JPH0566829B2 - - Google Patents
Info
- Publication number
- JPH0566829B2 JPH0566829B2 JP62102803A JP10280387A JPH0566829B2 JP H0566829 B2 JPH0566829 B2 JP H0566829B2 JP 62102803 A JP62102803 A JP 62102803A JP 10280387 A JP10280387 A JP 10280387A JP H0566829 B2 JPH0566829 B2 JP H0566829B2
- Authority
- JP
- Japan
- Prior art keywords
- neck
- copper alloy
- face
- beryllium copper
- face member
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 229910000881 Cu alloy Inorganic materials 0.000 claims description 23
- DMFGNRRURHSENX-UHFFFAOYSA-N beryllium copper Chemical compound [Be].[Cu] DMFGNRRURHSENX-UHFFFAOYSA-N 0.000 claims description 23
- 229910052802 copper Inorganic materials 0.000 description 5
- 239000010949 copper Substances 0.000 description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- 229910045601 alloy Inorganic materials 0.000 description 4
- 239000000956 alloy Substances 0.000 description 4
- 229910052790 beryllium Inorganic materials 0.000 description 3
- ATBAMAFKBVZNFJ-UHFFFAOYSA-N beryllium atom Chemical compound [Be] ATBAMAFKBVZNFJ-UHFFFAOYSA-N 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 229910052709 silver Inorganic materials 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 description 2
- 150000001572 beryllium Chemical class 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 239000011572 manganese Substances 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 239000004332 silver Substances 0.000 description 2
- 239000006104 solid solution Substances 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 239000011701 zinc Substances 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910000730 Beta brass Inorganic materials 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 239000012141 concentrate Substances 0.000 description 1
- 230000000994 depressogenic effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 239000011133 lead Substances 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 229910052748 manganese Inorganic materials 0.000 description 1
- 239000000155 melt Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000012778 molding material Substances 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 239000002244 precipitate Substances 0.000 description 1
- 238000004881 precipitation hardening Methods 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 229910052710 silicon Inorganic materials 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
Description
[発明の目的]
(産業上の利用分野)
本発明はベリリウム銅合金を用いたゴルフクラ
ブヘツドに関する。
(従来の技術)
ゴルフクラブの性能としては、より飛距離が出
ること、ならびに方向安定性に優れていることが
望まれる。ところでより高硬度の材料によりクラ
ブヘツドを構成すれば、飛距離を拡大し得ること
がわかつている。このため種々の材料から成るク
ラブヘツドが公知である。例えば実開昭59−
161851号公報においてはクラブヘツドを成形する
成形材料に、Ag1%、Cu4%をそれぞれ含有する
アルミニウム合金を用いたものであり、また特開
昭60−782号公報においてはフエース部を亜鉛
Zn、アルミニウムAl、ニツケルNi、シリコンSi、
スズSn、マンガンMn、銀Ag、マグネシウムMg
等を含む群から選択される1種以上の元素をβ黄
銅型構造を有し得る範囲で含有し、残部がCuよ
りなるβ黄銅型合金であつて、室温でオーステナ
イト相となるような組成の合金により構成される
ものである。
しかしながら、従来の素材においては飛距離を
伸ばすために高硬度化すると他の機械的性能、例
えば弾性係数、引張り強さ等の性能が劣化し、こ
の強度上の問題で飛距離を著しく伸ばすことがで
きなかつた。
このような問題点を解決する一手段として、同
一出願人は特願昭62−60567号において強度のみ
ならず弾力に優れるベリリウム銅合金を用いたゴ
ルフクラブヘツドを提案している。
(発明が解決しようとする問題点)
ベリリウム銅合金は鋼に比較して弾性係数、引
張り強さに優れているが、従来のヘツドと同じ形
状、構造ではその性能を有効に利用することはで
きない問題点があつた。
本発明は前記問題点に基づいて成されたもので
あり、ベリリウム銅合金の性能を有効に利用した
ゴルフクラブヘツドを提供することを目的とす
る。
[発明の構成]
(問題点を解決するための手段)
第1発明は、フエース3のヒール4側にネツク
5を斜設したヘツドをベリリウム銅合金により形
成すると共に、前記ネツク5のヒール4側をネツ
ク5の中央部5Bより径小に形成する。
第2発明は、薄肉化したフエース部材12のヒ
ール13にネツク14を斜設したベリリウム銅合
金から成るヘツド本体11の背面にバランスウエ
ート15を固設する。
(作用)
第1発明ではシヨツト時に径小なネツク5の下
端5Aによつて強力な弾力が発揮でき、飛距離を
伸ばすことができる。
第2発明では、シヨツト時に薄肉化したフエー
ス部材12によつて強力な弾力が発揮でき、飛距
離を伸ばすことができる。
(実施例)
第1図ないし第3図は第1発明を示す第1実施
例であつて、1はヘツド本体であつて、このヘツ
ド本体1は銅の中に3%以下のベリリウムを固溶
させ、これに少量の元素、例えばコバルト、ニツ
ケル、銀を添加した析出硬化型合金であるベリリ
ウム銅合金を後述する伸び率内の鍛造を繰り返し
て成形後、硬化のための熱処理を施したものであ
り、溝条2を形成したフエース3の一側、すなわ
ちヒール4に適度なライ角を有してネツク5を斜
設する。前記ネツク5のヒール4側、すなわちネ
ツク5の下端5Aの径Aをネツク5の中央部5B
の径Bより細く形成し、また前記ネツク5にはシ
ヤフト6を接続する。
次表は代表的なベリリウム銅合金の化学成分を
示す。
