Patent Publication Number: US-2017368417-A1

Title: Golf ball

Description:
This application claims priority on Patent Application No. 2016-125201 filed in JAPAN on Jun. 24, 2016. The entire contents of this Japanese Patent Application are hereby incorporated by reference. 
     BACKGROUND OF THE INVENTION 
     Field of the Invention 
     The present invention relates to golf balls. Specifically, the present invention relates to golf balls including a core, a mid layer, a cover, and dimples. 
     Description of the Related Art 
     The greatest interest to golf players concerning golf balls is flight distance. In particular, golf players place importance on flight distances upon shots with a driver. There have been various proposals for improvement of flight performance. JP2010-188199 discloses a golf ball including a core having a high hardness at the surface thereof and a low hardness at the central point thereof. JP2013-31778 discloses a golf ball of which the hardness gradually increases from the central point of a core toward the surface of the core. 
     Golf balls have a large number of dimples on the surfaces thereof. The dimples disturb the air flow around the golf ball during flight to cause turbulent flow separation. This phenomenon is referred to as “turbulization”. Due to the turbulization, separation points of the air from the golf ball shift backwards leading to a reduction of drag. The turbulization promotes the displacement between the separation point on the upper side and the separation point on the lower side of the golf ball, which results from the backspin, thereby enhancing the lift force that acts upon the golf ball. Excellent dimples efficiently disturb the air flow. The excellent dimples produce a long flight distance. 
     There have been various proposals for dimples. JP2009-172192 (US2009/0191982) discloses a golf ball on which dimples are randomly arranged. The dimple pattern of the golf ball is referred to as a random pattern. The random pattern can contribute to the flight performance of the golf ball. JP2012-10822 (US2012/0004053) also discloses a golf ball having a random pattern. 
     JP2007-175267 (US2007/0149321) discloses a dimple pattern in which the number of units in a high-latitude region is different from the number of units in a low-latitude region. JP2007-195591 (US2007/0173354) discloses a dimple pattern in which the number of the types of dimples in a low-latitude region is larger than the number of the types of dimples in a high-latitude region. JP2013-153966 (US2013/0196791) discloses a dimple pattern having a high dimple density and small variation in dimple size. 
     There have also been various proposals for improvement of compositions of cores for the purpose of enhancing flight performance. JP2008-212681 (US2008/0214324) discloses a golf ball including a core formed from a rubber composition including a copper salt. The core has excellent resilience performance upon a shot with a driver. JP2008-194471 (U.S. Pat. No. 7,344,455 and US2008/0194359) discloses a golf ball including a core formed from a rubber composition including an anti-aging agent. The core contributes to flight performance upon a shot with a driver at a low head speed. 
     Another interest to golf players concerning golf balls is feel at impact. In general, golf players prefer soft feel at impact. Hitherto, improvement in feel at impact upon shots with an iron has been made. However, there is room for improvement in feel at impact upon shots with a driver. 
     An object of the present invention is to provide a golf ball having excellent flight performance and feel at impact upon a shot with a driver. 
     SUMMARY OF THE INVENTION 
     A golf ball according to the present invention includes a core, a mid layer positioned outside the core, and a cover positioned outside the mid layer. A thickness Tm (mm) and a Shore D hardness Hm of the mid layer, a thickness Tc (mm) and a Shore D hardness Hc of the cover, and an amount of compressive deformation Sb (mm) of the golf ball meet the following mathematical formula (2). 
       (( Sb*Tc )/( Hc*Hm*Tm ))*1000&gt;0.75   (2)
 
     The golf ball has a plurality of dimples on a surface thereof. A ratio So of a sum of areas of the dimples relative to a surface area of a phantom sphere of the golf ball is equal to or greater than 81.0%. A ratio Rs of a number of the dimples each having a diameter of equal to or greater than 9.60% but equal to or less than 10.37%, of a diameter of the golf ball, relative to a total number of the dimples, is equal to or greater than 50%. A dimple pattern of each hemisphere of the phantom sphere includes three units that are rotationally symmetrical to each other. A dimple pattern of each unit includes two small units that are mirror-symmetrical to each other. The golf ball meets the following mathematical formula (3). 
         Rs ≧−2.5 *So +273   (3)
 
     The golf ball according to the present invention has excellent resilience performance when being hit with a driver. When the golf ball is hit with a driver, the spin rate is low. Furthermore, the dimple pattern of the golf ball has an excellent aerodynamic characteristic. The golf ball has excellent flight performance when being hit with a driver. When the golf ball is hit with a driver, the shock is small. When the golf ball is hit with a driver, the feel at impact is soft. The golf ball is excellent in both flight performance and feel at impact when being hit with a driver. 
     Preferably, a difference DH in Shore C hardness between a surface and a central point of the core meets the following mathematical formula (1). 
       ( DH*Hm )/( Hc*Tc )&gt;80   (1)
 
     Preferably, the hardness Hc of the cover is equal to or less than 40. 
     Preferably, the hardness Hm of the mid layer is equal to or greater than 55. 
     Preferably, the golf ball meets the following mathematical formula (4). 
         Rs ≧−2.5 *So +278   (4)
 
     Preferably, the golf ball meets the following mathematical formula (5). 
         Rs ≧−2.5 *So +283   (5)
 
     Preferably, a ratio Rs′ of a number of the dimples each having a diameter of equal to or greater than 10.10% but equal to or less than 10.37%, of the diameter of the golf ball, relative to the total number of the dimples, is equal to or greater than 50%. Preferably, the golf ball meets the following mathematical formula (6). 
         Rs ′≧−2.2 *So +245   (6)
 
     Preferably, the golf ball meets the following mathematical formula (7). 
         Rs ′≧−2.2* So +252   (7)
 
     Preferably, a depth of a deepest part of each dimple from a surface of the phantom sphere is equal to or greater than 0.10 mm but equal to or less than 0.65 mm. 
     Preferably, a total volume of the dimples is equal to or greater than 450 mm 3  but equal to or less than 750 mm 3 . 
    
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
         FIG. 1  is a cross-sectional view of a golf ball according to one embodiment of the present invention; 
         FIG. 2  is a plan view of the golf ball in  FIG. 1 ; 
         FIG. 3  is a front view of the golf ball in  FIG. 2 ; 
         FIG. 4  is a partially enlarged cross-sectional view of the golf ball in  FIG. 1 ; 
         FIG. 5  is a graph showing a relationship between a ratio So and a ratio Rs; 
         FIG. 6  is a graph showing a relationship between the ratio So and a ratio Rs′; 
         FIG. 7  is a plan view of a golf ball according to Example 2 of the present invention; 
         FIG. 8  is a front view of the golf ball in  FIG. 7 ; 
         FIG. 9  is a plan view of a golf ball according to Example 3 of the present invention; 
         FIG. 10  is a front view of the golf ball in  FIG. 9 ; 
         FIG. 11  is a plan view of a golf ball according to Example 4 of the present invention; 
         FIG. 12  is a front view of the golf ball in  FIG. 11 ; 
         FIG. 13  is a plan view of a golf ball according to Comparative Example 1 
         FIG. 14  is a front view of the golf ball in  FIG. 13 ; 
         FIG. 15  is a plan view of a golf ball according to Comparative Example 2; 
         FIG. 16  is a front view of the golf ball in  FIG. 15 ; 
         FIG. 17  is a plan view of a golf ball according to Comparative Example 3; 
         FIG. 18  is a front view of the golf ball in  FIG. 17 ; 
         FIG. 19  is a plan view of a golf ball according to Comparative Example 4; 
         FIG. 20  is a bottom view of the golf ball in  FIG. 19 ; 
         FIG. 21  is a right side view of the golf ball in FIG. 
         19 ; 
         FIG. 22  is a front view of the golf ball in  FIG. 19 ; 
         FIG. 23  is a left side view of the golf ball in  FIG. 19 ; 
         FIG. 24  is a back view of the golf ball in  FIG. 19 ; 
         FIG. 25  is a plan view of a golf ball according to Comparative Example 5; and 
         FIG. 26  is a front view of the golf ball in  FIG. 25 . 
     
    
    
