Ball

Abstract

A ball (100) for use in bat and ball games wherein the ball is struck with a bat having an untensioned, rigid ball-striking surface, includes a hollow spherical impact body (112) having a mass of between 10 g and 50 g which enables the use of lightweight bats. The wall of the impact body is of a resiliently compressible material and defines a convexly curved impact zone IB. The ball further includes a flight control assembly (114) including a tail (50) comprising flexible streamers (52), a spacer stem (54) and an anchor fitting (126) for anchoring the spacer stem to the impact body. The configuration of the impact body is such that the impact zone compresses to a minimum compression depth of 12 mm and the impact body bounces to a height of at least 100 cm when the impact body is subjected to a drop test wherein the impact body is dropped onto a test impact surface.

Claims

1. A ball for use in bat and ball games wherein the ball is struck with a bat having an untensioned, rigid ball-striking surface, the ball comprising: a hollow, impact body having a mass of between 10 g and 50 g, the impact body comprising a wall of a resiliently compressible material surrounding an internal space, the wall defining at least one impact zone configured for impact by the bat, the part of the wall of the impact body defining the impact zone having an average wall thickness of between 1 mm and 3 mm and a mass of between 0.15 g and 0.4 g per square centimeter of the wall; and flight control means which is attached to the impact body at an attachment point on the wall of the impact body, the flight control means being operable to control the orientation of the impact body in flight, the configuration of the impact body being such that the impact zone of the impact body compresses to a minimum compression depth of 12 mm and the impact body bounces to a height of at least 100 cm when subjected to a drop test wherein the impact body is dropped from a height of 254 cm onto a rigid test impact surface such that the impact zone of the impact body impacts the test impact surface, the impact body having a variable wall thickness wherein the thickness of the wall of the impact body within the impact zone is relatively thinner than the thickness of the wall of the impact body externally of the impact zone.

2. The ball as claimed in claim 1, wherein the impact zone has a wall thickness of between 1 mm and 3 mm.

3. The ball as claimed in claim 1, wherein the ball is configured for use as a streamer ball, the flight control means including a tail comprising at least one elongate thin, flexible streamer configured to trail behind the impact body in flight; and an elongate, resiliently flexible spacer stem having a proximal end which is attached to the wall of the impact body at said attachment point and a distal end which is attached to the tail.

4. The ball as claimed in claim 3, wherein the impact zone is disposed diametrically opposite the attachment point of the spacer stem to the impact body, the central longitudinal axis of the impact body passing through the attachment point and a centre of the impact zone.

5. The ball as claimed in claim 4, wherein the flight control means further includes an anchor fitting having an anchor body for anchoring the spacer stem to the wall of the impact body, the impact body defining a hole within which the anchor body is securely located.

6. The ball as claimed in claim 4, wherein the impact body defines an attachment formation for attaching the spacer stem to the wall of the impact body, the flight control means further including an anchor fitting including an anchor body which is integrally formed with the spacer stem and which is configured for attachment to the attachment formation of the impact body.

7. The ball as claimed in claim 1, wherein the ball is configured for use as a tethered ball, the flight control means including a tether cord having a proximal end which is attached to the wall of the impact body at said attachment point and a distal end which is rotatably attached to an anchor point at a location remote from the impact body and around which the impact body is struck, in use.

8. The ball as claimed in claim 7, and wherein the impact zone is in the form of an impact band extending around the impact body, a tether cord axis extending along the length of the tether cord and passing through the centre of mass of the impact body, passes through a centre of the impact band when the impact band is viewed in plan view.

9. The ball as claimed in claim 7, wherein the flight control means includes an anchor fitting having an anchor body for anchoring the tether cord to the wall of the impact body, the impact body defining a hole within which the anchor body is securely located.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) Further features of the drawings are described hereinafter by way of non-limiting examples of the invention, with reference to and as illustrated in the accompanying diagrammatic drawings. In the drawings:

(2) FIG. 1 shows a sectional top view of a ball in accordance with the invention, which is configured for use as a tethered ball;

(3) FIG. 2 shows a sectional front view of FIG. 1 as viewed along section line II-II of FIG. 1;

(4) FIG. 3 shows a side view of the ball of FIG. 1;

(5) FIG. 4 shows an opposite side view of the ball of FIG. 1;

