Patent Application
20230087352
The present invention relates generally to golf balls including a mark, or a plurality of marks, for improving the detection and tracking thereof by radar tracking systems.
Interest continues to increase in golf experiences which require a system for detecting golf ball launch conditions, such as golf simulators and golf equipment fitting. Radar tracking systems that are currently used for this purpose are limited, however, in their ability to accurately obtain launch condition data, for example, ball spin properties.
There are also disadvantages to the use of the radar reflective stickers that are commonly used with radar tracking systems. Radar reflective stickers are typically placed on the outer surface of the golf ball in order for radar tracking systems to obtain launch condition data. However, there are challenges associated with the use of these stickers, including, for example, accurate positioning of the stickers on the ball, alignment of the stickers relative to the golfer and tee, time and effort required to place the stickers on the ball, and lack of durability of the stickers, which further leads to a decrease in the quality of launch condition data and the need to replace the stickers.
Thus, there is a need for a golf ball that provides one or more of the following benefits: improved quality of golf ball launch condition data collected by radar tracking systems, and enhanced experience for the end users of these radar tracking systems.
The present invention is directed to a golf ball comprising at least one layer with a mark, or a plurality of marks, disposed on a surface thereof.
In a particular embodiment, the mark has a continuous shape and is formed from a radar detectable material. In a particular aspect of this embodiment, the golf ball additionally has one or more of the following properties:
In another particular embodiment, the mark is formed from a radar detectable material and has dimensions such that every great circle path on the golf ball layer surface on which the mark is disposed intersects the mark.
In another particular embodiment, the mark is formed from a radar detectable material and has a continuous shape comprising three or more intersecting stripes.
In another particular embodiment, the at least one layer has a plurality of radar detectable marks disposed on a surface thereof. In a particular aspect of this embodiment, the radar detectable marks have a resistivity of from 0.1 Ohms to 25 Ohms. In another particular aspect of this embodiment, every 0.025 inch wide great circle path on the golf ball layer surface on which the radar detectable marks are disposed intersects at least one of the marks. In another particular aspect of this embodiment, every great circle path on the golf ball layer surface on which the radar detectable marks are disposed intersects at least one of the marks. In another particular aspect of this embodiment, the plurality of radar detectable marks includes a first mark and a second mark, wherein the first mark has a continuous, irregular shape and the second mark has a basic shape selected from basic nonpolygonal shapes, regular polygons, and irregular polygons. Non-limiting examples of suitable basic nonpolygonal shapes include circles, rings, and crescents. Non-limiting examples of suitable regular polygons include squares and equilateral triangles. Non-limiting examples of suitable irregular polygons include rectangles, non-equilateral triangles, and chevrons. In another particular aspect of this embodiment, the plurality of radar detectable marks includes a first mark and a second mark, wherein the first mark has a continuous, irregular shape comprising a plurality of intersecting stripes, and the second mark has an irregular shape that is different from the first mark. In another particular aspect of this embodiment, the plurality of radar detectable marks includes a third mark, the third mark having either an irregular shape or a regular shape. In another particular aspect of this embodiment, when all of the radar detectable marks present on any layer of the ball are radially projected onto the outer surface of the ball, the radar detectable marks have a total surface coverage of from 1% to 20%.
In another particular embodiment, the golf ball comprises two or more layers, wherein at least two of the two or more layers have one or more radar detectable marks disposed on a surface thereof. When all of the radar detectable marks present on any layer of the ball are radially projected onto the outer surface of the ball, every 0.025 inch wide great circle path on the golf ball outer surface intersects at least one of the marks.
In another particular embodiment, the golf ball has a plurality of radar detectable marks disposed on a single layer thereof. The plurality of radar detectable marks includes at least eleven equally-spaced, non-circular-shaped marks. In a particular aspect of this embodiment, the number of equally-spaced, non-circular-shaped marks is a prime number from 11 to 37.
In another particular embodiment, the golf ball has a plurality of radar detectable marks disposed among two or more layers thereof. The plurality of radar detectable marks includes at least eleven non-circular-shaped marks. When all of the radar detectable marks present on any layer of the ball are radially projected onto the outer surface of the ball, the radar detectable marks are equally spaced. In a particular aspect of this embodiment, the number of equally-spaced, non-circular-shaped marks is a prime number from 11 to 37.
In another particular embodiment, the total surface coverage of all radar detectable marks present is from 0.1% to 4.0%. In a particular aspect of this embodiment, the golf ball has a layer with a radar detectable mark disposed on a surface thereof, and the mark has a continuous non-circular shape and a surface coverage of from 0.1% to 4.0%. In another particular aspect of this embodiment, the golf ball has a plurality of radar detectable marks disposed among two or more surfaces thereof, and, when all of the radar detectable marks present on any surface of any layer of the ball are radially projected onto the outer surface of the ball, the radar detectable marks have an overall continuous non-circular shape. In another particular aspect of this embodiment, the golf ball has one or more radar detectable marks disposed on a surface of at least one layer thereof, the total number of radar detectable marks present is two or more, and the radar detectable marks have a total surface coverage of from 0.1% to 4.0%.
In another particular embodiment, the golf ball has a plurality of radar detectable marks disposed on any single layer or among two or more layers thereof. When all of the radar detectable marks present on any layer of the ball are radially projected onto the outer surface of the ball, the resulting overall pattern of projected radar detectable marks comprises a series of three or more marks where each mark in the series has a geometric center located on a 1.5 mm wide great circle band on the outer surface of the ball. In a particular aspect of this embodiment, the overall pattern of projected marks consists essentially of the plurality of marks positioned along the great circle. In a further particular aspect of this embodiment, the portion of the great circle along which the plurality of marks are positioned has a length of no more than half the circumference of the ball.
