JP2010136908A - Method of manufacturing golf club shaft - Google Patents

Method of manufacturing golf club shaft Download PDF

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JP2010136908A
JP2010136908A JP2008316431A JP2008316431A JP2010136908A JP 2010136908 A JP2010136908 A JP 2010136908A JP 2008316431 A JP2008316431 A JP 2008316431A JP 2008316431 A JP2008316431 A JP 2008316431A JP 2010136908 A JP2010136908 A JP 2010136908A
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braided
orientation angle
braided layer
laminate
layer
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JP5287200B2 (en
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Masanari Yamamoto
真生 山本
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Yokohama Rubber Co Ltd
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<P>PROBLEM TO BE SOLVED: To provide a method of manufacturing a golf club shaft capable of improving the productivity and the quality by hardening a laminated body and facilitating polishing a braided layer, an object to be polished, in just proportion when using a braiding process. <P>SOLUTION: In this method of manufacturing the shaft, when base material fibers 3 impregnated with a resin material are braided on the periphery of a mandrel at a predetermined orientation angle with respect to a mandrel shaft direction and tapered cylindrical braided layers are sequentially superposed to form a tapered cylindrical laminated body 2, at least when the outermost peripheral third braided layer 2c is formed, the base material fibers 3 are braided by increasingly changing the orientation angle on the axial rear end side more than that of the axial end side, with defining the orientation angle a1 smaller than the orientation angle a2, and, after the formed laminated body 2 is heated and hardened, the surface of the laminated body 2 is polished at a fixed thickness. <P>COPYRIGHT: (C)2010,JPO&INPIT

Description

この発明は、ゴルフクラブ用シャフトの製造方法に関し、さらに詳しくは、ブレーディング製法を用いた際に、積層体を硬化させた後に研磨対象となる編組層を過不足なく研磨し易くして、生産性と品質の向上を図ることができるゴルフクラブ用シャフトの製造方法に関するものである。   The present invention relates to a method for manufacturing a shaft for a golf club, and more particularly, when a braided manufacturing method is used, a braided layer to be polished is easily polished without excess or deficiency after the laminate is cured, and is produced. The present invention relates to a method for manufacturing a golf club shaft capable of improving the performance and quality.

ゴルフクラブ用シャフトの製造方法としてブレーディング製法が知られている(例えば、特許文献1参照)。ブレーディング製法では、マンドレル上で樹脂材料を含浸させた基材繊維をマンドレル軸方向に対して対称の配向角度で編組させて編組層を形成し、この編組層を複数積層させて先細円筒状の積層体を成形する。その後、この積層体を加熱することにより、基材繊維に含浸させた樹脂材料を硬化させる。硬化させた積層体の表面は、編組された基材繊維の影響によって凹凸になるので、この凹凸を滑らかにするために硬化させた積層体の表面を研磨するようにしている。   As a method for manufacturing a golf club shaft, a braiding method is known (see, for example, Patent Document 1). In the braiding method, a base fiber impregnated with a resin material on a mandrel is braided at a symmetrical orientation angle with respect to the mandrel axial direction to form a braided layer, and a plurality of the braided layers are laminated to form a tapered cylindrical shape. A laminate is formed. Thereafter, the laminate is heated to cure the resin material impregnated in the base fiber. Since the surface of the cured laminate becomes uneven due to the influence of the braided base fiber, the surface of the cured laminate is polished to smooth the unevenness.

