The present disclosure relates to golf balls, particularly to golf balls including dimples having ridged and/or textured surfaces. More particularly, the present disclosure relates to golf balls including dimples constructed of radial channels.
Aerodynamic forces generated by a golf ball in flight are a result of its velocity and spin. These forces can be represented by a lift force and a drag force. Lift force is perpendicular to the direction of flight and is a result of air velocity differences above and below the rotating ball. This phenomenon is attributed to Magnus, who described it in 1853 after studying the aerodynamic forces on spinning spheres and cylinders, and is described by Bernoulli's Equation, a simplification of the first law of thermodynamics. Bernoulli's equation relates pressure and velocity where pressure is inversely proportional to the square of velocity. The velocity differential, due to faster moving air on top and slower moving air on the bottom created by the ball's spin, results in lower air pressure on top and an upward directed force on the ball.
Drag is opposite to the direction of flight and orthogonal to lift. The overall drag force on a ball is pressure drag and viscous or skin friction drag. A sphere is a bluff body, which is a somewhat inefficient aerodynamic shape. As a result, the accelerating flow field around the golf ball causes a large pressure differential with high-pressure forward and low-pressure behind the ball. The low-pressure area behind the ball is also known as the wake. In order to minimize pressure drag, dimples provide a means to energize the flow field and delay the separation of flow, or reduce the wake region behind the ball.
The industry has seen many efforts to improve the aerodynamic efficiency of golf balls, such as through variations in dimple configuration, dimple pattern, and other methods. For example, dimple properties such as number, shape, size, volume, edge angles and overall pattern have been manipulated in an attempt to generate a golf ball that has improved aerodynamic properties. A further consideration that may not be as thoroughly developed is the surface configuration and texture of the dimples themselves. Dimple surfaces can be adjusted and adapted to include non-smooth textures to introduce new air flow patterns and further refine the aerodynamic properties of the ball. The present disclosure relates to a development in surface texturing of a golf ball dimples to augment aerodynamic performance.
In one embodiment, the present disclosure describes a golf ball. The golf ball includes a generally spherical surface and a plurality of dimples separated by a land area formed on the surface. At least one of the dimples includes a perimeter edge connected to the land area and a dimple surface surrounded by the perimeter edge. The dimple surface defines a dimple point depth in relation to a phantom surface that is a continuation of the land area. The dimple surface includes a plurality of channels and a plurality of channel edges. At least one of (i) the plurality of channels or (ii) the plurality of channel edges extend continuously from the perimeter edge to an intersection at a dimple center. The plurality of channels include at least a first type channel and a second type channel. The plurality of channel edges include a plurality of shared edges, wherein each shared edge is shared between a first type channel that is directly adjacent to a second type channel. Each shared edge extends radially from the dimple center to a terminal end and includes an intersection point therebetween. The portion of the shared edge that extends from the intersection point to the terminal end is an extension edge, and the extension edge is a portion of the perimeter edge.
In another embodiment, the present disclosure describes a golf ball. The golf ball includes a generally spherical surface and a plurality of dimples separated by a land area formed on the surface. At least one of the dimples includes a perimeter edge connected to the land area; and a dimple surface surrounded by the perimeter edge and including a plurality of channels and a plurality of channel edges. The plurality of channels include at least a first type channel and a second type channel. The first type channels include an area having a plan shape of a first circular sector of a first channel circle and the second type channels include an area having a plan shape of a second circular sector of a second channel circle, and wherein a diameter of the first channel circle is greater than a diameter of the second channel circle such that the first type channels include extension areas.