In another particular embodiment, the golf ball has a plurality of radar detectable marks disposed on any single layer or among two or more layers thereof. When all of the radar detectable marks present on any layer of the ball are radially projected onto the outer surface of the ball, the resulting overall pattern of projected radar detectable marks comprises a first great circle series of three or more marks, where each mark in the series has a geometric center located on a first 1.5 mm wide great circle band on the outer surface of the ball, and a second great circle series of three or more marks, where each mark in the series has a geometric center located on a second 1.5 mm wide great circle band on the outer surface of the ball.
In the accompanying drawings, which form a part of the specification and are to be read in conjunction therewith, and in which like reference numerals are used to indicate like parts in the various views:
Golf balls of the present invention include one or more layers which have at least one radar detectable mark disposed on a surface thereof. Particularly suitable radar detectable materials for forming the mark include, but are not limited to, electrically conductive inks comprising a base resin and an electrically conductive material. The ink may be water-borne or solvent-borne. The ink may be a 1-component or 2-component ink. The ink may be cured with an isocyanate-based curing agent, UV cure, and/or thermal cure. The ink and the mark formed therefrom may be transparent or opaque. In a particular embodiment, the base resin of the ink is selected from the group consisting of vinyl polymers, urethane polymers, acrylic polymers, epoxy polymers, and combinations of two or more thereof. In another particular embodiment, the electrically conductive material of the ink is selected from the group consisting of silver, conductive carbon, aluminum, graphene, nanotubes, nanometals, and combinations of two or more thereof. Particularly suitable inks are those capable of producing a mark having a resistivity of 0.1 Ohms or 0.5 Ohms or 1 Ohm or 5 Ohms or 6 Ohms or 7 Ohms or 25 Ohms or 2,500 Ohms, or a resistivity within a range having a lower limit and an upper limit selected from these values. Non-limiting examples of suitable commercially available inks are Ink Lab 303 silver conductive ink, commercially available from ITW Trans Tech; silver inks, conductive carbon inks, aluminum inks, silver/carbon blend inks, and aluminum/carbon blend inks, commercially available from Creative Materials Inc. In embodiments of the present invention wherein the golf ball includes more than one radar detectable mark on a single layer, the radar detectable material used to form one mark may be the same as or different from the radar detectable material used to form another mark. In embodiments of the present invention wherein the golf ball includes at least two layers having one or more radar detectable marks disposed on a surface thereof, the radar detectable material used to form a mark on one layer may be the same as or different from the radar detectable material used to form a mark on another layer.
Radar detectable material is applied to the surface of a layer using any suitable technique. In a particular embodiment, a mark is formed by applying radar detectable material to a surface of a golf ball layer by pad printing. In a particular aspect of this embodiment, the pad printed mark has a film thickness of at least 0.5 μm, or a film thickness of 5 μm or less, or a film thickness within a range having a lower limit and an upper limit selected from 0.5 μm, 1 μm, 3 μm, 4 μm, and 5 μm.
The surface on which one or more radar detectable marks are disposed can be any surface of any layer of a golf ball having any number of layers. While the invention is not meant to be limited to the placement of one or more marks on the surface of a particular layer, golf balls of the present invention are designed to allow for the optional placement of radar detectable marks on a surface other than the outer surface of the ball because it is beneficial to some golfers to be able to obtain reliable launch condition data using a golf ball that looks the same on the outside as a conventional golf ball. Thus, in a particular embodiment, one or more radar detectable marks are disposed on any surface of any layer of the golf ball other than the outermost surface.
In another particular embodiment, the golf ball is a solid, one-piece golf ball, and one or more radar detectable marks are disposed on the outer surface of the ball.
In another particular embodiment, the golf ball is a two-piece golf ball consisting of an inner core layer and an outer cover layer, and one or more radar detectable marks are disposed on:
In another particular embodiment, the golf ball is a three-piece golf ball consisting of an inner core layer, an outer cover layer, and an intermediate layer disposed between the inner core layer and the outer cover layer, and one or more radar detectable marks are disposed on:
In another particular embodiment, the golf ball is a four-piece golf ball consisting of an inner core layer, a first intermediate layer, a second intermediate layer, and an outer cover layer, and one or more radar detectable marks are disposed on:
In another particular embodiment, the golf ball is a five- or more piece golf ball comprising an inner core layer, a first intermediate layer, a second intermediate layer, a third intermediate layer, optional additional intermediate layers, and an outer cover layer, and one or more radar detectable marks are disposed on:
For purposes of the present disclosure, the number of pieces/layers of a golf ball does not include any optional coatings, such as paint coatings, finish coatings, adhesive coatings, etc., even if the coating covers an entire surface of a golf ball layer. Such coatings have a thickness that is substantially less than conventional golf ball layer thicknesses, and are generally not considered by those of ordinary skill in the art to be “golf ball layers” when reference is made to a one-piece/one-layer golf ball, two-piece/two-layer golf ball, three-piece/three-layer golf ball, and so on, despite sometimes being referred to as an adhesive layer, a paint layer, a top coat layer, etc. Thus, a two-piece golf ball consisting of an inner core layer and an outer cover layer, for example, may additionally include one or more coatings.
Also, for purposes of the present disclosure, a mark is considered to be disposed on the surface of a layer regardless of whether a coating has previously been applied to the surface. In other words, if an adhesive coating is applied to a surface of a layer, and a mark is then applied on top of the adhesive coating, the mark is considered to be disposed on the surface of the layer, even though an adhesive coating is present therebetween. Likewise, if a coating is present between two layers of the ball, the layers are still considered to be adjacent to each other, even though a coating may be present therebetween.
In a particular embodiment, golf balls of the invention include an adhesive coating applied to a layer on which at least one radar detectable mark is disposed, before and/or after application of the mark(s) onto the layer. In a particular aspect of this embodiment, at least one mark is disposed on a surface of a golf ball layer and an adhesive coating is applied to the layer and on top of the mark(s). In another particular aspect of this embodiment, an adhesive coating is applied to a surface of a golf ball layer and at least one mark is disposed on the layer on top of the adhesive coating. In another particular aspect of this embodiment, a first adhesive coating is applied to a surface of a golf ball layer, at least one mark is disposed on the layer on top of the adhesive coating, and a second adhesive coating is applied to the layer and on top of the mark(s).