従来、ブレーディング製法では図8、図9に例示するように、積層するそれぞれの編組層(第1編組層2a、第2編組層2b、第3編組層2c)を形成する際に、基材繊維3の配向角度aを軸方向位置で変化させることなく一定にして編組している。そのため、成形した先細円筒状の積層体2の軸方向先端側の小径範囲では、図10に例示するように積層体2の外周長さに対する基材繊維3の断面積(層を形成する基材繊維3の断面積の総和)が大きくなるので、隣り合う基材繊維3どうしが圧縮しあって層厚t1が大きくなる傾向にある。一方、積層体2の軸方向後端側の大径範囲では、図11に例示するように先端側に比べて、積層体2の外周長さに対する基材繊維3の断面積(層を形成する基材繊維3の断面積の総和)が小さくなるので層厚t2が小さくなる傾向になる。即ち、図9に例示するように、それぞれの編組層2a、2b、2cにおいて、層厚が軸方向先端側が後端側よりも大きくなる。第3編組層2cに関していえば、層厚t1>層厚t2となっている。   Conventionally, in the braiding method, as illustrated in FIGS. 8 and 9, when forming each of the braided layers (the first braided layer 2 a, the second braided layer 2 b, and the third braided layer 2 c) to be laminated, The fiber 3 is braided with a constant orientation angle a without changing the axial position. Therefore, in the small diameter range on the tip end side in the axial direction of the formed tapered cylindrical laminate 2, the cross-sectional area of the base fiber 3 with respect to the outer peripheral length of the laminate 2 as shown in FIG. Since the sum of the cross-sectional areas of the fibers 3) increases, the adjacent base fibers 3 are compressed and the layer thickness t1 tends to increase. On the other hand, in the large diameter range on the rear end side in the axial direction of the laminated body 2, as shown in FIG. Since the sum of the cross-sectional areas of the base fibers 3 becomes smaller, the layer thickness t2 tends to become smaller. That is, as illustrated in FIG. 9, in each braided layer 2 a, 2 b, 2 c, the layer thickness is larger at the axial front end than at the rear end. Regarding the third braided layer 2c, the layer thickness t1> the layer thickness t2.

硬化させた積層体2の表面は、一般に、回転する研磨体を用いて、積層体2の軸方向に一定の厚さで研磨しているので、研磨対象となる最外周の第3編組層2cを研磨すると軸方向先端側の範囲には、第3編組層2cの研磨残りが生じる。積層体2の軸方向で一部に研磨残りがある場合、或いは、研磨残りの厚さにばらつきがあると、製造したシャフトの品質(性能)に悪影響が生じる。   Since the surface of the cured laminate 2 is generally polished with a constant thickness in the axial direction of the laminate 2 using a rotating abrasive body, the outermost third braid layer 2c to be polished is used. When polishing is performed, an unpolished portion of the third braided layer 2c is generated in the range on the tip side in the axial direction. If there is a part of the polishing residue in the axial direction of the laminate 2 or if the thickness of the polishing residue varies, the quality (performance) of the manufactured shaft is adversely affected.

そのため、この研磨残りをなくすため、或いは、研磨残りの厚さのばらつきをなくすために追加的に研磨作業をする必要があった。このように、シャフトの品質を維持、向上させるために、追加的な研磨作業を行なうので生産性を向上させるには限界があった。
特開2002−177424号公報
Therefore, it is necessary to perform additional polishing work in order to eliminate this polishing residue or to eliminate variations in the thickness of the polishing residue. Thus, in order to maintain and improve the quality of the shaft, additional polishing work is performed, so there is a limit to improving productivity.
JP 2002-177424 A

本発明の目的は、ブレーディング製法を用いた際に、積層体を硬化させた後に研磨対象となる編組層を過不足なく研磨し易くして、生産性と品質の向上を図ることができるゴルフクラブ用シャフトの製造方法を提供することにある。   An object of the present invention is to improve productivity and quality by making it easy to polish a braided layer to be polished without excess or deficiency after curing a laminate when using a braiding method. It is in providing the manufacturing method of the shaft for clubs.

上記目的を達成するため本発明のゴルフクラブ用シャフトの製造方法は、樹脂材料を含浸させた基材繊維を、マンドレル外周上にマンドレル軸方向に対して所定の配向角度で編組することにより順次、先細円筒状の編組層を積層して先細円筒状の積層体を成形し、この積層体を加熱することにより基材繊維に含浸させた樹脂材料を硬化させ、次いで、硬化させた積層体の表面を研磨するゴルフクラブ用シャフトの製造方法において、前記積層した編組層のうち、少なくとも最外周の編組層を形成する際には、前記配向角度が軸方向先端側よりも後端側が大きくなるように変化させて基材繊維を編組することを特徴とするものである。   In order to achieve the above object, the golf club shaft manufacturing method of the present invention sequentially braces base fibers impregnated with a resin material at a predetermined orientation angle with respect to the mandrel axial direction on the mandrel outer periphery. A tapered cylindrical braided layer is laminated to form a tapered cylindrical laminate, and the laminate is heated to cure the resin material impregnated in the base fiber, and then the surface of the cured laminate In the method for manufacturing a golf club shaft for polishing a golf club shaft, when forming at least the outermost outermost braided layer of the laminated braided layers, the rear end side is larger than the front end side in the axial direction. It is characterized by braiding the base fiber by changing.