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:
The aerodynamic characteristics of a golf ball are largely dependent on the dimples present on the outer surface. Golf balls typically include 250-500 dimples on the outer surface that range from about 0.080-0.200 in. in diameter (or effective diameter, if non-circular). The arrangement of these dimples on the outer surface (i.e., the “dimple pattern”), the dimple shapes, the edge angles, the cross-sectional profiles, the depths, etc., all contribute to the overall flight performance of the golf ball. Dimple surface configuration and texture is another characteristic that affects the aerodynamic performance because the interaction between the dimple surface and the surrounding air affects the overall drag characteristics. For example, surface texture may be introduced to enhance aerodynamics
The present disclosure includes a golf ball including dimples having a ridged/textured surface. For example, in an embodiment, a disclosed dimple includes a plurality of radially-arranged channels connected around the dimple center. The channels may include at least a portion that is in the shape of a circular sector. For example, the channels may appear in a plan view as a pie chart with “pie slices” arranged around the center. The channels may additionally have a second portion that connects the circular sector to the surrounding land area of the golf ball. For example, the arc portion of the circular sector may be connected to a curved entrance zone that has an edge flush with the land area of the golf ball. Each radial channel may be connected to two adjacent radial channels at channel edges. The channel edges extend from the dimple center to the dimple perimeter edge. The channels and channel edges, which alternate in a circumferential direction (i.e., in a circle around the dimple center 20) around the dimple, make up an entirety of the surface of the dimple.
In an exemplary embodiment, the perimeter edge 16 is non-circular and includes a scalloped edge shape that alternates between rounded peaks and pointed valleys in a plan view. The pointed valleys are connected to the terminal ends 24 of the channel edges 22. The scalloped edge shape of the perimeter edge accommodates an entrance zone into the plurality of channels 18 without an abrupt edge angle.
The dimple center 20 may be a point at an intersection of the plurality of channels 18 and/or the plurality of channel edges 22. As will be described, the channel edges 22 approach the dimple surface 17 at the dimple center 20. In this way, it can be considered that at least one of (i) the plurality of channels 18 or (ii) the plurality of channel edges 22 extend continuously from the perimeter edge 16 to an intersection at the dimple center 20. For instance, the dimple center 20 may be considered a combination of channels 18 coming together at one point, a combination of the tops of channel edges 22 intersecting at one point, or both.
In another aspect, the dimple center 20 may be considered the point in the plan view that corresponds to the centroid of the dimple 12 (which may coincide with the center of the dimple circle DC). In
In
In the dimple 12, the channel circle CC divides each channel 18 into a first area 42 and a second area 44 (shown for example with respect to channels 26, 28 in
The dimple surface 17 in the second area 44 is situated between the perimeter edge 16 and the channel circle CC. The second area of the first channel 26 is bounded by the segment 46 of the channel circle CC and a portion 50 of the perimeter edge 16. The portion 50 has a rounded shape in the plan view and is one of the repeating curved segments that make up the scalloped edge shape of the perimeter edge 16. The portion 50 has peak 52. The peak 52 is the point on the perimeter edge 16 that touches the dimple channel DC. The peak 52 may be the midpoint of the portion 50. The channels 18 include a channel centerline CCL that connects the dimple center 20, the central channel point 48, and the peak 52 of the portion 50.
Each channel 18 includes a channel length CL. The channel length CL is measured from the dimple center 20 to the furthest point of the channel measured along the channel centerline CCL (e.g., the dimple center 20 to the peak 52 of the portion 50 of the perimeter edge 16). The channel length CL may also be characterized as a radius of the dimple circle DC. A radius of the channel circle Rcc is a length of the first area 42 of the channel 18 and is less than the channel length CL. Each channel also includes a channel width CW. The channel width CW is the largest width of the channel 18, which in the depicted embodiment is measured as a straight-line distance between the terminal ends 24 of the channel edges 22. The channels 18 also include an angle of separation AS. The angle of separation AS is measured as the angle between the channel centerlines CCL. In the embodiment of
The channel 18 has a channel depth DC that is calculated as the distance between the channel edge 22 and the central channel point 48 on the dimple surface 17. The channel depth DC may differ slightly from that shown in
The channel depth DC is a channel parameter, indicating how deep the channel is at a point spaced from the center of the dimple. However, the channel point depth CPD, in general, may be measured at any point within a channel 18 and compared to the channel edge 22. The channel point depth CPD measurement may use a cross-section at the same radial points on the two channel edges 22 that delimit the channel being measured (such as in
The channel depth DC may be compared to the dimple depth DD in another dimple parameter. For example, a ratio between the channel depth DC and the dimple depth DD may further characterize the slope of the dimple surface 17 within the circular sector portions of the channels 18. In an exemplary embodiment, the channel depth DC at the channel circle CC is approximately 1-20% of the dimple depth DD at the dimple center 20.