Each radar detectable mark has a shape selected from a variety of suitable shapes, including regular shapes and irregular shapes. Suitable examples of regular shapes include, but are not limited to, circles, rings, crescents, squares, triangles, rectangles (also referred to herein as rectangular stripes), chevrons, and other regular polygons, irregular polygons, and basic nonpolygonal shapes. Suitable examples of irregular shapes include, but are not limited to, intersecting shapes, including, but not limited to, a series of intersecting stripes, other than chevrons (which are considered a regular shape despite consisting of two intersecting stripes), wherein the length and width of each stripe within the series of intersecting stripes may be different than or substantially the same as that of the other stripe(s) within the series. For purposes of the present disclosure, stripes have substantially the same length and/or width if their respective lengths and/or widths differ by no more than 10%. For purposes of the present disclosure, a “stripe” may be a rectangular stripe (i.e., wherein each of the four boundary lines defining the stripe is a straight line and wherein adjacent sides meet at right angles) or a non-rectangular stripe (i.e., wherein at least one of the four boundary lines defining the stripe is not a straight line or wherein adjacent sides meet at an angle other than a right angle, or both). Because the radar detectable marks are present on the surface of a spherical golf ball layer, it should be understood, for example, that the “straight line” boundary lines of a mark having the shape of a rectangular stripe are formed by drawing straight lines on a sphere, and, therefore, in a purely mathematical sense, are present on a golf ball layer as arcs. Additionally, for purpose of the present disclosure, stripes on a single layer are considered to intersect if they meet at one or more locations on the layer, regardless of whether or not one or more of the stripes continues past the point of intersection. Similarly, for purposes of the present disclosure, stripes that are disposed between two or more layers are considered to intersect if, when the stripes are radially projected onto the outer surface of the ball, they meet at one or more locations on the outer surface of the ball, regardless of whether or not one or more of the stripes continues past the point of intersection.
In a particular embodiment, the golf ball includes at least one radar detectable mark having an irregular shape defined by a series of intersecting rectangular stripes. In a particular aspect of this embodiment, the mark having an irregular shape additionally has one or more of the following properties:
In another particular embodiment, the golf ball includes at least eleven radar detectable marks. In a particular aspect of this embodiment, each of the at least eleven radar detectable marks has a non-circular shape independently selected from rings, ellipses, polygons, squares, chevrons, crescents, and stripes. In another particular aspect of this embodiment, the radar detectable marks are equally spaced. In another particular aspect of this embodiment, the radar detectable marks additionally have one or more of the following properties:
In another particular aspect of this embodiment, the centroid of each of the radar detectable marks is positioned at a vertex of one of a plurality of spherical triangles created from a plurality of great circle arcs, wherein:
2V−4=T
3T/2=E
T−E+V=2
where E is the total number of great circle arcs, T is the total number of spherical triangles, and V is the total number of vertices. The total surface area, A, of the spherical triangles is calculated as 4πr2/T=A. The position of the centroids of the radar detectable marks is determined with all of the marks present on the surface of any layer of the golf ball radially projected onto the outer surface of the ball.
For purposes of the present disclosure, marks on a layer are “equally spaced” if, when the distances between the centroid of each mark and the centroid of its adjacent marks is calculated, the maximum difference between any two of these distances is 0.040 inches or less. In embodiments of the present invention wherein the radar detectable marks are disposed among two or more layers of the golf ball, in order to determine if all of the radar detectable marks present on the ball are equally spaced, all of the radar detectable marks present on any layer of the ball are radially projected onto the outer surface of the ball.
In another particular embodiment, the golf ball includes a radar detectable mark having a continuous non-circular shape and a surface coverage of from 0.1% to 4.0%, or from 0.1% to 3.0%. The mark can be disposed on a single surface of a single layer of the ball; or, the mark can be disposed among two or more surfaces of the ball (i.e., the inner and outer surface of a single layer or any surface of two or more layers), such that, when all of the radar detectable marks present on any surface of any layer of the ball are radially projected onto the outer surface of the ball, the result is a projected mark having an overall continuous non-circular shape and a surface coverage of from 0.1% to 4.0%. In a particular aspect of this embodiment, the non-circular shape is independently selected from rings, ellipses, polygons, squares, crescents, stripes, two intersecting stripes (including chevrons and non-chevron shapes), and three or more intersecting stripes. In another particular aspect of this embodiment, the mark (or projected mark), is a continuous shape comprising two or more intersecting stripes, including a first stripe and a second stripe, and, optionally, has one or more of the following properties:
In another particular embodiment, the golf ball includes a plurality of radar detectable marks, and the total surface coverage of the radar detectable marks is from 0.1% to 4.0%, or from 0.1% to 3.0%. In a particular aspect of this embodiment, each of the radar detectable marks has a non-circular shape, and, optionally, each non-circular shape is independently selected from rings, ellipses, polygons, squares, crescents, chevrons, and stripes. In another particular aspect of this embodiment, the plurality of radar detectable marks comprises two or more non-intersecting stripes, including a first stripe and a second stripe, and, optionally, has one or more of the following properties:
In another particular embodiment, the golf ball includes a plurality of radar detectable marks wherein, when all of the radar detectable marks present on any layer of the ball are radially projected onto the outer surface of the ball, the resulting overall pattern of projected radar detectable marks includes at least one series of three or more radar detectable marks located on a 1.5 mm wide great circle band on the outer surface of the golf ball. For purposes of the present disclosure, a series of three or more radar detectable marks in the overall pattern of projected radar detectable marks, located on a 1.5 mm wide great circle band on the outer surface of the ball, is referred to herein as a “great circle series” of marks. For purposes of the present disclosure, the presence and number of great circle series within an overall pattern of projected radar detectable marks is determined as follows. First, as previously stated, all of the radar detectable marks present on any layer of the ball are radially projected onto the outer surface of the ball. The geometric center of each radially projected radar detectable mark is then determined using calculation methods well known to those of ordinary skill in the art. If the geometric centers of at least three radially projected radar detectable marks are located on the same 1.5 mm wide great circle band on the outer surface of the ball, then a great circle series is defined and each radially projected radar detectable mark having a geometric center located on that 1.5 mm wide great circle band is part of that great circle series. It should be noted that, so long as the geometric center of a given radially projected radar detectable mark is located on the 1.5 mm wide great circle band, the mark is part of that great circle series, regardless of whether any portion of the mark lies outside of the 1.5 mm wide great circle band defining that series. It should also be noted that, for purposes of the present disclosure, a single radar detectable mark can be part of more than one great circle series. In a particular aspect of this embodiment, the plurality of radar detectable marks additionally has one or more of the following properties:
For purposes of the present disclosure, unless otherwise noted, the length of the portion of the great circle band on which the marks of a given great circle series are located is calculated as the length of the smallest rectangular boundary (i.e., the arc length of the longest edge of the rectangular boundary) that can be drawn on the outer surface of the ball such that no portion of any mark of that great circle series lies outside of the boundary, as determined based on the radial projection of the marks onto the outer surface of the ball.