     DESCRIPTION OF THE PREFERRED EMBODIMENTS 
     The following will describe in detail the present invention based on preferred embodiments with appropriate reference to the drawings. 
     A golf ball  2  shown in  FIG. 1  includes a spherical core  4 , a midlayer  6  positioned outside the core  4 , and a cover  8  positioned outside the mid layer  6 . The golf ball  2  has a plurality of dimples  10  on the surface thereof. Of the surface of the golf ball  2 , a part other than the dimples  10  is a land  12 . The golf ball  2  includes a paint layer and a mark layer on the external side of the cover  8  although these layers are not shown in the drawing. The golf ball  2  may include another layer between the core  4  and the mid layer  6 . The golf ball  2  may include another layer between the midlayer  6  and the cover  8 . 
     The golf ball  2  preferably has a diameter of equal to or greater than 40 mm but equal to or less than 45 mm. From the standpoint of conformity to the rules established by the United States Golf Association (USGA), the diameter is particularly preferably equal to or greater than 42.67 mm. In light of suppression of air resistance, the diameter is more preferably equal to or less than 44 mm and particularly preferably equal to or less than 42.80 mm. The golf ball  2  preferably has a weight of equal to or greater than 40 g but equal to or less than 50 g. In light of attainment of great inertia, the weight is more preferably equal to or greater than 44 g and particularly preferably equal to or greater than 45.00 g. From the standpoint of conformity to the rules established by the USGA, the weight is particularly preferably equal to or less than 45.93 g. 
     The core  4  is formed by crosslinking a rubber composition. Examples of preferable base rubbers for use in the rubber composition include polybutadienes, polyisoprenes, styrene-butadiene copolymers, ethylene-propylene-diene copolymers, and natural rubbers. In light of resilience performance, polybutadienes are preferable. When a polybutadiene and another rubber are used in combination, it is preferred if the polybutadiene is a principal component. Specifically, the proportion of the polybutadiene to the entire base rubber is preferably equal to or greater than 50% by weight and particularly preferably equal to or greater than 80% by weight. A polybutadiene in which the proportion of cis-1,4 bonds is equal to or greater than 80% is particularly preferable. 
     The rubber composition of the core  4  preferably includes a co-crosslinking agent. Preferable co-crosslinking agents in light of resilience performance are monovalent or bivalent metal salts of an α, β-unsaturated carboxylic acid having 2 to 8 carbon atoms. Examples of preferable co-crosslinking agents include zinc acrylate, magnesium acrylate, zinc methacrylate, and magnesium methacrylate. In light of resilience performance, zinc acrylate and zinc methacrylate are particularly preferable. 
     The rubber composition may include a metal oxide and an α, β-unsaturated carboxylic acid having 2 to 8 carbon atoms. They both react with each other in the rubber composition to obtain a salt. The salt serves as a co-crosslinking agent. Examples of preferable α, β-unsaturated carboxylic acids include acrylic acid and methacrylic acid. Examples of preferable metal oxides include zinc oxide and magnesium oxide. 
     In light of resilience performance of the golf ball  2 , the amount of the co-crosslinking agent per 100 parts by weight of the base rubber is preferably equal to or greater than 10 parts by weight and particularly preferably equal to or greater than 15 parts by weight. In light of soft feel at impact, the amount is preferably equal to or less than 50 parts by weight and particularly preferably equal to or less than 45 parts by weight. 
     Preferably, the rubber composition of the core  4  includes an organic peroxide. The organic peroxide serves as a crosslinking initiator. The organic peroxide contributes to the resilience performance of the golf ball  2 . Examples of suitable organic peroxides include dicumyl peroxide, 1,1-bis(t-butylperoxy)-3,3,5-trimethylcyclohexane, 2,5-dimethyl-2,5-di(t-butylperoxy)hexane, and di-t-butyl peroxide. An organic peroxide with particularly high versatility is dicumyl peroxide. 
     In light of resilience performance of the golf ball  2 , the amount of the organic peroxide per 100 parts by weight of the base rubber is preferably equal to or greater than 0.1 parts by weight, more preferably equal to or greater than 0.3 parts by weight, and particularly preferably equal to or greater than 0.5 parts by weight. In light of soft feel at impact, the amount is preferably equal to or less than 3.0 parts by weight, more preferably equal to or less than 2.8 parts by weight, and particularly preferably equal to or less than 2.5 parts by weight. 
     Preferably, the rubber composition of the core  4  includes an organic sulfur compound. Organic sulfur compounds include naphthalenethiol compounds, benzenethiol compounds, and disulfide compounds. 
     Examples of naphthalenethiol compounds include 1-naphthalenethiol, 2-naphthalenethiol, 4-chloro-1-naphthalenethiol, 4-bromo-l-naphthalenethiol, 1-chloro-2-naphthalenethiol, 1-bromo-2-naphthalenethiol, 1-fluoro-2-naphthalenethiol, 1-cyano-2-naphthalenethiol, and 1-acetyl-2-naphthalenethiol. 
     Examples of benzenethiol compounds include benzenethiol, 4-chlorobenzenethiol, 3-chlorobenzenethiol, 4-bromobenzenethiol, 3-bromobenzenethiol, 4-fluorobenzenethiol, 4-iodobenzenethiol, 2,5-dichlorobenzenethiol, 3,5-dichlorobenzenethiol, 2,6-dichlorobenzenethiol, 2,5-dibromobenzenethiol, 3,5-dibromobenzenethiol, 2-chloro-5-bromobenzenethiol, 2,4,6-trichlorobenzenethiol, 2,3,4,5,6-pentachlorobenzenethiol, 2,3,4,5,6-pentafluorobenzenethiol, 4-cyanobenzenethiol, 2-cyanobenzenethiol, 4-nitrobenzenethiol, and 2-nitrobenzenethiol. 
     Examples of disulfide compounds include diphenyl disulfide, bis(4-chlorophenyl)disulfide, bis(3-chlorophenyl)disulfide, bis(4-bromophenyl)disulfide, bis(3-bromophenyl)disulfide, bis(4-fluorophenyl)disulfide, bis(4-iodophenyl)disulfide, bis(4-cyanophenyl)disulfide, bis(2,5-dichlorophenyl)disulfide, bis(3,5-dichlorophenyl)disulfide, bis(2,6-dichlorophenyl)disulfide, bis(2,5-dibromophenyl)disulfide, bis(3,5-dibromophenyl)disulfide, bis(2-chloro-5-bromophenyl) disulfide, bis(2-cyano-5-bromophenyl)disulfide, bis(2,4,6-trichlorophenyl)disulfide, bis(2-cyano-4-chloro-6-bromophenyl)disulfide, bis(2,3,5,6-tetrachlorophenyl)disulfide, bis(2,3,4,5,6-pentachlorophenyl)disulfide, and bis(2,3,4,5,6-pentabromophenyl) disulfide. 
     In light of resilience performance of the golf ball  2 , the amount of the organic sulfur compound per 100 parts by weight of the base rubber is preferably equal to or greater than 0.1 parts by weight and particularly preferably equal to or greater than 0.2 parts by weight. In light of soft feel at impact, the amount is preferably equal to or less than 1.5 parts by weight, more preferably equal to or less than 1.0 parts by weight, and particularly preferably equal to or less than 0.8 parts by weight. Two or more organic sulfur compounds may be used in combination. A naphthalenethiol compound and a disulfide compound are preferably used in combination. 
     Preferably, the rubber composition of the core  4  includes a carboxylic acid or a carboxylate. The core  4  including a carboxylic acid or a carboxylate has a low hardness around the central point thereof. The core  4  has an outer-hard/inner-soft structure. When the golf ball  2  including the core  4  is hit with a driver, the spin rate is low. With the golf ball  2  having a low spin rate, a large flight distance is obtained. Examples of preferable carboxylic acids include benzoic acid. Examples of preferable carboxylates include zinc octoate and zinc stearate. The rubber composition particularly preferably includes benzoic acid. The amount of the carboxylic acid and/or the carboxylate per 100 parts by weight of the base rubber is preferably equal to or greater than 1 parts by weight but equal to or less than 20 parts by weight. 
     The rubber composition of the core  4  may include a filler for the purpose of specific gravity adjustment and the like. Examples of suitable fillers include zinc oxide, barium sulfate, calcium carbonate, and magnesium carbonate. The amount of the filler is determined as appropriate so that the intended specific gravity of the core  4  is accomplished. The rubber composition may include various additives, such as sulfur, an anti-aging agent, a coloring agent, a plasticizer, a dispersant, and the like, in an adequate amount. The rubber composition may include crosslinked rubber powder or synthetic resin powder. 
     The core  4  preferably has a diameter of equal to or greater than 38.0 mm. The golf ball  2  including the core  4  having a diameter of equal to or greater than 38.0 mm has excellent resilience performance. In this respect, the diameter is more preferably equal to or greater than 38.5 mm and particularly preferably equal to or greater than 39.5 mm. From the standpoint that the midlayer  6  and the cover  8  can have sufficient thicknesses, the diameter is preferably equal to or less than 41.0 mm and particularly preferably equal to or less than 40.5 mm. 
     The core  4  has a weight of preferably equal to or greater than 10 g but equal to or less than 40 g. The temperature for crosslinking the core  4  is equal to or higher than 140° C. but equal to or lower than 180° C. The time period for crosslinking the core  4  is equal to or longer than 10 minutes but equal to or shorter than 60 minutes. The core  4  may have two or more layers. The core  4  may have a rib on the surface thereof. The core  4  may be hollow. 
     In the golf ball  2  , the difference DH between a hardness H1 at the central point of the core  4  and a hardness H2 at the surface of the core  4  is great. The core  4  having the great difference DH has a so-called outer-hard/inner-soft structure. When the golf ball  2  including the core  4  is hit with a driver, the spin is suppressed. When the golf ball  2  including the core  4  is hit with a driver, a high launch angle is obtained. 
     Upon a shot with a driver, an appropriate trajectory height and appropriate flight duration are required. With the golf ball  2  that achieves a desired trajectory height and desired flight duration at a high spin rate, the run after landing is short. With the golf ball  2  that achieves a desired trajectory height and desired flight duration at a high launch angle, the run after landing is long. In light of flight distance, the golf ball  2  that achieves a desired trajectory height and desired flight duration at a high launch angle is preferable. The core  4  having an outer-hard/inner-soft structure can contribute to a high launch angle and a low spin rate as described above. The golf ball  2  including the core  4  has excellent flight performance. 
     In light of flight performance, the difference DH is preferably equal to or greater than 20 and particularly preferably equal to or greater than 25. In light of ease of producing the core  4 , the difference DH is preferably equal to or less than 50 and particularly preferably equal to or less than 45. 
     In light of resilience performance, the central hardness H1 is preferably equal to or greater than 30, more bpreferably equal to or greater than 35, and particularly preferably equal to or greater than 40. In light of spin suppression and feel at impact, the hardness H1 is preferably equal to or less than 70, more preferably equal to or less than 65, and particularly preferably equal to or less than 60. 
     The hardness H1 is measured with a Shore C type hardness scale mounted to an automated hardness meter (trade name “digi test II” manufactured by Heinrich Bareiss Prüfgerätebau GmbH). The hardness scale is pressed against the central point of the cross-section of a hemisphere obtained by cutting the golf ball  2 . The measurement is conducted in the environment of 23° C. 
     In light of spin suppression, the surface hardness H2 is preferably equal to or greater than 70, more preferably equal to or greater than 72, and particularly preferably equal to or greater than 74. In light of durability of the golf ball  2  , the hardness H2 is preferably equal to or less than 90, more preferably equal to or less than 88, and particularly preferably equal to or less than 86. 
     The hardness H2 is measured with a Shore C type hardness scale mounted to an automated hardness meter (trade name “digi test II” manufactured by Heinrich Bareiss Prüfgerätebau GmbH). The hardness scale is pressed against the surface of the core  4 . The measurement is conducted in the environment of 23° C. 
     The midlayer  6  is positioned between the core  4  and the cover  8 . The midlayer  6  is formed from a thermoplastic resin composition. Examples of the base polymer of the resin composition include ionomer resins, thermoplastic polyester elastomers, thermoplastic polyamide elastomers, thermoplastic polyurethane elastomers, thermoplastic polyolefin elastomers, and thermoplastic polystyrene elastomers. Ionomer resins are particularly preferable. Ionomer resins are highly elastic. The golf ball  2  that includes the midlayer  6  including an ionomer resin has excellent resilience performance. 
     An ionomer resin and another resin may be used in combination. In this case, in light of resilience performance, the ionomer resin is included as the principal component of the base polymer. The proportion of the ionomer resin to the entire base polymer is preferably equal to or greater than 50% by weight, more preferably equal to or greater than 70% by weight, and particularly preferably equal to or greater than 85% by weight. 
     Examples of preferable ionomer resins include binary copolymers formed with an α-olefin and an α, β-unsaturated carboxylic acid having 3 to 8 carbon atoms. A preferable binary copolymer includes 80% by weight or more but 90% by weight or less of an α-olefin , and 10% by weight or more but 20% by weight or less of an α, β-unsaturated carboxylic acid. The binary copolymer has excellent resilience performance. Examples of other preferable ionomer resins include ternary copolymers formed with: an α-olefin ; an α, β-unsaturated carboxylic acid having 3 to 8 carbon atoms; and an α, β-unsaturated carboxylate ester having 2 to 22 carbon atoms. A preferable ternary copolymer includes 70% by weight or more but 85% by weight or less of an α-olefin , 5% by weight or more but 30% by weight or less of an α, β-unsaturated carboxylic acid, and 1% by weight or more but 25% by weight or less of an α, β-unsaturated carboxylate ester. The ternary copolymer has excellent resilience performance. For the binary copolymer and the ternary copolymer, preferable α-olefins are ethylene and propylene, while preferable α, β-unsaturated carboxylic acids are acrylic acid and methacrylic acid. A particularly preferable ionomer resin is a copolymer formed with ethylene and acrylic acid. Another particularly preferable ionomer resin is a copolymer formed with ethylene and methacrylic acid. 
     In the binary copolymer and the ternary copolymer, some of the carboxyl groups are neutralized with metal ions. Examples of metal ions for use in neutralization include sodium ion, potassium ion, lithium ion, zinc ion, calcium ion, magnesium ion, aluminum ion, and neodymium ion. The neutralization may be carried out with two or more types of metal ions. Particularly suitable metal ions in light of resilience performance and durability of the golf ball  2  are sodium ion, zinc ion, lithium ion, and magnesium ion. 
