together. Sole and/or crown and/or ribbon portions of the body contain a plurality of non-thru holes originating from the interior surface of the body.
Preformed construction is formed/molded sheet i.e., “multi-piece” construction.
Having briefly described the present invention, the above and further objects, features and advantages thereof will be recognized by those skilled in the pertinent art from the following detailed description of the invention when taken in conjunction with the accompanying drawings.
As shown in
The major body 50 is generally composed of a single piece of metal, and is preferably composed of a cast metal material. More preferably, the cast metal material is a stainless steel material or a titanium material such as pure titanium and titanium alloys such as 6-4 titanium alloy, SP-700 titanium alloy (available from Nippon Steel of Tokyo, Japan), DAT 55G titanium alloy available from Diado Steel of Tokyo, Japan, Ti 10-2-3 Beta-C titanium alloy available from RTI International Metals of Ohio, and the like. Alternatively, the major body may be manufactured through forging, welding, forming, machining, powdered metal forming, metal-injection-molding, electro-chemical milling, and the like.
The major body 50 generally includes a front wall section 72, a return section 74 extending laterally rearward from the upper perimeter of the front wall section 72, a sole section 76 extending laterally rearward from the front wall section 72, a ribbon section 78 extending upward from the sole section 76, and a ledge section 80 stepped inward for attachment of the minor body 60. The front wall section 72 has an opening for placement of the striking plate insert 55 therein.
The return section 74 extends inward, towards the minor body 60, and has a general curvature from the heel end 66 to the toe end 68. The return section 74 has a length from the perimeter 73 of the front wall section 72 that is preferably a minimal length near the center of the front wall section 72, and increases toward the toe end 68 and the heel end 66. A distance d represents the length of the return section 74 from the perimeter 73 at the center of the front wall section 72, a distance d′ from the perimeter 73 at the heel end 66 of the front wall section 72, and a distance d″ from the perimeter 73 at the toe end 68 of the front wall section 72. In a preferred embodiment, the distance d ranges from 0.2 inch to 1.5 inches, more preferably 0.30 inch to 1.25 inches, and most preferably from 0.60 inch to 1.0 inch, as measured from the perimeter 73 of the front wall section 72 to the rearward edge of the return section 74. In a preferred embodiment, the distance d′ ranges from 0.4 inch to 2.00 inches, more preferably 0.50 inch to 1.75 inches, and most preferably from 0.8 inch to 1.50 inches, as measured from the perimeter 73 of the front wall section 72 to the rearward edge of the return section 74. In a preferred embodiment, the distance d″ ranges from 0.4 inch to 2.25 inches, more preferably 0.50 inch to 2.00 inches, and most preferably from 0.9 inch to 1.50 inches, as measured from the perimeter 73 of the front wall section 72 to the rearward edge of the return section 74.
The perimeter 73 of the front wall section 72 is defined as the transition point where the major body 50 transitions from a plane substantially parallel to the front wall section 72 to a plane substantially perpendicular to the front wall section 72. Alternatively, one method for determining the transition point is to take a plane parallel to the front wall section 72 and a plane perpendicular to the front wall section 72, and then take a plane at an angle of forty-five degrees to the parallel plane and the perpendicular plane. Where the forty-five degrees plane contacts the major body 50 is the transition point thereby defining the perimeter 73 of the front wall section 72.
The golf club head 40 has striking plate insert 55 that is attached to the major body 50 over the opening 32 of the front wall 72. The striking plate insert 55 is preferably composed of a formed titanium alloy material. Such titanium materials include titanium alloys such as 6-22-22 titanium alloy and Ti 10-2-3 alloy, Beta-C titanium alloy, all available from RTI International Metals of Ohio, SP-700 titanium alloy (available from Nippon Steel of Tokyo, Japan), DAT 55G titanium alloy available from Diado Steel of Tokyo, Japan, and like materials. The preferred material for the striking plate insert 55 is a heat treated 6-22-22 titanium alloy which is a titanium alloy composed by weight of titanium, 6% aluminum, 2% tin, 2% chromium, 2% molybdenum, 2% zirconium and 0.23% silicon. The titanium alloy will have an alpha phase in excess of 40% of the overall microstructure. As shown in
As shown in
The minor body 60 is preferably composed of a low density material, preferably a metal or a polymer material. Preferably metals include magnesium alloys, aluminum alloys, magnesium or aluminum material. Exemplary magnesium alloys are available from Phillips Plastics Corporation under the brands AZ-91-D (nominal composition of magnesium with aluminum, zinc and manganese), AM-60-B (nominal composition of magnesium with aluminum and manganese) and AM-50-A (nominal composition of magnesium with aluminum and manganese). If metal, the minor body 60 is preferably manufactured through metal-injection-molding, casting, forming, machining, powdered metal forming, electro chemical milling, and the like.