In another particular embodiment, the golf ball includes a plurality of radar detectable marks wherein, when all of the radar detectable marks present on any layer of the ball are radially projected onto the outer surface of the ball, the resulting overall pattern of projected radar detectable marks includes at least two great circle series of marks. In a particular aspect of this embodiment, each of the plurality of radar detectable marks is part of at least one great circle series. In another particular aspect of this embodiment, the plurality of radar detectable marks includes at least one mark that is not part of a great circle series. In another particular aspect of this embodiment, for at least one great circle series, the portion of the great circle band on which the marks of that great circle series are located has a length of no more than half of the circumference of the ball; optionally, the length is at least 40%, or at least 42%, or at least 45% of the circumference of the ball. In another particular aspect of this embodiment, for at least one great circle series, the portion of the great circle band on which the marks of that great circle series are located has a length of greater than half of the circumference of the ball. In another particular aspect of this embodiment, a plane bisecting one of the at least two great circle series and a plane bisecting another of the at least two great circle series are separated by an angle of 30° or 60° or 80° or 90° or an angle within a range having a lower limit and an upper limit selected from these values, as determined based on the radial projection of the marks onto the outer surface of the ball. In another particular aspect of this embodiment, when all of the radar detectable marks present on any layer of the ball are radially projected onto the outer surface of the ball, every great circle on the outer surface of the ball divides the ball into two hemispheres, each of the two hemispheres containing at least a portion of a radar detectable mark on the outer surface thereof. In another particular aspect of this embodiment, each great circle series of marks independently has one or more of the following additional properties:
In embodiments of the present invention wherein the golf ball includes more than one radar detectable mark on a single layer, the shape and/or size of one mark may be the same as or different from the shape and/or size of another mark. In embodiments of the present invention wherein the golf ball includes at least two layers having one or more radar detectable marks disposed on a surface thereof, the shape and/or size of a mark on one layer may be the same as or different from the shape and/or size of a mark on another layer. In embodiments of the present invention wherein the golf ball includes radar detectable marks that are part of a great circle series, the shape and/or size of one mark in the series may be the same as or different from the shape and/or size of another mark in the series. In a particular embodiment, the golf ball includes at least one radar detectable mark that has a non-circular shape disposed on a surface of a layer thereof. In a particular aspect of this embodiment, the non-circular shape is an irregular shape.
Non-limiting examples of particularly suitable shapes for a single radar detectable mark or a plurality of radar detectable marks are illustrated in
In a particular embodiment, a surface of at least one layer of the golf ball includes a radar detectable mark disposed thereon and the mark is designed to have dimensions (i.e., size and shape) such that every mathematically possible 0.025 inch wide great circle path, or every mathematically possible 0.015 inch wide great circle path, or every mathematically possible 0.005 inch wide great circle path, or every mathematically possible great circle, on the golf ball layer surface on which the mark is disposed intersects the mark. For purposes of the present disclosure, a great circle path intersects a mark if any portion of the great circle path is in contact with any portion of the mark.
In another particular embodiment, a surface of at least one layer of the golf ball includes a plurality of radar detectable marks disposed thereon and the marks are designed to be sized, shaped, and positioned such that every mathematically possible 0.025 inch wide great circle path, or every mathematically possible 0.015 inch wide great circle path, or every mathematically possible 0.005 inch wide great circle path, or every mathematically possible great circle, on the golf ball layer surface on which the marks are disposed intersects at least one of the marks.
In another particular embodiment, the golf ball comprises two or more layers, wherein at least two of the two or more layers have one or more radar detectable marks disposed on a surface thereof and the marks are designed to be size, shaped, and positioned such that, when all of the radar detectable marks present on any layer of the ball are radially projected onto the outer surface of the ball, every mathematically possible 0.025 inch wide great circle path, or every mathematically possible 0.015 inch wide great circle path, or every mathematically possible 0.005 inch wide great circle path, or every mathematically possible great circle, on the golf ball outer surface intersects at least one of the marks.
In another particular embodiment, the radar detectable mark(s) have a total surface coverage of 1% or 2% or 5% or 8% or 9% or 10% or 12% or 15% or 20% or 25% or a total surface coverage within a range having a lower limit and an upper limit selected from these values. Alternatively, in another particular embodiment, the radar detectable mark(s) have a total surface coverage of 0.1% or 1.0% or 1.5% or 2.0% or 3% or 4% or a total surface coverage within a range having a lower limit and an upper limit selected from these values. For purposes of the present disclosure, total surface coverage is calculated as the sum of the surface area of each radar detectable mark present on any layer, as measured with all of the marks present on the surface of any layer of the golf ball radially projected onto the outer surface of the ball, divided by the total surface area of the outer surface of the ball.