ここで、前記配向角度を変化させて形成した編組層の最大層厚と最小層厚との差を、例えば、0.1mm以下にする。また、前記配向角度を変化させる範囲を、例えば、10°〜70°にする。前記硬化させた積層体を、例えば、回転する研磨体の間を通過させることにより、表面を一定厚さ研磨する。   Here, the difference between the maximum layer thickness and the minimum layer thickness of the braided layer formed by changing the orientation angle is set to 0.1 mm or less, for example. Moreover, the range which changes the said orientation angle shall be 10 degrees-70 degrees, for example. The cured laminate is, for example, passed between rotating abrasive bodies to polish the surface to a certain thickness.

本発明によれば、樹脂材料を含浸させた基材繊維を、マンドレル外周上にマンドレル軸方向に対して所定の配向角度で編組することにより順次、先細円筒状の編組層を積層して先細円筒状の積層体を成形し、この積層体を加熱することにより基材繊維に含浸させた樹脂材料を硬化させ、次いで、硬化させた積層体の表面を研磨するゴルフクラブ用シャフトの製造方法において、前記積層した編組層のうち、少なくとも最外周の編組層を形成する際には、前記配向角度が軸方向先端側よりも後端側が大きくなるように変化させて基材繊維を編組するので、配向角度を変化させた編組層では、先細円筒状の積層体の軸方向位置の違いによる層厚の差を小さくすることができる。これにより、積層体を硬化させた後に研磨対象となる編組層(主に最外周の編組層)を一定の厚さで研磨すれば、この編組層を設定どおり過不足なく研磨することが可能になる。即ち、積層体の表面を軸方向全長にわたって必要以上に研磨したり、必要以上に研磨残りが生じたりすることが回避できるので生産性と品質の向上を図ることができる。   According to the present invention, the base fiber impregnated with the resin material is braided on the outer periphery of the mandrel at a predetermined orientation angle with respect to the mandrel axial direction, so that the tapered cylindrical braided layer is sequentially laminated. In the method for manufacturing a golf club shaft, the resin material impregnated in the base fiber is cured by heating the laminate, and then the surface of the cured laminate is polished. Among the laminated braided layers, when forming at least the outermost braided layer, the base fiber is braided by changing the orientation angle so that the rear end side is larger than the axial front end side. In the braided layer with the angle changed, the difference in layer thickness due to the difference in the axial position of the tapered cylindrical laminate can be reduced. As a result, if the braided layer to be polished (mainly the outermost braided layer) is polished to a certain thickness after the laminate is cured, the braided layer can be polished without excess or deficiency as set. Become. That is, since it is possible to avoid unnecessarily polishing the surface of the laminate over the entire length in the axial direction and causing unnecessarily unpolished residues, productivity and quality can be improved.

本発明のゴルフクラブ用シャフトの製造方法を、図に示した実施形態に基づいて説明する。   A golf club shaft manufacturing method of the present invention will be described based on the embodiment shown in the drawings.

本発明によりゴルフクラブ用シャフト(以下、シャフト1という)を製造する際には、図5に例示するような一般的な編組装置6を用いる。この編組装置6は、基材繊維3を巻回した複数のボビン7を回転ベース6aに設置し、回転ベース6aの中心部には先細円筒状または円柱状のマンドレル5が挿通する構成になっている。基材繊維3には樹脂材料が含浸されている。   When manufacturing a golf club shaft (hereinafter referred to as shaft 1) according to the present invention, a general braiding device 6 as illustrated in FIG. 5 is used. This braiding device 6 has a configuration in which a plurality of bobbins 7 wound with base fibers 3 are installed on a rotating base 6a, and a tapered cylindrical or columnar mandrel 5 is inserted through the center of the rotating base 6a. Yes. The base fiber 3 is impregnated with a resin material.

基材繊維3としては、炭素繊維、アラミド繊維、金属繊維、ガラス繊維、ボロン繊維等を例示できる。基材繊維3に含浸させる樹脂材料としては、熱硬化性樹脂、例えば、エポキシ樹脂、不飽和ポリエステル樹脂等を用いる。   Examples of the base fiber 3 include carbon fiber, aramid fiber, metal fiber, glass fiber, and boron fiber. As a resin material to be impregnated into the base fiber 3, a thermosetting resin such as an epoxy resin or an unsaturated polyester resin is used.