As mentioned above with respect to
The disclosed embodiments include dimples having radial channels that have a portion that is a circular sector in a plan view. The channels include channel point depths CPD that approach zero at a dimple center and a dimple point depth DPD that approaches a maximum (i.e., the dimple depth DD) at the dimple center. The dimple surface that accommodates these characteristics may take different shapes and configurations and embodiments. The dimples 12 and channels 18 of the above embodiments have a half profile (also referred to herein as dimple profile) that follows a circular arc.
While the depicted examples include matches between the half profile shape of the channel surfaces and the channel edges, it should be understood that other embodiments may combine different profiles. For example, some embodiments may include a channel surface curved in a half profile according to a circular arc, combined with channel edges having a catenary or linear half profile. Other combinations are also possible.
The disclosed embodiments include radial channels and channel edges that alternate in a circumferential direction around the dimple center, making up an entirety of a dimple surface interior to a perimeter edge. As described herein, the radial channels make up an entirety of the dimple surface. As a result, the number of radial channels equals the number of channel edges. Disclosed embodiments may include more or less channels than those depicted. For example, it is contemplated that disclosed embodiments may include between 10 and 50 channels.
According to some embodiments, a disclosed dimple may include at least ten channels and ten channel edges. In other embodiments, a disclosed dimple may include at least twenty channels and twenty channel edges. Another embodiment of a disclosed dimple includes fifty channels and fifty channel edges.
In some embodiments, the channels and channel edges may be positioned such that the angle of separation AS is equal for each channel, such as in the dimple 12. This produces an axial symmetric configuration about the dimple center, with axial symmetry in number equal to the number of channels and number of channel edges. For example, the dimple 12 has 26-fold axial symmetry with 26 equal channels 18 and channel edges 22. In other embodiments, a dimple may have channels of different channel widths CW and angles of separation AS. These dimples may or may not have axial symmetry around the dimple center. For example, some dimples may have axial symmetry in number less than he number of channels and channel edges.
Dimples of the present disclosure, which are generally non-spherical in comparison to conventional dimples, may have a plan shape area and dimple volume within a range having a lower limit and an upper limit selected from the values within the region shown in
The plan shape area is based on a planar view of the dimple plan shape, such that the viewing plane is normal to an axis connecting the center of the ball to the point of the calculated surface depth. The dimple volume is the total volume encompassed by the dimple shape and the surface of the golf ball. The preferred dimple volume will be less than the upper limit volume calculated by
and greater than the lower limit calculated by
where x is the dimple plan shape area and x is between 0.0025 and 0.045 inclusive.
For purposes of the present disclosure, the plan shape area of a non-spherical dimple is based on a planar view of the dimple plan shape, such that the viewing plane is normal to an axis connecting the center of the ball to the point of the calculated surface depth.
An example of a dimple according to disclosed embodiments is further described below. The dimple may have a general appearance of the dimple 12 as shown in
These dimensions are exemplary and may be changed or altered to accommodate different aerodynamic performance of a golf ball. For example, one or more dimensions may be tuned such that the textured/ridged dimples enhance the aerodynamic performance of the golf ball. In another example, the dimensions may be tuned to limit the capabilities of the golf ball and thereby produce a reduced distance golf ball.
In some embodiments, dimples having radial channels may be specifically configured to tailor aerodynamic performance of the golf ball. In particular, some dimples may have radial channels that create a more complex perimeter edge that affects the air flow pattern around the dimple differently than other exemplary-disclosed dimples. For example, some dimples may be made up of radial channels that have different length dimensions relative to each other to create different edges and angles around the perimeter of the dimple to alter the air flow pattern in new and different ways. For instance, some dimples may include channels having extension areas that are located radially outward of comparable portions of other, shorter channels. The extension areas may include extension edges that are both a portion of a channel edge and a portion of the perimeter edge of the dimple.
The dimple surface 104 includes a plurality of channels 106 radiating from a dimple center 108. The plan view in
The dimple center 108 may be a point at an intersection of the plurality of channels 106 and/or the plurality of channel edges 110. The channel edges 110 approach the dimple surface 104 at the dimple center 108. As has been described in relation to other disclosed embodiments, it can be considered that at least one of (i) the plurality of channels 106 or (ii) the plurality of channel edges 110 extend continuously from the perimeter edge 102 to an intersection at the dimple center 108. For instance, the dimple center 108 may be considered a combination of channels 106 coming together at one point, a combination of the tops of channel edges 110 intersecting at one point, or both.