     Specific examples of ionomer resins include trade names “Himilan 1555”, “Himilan 1557”, “Himilan 1605”, “Himilan 1706”, “Himilan 1707”, “Himilan 1856”, “Himilan 1855”, “Himilan AM7311”, “Himilan AM7315”, “Himilan AM7317”, “Himilan AM7329”, and “Himilan AM7337”, manufactured by Du Pont-MITSUI PCLYCHEMICALS Co., Ltd.; trade names “Surlyn 6120”, “Surlyn 6910”, “Surlyn 7930”, “Surlyn 7940”, “Surlyn 8140”, “Surlyn 8150”, “Surlyn 8940”, “Surlyn 8945”, “Surlyn 9120”, “Surlyn 9150”, “Surlyn 9910”, “Surlyn 9945”, “Surlyn AD8546”, “HPF1000”, and “HPF2000”, manufactured by E.I. du Pont de Nemours and Company; and trade names “IOTEK 7010”, “IOTEK 7030”, “IOTEK 7510”, “IOTEK 7520”, “IOTEK 8000”, and “IOTEK 8030”, manufactured by ExxonMobil Chemical Corporation. Two or more ionomer resins may be used in combination. 
     The resin composition of the midlayer  6  may include a styrene block-containing thermoplastic elastomer. The styrene block-containing thermoplastic elastomer includes a polystyrene block as a hard segment, and a soft segment. A typical soft segment is a diene block. Examples of compounds for the diene block include butadiene, isoprene, 1,3-pentadiene, and 2,3-dimethyl-1,3-butadiene. Butadiene and isoprene are preferable. Two or more compounds may be used in combination. 
     Examples of styrene block-containing thermoplastic elastomers include styrene-butadiene-styrene block copolymers (SBS), styrene-isoprene-styrene block copolymers (SIS), styrene-isoprene-butadiene-styrene block copolymers (SIBS), hydrogenated SBS, hydrogenated SIS, and hydrogenated SIBS. Examples of hydrogenated SBS include styrene-ethylene-butylene-styrene block copolymers (SEBS). Examples of hydrogenated SIS include styrene-ethylene-propylene-styrene block copolymers (SEPS). Examples of hydrogenated SIBS include styrene-ethylene-ethylene-propylene-styrene block copolymers (SEEPS). 
     In light of resilience performance of the golf ball  2 , the content of the styrene component in the styrene block-containing thermoplastic elastomer is preferably equal to or greater than 10% by weight, more preferably equal to or greater than 12% by weight, and particularly preferably equal to or greater than 15% by weight. In light of feel at impact of the golf ball  2  , the content is preferably equal to or less than 50% by weight, more preferably equal to or less than 47% by weight, and particularly preferably equal to or less than 45% by weight. 
     In the present invention, styrene block-containing thermoplastic elastomers include an alloy of an olefin and one or more members selected from the group consisting of SBS, SIS, SIBS, SEBS, SEPS, and SEEPS. The olefin component in the alloy is presumed to contribute to improvement of compatibility with another base polymer. The alloy can contribute to the resilience performance of the golf ball  2 . An olefin having 2 to 10 carbon atoms is preferable. Examples of suitable olefins include ethylene, propylene, butene, and pentene. Ethylene and propylene are particularly preferable. 
     Specific examples of polymer alloys include trade names “RABALON T3221C”, “RABALON T3339C”, “RABALON SJ4400N”, “RABALON SJ5400N”, “RABALON SJ6400N”, “RABALON SJ7400N”, “RABALON SJ8400N”, “RABALON SJ9400N”, and “RABALON SR04”, manufactured by Mitsubishi Chemical Corporation. Other specific examples of styrene block-containing thermoplastic elastomers include trade name “Epofriend A1010” manufactured by Daicel Chemical Industries, Ltd., and trade name “SEPTON HG-252” manufactured by Kuraray Co., Ltd. 
     In light of feel at impact, the proportion of the styrene block-containing thermoplastic elastomer to the entire base polymer is preferably equal to or greater than 1% by weight and particularly preferably equal to or greater than 2% by weight. In light of spin suppression, the proportion is preferably equal to or less than 20% by weight, more preferably equal to or less than 15% by weight, and particularly preferably equal to or less than 10% by weight. 
     The resin composition of the midlayer  6  may include a polyamide. With the golf ball  2  that includes the mid layer  6  including a polyamide, the spin is suppressed. Specific examples of polyamides include polyamide 6, polyamide 11, polyamide 12, polyamide 66, and polyamide 610. In light of versatility, polyamide 6 is preferable. 
     The resin composition of the midlayer  6  may include a filler for the purpose of specific gravity adjustment and the like. Examples of suitable fillers include zinc oxide, barium sulfate, calcium carbonate, and magnesium carbonate. The resin composition may include powder of a metal with a high specific gravity. Specific examples of metals with a high specific gravity include tungsten and molybdenum. The amount of the filler is determined as appropriate so that the intended specific gravity of the midlayer  6  is accomplished. The resin composition may include a coloring agent, crosslinked rubber powder, or synthetic resin powder. When the hue of the golf ball  2  is white, a typical coloring agent is titanium dioxide. 
     The midlayer  6  preferably has a hardness Hm of equal to or greater than 55. With the golf ball  2  that includes the midlayer  6  having a hardness Hm of equal to or greater than 55, the spin rate upon a shot with a driver is suppressed. The midlayer  6  can contribute to the flight performance of the golf ball  2 . In this respect, the hardness Hm is more preferably equal to or greater than 58 and particularly preferably equal to or greater than 61. In light of feel at impact upon a shot with a driver, the hardness Hm is preferably equal to or less than 80, more preferably equal to or less than 75, and particularly preferably equal to or less than 72. 
     The hardness Hm of the midlayer  6  is measured according to the standards of “ASTM-D 2240-68”. The hardness Hm is measured with a Shore D type hardness scale mounted to an automated hardness meter (trade name “digi test II” manufactured by Heinrich Bareiss Prüfgerätebau GmbH). For the measurement, a sheet that is formed by hot press, is formed from the same material as that of the mid layer  6 , and has a thickness of about 2 mm is used. Prior to the measurement, a sheet is kept at 23° C. for two weeks. At the measurement, three sheets are stacked. 
     The midlayer  6  has a thickness Tm of preferably equal to or greater than 0.3 mm but equal to or less than 2.5 mm. With the golf ball  2  that includes a midlayer  6  having a thickness Tm of equal to or greater than 0.3 mm, the spin upon a shot with a driver is suppressed. In this respect, the thickness Tm is more preferably equal to or greater than 0.5 mm and particularly preferably equal to or greater than 0.8 mm. With the golf ball  2  that includes the mid layer  6  having a thickness Tm of equal to or less than 2.5 mm, soft feel at impact is obtained upon a shot with a driver. In this respect, the thickness Tm is more preferably equal to or less than 2.0 mm and particularly preferably equal to or less than 1.8 mm. The thickness Tm is measured at a position immediately below the land  12 . 
     The golf ball  2  may include two or more mid layers  6  positioned between the core  4  and the cover  8 . In this case, the thickness of each midlayer  6  preferably falls within the above range. 
     The cover  8  is the outermost layer except the mark layer and the paint layer. The cover  8  is formed from a resin composition. Examples of the base polymer of the resin composition include polyurethanes, ionomer resins, polyesters, polyamides, polyolefins, and polystyrenes. A preferable base polymer in light of scuff resistance is a polyurethane. When a polyurethane and another resin are used in combination for the cover  8 , the proportion of the polyurethane to the entire base resin is preferably equal to or greater than 50% by weight, more preferably equal to or greater than 60% by weight, and particularly preferably equal to or greater than 70% by weight. 
     The resin composition of the cover  8  may include a thermoplastic polyurethane, or may include a thermosetting polyurethane. In light of productivity of the golf ball  2  , the thermoplastic polyurethane is preferable. The thermoplastic polyurethane includes a polyurethane component as a hard segment, and a polyester component or a polyether component as a soft segment. The thermoplastic polyurethane is flexible. The cover  8  in which the polyurethane is used has excellent scuff resistance. 
     The thermoplastic polyurethane has a urethane bond within the molecule. The urethane bond can be formed by reacting a polyol with a polyisocyanate. The polyol, as a material for the urethane bond, has a plurality of hydroxyl groups. Low-molecular-weight polyols and high-molecular-weight polyols can be used. 
     Examples of low-molecular-weight polyols include diols, triols, tetraols, and hexaols. Specific examples of diols include ethylene glycol, diethylene glycol, triethylene glycol, 1,2-propanediol, 1,3-propanediol, 2-methyl-1,3-propanediol, dipropylene glycol, 1,2-butanediol, 1,3-butanediol, 1,4-butanediol, 2,3-butanediol, 2,3-dimethyl-2,3-butanediol, neopentyl glycol, pentanediol, hexanediol, heptanediol, octanediol, and 1,6-cyclohexanedimethylol. Aniline diols or bisphenol A diols may be used. Specific examples of triols include glycerin, trimethylol propane, and hexanetriol. Specific examples of tetraols include pentaerythritol and sorbitol. 
     Examples of high-molecular-weight polyols include polyether polyols such as polyoxyethylene glycol (PEG), polyoxypropylene glycol (PPG), and polytetramethylene ether glycol (PTMG); condensed polyester polyols such as polyethylene adipate (PEA), polybutylene adipate (PBA), and polyhexamethylene adipate (PHMA); lactone polyester polyols such as poly-ε-caprolactone (PCL); polycarbonate polyols such as polyhexamethylene carbonate; and acrylic polyols. Two or more polyols may be used in combination. In light of feel at impact of the golf ball  2  , the high-molecular-weight polyol has a number average molecular weight of preferably equal to or greater than 400 and more preferably equal to or greater than 1000. The number average molecular weight is preferably equal to or less than 10000. 
     Examples of polyisocyanates, as a material for the urethane bond, include aromatic diisocyanates, alicyclic diisocyanates, and aliphatic diisocyanates. Two or more types of diisocyanates may be used in combination. 
     Examples of aromatic diisocyanates include 2,4-toluene diisocyanate, 2,6-toluene diisocyanate, 4,4′-diphenylmethane diisocyanate (MDI), 1,5-naphthylene diisocyanate (NDI), 3,3′-bitolylene-4,4′-diisocyanate (TODI), xylylene diisocyanate (XDI), tetramethylxylylene diisocyanate (TMXDI), and paraphenylene diisocyanate (PPDI). One example of aliphatic diisocyanates is hexamethylene diisocyanate (HDI). Examples of alicyclic diisocyanates include 4,4′-dicyclohexylmethane diisocyanate (H 12 MDI), 1,3-bis(isocyanatemethyl)cyclohexane (H 6 XDI), isophorone diisocyanate (IPDI), and trans-1,4-cyclohexane diisocyanate (CHDI). 4,4′-dicyclohexylmethane diisocyanate is preferable. 
     Specific examples of the thermoplastic polyurethane include trade names “Elastollan NY80A”, “Elastollan NY82A”, “Elastollan NY84A”, “Elastollan NY85A”, “Elastollan NY90A”, “Elastollan NY95A”, “Elastollan NY97A”, “Elastollan NY585”, and “Elastollan KP016N”, manufactured by BASF Japan Ltd.; and trade names “RESAMINE P4585LS” and “RESAMINE PS62490”, manufactured by Dainichiseika Color &amp; Chemicals Mfg. Co., Ltd. 
     The resin composition of the cover  8  may include a coloring agent, a filler, a dispersant, an antioxidant, an ultraviolet absorber, a light stabilizer, a fluorescent material, a fluorescent brightener, and the like in an adequate amount. When the hue of the golf ball  2  is white, a typical coloring agent is titanium dioxide. 
     In light of durability of the cover  8  , the cover  8  has a Shore D hardness Hc of preferably equal to or greater than 15, more preferably equal to or greater than 18, and particularly preferably equal to or greater than 20. In light of feel at impact upon a shot with a driver, the hardness Hc is preferably equal to or less than 40, more preferably equal to or less than 37, and particularly preferably equal to or less than 34. 
     The hardness Hc of the cover  8  is measured according to the standards of “ASTM-D 2240-68”. The hardness Hc is measured with a Shore D type hardness scale mounted to an automated hardness meter (trade name “digi test II” manufactured by Heinrich Bareiss Prüfgerätebau GmbH). For the measurement, a sheet that is formed by hot press, is formed from the same material as that of the cover  8 , and has a thickness of about 2 mm is used. Prior to the measurement, a sheet is kept at 23° C. for two weeks. At the measurement, three sheets are stacked. 
     In light of feel at impact upon a shot with a driver, the cover  8  has a thickness Tc of preferably equal to or greater than 0.1 mm, more preferably equal to or greater than 0.3 mm, and particularly preferably equal to or greater than 0.4 mm. In light of spin suppression upon a shot with a driver, the thickness Tc is preferably equal to or less than 2.0 mm, more preferably equal to or less than 1.5 mm, and particularly preferably equal to or less than 1.0 mm. The thickness Tc is measured at a position immediately below the land  12 . 
     For forming the cover  8 , known methods such as injection molding, compression molding, and the like can be used. When forming the cover  8 , the dimples  10  are formed by pimples formed on the cavity face of a mold. 
     The golf ball  2  may include a reinforcing layer between the midlayer  6  and the cover  8 . The reinforcing layer firmly adheres to the midlayer  6  and also to the cover  8 . The reinforcing layer suppresses separation of the midlayer  6  from the cover  8 . The reinforcing layer is formed from a resin composition. Examples of a preferable base polymer of the reinforcing layer include two-component curing type epoxy resins and two-component curing type urethane resins. 
     The golf ball  2  has an amount of compressive deformation Sb of preferably equal to or greater than 2.0 mm but equal to or less than 3.5 mm. The golf ball  2  having an amount of compressive deformation of equal to or greater than 2.0 mm has excellent feel at impact upon a shot with a driver. In this respect, the amount of compressive deformation Sb is preferably equal to or greater than 2.2 mm and particularly preferably equal to or greater than 2.3 mm. The golf ball  2  having an amount of compressive deformation Sb of equal to or less than 3.5 mm has excellent flight performance upon a shot with a driver. In this respect, the amount of compressive deformation Sb is more preferably equal to or less than 3.2 mm and particularly preferably equal to or less than 3.0 mm. 
     For measurement of the amount of compressive deformation, a YAMADA type compression tester is used. In the tester, the golf ball  2  is placed on a hard plate made of metal. Next, a cylinder made of metal gradually descends toward the golf ball  2 . The golf ball  2  , squeezed between the bottom face of the cylinder and the hard plate, becomes deformed. A migration distance of the cylinder, starting from the state in which an initial load of 98 N is applied to the golf ball  2  up to the state in which a final load of 1274 N is applied thereto, is measured. A moving speed of the cylinder until the initial load is applied is 0.83 mm/s. A moving speed of the cylinder after the initial load is applied until the final load is applied is 1.67 mm/s. 
     In the golf ball  2  , a value V 1 calculated by the following mathematical formula exceeds 80. 
         V 1=( DH*Hm )/( Hc*Tc ) 
     In other words, the golf ball  2  meets the following mathematical formula (1). 
       ( DH*Hm )/( Hc*Tc )&gt;80   (1)
 