[Object of the Invention] (Industrial Application Field) The present invention relates to a golf club head using beryllium copper alloy. (Prior Art) As for the performance of a golf club, it is desired that the golf club has greater flight distance and excellent directional stability. However, it has been found that if the club head is made of a material with higher hardness, it is possible to increase the flight distance. Club heads made of various materials are known for this purpose. For example, Utsukai Showa 59-
In JP-A No. 161851, an aluminum alloy containing 1% Ag and 4% Cu was used as the molding material for the club head, and in JP-A-60-782, the face part was made of zinc.
Zn, Aluminum Al, Nickel Ni, Silicon Si,
Tin Sn, manganese Mn, silver Ag, magnesium Mg
A β-brass type alloy containing one or more elements selected from the group including It is composed of an alloy. However, with conventional materials, when hardness is increased in order to increase flight distance, other mechanical properties such as elastic modulus and tensile strength deteriorate, and this strength problem makes it difficult to significantly increase flight distance. I couldn't do it. As a means of solving these problems, the same applicant proposed a golf club head using beryllium copper alloy, which has excellent not only strength but also elasticity, in Japanese Patent Application No. 60567/1982. (Problem to be solved by the invention) Beryllium copper alloy has superior elastic modulus and tensile strength compared to steel, but its performance cannot be effectively utilized with the same shape and structure as conventional heads. There was a problem. The present invention has been made based on the above-mentioned problems, and an object of the present invention is to provide a golf club head that effectively utilizes the performance of beryllium copper alloy. [Structure of the Invention] (Means for Solving the Problems) The first invention forms a head having a neck 5 obliquely provided on the heel 4 side of the face 3 from a beryllium copper alloy, and also forms a head with a beryllium copper alloy on the heel 4 side of the neck 5. is formed to have a smaller diameter than the center portion 5B of the neck 5. In the second invention, a balance weight 15 is fixed to the back surface of a head body 11 made of a beryllium copper alloy, in which a neck 14 is obliquely provided on a heel 13 of a face member 12 having a thinner wall. (Function) In the first invention, strong elasticity can be exerted by the lower end 5A of the neck 5 having a small diameter at the time of shot, and the flight distance can be extended. In the second invention, strong elasticity can be exerted by the thinned face member 12 at the time of shot, and flight distance can be extended. (Embodiment) Figures 1 to 3 show a first embodiment of the first invention, in which 1 is a head body, and this head body 1 contains 3% or less of beryllium as a solid solution in copper. A beryllium-copper alloy, which is a precipitation-hardening alloy made by adding small amounts of elements such as cobalt, nickel, and silver, is repeatedly forged within the elongation rate described below, and then heat-treated for hardening. A neck 5 is provided obliquely on one side of the face 3 on which the grooves 2 are formed, that is, on the heel 4, with an appropriate lie angle. The diameter A of the heel 4 side of the neck 5, that is, the lower end 5A of the neck 5 is the center part 5B of the neck 5.
A shaft 6 is connected to the neck 5. The following table shows the chemical composition of typical beryllium copper alloys.
【表】
〓単位%〓
前記ベリリウム銅合金は、例えば800℃で2%
のベリリウムが銅に溶け込み後、……常温では
0.2%位しか溶けない……高温から急冷すれば過
飽和となつたベリリウムを固溶したままのα相の
組織が容体化処理によつて得られ、そして溶体化
処理したものを例えば315℃程度に加熱した後自
然冷却すると、過飽和のベリリウムはγ相、銅と
ベリリウムの金属間化合物として析出し、該熱処
理によつて著しく硬くなる。
次表は溶体化処理及び硬化処理の処理温度を示
している。[Table] 〓Unit %〓
The beryllium copper alloy is, for example, 2% at 800°C.