このマンドレル5を軸方向に移動させて回転ベース6aに挿通させつつ、回転ベース6aをマンドレル5を中心にして回転させることにより、それぞれのボビン7から基材繊維3を引出す。これにより、マンドレル5の外周上にマンドレル5の軸方向(マンドレル5の軸心CL)に対して対称に所定の配向角度aで基材繊維3が編組され、先細円筒状の第1編組層2aが形成される。この第1編組層2aの外周上に同様に第2編組層2b、第2編組層2bの外周上に同様に第3編組層3cを、マンドレル5の軸心CL(即ち、成形する積層体2の軸心CL)を中心にして同軸上に順次積層して先細円筒状の積層体2を成形する。   The base fiber 3 is pulled out from each bobbin 7 by rotating the mandrel 5 around the mandrel 5 while moving the mandrel 5 in the axial direction and inserting the mandrel 5 through the rotation base 6a. As a result, the base fiber 3 is braided on the outer periphery of the mandrel 5 at a predetermined orientation angle a symmetrically with respect to the axial direction of the mandrel 5 (axis CL of the mandrel 5), and the tapered first cylindrical braided layer 2a. Is formed. Similarly, the second braided layer 2b on the outer periphery of the first braided layer 2a, the third braided layer 3c in the same manner on the outer periphery of the second braided layer 2b, and the axial center CL of the mandrel 5 (that is, the laminate 2 to be molded). Are laminated in order on the same axis around the axis CL) to form a tapered cylindrical laminate 2.

ここで、例えば、第1編組層2a、第2編組層2bを形成する際には、マンドレル5の軸方向で基材繊維3の配向角度aを変化させることなく一定の角度にする。そして、積層体2の最外周の第3編組層2cを形成する際には、基材繊維3の配向角度aがマンドレル5の軸方向先端側よりも後端側が大きくなるように変化させて編組する。   Here, for example, when forming the first braided layer 2 a and the second braided layer 2 b, the orientation angle a of the base fiber 3 is set to a constant angle in the axial direction of the mandrel 5. Then, when forming the outermost third braided layer 2 c of the laminate 2, the orientation angle a of the base fiber 3 is changed so that the rear end side is larger than the axial front end side of the mandrel 5. To do.

第3編組層2cの基材繊維3の配向角度aを変化させるには、回転ベース6aの回転速度を一定に維持しながらマンドレル5の軸方向の送り速度を変化させることよって、容易に変化させることができる。例えば、配向角度aを大きくする場合には、マンドレル5の軸方向の送り速度を遅くし、配向角度aを小さくする場合には、マンドレル5の軸方向の送り速度を速くすればよい。   In order to change the orientation angle a of the base fiber 3 of the third braided layer 2c, it is easily changed by changing the axial feed speed of the mandrel 5 while keeping the rotation speed of the rotation base 6a constant. be able to. For example, when the orientation angle a is increased, the axial feed rate of the mandrel 5 is decreased, and when the orientation angle a is decreased, the axial feed rate of the mandrel 5 is increased.

これにより、図1に例示するように、最外周の第3編組層2cの基材繊維3の配向角度aを軸方向先端側よりも後端側が大きくなるように変化させた先細円筒状の積層体2を成形することができる。この積層体2では、先端側の配向角度a1よりも後端側の配向角度a2が大きくなっている(a1<a2)。   Thus, as illustrated in FIG. 1, a tapered cylindrical laminate in which the orientation angle a of the base fiber 3 of the third outermost braided layer 2c is changed so that the rear end side is larger than the axial front end side. The body 2 can be molded. In the laminated body 2, the orientation angle a2 on the rear end side is larger than the orientation angle a1 on the front end side (a1 <a2).

ここで、積層体2の第1編組層2a、第2編組層2b、第3編組層2cの層厚と、基材繊維3の配向角度aとの関係は以下のとおりである。積層体2の横断面(軸心CLと直交する横断面)において、基材繊維3の配向角度aが小さくなる程、基材繊維3の断面積は小さくなる。そして、積層体2のその横断面位置での基材繊維3の配置数は、配向角度aに関わらず一定である。したがって、基材繊維3の配向角度aが小さい程、その横断面位置での基材繊維3の断面積の総和は小さくなるので、層厚の増大を抑制することができる。換言すると、基材繊維3の配向角度aを大きくする程、その横断面位置での基材繊維3の断面積の総和は大きくなるので、必然的に層厚は増大する。   Here, the relationship between the layer thickness of the 1st braided layer 2a, the 2nd braided layer 2b, and the 3rd braided layer 2c of the laminated body 2 and the orientation angle a of the base fiber 3 is as follows. In the cross section of the laminate 2 (cross section perpendicular to the axis CL), the cross-sectional area of the base fiber 3 decreases as the orientation angle a of the base fiber 3 decreases. And the arrangement | positioning number of the base fiber 3 in the cross-sectional position of the laminated body 2 is constant irrespective of the orientation angle a. Therefore, the smaller the orientation angle a of the base fiber 3 is, the smaller the sum of the cross-sectional areas of the base fiber 3 at the cross-sectional position is, so that an increase in the layer thickness can be suppressed. In other words, as the orientation angle “a” of the base fiber 3 is increased, the sum of the cross-sectional areas of the base fiber 3 at the cross-sectional position is increased, so that the layer thickness is inevitably increased.