(6) FIG. 5 shows a sectional top view of the ball of FIG. 1, sectioned along sectional line V-V of FIG. 1, illustrating the deformation of the impact body when struck by a bat;

(7) FIG. 6 shows a sectional top view of another embodiment of a ball in accordance with the invention, which is configured for use as a streamer ball;

(8) FIG. 7 shows a sectional front view of the ball of FIG. 6, sectioned along section line VII-VII of FIG. 6;

(9) FIG. 8 shows a front view of the ball of FIG. 6;

(10) FIG. 9 shows a sectional top view of the ball of FIG. 6, sectioned along section line IX-IX of FIG. 6, illustrating the deformation of the impact body when struck by a bat;

(11) FIGS. 10a and 10b show sectional side views of an impact body of the ball of FIG. 6 which is subjected to a drop test, before and upon impact with a test impact surface, respectively, illustrating compression of the impact zone of the impact body upon impact with the test impact surface;

(12) FIG. 11 shows a sectional top view of a further embodiment of a ball in accordance with the invention, configured for use as a tethered ball;

(13) FIG. 12 shows a sectional side view of yet another embodiment of a ball in accordance with the invention, configured for use as a streamer ball;

(14) FIG. 13 shows a sectional side view of a further embodiment of a ball in accordance with the invention, which is configured for use as a streamer ball;

(15) FIG. 14a shows the flight orientation and deformation of a streamer ball having a relatively thicker-walled impact body, before, during and after impact by a bat; and

(16) FIG. 14b shows the flight orientation and deformation of a streamer ball having a relatively thinner-walled impact body, before, during and after impact by a bat.

DESCRIPTION OF PREFERRED EMBODIMENTS

(17) With reference to FIGS. 1 to 5 of the drawings, a ball in accordance with the invention which is configured for use as a tethered ball, is designated generally by the reference numeral 10. The ball 10 is specifically configured for use with bats having untensioned rigid ball-striking surfaces. The ball 10 comprises, broadly, a hollow spherical impact body 12 and flight control means in the form of a flight control assembly designated generally by the reference numeral 14.

(18) The impact body comprises a wall 16 of a resiliently compressible high grade rubber or rubber-like material surrounding an internal space 18. The wall defines a substantially smooth external surface 20. The impact body has a mass of between 10 g and 50 g and defines a centre of mass CM. The impact body defines a hole 22 of between 3 mm and 20 mm in diameter, providing an attachment point for the flight control assembly 14.

(19) The impact body defines an impact zone IA in the form of a circular impact band which extends around the impact body as is shown more clearly in FIGS. 2, 3 and 4. The impact band is defined by the wall of the impact body and preferably has a wall thickness between a minimum of 1 mm and a maximum of 3 mm. In the illustrated example, the wall thickness of the wall of the impact zone, is uniform. It will be appreciated, however, that the wall thickness of the impact body within the impact zone IA may vary between 1 mm and 3 mm. The thickness of the wall of the impact body in regions outside of the impact zone of the impact body 12, is relatively thicker. The impact zone is thus defined by a reduction in the wall thickness of the impact body. The extra weight provided by the thicker wall section outside of the impact zone contributes to the overall weight of the impact body thereby increasing the compression depth of the impact body at impact. The impact zone IA is convexly curved and has a predetermined radius of curvature “R” defined along an outer profile of the wall. The part of the wall of the impact body defining the impact zone, has a mass of between 0.15 g and 0.4 g per square centimeter of the wall, corresponding to an average wall thickness of between 1 mm and 3 mm.

(20) The flight control assembly 14 includes a tether cord 24 and an anchor fitting 26 for anchoring the tether cord to the wall of the impact body. More specifically, the tether cord has a proximal end 28 and a distal end 30, with the distal end 30 being rotatably attached to an upright post 32 which is anchored in the ground, in use.