The mass of the club head 40 of the present invention ranges from 165 grams to 250 grams, preferably ranges from 175 grams to 230 grams, and most preferably from 190 grams to 205 grams. Preferably, the major body 50 has a mass ranging from 140 grams to 200 grams, more preferably ranging from 150 grams to 180 grams, yet more preferably from 155 grams to 166 grams, and most preferably 161 grams. The minor body 60 has a mass preferably ranging from 4 grams to 20 grams, more preferably from 5 grams to 15 grams, and most preferably 7 grams. Each stiffening member 122 has a mass preferably ranging from 1 gram to 50 grams, more preferably from 5 grams to 25 grams, and most preferably 10 grams. Additionally, epoxy, or other like flowable materials, in an amount ranging from 0.5 grams to 5 grams, may be injected into the hollow interior 46 of the golf club head 40 for selective weighting thereof. The golf club head preferably has a coefficient of restitution a (“COR”) ranging from 0.81 to 0.875, and more preferably from 0.82 to 0.84. The golf club head preferably has a characteristic time (“CT”) as measured under USGA conditions of 256 microseconds.
The golf club head 40 preferably has that ranges from 290 cubic centimeters to 600 cubic centimeters, and more preferably ranges from 330 cubic centimeters to 510 cubic centimeters, even more preferably 350 cubic centimeters to 495 cubic centimeters, and most preferably 415 cubic centimeters or 460 cubic centimeters.
As defined in Golf Club Design, Fitting, Alteration & Repair, 4th Edition, by Ralph Maltby, the center of gravity, or center of mass, of the golf club head is a point inside of the club head determined by the vertical intersection of two or more points where the club head balances when suspended. A more thorough explanation of this definition of the center of gravity is provided in Golf Club Design, Fitting, Alteration & Repair.
The center of gravity and the moment of inertia of a golf club head 40 are preferably measured using a test frame (XT, YT, ZT), and then transformed to a head frame (XH, YH, ZH) The center of gravity of a golf club head may be obtained using a center of gravity table having two weight scales thereon, as disclosed in U.S. Pat. No. 6,607,452, entitled High Moment Of Inertia Composite Golf Club, and hereby incorporated by reference in its entirety.
In general, the moment of inertia, Izz, about the Z axis for the golf club head 40 preferably ranges from 2800 g-cm2 to 5000 g-cm2, preferably from 3000 g-cm2 to 4500 g-cm2, and most preferably from 3750 g-cm2 to 4250 g-cm2. The moment of inertia, Iyy, about the Y axis for the golf club head 40 preferably ranges from 1500 g-cm2 to 4000 g-cm2, preferably from 2000 g-cm2 to 3500 g-cm2, and most preferably from 2400 g-cm2 to 2900 g-cm2. The moment of inertia, Ixx, about the X axis for the golf club head 40 preferably ranges from 1500 g-cm2 to 4000 g-cm2, preferably from 2000 g-cm2 to 3500 g-cm2, and most preferably from 2500 g-cm2 to 3000 g-cm2.
In general, the golf club head 40 has products of inertia such as disclosed in U.S. Pat. No. 6,425,832, and is hereby incorporated by reference in its entirety. Preferably, each of the products of inertia, Ixy, Ixz and Iyz, of the golf club head 40 have an absolute value less than 100 grams-centimeter squared. Alternatively, the golf club head 40 has a at least one or two products of inertia, Ixy, Ixz and Iyz, with an absolute value less than 100 grams-centimeter squared.
As shown in
Those skilled in the pertinent art will recognize that other types of golf club heads can be utilized with the present invention, such as cast body two piece golf club heads with a body and attachable striking plate, sole or crown, a multiple-piece construction golf club heads composed of four or more pieces.
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.
The Present Application claims priority upon U.S. Provisional Application No. 61/234,384 filed on Aug. 17, 2009.
| Number | Date | Country | |
|---|---|---|---|
| 61234384 | Aug 2009 | US |