The present invention is not meant to be limited by the material used to form each layer of the golf ball. Particularly suitable materials include, but are not limited to, thermosetting materials, such as polybutadiene, styrene butadiene, isoprene, polyisoprene, and trans-isoprene; thermoplastics, such as ionomer resins, polyamides and polyesters; and thermoplastic and thermosetting polyurethane and polyureas.
Particularly suitable thermosetting materials, include, but are not limited to, thermosetting rubber compositions comprising a base polymer, an initiator agent, a coagent and/or a curing agent, and optionally one or more of a metal oxide, metal fatty acid or fatty acid, antioxidant, soft and fast agent, fillers, and additives. Suitable base polymers include natural and synthetic rubbers including, but not limited to, polybutadiene, polyisoprene, ethylene propylene rubber (“EPR”), styrene-butadiene rubber, styrenic block copolymer rubbers (such as SI, SIS, SB, SBS, SIBS, and the like, where “S” is styrene, “I” is isobutylene, and “B” is butadiene), butyl rubber, halobutyl rubber, polystyrene elastomers, polyethylene elastomers, polyurethane elastomers, polyurea elastomers, metallocene-catalyzed elastomers and plastomers, copolymers of isobutylene and para-alkylstyrene, halogenated copolymers of isobutylene and para-alkylstyrene, acrylonitrile butadiene rubber, polychloroprene, alkyl acrylate rubber, chlorinated isoprene rubber, acrylonitrile chlorinated isoprene rubber, polyalkenamers, and combinations of two or more thereof. Suitable initiator agents include organic peroxides, high energy radiation sources capable of generating free radicals, C—C initiators, and combinations thereof. Suitable coagents include, but are not limited to, metal salts of unsaturated carboxylic acids; unsaturated vinyl compounds and polyfunctional monomers (e.g., trimethylolpropane trimethacrylate); phenylene bismaleimide; and combinations thereof. Suitable curing agents include, but are not limited to, sulfur; N-oxydiethylene 2-benzothiazole sulfenamide; N,N-di-ortho-tolylguanidine; bismuth dimethyldithiocarbamate; N-cyclohexyl 2-benzothiazole sulfenamide; N,N-diphenylguanidine; 4-morpholinyl-2-benzothiazole disulfide; dipentamethylenethiuram hexasulfide; thiuram disulfides; mercaptobenzothiazoles; sulfenamides; dithiocarbamates; thiuram sulfides; guanidines; thioureas; xanthates; dithiophosphates; aldehyde-amines; dibenzothiazyl disulfide; tetraethylthiuram disulfide; tetrabutylthiuram disulfide; and combinations thereof. Suitable types and amounts of base polymer, initiator agent, coagent, filler, and additives are more fully described in, for example, U.S. Pat. Nos. 6,566,483, 6,695,718, 6,939,907, 7,041,721 and 7,138,460, the entire disclosures of which are hereby incorporated herein by reference. Particularly suitable diene rubber compositions are further disclosed, for example, in U.S. Patent Application Publication No. 2007/0093318, the entire disclosure of which is hereby incorporated herein by reference.
Particularly suitable materials also include, but are not limited to:
Compositions comprising an ionomer or a blend of two or more E/X- and E/X/Y-type ionomers are particularly suitable intermediate and cover layer materials. Preferred E/X- and E/X/Y-type ionomeric cover compositions include:
Surlyn 8150®, Surlyn® 8940, and Surlyn® 8140 are different grades of E/MAA copolymer in which the acid groups have been partially neutralized with sodium ions. Surlyn® 9650, Surlyn® 9910, and Surlyn® 9120 are different grades of E/MAA copolymer in which the acid groups have been partially neutralized with zinc ions. Surlyn® 7940 is an E/MAA copolymer in which the acid groups have been partially neutralized with lithium ions. Surlyn® 6320 is a very low modulus magnesium ionomer with a medium acid content. Nucrel® 960 is an E/MAA copolymer resin nominally made with 15 wt % methacrylic acid. Surlyn® ionomers, Fusabond® polymers, and Nucrel® copolymers are commercially available from The Dow Chemical Company.
Suitable E/X- and E/X/Y-type ionomeric cover materials are further disclosed, for example, in U.S. Pat. Nos. 6,653,382, 6,756,436, 6,894,098, 6,919,393, and 6,953,820, the entire disclosures of which are hereby incorporated by reference.
Suitable polyurethanes, polyureas, and blends and hybrids of polyurethane/polyurea are further disclosed, for example, in U.S. Pat. Nos. 5,334,673, 5,484,870, 6,506,851, 6,756,436, 6,835,794, 6,867,279, 6,960,630, and 7,105,623; U.S. Patent Application Publication No. 2009/0011868; U.S. Patent Application No. 60/401,047; U.S. patent application Ser. No. 16/590,317, filed Oct. 1, 2019; U.S. Patent Application Publication No. 2007/0117923; and U.S. Pat. Nos. 8,865,052, 6,734,273, and 8,034,873; the entire disclosures of which are hereby incorporated herein by reference.
Suitable UV absorbers that are optionally included in cover layer compositions are further disclosed, for example, in U.S. Pat. No. 5,156,405 to Kitaoh; U.S. Pat. No. 5,840,788 to Lutz; and U.S. Pat. No. 7,722,483 to Morgan; the entire disclosures of which are hereby incorporated herein by reference.
Dimensions of each golf ball layer, i.e., thickness/diameter, may vary depending on the desired properties.
The United States Golf Association specifications limit the minimum size of a competition golf ball to 1.680 inches. There is no specification as to the maximum diameter, and golf balls of any size can be used for recreational play. Golf balls of the present invention can have an overall diameter of any size, and, typically, have an overall diameter of from 1.680 inches to 1.780 inches.