In an exemplary embodiment, the plurality of channels 106 include at least a first type channel 114 and a second type channel 116. Each first type channel 114 differs in a length dimension from each second type channel 116. In an exemplary embodiment, the first type channels 114 are longer in a radial direction than the second type channels 116. In the embodiment shown in
In dimple 100, the terminal ends 112 are only connected to each other at the distal ends of the first type channels 114, while the distal ends of the second type channels 116 are formed interior to the terminal ends 112. In an exemplary embodiment, the distal ends of the second type channels 116 are formed by connecting intersection points 118, where the intersection points 118 are a point on the channel edges 110 interior to the terminal ends 112. As a result, the first type channels 114 are longer than the second type channels 116. The positioning of the intersection points 118 relative to the terminal ends 112 defines, at least in part, the difference between the lengths of the different channel types.
In some embodiments, a mean circle (not shown) is a circle having its center at the dimple center 108 and having a diameter that is an average of the diameters of two or more of the circles ODC, IDC, OCC, ICC. For example, the mean circle diameter may be an average of all four circles. According to an exemplary embodiment, the diameter of the mean circle is considered the effective diameter of the dimple 100.
In some aspects, the dimple center 108 may be considered the point in the plan view that corresponds to the centroid of the dimple 100. In
At least some of the terminology, descriptions, and dimensions used to describe channels 18 (e.g., as shown in
The outer channel circle OCC divides each first type channel 114 into a first area 120 and a second area 122 and the inner channel circle ICC divides each second type channel 116 into a first area 124 and a second area 126. The dimple surface 104 in the first areas 120, 124 has a shape of a circular sector of the respective channel circle OCC or ICC in the plan view. A circular sector is a pie-shaped part of a circle consisting of an arc of the circle along with the two radii of the circle that connect to the ends of the arc. Each of the first areas 120 of the first type channels 114 is bounded by an entirety of the respective immediately adjacent channel edges 110 and a segment 128 of the outer channel circle OCC that connects the terminal ends 112. Each of the first areas 124 of the second type channels 116 is bounded by portions of the respective immediately adjacent channel edges 110, up to the intersection points 118, and a segment 130 of the inner channel circle ICC that connects the intersection points 118.
The dimple surface 104 in the second area 122 is situated between the perimeter edge 102 and the outer channel circle OCC. The second area 122 is bounded by the segment 128 of the outer channel circle OCC and a connector edge portion 132 of the perimeter edge 102. In an exemplary embodiment, the connector edge portion 132 of the perimeter edge 102 has a rounded shape in the plan view, although other shapes are possible. The connector edge portions 132 close the distal ends of the first type channels 114 to thereby connect the dimple surface 104 to the land area of the golf ball. The connector edge portions 132 thereby partially define an edge angle of the perimeter edge 102. The connector edge portions 132 also define the extent of the outer dimple circle ODC. For example, a peak of the connector edge portions 132 touches the outer dimple circle ODC. The peak may be the midpoint of the connector edge portion 132, but is not necessarily limited thereto.
The dimple surface 104 in the second area 126 is situated between the perimeter edge 102 and the inner channel circle ICC. The second area 126 is bounded by the segment 130 of the inner channel circle ICC and a connector edge portion 134 of the perimeter edge 102. In an exemplary embodiment, the connector edge portion 134 of the perimeter edge 102 has a rounded shape in the plan view, although, like the connector edge portion 132, other shapes are possible. The connector edge portions 134 close the distal ends of the second type channels 114 to thereby connect the dimple surface to the land area of the golf ball. The connector edge portions 134 thereby partially define an edge angle of the perimeter edge 102. The connector edge portions 134 also define the extent of the inner dimple circle IDC. For example, a peak of the portions 134 touches the inner dimple circle IDC. The peak may be the midpoint of the connector edge portion 134, but is not necessarily limited thereto.