     According to the finding by the present inventor, the value V 1 correlates with the spin rate upon a shot with a driver. With the golf ball  2  that meets the mathematical formula (1), the spin upon a shot with a driver is suppressed. The golf ball  2  has excellent flight performance upon a short with a driver. In this respect, the value V 1  is more preferably equal to or greater than 90 and particularly preferably equal to or greater than 100. In light of feel at impact, the value V 1  is preferably equal to or less than 135. 
     In the golf ball  2  , a value V 2  calculated by the following mathematical formula exceeds 0.75. 
         V 2=(( Sb*Tc )/( Hc*Hm*Tm ))*1000) 
     In other words, the golf ball  2  meets the following mathematical formula(2). 
       (( Sb*Tc )/( Hc*Hm*Tm ))*1000&gt;0.75   (2)
 
     According to the finding by the present inventor, the value V2 correlates with the feel at impact upon a shot with a driver. With the golf ball  2  that meets the mathematical formula (2), soft feel at impact is obtained upon a shot with a driver. In this respect, the value V 2  is more preferably equal to or greater than 0.81 and particularly preferably equal to or greater than 0.90. In light of flight performance, the value V 2  is preferably equal to or less than 1.30. 
     In the golf ball  2  that includes the cover  8  having a low hardness Hc and a small thickness Tc, the mathematical formulas (1) and (2) can be met. 
     As shown in  FIGS. 2 and 3 , the contour of each dimple  10  is circular. The golf ball  2  has: dimples A each having a diameter of 4.60 mm; dimples B each having a diameter of 4.50 mm; dimples C each having a diameter of 4.40 mm; dimples D each having a diameter of 4.30 mm; dimples E each having a diameter of 4.20 mm; and dimples F each having a diameter of 3.05 mm. The number of types of the dimples  10  is six. The golf ball  2  may have non-circular dimples instead of the circular dimples  10  or together with circular dimples  10 . 
     The number of the dimples A is 12, the number of the dimples B is 48, the number of the dimples C is 86, the number of the dimples D is 60, the number of the dimples E is 120, and the number of the dimples F is 12. The total number of the dimples  10  is 338. A dimple pattern is formed by these dimples  10  and the land  12 . 
       FIG. 4  shows a cross section of the golf ball  2  along a plane passing through the central point of the dimple  10  and the central point of the golf ball  2 . In  FIG. 4 , the top-to-bottom direction is the depth direction of the dimple  10 . In  FIG. 4 , a chain double-dashed line  14  indicates a phantom sphere  14 . The surface of the phantom spere  14  is the surface of the golf ball  2  when it is postulated that no dimple  10  exists. The diameter of the phantom spere  14  is equal to the diameter of the golf ball  2 . The dimple  10  is recessed from the surface of the phantom sphere  14 . The land  12  coincides with the surface of the phantom sphere  14 . In the present embodiment, the cross-sectional shape of each dimple  10  is substantially a circular arc. 
     In  FIG. 4 , an arrow Dm indicates the diameter of the dimple  10 . The diameter Dm is the distance between two tangent points Ed appearing on a tangent line Tg that is drawn tangent to the far opposite ends of the dimple  10 . Each tangent point Ed is also the edge of the dimple  10 . The edge Ed defines the contour of the dimple  10 . In  FIG. 4 , a double ended arrow DP 1  indicates a first depth of the dimple  10 . The first depth DP 1  is the distance between the deepest part of the dimple  10  and the surface of the phantom sphere  14 . In  FIG. 4 , a double ended arrow Dp 2  ind icates a second depth of the dimple  10 . The second depth Dp 2  is the distance between the deepest part of the dimple  10  and the tangent line Tg. 
     The diameter Dm of each dimple  10  is preferably equal to or greater than 2.0 mm but equal to or less than 6.0 mm. The dimple  10  having a diameter Dm of equal to or greater than 2.0 mm contributes to turbulization. In this respect, the diameter Dm is more preferably equal to or greater than 2.5 mm and particularly preferably equal to or greater than 2.8 mm. The dimple  10  having a diameter Dm of equal to or less than 6.0 mm does not impair a fundamental feature of the golf ball  2  being substantially a sphere. In this respect, the diameter Dm is more preferably equal to or less than 5.5 mm and particularly preferably equal to or less than 5.0 mm. 
     In the case of a non-circular dimple, a circular dimple  10  having the same area as that of the non-circular dimple is assumed. The diameter of the assumed dimple  10  can be regarded as the diameter of the non-circular dimple. 
     The ratio Pd of the diameter Dm of each dimple  10  relative to the diameter of the golf ball  2  is preferably equal to or greater than 9.60% but equal to or less than 10.37%. The dimple  10  having a ratio Pd of equal to or greater than 9.60% contributes to turbulization. In this respect, the ratio Pd is more preferably equal to or greater than 9.90% and particularly preferably equal to or greater than 10.10%. The dimple  10  having a ratio Pd of equal to or less than 10.37% does not impair a fundamental feature of the golf ball  2  being substantially a sphere. In this respect, the ratio Pd is more preferably equal to or less than 10.32% and particularly preferably equal to or less than 10.27%. 
     The ratio Rs of the number of the dimples  10  each having a ratio Pd of equal to or greater than 9.60% but equal to or less than 10.37%, relative to the total number of the dimples  10 , is preferably equal to or greater than 50%. The dimple pattern having a ratio Rs of equal to or greater than 50% contributes to turbulization. In this respect, the ratio Rs is more preferably equal to or greater than 60% and particularly preferably equal to or greater than 70%. The ratio Rs may be 100%. 
     The ratio Rs′ of the number of the dimples  10  each having a ratio Pd of equal to or greater than 10.10% but equal to or less than 10.37%, relative to the total number of the dimples  10 , is preferably equal to or greater than 50%. The dimple pattern having a ratio Rs′ of equal to or greater than 50% contributes to turbulization. In this respect, the ratio Rs′ is more preferably equal to or greater than 60% and particularly preferably equal to or greater than 70%. The ratio Rs′ may be 100%. 
     The ratio of the number of the dimples  10  each having a ratio Pd exceeding 10.37%, relative to the total number of the dimples  10 , is preferably less than 50%. With the dimple pattern in which this ratio is less than 50%, the degree of freedom in designing a dimple pattern is high, and therefore the width of the land  12  is less likely to be excessively large. In this respect, this ratio is more preferably equal to or less than 30% and particularly preferably equal to or less than 10%. This ratio may be zero. 
     In light of suppression of rising of the golf ball  2  during flight, the first depth Dp 1  of each dimple  10  is preferably equal to or greater than 0.10 mm, more preferably equal to or greater than 0.13 mm, and particularly preferably equal to or greater than 0.15 mm. In light of suppression of dropping of the golf ball  2  during flight, the first depth Dp 1  is preferably equal to or less than 0.65 mm, more preferably equal to or less than 0.60 mm, and particularly preferably equal to or less than 0.55 mm. 
     The area S of the dimple  10  is the area of a region surrounded by the contour line of the dimple  10  when the central point of the golf ball  2  is viewed at infinity. In the case of a circular dimple  10 , the area S is calculated by the following mathematical formula. 
         S =( Dm /2) 2 *n 
     In the golf ball  2  shown in  FIGS. 2 and 3 , the area of each dimple A is 16.62 mm 2 , the area of each dimple B is 15.90 mm 2 , the area of each dimple C is 15.21 mm 2 , the area of each dimple D is 14.52 mm 2 , the area of each dimple E is 13.85 mm 2 , and the area of each dimple E is 7.31 mm 2 . 
     In the present invention, the ratio of the sum of the areas S of all the dimples  10  relative to the surface area of the phantom spere  14  is referred to as an occupation ratio So. From the standpoint that sufficient turbulization is achieved, the occupation ratio So is preferably equal to or greater than 81.0%, more preferably equal to or greater than 82.0%, and particularly preferably equal to or greater than 83.0%. The occupation ratio So is preferably equal to or less than 95%. In the golf ball  2  shown in  FIGS. 2 and 3 , the total area of the dimples  10  is 4891.6 mm 2 . The surface area of the phantom spere  14  of the golf ball  2  is 5728.0 mm 2 , so that the occupation ratio So is 85.4%. 
     From the standpoint that a sufficient occupation ratio is achieved, the total number N of the dimples  10  is preferably equal to or greater than 250, more preferably equal to or greater than 280, and particularly preferably equal to or greater than 300. From the standpoint that each dimple  10  can contribute to turbulization, the total number N of the dimples  10  is preferably equal to or less than 450, more preferably equal to or less than 400, and particularly preferably equal to or less than 380. 
     In the present invention, the “volume of the dimple” means the volume of a portion surrounded by the surface of the phantom spere  14  and the surface of the dimple  10 . In light of suppression of rising of the golf ball  2  during flight, the total volume of all the dimples  10  is preferably equal to or greater than 450 mm 3 , more preferably equal to or greater than 480 mm 3 , and particularly preferably equal to or greater than 500 mm 3 . In light of suppression of dropping of the golf ball  2  during flight, the total volume is preferably equal to or less than 750 mm 3 , more preferably equal to or less than 730 mm 3 , and particularly preferably equal to or less than 710 mm 3 . 
     In a graph shown in  FIG. 5 , the horizontal axis indicates the occupation ratio So of the dimples. In this graph, the vertical axis indicates the ratio Rs of the number of the dimples  10  each having a ratio Pd of equal to or greater than 9.60% but equal to or less than 10.37%, relative to the total number of the dimples  10 . A straight line indicated by reference sign L 1  in this graph is represented by the following mathematical formula. 
         Rs =−2.5 *So +273
 