Golf balls of the present invention have a plurality of dimples on the outer surface thereof, and, typically, have an overall dimple surface coverage of 60% or greater, or 65% or greater, or 75% or greater or 80% or greater.
It should be understood that the examples below are merely illustrative of particular embodiments of the present invention, and are not to be construed as limiting the invention, the scope of which is defined by the appended claims.
In each of examples 1-11 below, a golf ball subassembly having a diameter of about 1.630 inches and consisting of a solid rubber core and an ionomer casing layer was provided. A mark, or a plurality of marks, as indicated below, was pad printed on the outer surface of each subassembly using electrically conductive ink to produce a marked subassembly.
In this example, the mark consists of a single stripe, according to the embodiment illustrated in
In this example, the mark consists of two stripes intersecting at two locations, according to the embodiment illustrated in
In this example, the mark consists of two stripes intersecting at one location, according to the embodiment illustrated in
In this example, the mark consists of four stripes forming a closed loop in the form of a spherical rectangle, according to the embodiment illustrated in
In this example, the mark consists of a single curvilinear stripe creating a closed loop, according to the embodiment illustrated in
In this example, the plurality of marks consists of sixty stripes arranged in an icosahedral pattern, according to the embodiment illustrated in
In this example, the mark consists of three intersecting stripes according to the embodiment illustrated in
In this example, the mark consists of four intersecting stripes, according to the embodiment illustrated in
In this example, the plurality of marks consists of a first mark and a second mark, according to the embodiment illustrated in
The first mark consists of three intersecting stripes, including a first stripe, a second stripe, and a third stripe. The first stripe and the second stripe of the first mark have substantially the same length, each of the first stripe and the second stripe having a length of about 2.60 inches. The third stripe of the first mark has a length of about 0.25 inches. The first stripe, the second stripe, and the third stripe of the first mark have substantially the same width, each stripe of the first mark having a width of about 0.12 inches. The first mark has an average width of about 0.12 inches. A plane bisecting the first stripe and a plane bisecting the second stripe are separated by an angle of about 90°, as illustrated in the front view and the rear view of
The second mark consists of a single stripe having a length of about 0.40 inches and a width of about 0.12 inches.
The plurality of marks has a total surface coverage of about 8%.
In this example, the plurality of marks consists of a first mark, a second mark, and a third mark, according to the embodiment illustrated in
The first mark consists of five intersecting stripes, including a first stripe, a second stripe, a third stripe, a fourth stripe, and a fifth stripe. The first stripe and the second stripe of the first mark have substantially the same length, each of the first stripe and the second stripe having a length of about 2.15 inches. The third stripe and the fourth stripe of the first mark connect the ends of the first and second stripes. The third stripe and the fourth stripe of the first mark have substantially the same length, each of the third stripe and the fourth stripe having a length of about 0.30 inches. The fifth stripe of the first mark has a length of about 0.40 inches. The first stripe, the second stripe, the third stripe, the fourth stripe, and the fifth stripe of the first mark have substantially the same width, each stripe of the first mark having a width of about 0.12 inches. The first mark has an average width of about 0.12 inches. A plane bisecting the first stripe and a plane bisecting the second stripe are separated by an angle of about 90°, as illustrated in the front view and the rear view of
The second mark consists of a single stripe having a length of about 0.40 inches and a width of about 0.12 inches.
The third mark consists of a single stripe having a length of about 0.40 inches and a width of about 0.12 inches.
The plurality of marks has a total surface coverage of about 9%
In this example, the plurality of marks consists of a first mark, a second mark, and a third mark, according to the embodiment illustrated in
The first mark consists of four intersecting stripes, including a first stripe, a second stripe, a third stripe, and a fourth stripe. The first stripe, the second stripe, and the third stripe of the first mark have substantially the same length, each of the first stripe, the second stripe, and the third stripe having a length of about 2.50 inches. The fourth stripe of the first mark has a length of about 0.25 inches. The first stripe, the second stripe, the third stripe, and the fourth stripe of the first mark have substantially the same width, each stripe of the first mark having a width of about 0.12 inches. The first mark has an average width of about 0.12 inches. A plane bisecting the first stripe and a plane bisecting the second stripe are separated by an angle of about 60°, as illustrated in the front view and the rear view of
The second mark consists of a single stripe having a length of about 0.40 inches and a width of about 0.12 inches.
The third mark consists of a single stripe having a length of about 0.40 inches and a width of about 0.12 inches.
The plurality of marks has a total surface coverage of about 12%.
In each of examples 1-11 above, a finished golf ball was formed by molding a cover layer about the marked subassembly. The finished golf balls were repeatedly fired via air cannon to a mass plate, simulating golf ball driver impact speed greater than 175 miles per hour. Subsequent to repeated testing, the balls were tested using a mechanical robot swinging a driver. The average launch condition for the balls was 175 mph, 9.5 degrees, 2600 rpm, as measured using a photogrammetric system. The radar tracking system was able to accurately measure spin at a capture rate of greater than 96% utilizing 16 feet of ball flight. The radar tracking system used for testing was a TrackMan golf radar, commercially available from TrackMan Golf, with the TrackMan set to indoor mode.
In this example, a plurality of marks was pad printed on the outer surface of a golf ball core having a diameter of about 1.630 inches using electrically conductive ink, according to the embodiment illustrated in
The plurality of marks has a total surface coverage of about 9.5%.
The centroid of each of the marks is positioned at a vertex of one of 30 spherical triangles covering the entire surface of the core layer.
In this example, a plurality of marks was pad printed on the outer surface of a golf ball core having a diameter of about 1.630 inches using electrically conductive ink. The plurality of marks consists of 13 equally spaced markings, each marking having the shape of a stripe. Each of the 13 stripes has a length of about 0.30 inches and a width of about 0.125 inches.