Each channel 106 includes a channel length. The channel length is measured from the dimple center 108 to the most radially-distant point of the channel 106 (e.g., measured along the channel centerline CCL). The channel length of each first type channel 114 may be equivalent to a radius of the outer dimple circle ODC and the channel length of each second type channel 116 may be equivalent to a radius of the inner dimple circle IDC. A radius of the outer channel circle ROCC is a measure of the length of the first area 120 of the channels 114 and is less than the channel length of the first type channel 114. A radius of the inner channel circle RICC is a measure of the length of the first area 124 of the second type channels 116 and is less than the channel length of the second type channels 116. While either or both dimensions may be adjusted to achieve a desired aerodynamic performance, the radii of the channel circles may be more representative of the configuration of the dimple 100 and other similar dimples of the disclosure. For instance, a difference between RICC and ROCC may be equal to an extension length EL that quantifies the degree to which the channel types are different in length, regardless of the shape of the connector edge portions 132, 134.
Each channel 106 also includes a channel width. The channel width is the largest width of the channel 106, which in an exemplary embodiment is measured as a straight-line distance. For the first type channels 114, this distance is measured between the terminal ends 112 of the channel edges 110. For the second type channels 116, this distance is measured between the intersection points 118 on the channel edges 110. According to the embodiment of
Consistent with disclosed embodiments, the extension edges 136 are a portion of the channel edges 100 and also define part of the perimeter edge 102. For example, the extension edges 136 define the portions of the perimeter edge 102 that connect the connector edge portions 132 of the first type channels 114 to the connector edge portions 134 of the second type channels 116. The extension edges 136 connect the intersection points 118 to the terminal ends 112. The extension edges 136 produce abrupt directional changes in the shape of the perimeter edge 102. Moreover, the extension edges 136 create localized areas 140 of edge angle discontinuity as the land area around the dimple 100 accommodates the prong-shaped portions of the perimeter edge 102.
According to disclosed embodiments, the perimeter edge shape and corresponding variation in edge angle as a result of the extension edges 136 may produce a different air flow pattern than radial channel embodiments in which the perimeter edge connects only to terminal ends of channel edges. The extension areas within dimples having radial channels thereby provides another modifiable dimension in the surface texture of the golf ball, enabling further refinement of its aerodynamic performance.
There are several options for parameters that quantify the pronged shape of the perimeter edge of the disclosed dimples. In one example, the extension length EL may be used as a measure of a degree to which the channels extend beyond each other. A ratio
similarly identifies the relative extension of the terminal ends past the intersection points. In other embodiments, a total edge length from intersection point to intersection point may be considered.
The number of channels and channel types is also a relevant variable that could affect aerodynamic performance of a disclosed dimple (e.g., by indicating how many extension areas and/or intersection points are present). For example, a dimple may have a total extension length LTE that is equivalent to the EL multiplied by the number of extension edges (i.e., when EL is constant). In another example, a total extension area ATE may be defined as a sum total area of all extension areas of the dimple.
According to some embodiments, disclosed dimples may satisfy one or more of the following such that the dimple produces a sufficient interaction with the surrounding air flow so as to affect aerodynamic performance. In one aspect, a minimum channel length (i.e. as defined by a radius of a circular channel) may be compared to a maximum channel length (i.e., as defined by a radius of another circular channel). For example, a minimum channel length is at least 10% smaller than the maximum channel length. In other embodiments, a minimum channel length is at least 15% smaller than the maximum channel length. In still other embodiments, the minimum channel length is at least 20% smaller than the maximum channel length.
In other aspects, disclosed dimples may be defined based on more measurements relating to the extension edges. For example, a dimple may define an extension length of at least 0.015 in., a ratio
of at least 1.1, a total extension length LTE of at least 0.2 in., and/or a total extension area of at least 0.0025 in2. In other embodiments, the extension length may be at least 0.020 in., 0.025 in., 0.030 in., 0.035 in. or 0.050 in. In other embodiments, the ratio
may be at least 1.15, 1.20, 1.25, 1.30, 1.50, or 2.00. In still other embodiments, the total extension length LTE may be at least 0.25 in., 0.30 in., 0.35 in., or 0.50 in. Higher ranges and minimum values for extension area and total extension area are similarly possible. Moreover, dimples may be required to have a minimum number of extension edges in order to produce the desired aerodynamic effect. For example, in some embodiments, a dimple may include at least 10 extension edges. In other embodiments, a dimple may have at least 15, 20, 25, or 30 extension edges.