     The golf ball  2  that is plotted in the zone above the straight line L 1  in this graph meets the following mathematical formula (3). 
         Rs ≧−2.5 *So +273   (3)
 
     With the golf ball  2  that meets the mathematical formula (3), turbulization is promoted. The golf ball  2  has excellent flight performance upon a shot with a driver. 
     A straight line indicated by reference sign L 2  in the graph of  FIG. 5  is represented by the following mathematical formula. 
         Rs =−2.5 *So +278
 
     The golf ball  2  that is plotted in the zone above the straight line L 2  in this graph meets the following mathematical formula (4). 
         Rs ≧−2.5 *So +278   (4)
 
     With the golf ball  2  that meets the mathematical formula (4), turbulization is promoted. The golf ball  2  has excellent flight performance upon a shot with a driver. 
     A straight line indicated by reference sign L 3  in the graph of  FIG. 5  is represented by the following mathematical formula. 
         Rs =−2.5 *So +283
 
     The golf ball  2  that is plotted in the zone above the straight line L 3  in this graph meets the following mathematical formula (5). 
         Rs ≧−2.5 *So +283   (5)
 
     With the golf ball  2  that meets the mathematical formula (5), turbulization is promoted. The golf ball  2  has excellent flight performance upon a shot with a driver. 
     In a graph shown in  FIG. 6 , the horizontal axis indicates the occupation ratio So of the dimples. In this graph, the vertical axis indicates the ratio Rs′ of the number of the dimples  10  each having a ratio Pd of equal to or greater than 10.10% but equal to or less than 10.37%, relative to the total number of the dimples  10 . A straight line indicated by reference sign L 4  in this graph is represented by the following mathematical formula. 
         Rs ′=−2.2 *So +245
 
     The golf ball  2  that is plotted in the zone above the straight line L 4  in this graph meets the following mathematical formula (6). 
         Rs ′≧−2.2 *So +245   (6)
 
     With the golf ball  2  that meets the mathematical formula (6), turbulization is promoted. The golf ball  2  has excellent flight performance upon a shot with a driver. 
     A straight line indicated by reference sign L 5  in the graph of  FIG. 6  is represented by the following mathematical formula. 
         Rs ′=−2.2 *So +252
 
     The golf ball  2  that is plotted in the zone above the straight line L 5  in this graph meets the following mathematical formula (7). 
         Rs ′≧−2.2 *So +252   (7)
 
     With the golf ball  2  that meets the mathematical formula (7), turbulization is promoted. The golf ball  2  has excellent flight performance upon a shot with a driver. 
     As shown in  FIG. 3 , the surface of the golf ball  2  (or the phantom sphere  14 ) can be divided into two hemispheres HE by an equator Eq. Specifically, the surface can be divided into a northern hemisphere NH and a southern hemisphere SH. Each hemisphere HE has a pole P. The pole P corresponds to a deepest point of a mold for the golf ball  2 . 
       FIG. 2  shows the northern hemisphere. The southern hemisphere has a pattern obtained by rotating the dimple pattern in  FIG. 2  about the pole P. Line segments S 1 , S 2 , and S 3  shown in  FIG. 2  each extend from the pole P. The angle at the pole P between the line segment S 1  and the line segment S 2  is 120°. The angle at the pole P between the line segment S 2  and the line segment S 3  is 120°. The angle at the pole P between the line segment S 3  and the line segment S 1  is 120°. 
     Of the surface of the golf ball  2  (or the phantom sphere  14 ), a zone surrounded by the line segment S 1  the line segment S 2 , and the equator Eq is a first spherical triangle T 1 . Of the surface of the golf ball  2  (or the phantom sphere  14 ), a zone surrounded by the line segment S 2 , the line segment S 3 , and the equator Eq is a second spherical triangle T 2 . Of the surface of the golf ball  2  (or the phantom sphere  14 ), a zone surrounded by the line segment S 3 , the line segment S 1  and the equator Eq is a third spherical triangle T 3 . Each spherical triangle is a unit. The hemisphere HE can be divided into the three units. 
     When the dimple pattern of the first spherical triangle T 1  is rotated by 120° about a straight line connecting the two poles P, the resultant dimple pattern substantially overlaps the dimple pattern of the second spherical triangle T 2 . When the dimple pattern of the second spherical triangle T 2  is rotated by 120° about the straight line connecting the two poles P, the resultant dimple pattern substantially overlaps the dimple pattern of the third spherical triangle T 3 . When the dimple pattern of the third spherical triangle T 3  is rotated by 120° about the straight line connecting the two poles P, the resultant dimple pattern substantially overlaps the dimple pattern of the first spherical triangle T 1 . In other words, the dimple pattern of the hemisphere is composed of three units that are rotationally symmetrical to each other. 
     A pattern obtained by rotating the dimple pattern of each hemisphere HE by 120° about the straight line connecting the two poles P substantially overlaps the dimple pattern that has not been rotated. The dimple pattern of each hemisphere HE has 120° rotational symmetry. 
     A line segment S 4  shown in  FIG. 2  extends from the pole P. The angle at the pole P between the line segment S 4  and the line segment S 1  is 60°. The angle at the pole P between the line segment S 4  and the line segment S 2  is 60°. The first spherical triangle T 1  (unit) can be divided into a small spherical triangle T 1   a  and a small spherical triangle T 1   b  by the line segment S 4 . The spherical triangle T 1   a  and the spherical triangle T 1   b  are small units. 
     A pattern obtained by inverting the dimple pattern of the spherical triangle T 1   a  with respect to a plane containing the line segment S 4  and the straight line connecting both poles P substantially overlaps the dimple pattern of the spherical triangle T 1   b . In other words, the dimple pattern of each unit is composed of two small units that are mirror-symmetrical to each other. 
     Similarly, the dimple pattern of the second spherical triangle T 2  is also composed of two small units that are mirror-symmetrical to each other. The dimple pattern of the third spherical triangle T 3  is also composed of two small units that are mirror-symmetrical to each other. The dimple pattern of the hemisphere HE is composed of the six small units. 
     According to the finding by the present inventor, with the golf ball  2  of which the dimple pattern of each hemisphere is composed of three units that are rotationally symmetrical to each other by 120° and the dimple pattern of each unit is composed of two small units that are mirror-symmetrical to each other, turbulization is promoted. The golf ball  2  has excellent flight performance upon a shot with a driver. 
     EXAMPLES 
     Example 1 
     A rubber composition was obtained by kneading  100  parts by weight of a high-cis polybutadiene (trade name “BR-730”, manufactured by JSR Corporation), 29.5 parts by weight of zinc diacrylate, 12 parts by weight of zinc oxide, an appropriate amount of barium sulfate, 0.1 parts by weight of 2-naphthalenethiol, 0.3 parts by weight of pentabromo diphenyl disulfide, 0.85 parts by weight of dicumyl peroxide, and 2 parts by weight of benzoic acid. This rubber composition was placed into a mold including upper and lower mold halves each having a hemispherical cavity, and heated at 150° C. for 20 minutes to obtain a core with a diameter of 39.7 mm. 
     A resin composition M 1  was obtained by kneading  47  parts by weight of an ionomer resin (the aforementioned “Himilan 1605”), 50 parts by weight of another ionomer resin (the aforementioned “Himilan AM7329”), 3 parts by weight of a styrene block-containing thermoplastic elastomer (the aforementioned “RABALON T3221C”), and 3 parts by weight of titanium dioxide with a twin-screw kneading extruder. The core was covered with the resin composition M 1  by injection molding to form a mid layer with a thickness of 1.0 mm. 
     A paint composition (trade name “POLIN 750LE”, manufactured by SHINTO PAINT CO., LTD.) including a two-component curing type epoxy resin as a base polymer was prepared. The base material liquid of this paint composition includes 30 parts by weight of a bisphenol A type epoxy resin and 70 parts by weight of a solvent. The curing agent liquid of this paint composition includes 40 parts by weight of a modified polyamide amine, 55 parts by weight of a solvent, and 5 parts by weight of titanium dioxide. The weight ratio of the base material liquid to the curing agent liquid is 1/1. This paint composition was applied to the surface of the mid layer with a spray gun, and kept at 23° C. for 12 hours to obtain a reinforcing layer with a thickness of 10 μm. 
     A resin composition C 1  was obtained by kneading  100  parts by weight of a thermoplastic polyurethane elastomer (the aforementioned “Elastollan NY80A”), 0.2 parts by weight of a light stabilizer (trade name “TINUVIN 770”), 4 parts by weight of titanium dioxide, and 0.04 parts by weight of ultramarine blue with a twin-screw kneading extruder. Half shells were obtained from this resin composition by compression molding. The sphere consisting of the core, the mid layer, and the reinforcing layer was covered with two of these half shells. These half shells and the sphere were placed into a final mold that includes upper and lower mold halves each having a hemispherical cavity and having a large number of pimples on its cavity face, and a cover was obtained by compression molding. The thickness of the cover was 0.5 mm. Dimples having a shape that is the inverted shape of the pimples were formed on the cover. 
     A clear paint including a two-component curing type polyurethane as a base material was applied to this cover to obtain a golf ball of Example 1 with a diameter of about 42.7 mm and a weight of about 45.6 g. Dimple specifications D 1  of the golf ball are shown in detail in Tables 4 and 6 below.  FIG. 2  is a plan view of the golf ball, and  FIG. 3  is a front view of the golf ball. The dimple pattern of each hemisphere of the golf ball has 60° rotational symmetry, has 120° rotational symmetry, and has 180° rotational symmetry. 
     Examples 2 to 4 and Comparative Examples 1 to 3 
     Golf balls of Examples 2 to 4 and Comparative Examples 1 to 3 were obtained in the same manner as Example 1, except the specifications of the dimples were as shown in Tables 8 and 9 below. The specifications of the dimples are shown in detail in Tables 4 to 7 below. In each golf ball, the dimple pattern of each hemisphere is composed of three units that are rotationally symmetrical to each other. The dimple pattern of each unit is composed of two small units that are mirror-symmetrical to each other. The number of the small units in each hemisphere is six. 
     Comparative Examples 4 and 5 
     Golf balls of Comparative Examples 4 and 5 were obtained in the same manner as Example 1, except the specifications of the dimples were as shown in Table 9 below. The specifications of the dimples are shown in detail in Tables 5 and 7 below. The dimple pattern of the golf ball according to Comparative Example 4 is the same as the dimple pattern of the golf ball according to Example 1 in JP2013-153966. The dimple pattern of each hemisphere of the golf ball according to Comparative Example 4 does not have rotational symmetry. The dimple pattern of the golf ball according to Comparative Example 5 is the same as the dimple pattern of the golf ball according to Comparative Example 1 in JP2013-153966. The dimple pattern of each hemisphere of the golf ball according to Comparative Example 5 does not have rotational symmetry. 
     Examples 5 to 8 and Comparative Examples 6 to 10 
     Golf balls of Examples 5 to 8 and Comparative Examples 6 to 10 were obtained in the same manner as Example 1, except the specifications of the core, the mid layer, the cover, and the dimples were as shown in Tables 10 and 11 below. The specifications of the core are shown in detail in Table 1 below. The specifications of the mid layer are shown in detail in Table 2 below. The specifications of the cover are shown in detail in Table 3 below. The specifications of the dimples are shown in detail in Tables 4 to 7 below. 
     [Flight Test] 
     A driver (trade name “XXIO9”, manufactured by DUNLOP SPORTS CO. LTD., shaft hardness: S, loft angle: 9.5°) was attached to a swing machine manufactured by Golf Laboratories, Inc. A golf ball was hit under a condition of a head speed of 50 m/sec, and the ball speed, the spin rate, and the flight distance were measured. The flight distance is the distance between the point at the hit and the point at which the ball stopped. The average value of data obtained by 12 measurements is shown in Tables 8 to 11 below. 
     [Feel at Impact] 
     Thirty golf players hit golf balls with drivers (trade name “XXIO9”, manufactured by DUNLOP SPORTS CO. LTD., shaft hardness: S, loft angle: 9.5°) and were asked about feel at impact. The evaluation was categorized as follows on the basis of the number of golf players who answered, “the feel at impact was favorable”.
         A: 25 persons or more   B: 20 to 24 persons   C: 15 to 19 persons   D: 14 persons or less The results are shown in Tables 8 to 11 below.       