(21) The anchor fitting 26 comprises, broadly, an anchor body 34, a disc-shaped shoulder-defining body 36, a flexible resilient cushioning washer 38 and a bearing body 40 which is connected to the distal end 28 of the tether cord 24. More specifically, the anchor body 34 comprises an elongate shank portion 42 and a head 44 at an inner end of shank portion, the shank portion operatively extending through the hole 22 defined in the wall of the impact body. The anchor body defines an axial passage which extends along the elongate shank portion and the head and through which the tether cord 24 extends. The tether cord has a stop formation 46 at its distal end, with the bearing body being operatively located between the stop formation and the head 44 of the anchor body thereby to operatively bear against the head of the anchor body, in use, so as to be rotatable relative to the head 44 to permit free rotation of the tether cord within the axial passage defined through the elongate shank portion on the head of the anchor body. It will be appreciated that the axial passage in the anchor body permits air flow communication between the internal space 18 of the impact body and ambient pressure externally of the impact body, thereby resulting in the internal space 18 of the impact body having an internal pressure equal to ambient pressure when the impact body is in a relaxed state and not deformed inwardly by a blow from a bat. The washer 38 is located between the shoulder-defining body 36 and an interior side of the wall 16 and serves to cushion and absorb impacts from blows to the impact body by a bat so as to protect the interior side of the wall of the impact body from point loads applied to the impact body from blows by a bat, in the region where the anchor fitting is fitted to the impact body.

(22) The tether cord 24 defines a tether cord axis Q which extends along the length of the tether cord and passes through the centre of mass CM of the impact body and extends through the centre of the impact band IA of the impact body when the tether cord is under tension, in use.

(23) The ball 10 is configured to be struck at the impact zone IA during a tether tennis-type ball game. It will be appreciated that after being struck by a bat, the impact body changes direction and typically spins on its axis after impact.

(24) The configuration of the impact body and in particular, the reduced wall thickness of the impact body within the impact zone, is such that the impact zone at the leading end region, of the impact body compresses to a minimum compression depth of 12 mm upon impact by a bat and bounces to a height of at least 100 cm when the impact body is subjected to the drop test as described hereinabove.

(25) FIG. 5 illustrates the deformation of the impact zone of the impact body when the impact body is struck by a bat 39.

(26) With reference to FIGS. 6 to 9 of the drawings, a ball in accordance with the invention which is configured for use as a streamer ball, is designated generally by the reference numeral 100. The ball 100 is similar to the ball 10. As such, features of the ball 100 which are the same as and/or similar to features of the ball 10, are designated in FIGS. 6 to 9 by the same and/or similar reference numerals.

(27) The ball 100 is configured for use with bats having untensioned rigid ball striking surfaces and comprises, broadly, a hollow spherical impact body 112 and flight control means in the form of a flight control assembly designated generally by the reference numeral 114.

(28) The impact body comprises a wall 116 of a resiliently compressible high grade rubber or rubber-like material surrounding an internal space 118. Due to the provision of the hole 122, the internal space 118 has a pressure approximately equal to atmospheric pressure when the ball is in a relaxed state and not deformed inwardly by a blow from a bat. The wall 116 defines a substantially smooth external surface 120. The impact body has a mass of between 10 g and 50 g and a diameter of between 25 mm and 95 mm and defines a centre of mass CM. The impact body defines a hole 122 of between 3 mm and 20 mm in diameter, providing an attachment point for the flight control assembly 114.

(29) The impact body defines a single impact zone IB which is defined by the wall of the impact body and which has a wall thickness of between 1 mm and 3 mm. In the illustrated example, the wall thickness of the wall of the impact zone, is uniform. It will be appreciated, however, that the wall thickness of the impact body within the impact zone IB may preferably vary between a minimum of 1 mm and a maximum of 3 mm. The part of the wall of the impact body defining the impact zone, has a mass of between 0.15 g and 0.4 g per square centimeter of the wall, corresponding to an average wall thickness of between 1 mm and 3 mm. The thickness of the wall of the impact body in regions of the impact body outside of the impact zone is relatively thicker. The impact zone is thus defined by a reduction in the wall thickness of the impact body in the impact zone. The impact zone IB is convexly curved and has a predetermined radius of curvature “R” defined along an outer profile of the wall.

(30) The flight control assembly 114 includes a tail 50 comprising one or more elongate thin flexible streamers 52, an elongate resiliently flexible spacer stem 54 and an anchor fitting 126. The spacer stem has a proximal end 56 which is attached to the impact body and a distal end 58 having an attachment formation 60 providing for attachment of the tail 50 to the spacer stem.