After the beryllium dissolves into the copper...at room temperature...
Only about 0.2% melts...If rapidly cooled from a high temperature, an α-phase structure containing supersaturated beryllium as a solid solution can be obtained by solution treatment. When naturally cooled after heating, supersaturated beryllium precipitates as a γ phase, an intermetallic compound of copper and beryllium, and becomes extremely hard due to the heat treatment. The following table shows the processing temperatures for solution treatment and hardening treatment.
【表】【table】
【表】
次表はベリリウム銅合金の機械的特性及び他の
合金との比較を示している。[Table] The following table shows the mechanical properties of beryllium copper alloys and comparisons with other alloys.
【表】
次に前記構成につきその作用を説明する。
シヨツト時において、ゴルフボール(図示せ
ず)がフエース3に当つて衝撃力が加わると該衝
撃がネツク5の下端5Aに集中し歪が生ずる。そ
してゴルフボールが離れる際には下端5Aの復元
力により強力な反発力が生じ、飛距離を伸ばすこ
とができる。
以上のように、ヘツド本体1全体をベリリウム
銅合金によつて成形してフエース3を硬化処理す
ることによつて、ゴルフボールの打球面を高硬度
化でき飛距離を伸ばすことができる。
さらにベリリウム銅合金によりヘツド本体1を
成形することによつて、高い強度と適度な縦弾性
係数、すなわち優れたばね特性を有することがで
きる。この結果ゴルフボールに高い接触圧力を与
えることができ、シヨツト時のゴルフボールの初
速度を大きくでき飛距離をさらに伸ばすことがで
きる。またシヨツト数に伴つてフエース3には衝
撃が繰り返されるが高い耐疲労性をもつているた
め長期間当初の性能を保つことができる。
特に、ネツク5の下端5Aを中央部5Bより径
小に形成したためフエース3がゴルフボールに当
つた際の衝撃力が下端5Aに集中して歪が生じ、
そして該下端5Aの復元力、すなわち弾力による
反発力によつてゴルフボールを打球して、飛距離
を伸ばすことができる。この際ネツク5の下端5
Aはベリリウム銅合金の特性により高強度を発揮
でき折れ曲る虞れもない。
第4図及び第5図は第2発明を示す第2実施例
であつて、11は板状のフエース部材12のヒー
ル13側にネツク14を所定のライ角を有して斜
設したヘツド本体であつて、このヘツド本体11
はベリリウム銅合金から成る。15は前記フエー
ス部材12の背面に上部を開口した中空部16を
介して固設するバランスウエートであつて、例え
ばベリリウム銅合金、鉛、銅等比較的比重の大き
い金属から成り、ヘツドの重心位置を調節するた
めにソール15A寄りを大きく形成する等所定の
形状に形成する。
前記ベリリウム銅合金から成るフエース部材1
2は従来の中空アイアンヘツドより薄い、例えば
2〜4mm、望ましくは略3mmの厚みTを有するよ
うに設定する。
次に前記構成につきその作用を説明する。
シヨツト時にゴルフボール(図示せず)がフエ
ース12Aに当つて衝撃力が加わると、該衝撃力
によつてフエース部材12は窪む。次にフエース
部材12の窪み箇所がベリリウム銅合金の弾性に
より復元し、ゴルフボールが離れる際強力な前記
復元弾力によつてゴルフボールをシヨツトでき
る。
以上のようにフエース部材12にベリリウム銅
合金を用いることによつて、高硬度化、強力な引
張り強さを図ることができ、ゴルフボールの飛距
離を伸ばすことができる。特にフエース部材12
の厚みTを2〜4mm、望ましくは略3mmにして薄
肉化することにより、シヨツト時における窪みを
大きくでき、すなわち弾性エネルギーの蓄積量を
大きくでき、ゴルフボールが離れる際には、強力
な復元力を発揮でき、飛距離を伸ばすことができ
る。
第6図は他の実施例であり、前記第2実施例と
同一部分には同一符号を付して説明する。
薄肉化したフエース部材12の背面に密閉状の
中空部16を介してバランスウエート15を固着
する。
尚、本発明は前記各実施例に限定されるもので
はなく、例えば第1実施例においては第2実施例
と同様に中空構造としてもよく、また第2実施例
においては中空部に発泡樹脂を充填してもよい等
種々の変形が可能である。
[発明の効果]
第1発明はフエースと共にネツクをベリリウム
銅合金により成形すると共に、前記ネツクの下端
を径小に形成することによつて、ネツクの下端に
おいて強力なばね性を発揮でき飛距離を伸ばすこ
とができる。
第2発明はベリリウム銅合金から成るフエース
部材を肉薄化することによつて、シヨツト時にフ
エース部材が強力なばね性を発揮でき飛距離を伸
ばすことができる。[Table] Next, the operation of the above structure will be explained. During a shot, when a golf ball (not shown) hits the face 3 and an impact force is applied, the impact concentrates on the lower end 5A of the neck 5, causing distortion. When the golf ball leaves the golf ball, a strong repulsive force is generated by the restoring force of the lower end 5A, and the flight distance can be increased. As described above, by molding the entire head body 1 from beryllium copper alloy and hardening the face 3, the hitting surface of the golf ball can be made highly hard and the flight distance can be increased. Furthermore, by molding the head body 1 from a beryllium copper alloy, it can have high strength and an appropriate modulus of longitudinal elasticity, that is, excellent spring characteristics. As a result, a high contact pressure can be applied to the golf ball, and the initial velocity of the golf ball at the time of shot can be increased, making it possible to further extend the flight distance. Further, as the number of shots increases, the face 3 is subjected to repeated impacts, but since it has high fatigue resistance, it can maintain its original performance for a long period of time. In particular, since the lower end 5A of the net 5 is formed to have a smaller diameter than the central portion 5B, the impact force when the face 3 hits the golf ball is concentrated on the lower end 5A, causing distortion.