     
       
         
           
               
             
               
                 TABLE 1 
               
             
            
               
                   
               
               
                 Specifications of Core (parts by weight) 
               
            
           
           
               
               
               
               
               
            
               
                   
                 I 
                 II 
                 III 
                 IV 
               
               
                   
                   
               
            
           
           
               
               
               
               
               
            
               
                 Polybutadiene 
                 100 
                 100 
                 100 
                 100 
               
               
                 Zinc diacrylate 
                 29.5 
                 34.5 
                 29.5 
                 28.5 
               
               
                 Zinc oxide 
                 12 
                 12 
                 12 
                 12 
               
               
                 Barium sulfate 
                 * 
                 * 
                 * 
                 * 
               
               
                 2-naphthalenethiol 
                 0.1 
                 0.1 
                 0 
                 0 
               
               
                 Pentabromo diphenyl disulfide 
                 0.3 
                 0.3 
                 0.1 
                 0.3 
               
               
                 Dicumyl peroxide 
                 0.85 
                 0.85 
                 0.85 
                 0.85 
               
               
                 Benzoic acid 
                 2 
                 2 
                 0 
                 0 
               
               
                 Crosslinking temperature (° C.) 
                 150 
                 150 
                 140 
                 160 
               
               
                 Crosslinking time period (min) 
                 20 
                 20 
                 20 
                 20 
               
               
                 Central hardness H1 (Shore-C) 
                 54 
                 60 
                 60 
                 58 
               
               
                 Surface hardness H2 (Shore-C) 
                 80 
                 85 
                 70 
                 78 
               
               
                 H2 − H1 
                 26 
                 25 
                 10 
                 20 
               
               
                   
               
               
                 * Appropriate amount 
               
            
           
         
       
     
     
       
         
           
               
             
               
                 TABLE 2 
               
             
            
               
                   
               
               
                 Composition of Mid Layer (parts by weight) 
               
            
           
           
               
               
               
               
               
            
               
                   
                 M1 
                 M2 
                 M3 
                 M4 
               
               
                   
                   
               
            
           
           
               
               
               
               
               
               
            
               
                   
                 Surlyn 8150 
                 — 
                 50 
                 — 
                 32.5 
               
               
                   
                 Surlyn 9150 
                 — 
                 — 
                 — 
                 32.5 
               
               
                   
                 Polyamide 6 
                 — 
                 — 
                 — 
                 35 
               
               
                   
                 Himilan 1605 
                 47 
                 — 
                 — 
                 — 
               
               
                   
                 Himilan AM7329 
                 50 
                 50 
                 — 
                 — 
               
               
                   
                 Himilan 1555 
                 — 
                 — 
                 47 
                 — 
               
               
                   
                 Himilan 1557 
                 — 
                 — 
                 46 
                 — 
               
               
                   
                 RABALON T3221C 
                 3 
                 — 
                 7 
                 — 
               
               
                   
                 Titanium dioxide 
                 3 
                 3 
                 3 
                 4 
               
               
                   
                 Hardness (Shore-D) 
                 63 
                 68 
                 57 
                 72 
               
               
                   
                   
               
            
           
         
       
     
     
       
         
           
               
             
               
                 TABLE 3 
               
             
            
               
                   
               
               
                 Composition of Cover (parts by weight) 
               
            
           
           
               
               
               
               
               
            
               
                   
                 C1 
                 C2 
                 C3 
                 C4 
               
               
                   
                   
               
            
           
           
               
               
               
               
               
               
            
               
                   
                 Elastollan NY80A 
                 100 
                 — 
                 — 
                 — 
               
               
                   
                 Elastollan NY84A 
                 — 
                 — 
                 — 
                 100 
               
               
                   
                 Elastollan NY90A 
                 — 
                 100 
                 — 
                 — 
               
               
                   
                 Elastollan NY95A 
                 — 
                 — 
                 100 
                 — 
               
               
                   
                 TINUVIN 770 
                 0.2 
                 0.2 
                 0.2 
                 0.2 
               
               
                   
                 Titanium dioxide 
                 4 
                 4 
                 4 
                 4 
               
               
                   
                 Ultramarine blue 
                 0.04 
                 0.04 
                 0.04 
                 4 
               
               
                   
                 Hardness (Shore-D) 
                 27 
                 38 
                 45 
                 31 
               
               
                   
                   
               
            
           
         
       
     
     
       
         
           
               
             
               
                 TABLE 4 
               
             
            
               
                   
               
               
                 Specifications of Dimples 
               
            
           
           
               
               
               
               
               
               
               
               
            
               
                   
                   
                 Dm 
                 Dp2 
                 Dp1 
                 R 
                 Volume 
                 Pd 
               
               
                   
                 Number 
                 (mm) 
                 (mm) 
                 (mm) 
                 (mm) 
                 (mm 3 ) 
                 (%) 
               
               
                   
                   
               
            
           
           
               
               
               
               
               
               
               
               
               
            
               
                 D1 
                 A 
                 12 
                 4.60 
                 0.135 
                 0.2592 
                 19.66 
                 1.123 
                 10.77 
               
               
                   
                 B 
                 48 
                 4.50 
                 0.135 
                 0.2539 
                 18.82 
                 1.075 
                 10.54 
               
               
                   
                 C 
                 86 
                 4.40 
                 0.135 
                 0.2487 
                 17.99 
                 1.028 
                 10.30 
               
               
                   
                 D 
                 60 
                 4.30 
                 0.135 
                 0.2435 
                 17.19 
                 0.982 
                 10.07 
               
               
                   
                 E 
                 120 
                 4.20 
                 0.135 
                 0.2385 
                 16.40 
                 0.936 
                 9.84 
               
               
                   
                 F 
                 12 
                 3.05 
                 0.135 
                 0.1895 
                 8.68 
                 0.494 
                 7.14 
               
               
                 D2 
                 A 
                 30 
                 4.70 
                 0.135 
                 0.2647 
                 20.52 
                 1.172 
                 11.01 
               
               
                   
                 B 
                 30 
                 4.60 
                 0.135 
                 0.2592 
                 19.66 
                 1.123 
                 10.77 
               
               
                   
                 C 
                 150 
                 4.40 
                 0.135 
                 0.2487 
                 17.99 
                 1.028 
                 10.30 
               
               
                   
                 D 
                 90 
                 4.30 
                 0.135 
                 0.2435 
                 17.19 
                 0.982 
                 10.07 
               
               
                   
                 E 
                 12 
                 3.00 
                 0.135 
                 0.1878 
                 8.40 
                 0.478 
                 7.03 
               
               
                 D3 
                 A 
                 24 
                 4.60 
                 0.135 
                 0.2592 
                 19.66 
                 1.123 
                 10.77 
               
               
                   
                 B 
                 54 
                 4.50 
                 0.135 
                 0.2539 
                 18.82 
                 1.075 
                 10.54 
               
               
                   
                 C 
                 210 
                 4.40 
                 0.135 
                 0.2487 
                 17.99 
                 1.028 
                 10.30 
               
               
                   
                 D 
                 24 
                 4.00 
                 0.135 
                 0.2289 
                 14.88 
                 0.850 
                 9.37 
               
               
                   
                 E 
                 12 
                 3.00 
                 0.135 
                 0.1878 
                 8.40 
                 0.478 
                 7.03 
               