(31) The anchor fitting 126 comprises, broadly, an anchor body 134 which is integrally formed with the spacer stem, a disc-shaped shoulder-defining body 36, a flexible resilient internal cushioning washer 38 and a flexible resilient external retaining washer 62. More specifically, the anchor body 134 comprises an elongate shank portion 142 which operatively extends through the hole 122 defined in the wall of the impact body. The shank portion has a pair of flanges 144.1 and 144.2 at opposite ends thereof. More particularly, the flange 144.1 is disposed at an inner end of the shank portion and abuts an inner side of the shoulder-defining body 36, with the flange 144.2 being disposed at an outer end of the shank portion, externally of the impact body. The external washer 62 is located between an external side of the impact body and the flange 144.2 in a tensioned state, thereby limiting axial displacement of the shank portion within the hole 122.

(32) The shank portion 142 of the anchor body 134 is received in the hole 122 in a fit which is not airtight, thereby resulting in the internal space 18 of the impact body, having an internal pressure equal to ambient pressure when the impact body is in a relaxed state and not deformed inwardly by a blow from a bat.

(33) The elongate spacer stem 54 defines a longitudinal axis L along the length thereof which intersects the centre of mass CM of the impact body and passes through a centre of the impact zone IB. The impact zone IB is thus disposed diametrically opposite the attachment point defined by the hole 122 of the impact body. It will be appreciated that the impact zone IB defines a leading end of the impact body and the attachment point defined by the hole 122 defines a trailing end of the impact body in flight. The configuration of the impact body and in particular, the reduced wall thickness of the impact body within the impact zone is such that the impact zone compresses to a minimum compression depth of 12 mm and the impact body bounces to a height of at least 100 cm when the impact body is subjected to the drop test as described hereinabove.

(34) FIG. 9 illustrates the deformation of the impact zone IB of the impact body when the impact body is struck by a bat 39.

(35) FIG. 10a shows a sectional side view of the impact body 112 of the streamer ball 100 in a relaxed, uncompressed state prior to impact with a test impact surface 139, while FIG. 10b shows a sectional side view of the impact 112 upon impact with the test impact surface when the impact body is subjected to a drop test. It will be appreciated that impact with the test impact surface simulates impact by a bat.

(36) FIG. 10b illustrates the compression of the impact zone IB of the impact body 112 upon impact with the test impact surface. At maximum compression of the impact zone, the impact zone compresses to a minimum compression depth of 12 mm. Thereafter, the impact body bounces to a height of at least 100 cm.

(37) It will be appreciated that in a similar drop test, the impact body 12 of the tethered ball 10, exhibits the same test results wherein the impact zone IA compresses to a minimum compression depth of 12 mm. Thereafter, the impact body bounces to a height of at least 100 cm.

(38) FIG. 11 shows a further embodiment of a ball in accordance with the invention which is designated by the reference numeral 200 and which is configured for use as a tethered ball. The ball 200 is similar to the ball 10, with the only difference being that the wall of the impact body of the ball 200 has a uniform thickness throughout of between 1 mm and 3 mm resulting in the entire wall having the characteristics of an impact zone which compresses to a minimum compression depth of 12 mm and bounces to a height of at least 100 cm when the impact body is subjected to the drop test described hereinabove.

(39) FIG. 12 shows yet another embodiment of a ball in accordance with the invention which is designated by the reference numeral 300 and which is configured for use as a streamer ball. The ball 300 is similar to the ball 100 with the only difference being that the wall of the impact body has a uniform thickness throughout of between 1 mm and 3 mm resulting in the entire wall constituting an impact zone wherein the impact body compresses to a minimum compression depth of 12 mm and bounces to a height of at least 100 cm when the impact body is subject to the drop test described hereinabove.

(40) FIG. 13 shows a further embodiment of a ball in accordance with the invention, which is designated by the reference 400. The ball 400 is similar to the ball 300, with the main difference being that ball includes flight control means in the form of a flight control assembly 414 which is attached to an external side of the wall 416 of the impact body 412. Features of the ball 400 which are the same as and/or similar to features of the ball 300, are designated in FIG. 13 by the same and/or similar reference numerals.

(41) The impact body defines a spigot formation 80 which projects from the wall 412 thereof for attachment of the flight control assembly to the impact body. The flight control assembly 414 includes a tail 50 comprising streamers 52 and an elongate resiliently flexible spacer stem 454 having a proximal end 456 and a distal end 458. The distal end has an attachment formation 60 providing for attachment of the tail to the spacer stem. The proximal end of the spacer stem defines a socket formation 82 defining a socket within which the spigot formation 80 of the impact body is securely received for securely attaching the spacer stem to the impact body.