The restoring force of the lower end 5A, that is, the repulsive force due to the elasticity, allows the golf ball to be hit and the flight distance to be extended. At this time, the lower end 5 of the net 5
A exhibits high strength due to the characteristics of beryllium copper alloy and has no risk of bending. 4 and 5 show a second embodiment of the second invention, in which reference numeral 11 denotes a head body in which a neck 14 is provided obliquely at a predetermined lie angle on the heel 13 side of a plate-shaped face member 12. And this head body 11
consists of a beryllium-copper alloy. A balance weight 15 is fixed to the back surface of the face member 12 through a hollow part 16 having an open top, and is made of a metal with relatively high specific gravity such as beryllium copper alloy, lead, copper, etc. In order to adjust this, the sole 15A is formed into a predetermined shape, such as by making the part closer to the sole 15A larger. Face member 1 made of the beryllium copper alloy
2 is set to have a thickness T which is thinner than a conventional hollow iron head, for example, 2 to 4 mm, preferably approximately 3 mm. Next, the operation of the above structure will be explained. When a golf ball (not shown) hits the face 12A during a shot and an impact force is applied, the face member 12 is depressed by the impact force. Next, the recessed portion of the face member 12 is restored by the elasticity of the beryllium copper alloy, and when the golf ball is released, the strong restoring elasticity allows the golf ball to be shot. As described above, by using beryllium copper alloy for the face member 12, high hardness and strong tensile strength can be achieved, and the flight distance of the golf ball can be extended. Especially the face member 12
By reducing the thickness T to 2 to 4 mm, preferably approximately 3 mm, it is possible to increase the depression during shot, which means that the amount of elastic energy stored can be increased, and when the golf ball is released, it has a strong restoring force. You can demonstrate this and increase your flying distance. FIG. 6 shows another embodiment, and the same parts as in the second embodiment will be described with the same reference numerals. A balance weight 15 is fixed to the back surface of the thinned face member 12 via a sealed hollow part 16. It should be noted that the present invention is not limited to the above embodiments; for example, the first embodiment may have a hollow structure similar to the second embodiment, and the second embodiment may have a hollow structure filled with foamed resin. Various modifications are possible, such as filling. [Effects of the Invention] In the first invention, the face and the neck are molded from a beryllium copper alloy, and the lower end of the neck is formed to have a small diameter, so that the lower end of the neck can exhibit strong spring properties and increase flight distance. It can be stretched. In the second aspect of the invention, by thinning the face member made of beryllium copper alloy, the face member can exhibit strong springiness during shot, thereby increasing flight distance.