               
                 D4 
                 A 
                 24 
                 4.60 
                 0.135 
                 0.2592 
                 19.66 
                 1.123 
                 10.77 
               
               
                   
                 B 
                 12 
                 4.50 
                 0.135 
                 0.2539 
                 18.82 
                 1.075 
                 10.54 
               
               
                   
                 C 
                 252 
                 4.35 
                 0.135 
                 0.2461 
                 17.59 
                 1.004 
                 10.19 
               
               
                   
                 D 
                 24 
                 4.00 
                 0.135 
                 0.2289 
                 14.88 
                 0.850 
                 9.37 
               
               
                   
                 E 
                 12 
                 3.00 
                 0.135 
                 0.1878 
                 8.40 
                 0.478 
                 7.03 
               
               
                   
               
            
           
         
       
     
     
       
         
           
               
             
               
                 TABLE 5 
               
             
            
               
                   
               
               
                 Specifications of Dimples 
               
            
           
           
               
               
               
               
               
               
               
               
            
               
                   
                   
                 Dm 
                 Dp2 
                 Dp1 
                 R 
                 Volume 
                 Pd 
               
               
                   
                 Number 
                 (mm) 
                 (mm) 
                 (mm) 
                 (mm) 
                 (mm 3 ) 
                 (%) 
               
               
                   
                   
               
            
           
           
               
               
               
               
               
               
               
               
               
            
               
                 D5 
                 A 
                 108 
                 4.60 
                 0.135 
                 0.2592 
                 19.66 
                 1.123 
                 10.77 
               
               
                   
                 B 
                 84 
                 4.50 
                 0.135 
                 0.2539 
                 18.82 
                 1.075 
                 10.54 
               
               
                   
                 C 
                 108 
                 4.40 
                 0.135 
                 0.2487 
                 17.99 
                 1.028 
                 10.30 
               
               
                   
                 D 
                 12 
                 3.00 
                 0.135 
                 0.1878 
                 8.40 
                 0.478 
                 7.03 
               
               
                 D6 
                 A 
                 30 
                 4.70 
                 0.135 
                 0.2647 
                 20.52 
                 1.172 
                 11.01 
               
               
                   
                 B 
                 18 
                 4.65 
                 0.135 
                 0.2620 
                 20.09 
                 1.148 
                 10.89 
               
               
                   
                 C 
                 48 
                 4.40 
                 0.135 
                 0.2487 
                 17.99 
                 1.028 
                 10.30 
               
               
                   
                 D 
                 66 
                 4.35 
                 0.135 
                 0.2461 
                 17.59 
                 1.004 
                 10.19 
               
               
                   
                 E 
                 126 
                 4.20 
                 1.135 
                 1.2385 
                 2.51 
                 8.628 
                 9.84 
               
               
                   
                 F 
                 12 
                 4.00 
                 2.135 
                 2.2289 
                 2.00 
                 18.510 
                 9.37 
               
               
                   
                 G 
                 12 
                 3.00 
                 3.135 
                 3.1878 
                 1.93 
                 27.213 
                 7.03 
               
               
                 D7 
                 A 
                 24 
                 4.60 
                 0.135 
                 0.2592 
                 19.66 
                 1.123 
                 10.77 
               
               
                   
                 B 
                 12 
                 4.50 
                 0.135 
                 0.2539 
                 18.82 
                 1.075 
                 10.54 
               
               
                   
                 C 
                 210 
                 4.35 
                 0.135 
                 0.2461 
                 17.59 
                 1.004 
                 10.19 
               
               
                   
                 D 
                 66 
                 4.05 
                 0.135 
                 0.2313 
                 15.26 
                 0.871 
                 9.48 
               
               
                   
                 E 
                 12 
                 3.00 
                 0.135 
                 0.1878 
                 8.40 
                 0.478 
                 7.03 
               
               
                 D8 
                 A 
                 16 
                 4.60 
                 0.135 
                 0.2592 
                 19.66 
                 1.123 
                 10.77 
               
               
                   
                 B 
                 30 
                 4.50 
                 0.135 
                 0.2539 
                 18.82 
                 1.075 
                 10.54 
               
               
                   
                 C 
                 30 
                 4.40 
                 0.135 
                 0.2487 
                 17.99 
                 1.028 
                 10.30 
               
               
                   
                 D 
                 150 
                 4.30 
                 0.135 
                 0.2435 
                 17.19 
                 0.982 
                 10.07 
               
               
                   
                 E 
                 30 
                 4.20 
                 0.135 
                 0.2385 
                 16.40 
                 0.936 
                 9.84 
               
               
                   
                 F 
                 66 
                 4.10 
                 0.135 
                 0.2336 
                 15.63 
                 0.892 
                 9.60 
               
               
                   
                 G 
                 10 
                 3.80 
                 0.135 
                 0.2197 
                 13.44 
                 0.767 
                 8.90 
               
               
                   
                 H 
                 12 
                 3.40 
                 0.135 
                 0.2028 
                 10.77 
                 0.614 
                 7.96 
               
               
                 D9 
                 A 
                 26 
                 4.50 
                 0.135 
                 0.2539 
                 18.82 
                 1.075 
                 10.54 
               
               
                   
                 B 
                 88 
                 4.40 
                 0.135 
                 0.2487 
                 17.99 
                 1.028 
                 10.30 
               
               
                   
                 C 
                 102 
                 4.30 
                 0.135 
                 0.2435 
                 17.19 
                 0.982 
                 10.07 
               
               
                   
                 D 
                 94 
                 4.10 
                 0.135 
                 0.2336 
                 15.63 
                 0.892 
                 9.60 
               
               
                   
                 E 
                 14 
                 3.60 
                 0.135 
                 0.2110 
                 12.07 
                 0.688 
                 8.43 
               
               
                   
               
            
           
         
       
     
     
       
         
           
               
             
               
                 TABLE 6 
               
             
            
               
                   
               
               
                 Specifications of Dimples 
               
            
           
           
               
               
               
               
               
            
               
                   
                 D1 
                 D2 
                 D3 
                 D4 
               
               
                   
                   
               
            
           
           
               
               
               
               
               
            
               
                 Plan view 
                 FIG. 2 
                 FIG. 7 
                 FIG. 9 
                 FIG. 11 
               
               
                 Front view 
                 FIG. 3 
                 FIG. 8 
                 FIG. 10 
                 FIG. 12 
               
               
                 Number 
                 338 
                 312 
                 324 
                 324 
               
               
                 Number of units 
                 3 
                 3 
                 3 
                 3 
               
               
                 Number of small 
                 6 
                 6 
                 6 
                 6 
               
               
                 units 
               
               
                 So (%) 
                 85.4 
                 81.9 
                 84.4 
                 82.4 
               
               
                 Rs (%) 
                 78.7 
                 76.9 
                 64.8 
                 77.8 
               
               
                 Rs + 2.5 * So − 273 
                 19.20 
                 8.65 
                 2.80 
                 10.80 
               
               
                 M.F. (1) 
                 Met 
                 Met 
                 Met 
                 Met 
               
               
                 Rs + 2.5 * So − 278 
                 14.20 
                 3.65 
                 −2.20 
                 5.80 
               
               
                 M.F. (2) 
                 Met 
                 Met 
                 Unmet 
                 Met 
               
               
                 Rs + 2.5 * So − 283 
                 9.20 
                 −1.35 
                 −7.20 
                 0.80 
               
               
                 M.F. (3) 
                 Met 
                 Unmet 
                 Unmet 
                 Met 
               
               
                 Rs′ (%) 
                 25.4 
                 48.1 
                 64.8 
                 77.8 
               
               
                 Rs′ + 2.2 * So − 245 
                 −31.72 
                 −16.72 
                 5.48 
                 14.08 
               
               
                 M.F. (4) 
                 Unmet 
                 Unmet 
                 Met 
                 Met 
               
               
                 Rs′ + 2.2 * So − 252 
                 −38.72 
                 −23.72 
                 −1.52 
                 7.08 
               
               
                 M.F. (5) 
                 Unmet 
                 Unmet 
                 Unmet 
                 Met 
               
               
                   
               
               
                 M.F.: Mathematical formula 
               
            
           
         
       
     
     
       
         
           
               
             
               
                 TABLE 7 
               
             
            
               
                   
               
               
                 Specifications of Dimples 
               
            
           
           
               
               
               
               
               
               
            
               
                   
                 D5 
                 D6 
                 D7 
                 D8 
                 D9 
               
               
                   
                   
               
            
           
           
               
               
               
               
               
               
            
               
                 Plan view 
                 FIG. 13 
                 FIG. 15 
                 FIG. 17 
                 FIG. 19 
                 XFIG. 25 
               
               
                 Front view 
                 FIG. 14 
                 FIG. 16 
                 FIG. 18 
                 FIG. 22 
                 FIG. 26 
               
               
                 Number 
                 312 
                 312 
                 324 
                 344 
                 324 
               
               
                 Number of units 
                 3 
                 3 
                 3 
                 — 
                 — 
               
               
                 Number of small 
                 6 
                 6 
                 6 
                 — 
                 — 
               
               
                 units 
               
               
                 So (%) 
                 84.8 
                 78.9 
                 81.1 
                 85.3 
                 80.6 
               
               
                 Rs (%) 
                 34.6 
                 76.9 
                 64.8 
                 61.0 
                 87.7 
               
               
                 Rs + 2.5 * So − 273 
                 −26.40 
                 1.15 
                 −5.45 
                 1.25 
                 16.20 
               
               
                 M.F. (1) 
                 Unmet 
                 Met 
                 Unmet 
                 Met 
                 Met 
               
               
                 Rs + 2.5 * So − 278 
                 −31.40 
                 −3.85 
                 −10.45 
                 −3.75 
                 11.20 
               
               
                 M.F. (2) 
                 Unmet 
                 Unmet 
                 Unmet 
                 Unmet 
                 Met 
               
               
                 Rs + 2.5 * So − 283 
                 −36.40 
                 −8.85 
                 −15.45 
                 −8.75 
                 6.20 
               
               
                 M.F. (3) 
                 Unmet 
                 Unmet 
                 Unmet 
                 Unmet 
                 Met 
               
               
                 Rs′ (%) 
                 34.6 
                 36.5 
                 64.8 
                 8.7 
                 27.2 
               
               
                 Rs′ + 2.2 * So − 245 
                 −23.84 
                 −34.92 
                 −1.78 
                 −48.64 
                 −40.48 
               
               
                 M.F. (4) 
                 Unmet 
                 Unmet 
                 Unmet 
                 Unmet 
                 Unmet 
               
               
                 Rs′ + 2.2 * So − 252 
                 −30.84 
                 −41.92 
                 −8.78 
                 −55.64 
                 −47.48 
               
               
                 M.F. (5) 
                 Unmet 
                 Unmet 
                 Unmet 
                 Unmet 
                 Unmet 
               
               
                   
               
               
                 M.F.: Mathematical formula 
               
            
           
         
       
     
     
       
         
           
               
             
               
                 TABLE 8 
               
             
            
               
                   
               
               
                 Results of Evaluation 
               
            
           
           
               
               
               
               
               
            
               