As one example, the dimple 100 as defined in Table 2 includes an extension length EL of 0.018 in., ratio
of approximately 1.25, total extension length LTE of approximately 0.42 in., an extension area of approximately 0.00028 in2 and a total extension area ATE equal to approximately 0.003 in2. The dimple 100 includes 24 extension edges (two for each first type channel 114).
The dimple 100 is one example of a dimple having radial channels with extension areas to produce a prong-shaped perimeter edge. Other dimples consistent with the disclosure may have the same or different characteristics. For instance, the dimple 100 includes alternating types of channels such that the dimple is rotationally symmetric. In other embodiments, a dimple may include various types of channels arranged such that the dimple is not rotationally symmetric.
In other embodiments, the count of the different types of channels may be varied in order to produce different dimples consistent with the disclosure. For example, depending on the relative sizes of the different types of channels, the channels may be arranged such that there are the same number of each type of channel, or, in other embodiments, the number of each type of channel may be unique.
In another example, the relative dimensions of the different channel types may be varied. For example, in the dimple 100, the first type channels 114 are longer and narrower than the second type channels 116, but other combinations are possible for dimples having two different channel types. For example, a first type of channel may be longer and wider than a second type of channel. Table 3 includes exemplary parameters for an embodiment consistent with this type of dimple.
In addition, while the dimple 100 includes two channel types, other dimples consistent with the disclosed embodiments may include three or more different types of channels (e.g., dimples of three different lengths).
In the dimple 150, extension edges 162 are present for some, but not all of the channel edges 158, as a result of some same-type channels being directly adjacent to each other. In other locations on the dimple 150, however, extension edges 162 are present where different types of channels are directly adjacent to each other. The dimple 150 may be characterized as having a total extension length LTE equal to the sum of the extension length of each extension edge 162 that makes up a portion of the perimeter edge of the dimple 150. For example, the dimple 150 includes nineteen extension edges and a total extension length LTE of approximately 0.24 in.
Some of the disclosed embodiments include dimples having different types of radial channels, where the different types of channels differ at least in a length dimension. As a result, the perimeter edge includes a pronged shape in which some of the radial channels include extension areas that extend radially beyond that of other, shorter radial channels. The extension areas result in extension edges that are both a channel edge and a part of the perimeter edge of the dimple. This configuration results in more complex perimeter edge shapes that include variation in edge angle and edge orientation to thereby create dimples that induce different air flow patterns relative to conventional circular dimples and, in some instances, dimples having radial channels of constant radial length. For instance, the juxtaposition of longer and shorter channels creates a more complex perimeter edge with edge angle variation that, for example, may be selectively implemented on a golf ball to trip the boundary layer at lower Reynolds numbers and reduce drag in the low-speed regime more effectively than dimples with other shapes. In addition, the extension areas (and corresponding recessed areas therebetween) also provide opportunities for greater interdigitation of multiple dimples as laid out on a golf ball. For example, the extension areas of a first dimple on a golf ball may be positioned between corresponding extension areas of a second dimple on the golf ball.
Golf balls consistent with the disclosure include at least one disclosed dimple having radial channels. Some golf balls may include a plurality of golf dimples, where all of the dimples have radial channels as disclosed. Other embodiments of golf balls may include a plurality of dimples, with at least one of the dimples being different than the disclosed dimples having radial channels. For example, a golf ball may include a combination of conventional smooth-surface spherical dimples and disclosed dimples having radial channels. The combination of dimples may be arranged in a dimple pattern to produce a desired aerodynamic performance of the golf ball.
Disclosed embodiments may further include methods of manufacturing golf balls having disclosed dimples constructed of radial channels. The disclosed methods may include compression molding, injection molding, or other golf ball manufacturing methods. Golf balls manufactured to include the disclosed dimples on the generally spherical surface may have any golf ball construction known in the art, such as one or more core layers, a casing layer, and a cover layer. The disclosed dimples may be included in the cover layer, which may be covered by one or more paint and/or coating layers.
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 numerical values and ranges set forth herein are approximate.
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.
This application is a continuation-in-part of U.S. patent application Ser. No. 17/747,248, filed May 18, 2022, which is hereby incorporated herein in its entirety.
Number | Date | Country | |
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Parent | 17747248 | May 2022 | US |
Child | 18953492 | US |