第1図ないし第3図は第1実施例を示してお
り、第1図は正面図、第2図は斜視図、第3図A
は第1図の−線断面図、第3図Bは第1図の
−線断面図、第4図及び第5図は第2実施例
を示しており、第4図は一部切欠き斜視図、第5
図は正面図、第6図は他の実施例の一部切欠き斜
視図である。
1,11……ヘツド本体、3……フエース、
5,14……ネツク、5A……下端、5B……中
空部、12……フエース部材、15……バランス
ウエート、16……中空部、T……厚み。
Figures 1 to 3 show the first embodiment, where Figure 1 is a front view, Figure 2 is a perspective view, and Figure 3A is a perspective view.
1 is a sectional view taken along the - line in FIG. 1, FIG. 3B is a sectional view taken along the - line in FIG. 1, FIGS. 4 and 5 show the second embodiment, and FIG. Figure, 5th
The figure is a front view, and FIG. 6 is a partially cutaway perspective view of another embodiment. 1, 11...Head body, 3...Face,
5, 14...Net, 5A...Lower end, 5B...Hollow part, 12...Face member, 15...Balance weight, 16...Hollow part, T...Thickness.
Claims (1)
体をベリリウム銅合金により形成すると共に、前
記ネツクの下端をネツクの中央部より径小に形成
することを特徴とするゴルフクラブヘツド。 2 板状のフエース部材の一側にネツクを斜設し
たヘツド本体をベリリウム銅合金により形成し、
前記フエース部材の背面に中空部を介してバラン
スウエートを固設すると共に、前記フエース部材
を薄く形成することを特徴とするゴルフクラブヘ
ツド。 3 前記フエースの厚みが2〜4mmであることを
特徴とする特許請求の範囲第1項記載のゴルフク
ラブヘツド。[Scope of Claims] 1. A golf club characterized in that a head body having a neck obliquely provided on one side of the face is formed of a beryllium copper alloy, and the lower end of the neck is formed to have a smaller diameter than the center of the neck. Head. 2. A head body with a diagonal neck on one side of a plate-shaped face member is formed of beryllium copper alloy,
A golf club head characterized in that a balance weight is fixed to the back surface of the face member via a hollow part, and the face member is formed thin. 3. The golf club head according to claim 1, wherein the face has a thickness of 2 to 4 mm.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP62102803A JPS63267376A (en) | 1987-04-25 | 1987-04-25 | Golf club head |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP62102803A JPS63267376A (en) | 1987-04-25 | 1987-04-25 | Golf club head |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP6202390A Division JPH07144030A (en) | 1994-08-26 | 1994-08-26 | Golf club head |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS63267376A JPS63267376A (en) | 1988-11-04 |
JPH0566829B2 true JPH0566829B2 (en) | 1993-09-22 |
Family
ID=14337224
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP62102803A Granted JPS63267376A (en) | 1987-04-25 | 1987-04-25 | Golf club head |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS63267376A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2010017475A (en) * | 2008-07-14 | 2010-01-28 | Mizuno Corp | Iron golf club head and iron golf club |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5626530A (en) * | 1992-08-05 | 1997-05-06 | Callaway Golf Company | Golf club head with sole bevel indicia |
US5409229A (en) * | 1992-08-05 | 1995-04-25 | Callaway Golf Company | Golf club head with audible vibration attenuation |
US5330187A (en) * | 1992-08-05 | 1994-07-19 | Callaway Golf Company | Iron golf club head with dual intersecting recesses |
US5472203A (en) * | 1992-08-05 | 1995-12-05 | Callaway Golf Company | Iron golf club head with dual intersecting recesses |
US5603667A (en) * | 1993-12-28 | 1997-02-18 | Bridgestone Sports Co., Ltd. | Golf club head |
US5776010A (en) * | 1997-01-22 | 1998-07-07 | Callaway Golf Company | Weight structure on a golf club head |
JP3269075B2 (en) * | 1998-03-23 | 2002-03-25 | 株式会社遠藤製作所 | Golf club and manufacturing method thereof |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5977874A (en) * | 1982-08-30 | 1984-05-04 | カ−ステン・マニユフアクチユアリング・コ−ポレ−シヨン | Golf club set having improved off-center impact capacity |
-
1987
- 1987-04-25 JP JP62102803A patent/JPS63267376A/en active Granted
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5977874A (en) * | 1982-08-30 | 1984-05-04 | カ−ステン・マニユフアクチユアリング・コ−ポレ−シヨン | Golf club set having improved off-center impact capacity |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2010017475A (en) * | 2008-07-14 | 2010-01-28 | Mizuno Corp | Iron golf club head and iron golf club |
Also Published As
Publication number | Publication date |
---|---|
JPS63267376A (en) | 1988-11-04 |
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