                   
                 Ex. 1 
                 Ex. 2 
                 Ex. 3 
                 Ex. 4 
               
               
                   
                   
               
            
           
           
               
               
               
               
               
            
               
                 Core 
                   
                   
                   
                   
               
               
                 Composition 
                 I 
                 I 
                 I 
                 I 
               
               
                 Diameter (mm) 
                 39.7 
                 39.7 
                 39.7 
                 39.7 
               
               
                 Central hardness 
                 54 
                 54 
                 54 
                 54 
               
               
                 (Shore-C) 
               
               
                 Surface hardness 
                 80 
                 80 
                 80 
                 80 
               
               
                 (Shore-C) 
               
               
                 Difference DH 
                 26 
                 26 
                 26 
                 26 
               
               
                 (Shore-C) 
               
               
                 Mid layer 
               
               
                 Composition 
                 M1 
                 M1 
                 M1 
                 M1 
               
               
                 Hm (Shore-D) 
                 63 
                 63 
                 63 
                 63 
               
               
                 Thickness Tm (mm) 
                 1.0 
                 1.0 
                 1.0 
                 1.0 
               
               
                 Cover 
               
               
                 Composition 
                 C1 
                 C1 
                 C1 
                 C1 
               
               
                 Hc (Shore-D) 
                 27 
                 27 
                 27 
                 27 
               
               
                 Tc (mm) 
                 0.5 
                 0.5 
                 0.5 
                 0.5 
               
               
                 Dimple 
                 D1 
                 D2 
                 D3 
                 D4 
               
               
                 (DH * Hm)/(Hc * Tc) 
                 121 
                 121 
                 121 
                 121 
               
               
                 (Sb * Tc)/(Hc * Hm * Tm) * 
                 0.82 
                 0.82 
                 0.82 
                 0.82 
               
               
                 1000 
               
               
                 Deformation Sb (mm) 
                 2.8 
                 2.8 
                 2.8 
                 2.8 
               
               
                 Ball speed (m/s) 
                 73.2 
                 73.2 
                 73.2 
                 73.2 
               
               
                 Spin rate (rpm) 
                 2600 
                 2600 
                 2600 
                 2600 
               
               
                 Flight distance (yd) 
                 290 
                 289.7 
                 290.3 
                 290.5 
               
               
                 Feel at impact 
                 B 
                 B 
                 B 
                 B 
               
               
                   
               
            
           
         
       
     
     
       
         
           
               
             
               
                 TABLE 9 
               
             
            
               
                   
               
               
                 Results of Evaluation 
               
            
           
           
               
               
               
               
               
               
            
               
                   
                 Comp. 
                 Comp. 
                 Comp. 
                 Comp. 
                 Comp. 
               
               
                   
                 Ex. 1 
                 Ex. 2 
                 Ex. 3 
                 Ex. 4 
                 Ex. 5 
               
               
                   
                   
               
            
           
           
               
               
               
               
               
               
            
               
                 Core 
                   
                   
                   
                   
                   
               
               
                 Composition 
                 I 
                 I 
                 I 
                 I 
                 I 
               
               
                 Diameter (mm) 
                 39.7 
                 39.7 
                 39.7 
                 39.7 
                 39.7 
               
               
                 Central hardness 
                 54 
                 54 
                 54 
                 54 
                 54 
               
               
                 (Shore-C) 
               
               
                 Surface hardness 
                 80 
                 80 
                 80 
                 80 
                 80 
               
               
                 (Shore-C) 
               
               
                 Difference DH 
                 26 
                 26 
                 26 
                 26 
                 26 
               
               
                 (Shore-C) 
               
               
                 Mid layer 
               
               
                 Composition 
                 M1 
                 M1 
                 M1 
                 M1 
                 M1 
               
               
                 Hm (Shore-D) 
                 63 
                 63 
                 63 
                 63 
                 63 
               
               
                 Tm (mm) 
                 1.0 
                 1.0 
                 1.0 
                 1.0 
                 1.0 
               
               
                 Cover 
               
               
                 Composition 
                 C1 
                 C1 
                 C1 
                 C1 
                 C1 
               
               
                 Hc (Shore-D) 
                 27 
                 27 
                 27 
                 27 
                 27 
               
               
                 Tc (mm) 
                 0.5 
                 0.5 
                 0.5 
                 0.5 
                 0.5 
               
               
                 Dimple 
                 D5 
                 D6 
                 D7 
                 D8 
                 D9 
               
               
                 (DH * Hm)/(Hc * Tc) 
                 121 
                 121 
                 121 
                 121 
                 121 
               
               
                 (Sb * Tc)/ 
                 0.82 
                 0.82 
                 0.82 
                 0.82 
                 0.82 
               
               
                 (Hc * Hm * Tm) * 1000 
               
               
                 Deformation Sb (mm) 
                 2.8 
                 2.8 
                 2.8 
                 2.8 
                 2.8 
               
               
                 Ball speed (m/s) 
                 73.2 
                 73.2 
                 73.2 
                 73.2 
                 73.2 
               
               
                 Spin rate (rpm) 
                 2600 
                 2600 
                 2600 
                 2600 
                 2600 
               
               
                 Flight distance (yd) 
                 285.9 
                 286.1 
                 289.3 
                 289.1 
                 283.9 
               
               
                 Feel at impact 
                 B 
                 B 
                 B 
                 B 
                 B 
               
               
                   
               
            
           
         
       
     
     
       
         
           
               
             
               
                 TABLE 10 
               
             
            
               
                   
               
               
                 Results of Evaluation 
               
            
           
           
               
               
               
               
               
            
               
                   
                 Ex. 5 
                 Ex. 6 
                 Ex. 7 
                 Ex. 8 
               
               
                   
                   
               
            
           
           
               
               
               
               
               
            
               
                 Core 
                   
                   
                   
                   
               
               
                 Composition 
                 I 
                 I 
                 IV 
                 II 
               
               
                 Diameter (mm) 
                 40.1 
                 40.1 
                 39.7 
                 39.5 
               
               
                 Central hardness 
                 54 
                 54 
                 58 
                 60 
               
               
                 (Shore-C) 
               
               
                 Surface hardness 
                 80 
                 80 
                 78 
                 85 
               
               
                 (Shore-C) 
               
               
                 Difference DH 
                 26 
                 26 
                 20 
                 25 
               
               
                 (Shore-C) 
               
               
                 Mid layer 
               
               
                 Composition 
                 M1 
                 M1 
                 M1 
                 M1 
               
               
                 Hm (Shore-D) 
                 63 
                 63 
                 63 
                 63 
               
               
                 Tm (mm) 
                 0.8 
                 0.8 
                 1.0 
                 1.0 
               
               
                 Cover 
               
               
                 Composition 
                 C1 
                 C4 
                 C4 
                 C1 
               
               
                 Hc (Shore-D) 
                 27 
                 31 
                 31 
                 27 
               
               
                 Tc (mm) 
                 0.5 
                 0.5 
                 0.5 
                 0.6 
               
               
                 Dimple 
                 D1 
                 D4 
                 D4 
                 D1 
               
               
                 (DH * Hm)/(Hc * Tc) 
                 121 
                 106 
                 81 
                 97 
               
               
                 (Sb * Tc)/(Hc * Hm * Tm) * 
                 1.03 
                 0.90 
                 0.77 
                 0.81 
               
               
                 1000 
               
               
                 Deformation Sb (mm) 
                 2.8 
                 2.8 
                 3.0 
                 2.3 
               
               
                 Ball speed (m/s) 
                 73.3 
                 73.3 
                 72.7 
                 73.7 
               
               
                 Spin rate (rpm) 
                 2700 
                 2550 
                 2400 
                 2800 
               
               
                 Flight distance (yd) 
                 289.5 
                 291.5 
                 290 
                 290.5 
               
               
                 Feel at impact 
                 A 
                 B 
                 B 
                 B 
               
               
                   
               
            
           
         
       
     
     
       
         
           
               
             
               
                 TABLE 11 
               
             
            
               
                   
               
               
                 Results of Evaluation 
               
            
           
           
               
               
               
               
               
               
            
               
                   
                   
                   
                   
                   
                 Comp. 
               
               
                   
                 Comp. 
                 Comp. 
                 Comp. 
                 Comp. 
                 Ex. 
               
               
                   
                 Ex. 6 
                 Ex. 7 
                 Ex. 8 
                 Ex. 9 
                 10 
               
               
                   
                   
               
            
           
           
               
               
               
               
               
               
            
               
                 Core 
                   
                   
                   
                   
                   
               
               
                 Composition 
                 I 
                 I 
                 III 
                 I 
                 II 
               
               
                 Diameter (mm) 
                 39.7 
                 39.1 
                 39.7 
                 38.3 
                 39.1 
               
               
                 Central hardness 
                 54 
                 54 
                 60 
                 54 
                 60 
               
               
                 (Shore-C) 
               
               
                 Surface hardness 
                 80 
                 80 
                 70 
                 80 
                 85 
               
               
                 (Shore-C) 
               
               
                 Difference DH 
                 26 
                 26 
                 10 
                 26 
                 25 
               
               
                 (Shore-C) 
               
               
                 Mid layer 
               
               
                 Composition 
                 M4 
                 M1 
                 M2 
                 M3 
                 M2 
               
               
                 Hm (Shore-D) 
                 72 
                 63 
                 68 
                 57 
                 68 
               
               
                 Tm (mm) 
                 1.0 
                 1.0 
                 1.0 
                 1.6 
                 1.0 
               
               
                 Cover 
               
               
                 Composition 
                 C1 
                 C1 
                 C1 
                 C2 
                 C3 
               
               
                 Hc (Shore-D) 
                 27 
                 27 
                 27 
                 38 
                 45 
               
               
                 Tc (mm) 
                 0.5 
                 0.8 
                 0.5 
                 0.6 
                 0.8 
               
               
                 Dimple 
                 D1 
                 D1 
                 D1 
                 D4 
                 D1 
               
               
                 (DH * Hm)/(Hc * Tc) 
                 139 
                 76 
                 50 
                 65 
                 47 
               
               
                 (Sb * Tc)/ 
                 0.69 
                 1.32 
                 0.74 
                 0.50 
                 0.58 
               
               
                 (Hc * Hm * Tm) * 1000 
               
               
                 Deformation Sb (mm) 
                 2.7 
                 2.8 
                 2.7 
                 2.9 
                 2.2 
               
               
                 Ball speed (m/s) 
                 73.4 
                 73.2 
                 73.5 
                 72.9 
                 73.8 
               
               
                 Spin rate (rpm) 
                 2700 
                 2800 
                 3000 
                 2900 
                 3200 
               
               
                 Flight distance (yd) 
                 290 
                 288 
                 287.5 
                 286 
                 287 
               
               
                 Feel at impact 
                 C 
                 A 
                 C 
                 C 
                 D 
               
               
                   
               
            
           
         
       
     
     As shown in Tables 8 to 11, the golf ball of each Example is excellent in flight performance and feel at impact upon a shot with a driver. From the results of evaluation, advantages of the present invention are clear. 
     The golf ball according to the present invention is suitable for, for example, playing golf on golf courses and practicing at driving ranges. The above descriptions are merely illustrative examples, and various modifications can be made without departing from the principles of the present invention.