The plurality of marks has a total surface coverage of about 5.8%.
The centroid of each of the marks is positioned at a vertex of one of 22 spherical triangles covering the entire surface of the core layer.
In this example, a plurality of marks was pad printed on the outer surface of a golf ball core having a diameter of about 1.630 inches using electrically conductive ink. The plurality of marks consists of 19 equally spaced markings, each marking having the shape of an annulus. Each of the 19 annuli has an outer diameter of about 0.30 inches and an inner diameter of about 0.15 inches. Each of the 19 annuli has a printed line thickness of about 0.075 inches.
The plurality of marks has a total surface coverage of about 12.0%.
The centroid of each of the marks is positioned at a vertex of one of 34 spherical triangles covering the entire surface of the core layer.
In this example, a mark was pad printed on the outer surface of a golf ball cased core having a diameter of about 1.630 inches using electrically conductive ink. The mark is a continuous mark consisting of a first stripe, a second stripe, and a third stripe, according to the embodiment illustrated in
The first stripe and the second stripe have substantially the same length, each of the first stripe and the second stripe having a length of about 0.90 inches. The third stripe has a length of about 0.38 inches. The first stripe, the second stripe, and the third stripe have substantially the same width, each stripe having a width of about 0.12 inches. A plane bisecting the first stripe and a plane bisecting the second stripe are separated by an angle of about 90°, as illustrated in the front view and the rear view of
In this example, a mark was pad printed on the outer surface of a golf ball cased core having a diameter of about 1.630 inches using electrically conductive ink. The mark is a continuous mark consisting of a first stripe and a second stripe, according to the embodiment illustrated in
The first stripe and the second stripe have substantially the same length, each of the first stripe and the second stripe having a length of about 0.90 inches. The first stripe and the second stripe have substantially the same width, each stripe having a width of about 0.12 inches. A plane bisecting the first stripe and a plane bisecting the second stripe are separated by an angle of about 90°, as illustrated in the front view and the rear view of
In this example, a plurality of marks was pad printed on the outer surface of a golf ball cased core having a diameter of about 1.630 inches using electrically conductive ink. The plurality of marks consists of two non-intersecting stripes, including a first stripe and a second stripe, according to the embodiment illustrated in
The first stripe and the second stripe have substantially the same length, each of the first stripe and the second stripe having a length of about 0.88 inches. The first stripe and the second stripe have substantially the same width, each stripe having a width of about 0.12 inches. A plane bisecting the first stripe and a plane bisecting the second stripe are separated by an angle of about 90°, as illustrated in the front view and the rear view of
In this example, four radar detectable marks were pad printed using electrically conductive ink on the spherical outer surface of a golf ball cased core having a circumference of about 130 mm. Each of the four marks is a rectangular stripe having a length, calculated as the arc length of the longest edge, of about 7.0 mm and a width, calculated as the arc length of the shortest edge, of about 1.5 mm. The geometric center of each of the four marks is located on the same great circle on the outer surface of the cased core, allowing for a manufacturing tolerance of about 1.5 mm, and the great circle bisects each of the four marks lengthwise. The arc length on the outer surface of the cased core between the geometric centers of each pair of adjacent marks is about 16.6 mm. The smallest rectangular stripe encompassing the boundary of each of the four marks has a length of about 56.8 mm.
In this example, eight radar detectable marks were pad printed using electrically conductive ink on the spherical outer surface of a golf ball cased core having a circumference of about 130 mm. Each of the eight marks is a rectangular stripe having a length, calculated as the arc length of the longest edge, of about 3.5 mm and a width, calculated as the arc length of the shortest edge, of about 1.5 mm. The geometric center of each of the eight marks is located on the same great circle on the outer surface of the cased core, allowing for a manufacturing tolerance of about 1.5 mm, and the great circle bisects each of the eight marks lengthwise. The arc length on the outer surface of the cased core between the geometric centers of each pair of adjacent marks is about 8.3 mm. The smallest rectangular stripe encompassing the boundary of each of the eight marks has a length of about 61.6 mm.
In this example, ten radar detectable marks were pad printed using electronically conductive ink on the spherical outer surface 10 of a golf ball cased core having a circumference of about 130 mm, according to the embodiment illustrated in
The geometric centers of marks 12, 13, 14, 15 and 16 are located on the same great circle on the outer surface of the cased core, allowing for a manufacturing tolerance of about 1.5 mm. The geometric centers of marks 22, 23, 24, 25 and 26 are located on the same great circle on the outer surface of the cased core, allowing for a manufacturing tolerance of about 1.5 mm. Thus, marks 12, 13, 14, 15, and 16 are part of a first great circle series of marks, and marks 22, 23, 24, 25 and 26 are part of a second great circle series of marks.
Regarding the first great circle series, each of marks 12, 13, 14 and 15 has a length of about 6.6 mm, and mark 16 has a length of about 8.1 mm, length being calculated as the arc length of the longest edge of the mark. Each of marks 12, 13, 14, 15 and 16 has a width of about 1.0 mm, width being calculated as the arc length of the shortest edge of the mark. The separation distance between each pair of adjacent marks in the first great circle series is about 6.6 mm, separation distance being calculated as the spherical length of the shortest great circle arc that can be drawn on the surface of the cased core that connects any point on one mark in the pair of adjacent marks to any point on the other mark in the pair of adjacent marks. The smallest rectangular stripe encompassing the boundary of each of the marks in the first great circle series has a length of about 60.9 mm. Thus, the portion of the great circle on which the marks of the first great circle series are located has a length of about 47% of the circumference of the cased core. The angular length of the first great circle series is about 166°.