(42) The Applicant believes that the flight-controlled tethered and streamer balls, in accordance with the invention, provide the characteristics required for use with lightweight bats having untensioned, rigid ball-striking surfaces. More specifically, the impact body of the flight-controlled balls in accordance with the invention, are relatively light in weight as is required for use with lightweight bats and exhibit a sufficiently high degree of compression upon impact by a bat so as to achieve a solid contact between the impact body and the bat with minimal unpleasant handle vibration. The applicant believes that this characteristic is due to the fact that the impact body spreads out over the ball-striking surface of the bat thereby making contact with the bat over a relatively large surface area which has the result of reducing the contact pressure between the bat and the impact body upon impact by the bat.

(43) Reducing the weight of the impact body to between 10 g and 50 g enables the use of a bat weighing at most only 250 g (based on an impact body to bat weight ratio of 1:5 using the maximum impact body weight of 50 g). This allows significant drop in the bat weight from around 300 g for a conventional unstrung, rigid-faced bat as described hereinafter in the “Background To Invention” section of this specification.

(44) It should also be appreciated that the average wall thickness of the rubber core of a regulation tennis ball is approximately 3.5 mm. A maximum wall thickness of the impact zone of the impact body of the balls in accordance with the present invention, of 3 mm, is envisaged which results in the significant advantageous performance characteristics described herein.

(45) Furthermore, the provision of a relatively thin wall at least in the impact zone of the impact body, renders the impact zone of the impact body relatively more flexible so that the impact body compresses more on impact (as measured by the size of the impact contact mark made by the impact body during impact as is evident from the drop test described herein) despite the lighter weight of the impact body. This permits the transfer of more kinetic energy from the moving bat to the impact body during contact with the impact body as the impact body is in contact with the bat for a longer period of time. The relatively thinner wall of the impact body at least in the region of the impact zone, causes less energy to be expended in the deformation process when the impact zone of the impact body flattens upon impact by a bat. As a result, more energy is available to be transferred to the impact body itself enabling enhanced spring off the bat. Tests conducted by the Applicant on the bounce characteristics of such thin-walled impact bodies support this contention as is further evidenced by the drop test characteristics for the impact body, as described hereinabove.

(46) Furthermore, it follows that the performance of such balls may be enhanced by providing an impact body having a variable wall thickness wherein the wall thickness of the impact body outside the impact zone may be selectively made relatively thicker so as to avoid excessive loss of weight of the impact body as a whole. The extra weight provided by the thicker wall section contributes to the overall weight of the impact body thereby increasing the compression depth of the impact body at impact.

(47) In FIGS. 14a and 14b of the drawings, a comparison is provided illustrating the difference in flight characteristics and deformation of a streamer ball having a relatively thicker-walled impact body (as shown in FIG. 14a) and a streamer ball having a relatively thinner-walled impact body (as shown in FIG. 14b). As the comparison requires the thicker and thinner-walled impact bodies to be the same mass it follows that the thicker-walled impact body will have a relatively smaller diameter than the thinner-walled impact body. From the comparison, it can be seen that the thinner-walled impact body spreads out more over the bat surface at impact compared to the thicker-walled impact body, resulting in a bigger contact footprint. This results in a more desirable solid impact feel with less vibration of the bat. It will be appreciated that the bigger contact footprint of a thinner-walled impact body means that the impact body has compressed more and is thus in contact with the bat for longer, resulting in more energy being imparted to the impact body during this time so as to result in a increased departure speed of the impact body off the bat.

(48) More specifically, a thinner-walled impact body absorbs less energy while deforming compared to a thicker-walled impact body and as a result, springs back to its original shape more quickly while pressing against the bat and therefore departs from the bat at greater speed.

(49) FIGS. 14a and 14b therefore illustrate the beneficial characteristics imparted to the balls 10, 100, 200, 300 and 400 in accordance with the invention, by the relatively thinner-walled impact zones of each of the impact bodies of the balls which thus provide for departure of the impact body at a higher speed off a bat at impact, the dispersal of the impact shock over a wider area of the impact body and the bat and a longer dwell time on the bat, resulting in a sweeter impact feel with less shock and vibration.