Regarding the second great circle series, each of marks 22, 23, 24 and 25 has a length of about 6.6 mm, and mark 26 has a length of about 8.1 mm, length being calculated as the arc length of the longest edge of the mark. Each of marks 22, 23, 24, 25 and 26 has a width of about 1.0 mm, width being calculated as the arc length of the shortest edge of the mark. The separation distance between each pair of adjacent marks in the second great circle series is about 6.6 mm, separation distance being calculated as the spherical length of the shortest great circle arc that can be drawn on the surface of the cased core that connects any point on one mark in the pair of adjacent marks to any point on the other mark in the pair of adjacent marks. The smallest rectangular stripe encompassing the boundary of each of the marks in the second great circle series has a length of about 60.9 mm. Thus, the portion of the great circle on which the marks of the second great circle series are located has a length of about 47% of the circumference of the cased core. The angular length of the second great circle series is about 166°.
Bisecting plane 11 is the plane that bisects the first great circle series. Bisecting plane 21 is the plane that bisects the second great circle series. Bisecting plane 11 and bisecting plane 21 are separated by an angle of about 90°, as illustrated in the front view and the rear view of
In this example, eleven radar detectable marks were pad printed using electronically conductive ink on the spherical outer surface 10 of a golf ball cased core having a circumference of about 130 mm, according to the embodiment illustrated in
The geometric centers of marks 12, 13, 14, 15 and 16 are located on the same great circle on the outer surface of the cased core, allowing for a manufacturing tolerance of about 1.5 mm. The geometric centers of marks 22, 23, 24, 25 and 26 are located on the same great circle on the outer surface of the cased core, allowing for a manufacturing tolerance of about 1.5 mm. Thus, marks 12, 13, 14, 15, and 16 are part of a first great circle series of marks, and marks 22, 23, 24, 25 and 26 are part of a second great circle series of marks. The geometric center of mark 32 does not lie on the same great circle as the first great circle series or the second great circle series, and, thus, is not part of a great circle series.
Regarding the first great circle series, each of marks 12, 13, 14 and 15 has a length of about 6.6 mm, and mark 16 has a length of about 8.1 mm, length being calculated as the arc length of the longest edge of the mark. Each of marks 12, 13, 14, 15 and 16 has a width of about 1.0 mm, width being calculated as the arc length of the shortest edge of the mark. The separation distance between each pair of adjacent marks in the first great circle series is about 6.6 mm, separation distance being calculated as the spherical length of the shortest great circle arc that can be drawn on the surface of the cased core that connects any point on one mark in the pair of adjacent marks to any point on the other mark in the pair of adjacent marks. The smallest rectangular stripe encompassing the boundary of each of the marks in the first great circle series has a length of about 60.9 mm. Thus, the portion of the great circle on which the marks of the first great circle series are located has a length of about 47% of the circumference of the cased core. The angular length of the first great circle series is about 166°.
Regarding the second great circle series, each of marks 22, 23, 24 and 25 has a length of about 6.6 mm, and mark 26 has a length of about 8.1 mm, length being calculated as the arc length of the longest edge of the mark. Each of marks 22, 23, 24, 25 and 26 has a width of about 1.0 mm, width being calculated as the arc length of the shortest edge of the mark. The separation distance between each pair of adjacent marks in the second great circle series is about 6.6 mm, separation distance being calculated as the spherical length of the shortest great circle arc that can be drawn on the surface of the cased core that connects any point on one mark in the pair of adjacent marks to any point on the other mark in the pair of adjacent marks. The smallest rectangular stripe encompassing the boundary of each of the marks in the second great circle series has a length of about 60.9 mm. Thus, the portion of the great circle on which the marks of the second great circle series are located has a length of about 47% of the circumference of the cased core. The angular length of the second great circle series is about 166°, according to the calculation method disclosed below.
Mark 32 has a length of about 6.6 mm and a width of about 1.0 mm, length and width being calculated as the arc length of the longest edge and shortest edge of the mark, respectively.
Bisecting plane 11 is the plane that bisects the first great circle series. Bisecting plane 21 is the plane that bisects the second great circle series. Bisecting plane 11 and bisecting plane 21 are separated by an angle of about 90°, as illustrated in the front view and the rear view of
When numerical lower limits and numerical upper limits are set forth herein, it is contemplated that any combination of these values may be used.
All patents, publications, test procedures, and other references cited herein, including priority documents, are fully incorporated by reference to the extent such disclosure is not inconsistent with this invention and for all jurisdictions in which such incorporation is permitted.
While the illustrative embodiments of the invention have been described with particularity, it will be understood that various other modifications will be apparent to and can be readily made by those of ordinary skill in the art without departing from the spirit and scope of the invention. Accordingly, it is not intended that the scope of the claims appended hereto be limited to the examples and descriptions set forth herein, but rather that the claims be construed as encompassing all of the features of patentable novelty which reside in the present invention, including all features which would be treated as equivalents thereof by those of ordinary skill in the art to which the invention pertains.
The present application is a continuation-in-part of U.S. patent application Ser. No. 17/553,122, filed Dec. 16, 2021, which is a continuation-in-part of U.S. patent application Ser. No. 17/552,380, filed Dec. 16, 2021, which is a continuation-in-part of U.S. patent application Ser. No. 17/515,971, filed Nov. 1, 2021, which claims the benefit of U.S. Provisional Application No. 63/116,535, filed Nov. 20, 2020, U.S. Provisional Application No. 63/116,803, filed Nov. 20, 2020, and U.S. Provisional Application No. 63/212,225, filed Jun. 18, 2021, the entire disclosures of which are hereby incorporated herein by reference.
| Number | Date | Country | |
|---|---|---|---|
| 63116535 | Nov 2020 | US | |
| 63116803 | Nov 2020 | US | |
| 63212225 | Jun 2021 | US |
| Number | Date | Country | |
|---|---|---|---|
| Parent | 17553122 | Dec 2021 | US |
| Child | 18072791 | US | |
| Parent | 17552380 | Dec 2021 | US |
| Child | 17553122 | US | |
| Parent | 17515971 | Nov 2021 | US |
| Child | 17552380 | US |