本発明では、積層体2の先端側では後端側に比べて基材繊維3の配向角度aが小さくなっているので、積層体2の先端側の第3編組層2cでは、図3に例示するように層厚がtとなり、積層体2の後端側の第3編組層2cでは、図4に例示するように層厚tとなり、ほぼ同じ層厚になっている。   In the present invention, since the orientation angle a of the base fiber 3 is smaller on the front end side of the laminate 2 than on the rear end side, the third braided layer 2c on the front end side of the laminate 2 is illustrated in FIG. Thus, the layer thickness is t, and the third braided layer 2c on the rear end side of the laminate 2 has the layer thickness t as illustrated in FIG.

この積層体2を縦断面で見ると、図2に例示するように、第1編組層2a、第2編組層2bは、それぞれ基材繊維3の配向角度aを一定にしているので、層厚は後端側よりも先端側が大きくなっている。一方、第3編組層2cは、配向角度aを軸方向で徐々に変化させて後端側をより大きくしているので、軸方向位置による層厚の変化が小さく、ほぼ一定の層厚tになっている。   When this laminated body 2 is viewed in a longitudinal section, as illustrated in FIG. 2, the first braided layer 2 a and the second braided layer 2 b each have a constant orientation angle a of the base fiber 3. The tip side is larger than the rear end side. On the other hand, since the third braided layer 2c gradually changes the orientation angle a in the axial direction to increase the rear end side, the change in the layer thickness due to the axial position is small, and the layer thickness t is substantially constant. It has become.

成形した先細円筒状の積層体2は加熱して、基材繊維3に含浸させた樹脂材料を硬化させる。このようにして得られた硬化した積層体2は、その表面が編組された基材繊維3の影響によって凹凸になっている。   The formed tapered cylindrical laminate 2 is heated to cure the resin material impregnated in the base fiber 3. The cured laminate 2 obtained in this manner is uneven due to the influence of the base fiber 3 whose surface is braided.

そこで、次に、硬化させた積層体2は、第3編組層2cを実質的にすべて除去するように、図6に例示する研磨装置8によってその表面を研磨する。この研磨装置8は、回転軸を平行にして対向する一対の研磨体8a、8aを有している。この回転する一対の円筒状の研磨体8a、8aの間に積層体2を通過させることにより、その表面全体を一定厚さ研磨する。   Therefore, next, the surface of the cured laminate 2 is polished by the polishing apparatus 8 illustrated in FIG. 6 so as to remove substantially all of the third braided layer 2c. The polishing apparatus 8 has a pair of polishing bodies 8a and 8a facing each other with the rotation axis in parallel. By passing the laminate 2 between the rotating pair of cylindrical polishing bodies 8a, 8a, the entire surface is polished to a certain thickness.

上述したように、この積層体2の研磨対象となる第3編組層2cは層厚が軸方向位置に関わらず、ほぼ一定になっているので、回転する研磨体8a、8aの間を通過させて表面を一定厚さ研磨すると、第3編組層2cの研磨残りがなく、或いは、研磨残りの厚さのばらつきを小さくすることができる。したがって、追加的に大幅な研磨作業を行なう必要がなくなり生産性の向上に寄与する。尚、この研磨装置8による研磨の後に、微調整の研磨等を行なって積層体2の表面を最終的に滑らかに仕上げる。   As described above, since the layer thickness of the third braided layer 2c to be polished of the laminate 2 is substantially constant regardless of the axial position, the third braided layer 2c is passed between the rotating polishing bodies 8a and 8a. When the surface is polished to a certain thickness, there is no polishing residue of the third braided layer 2c, or the variation in the thickness of the polishing residue can be reduced. Therefore, it is not necessary to perform additional significant polishing work, which contributes to the improvement of productivity. After the polishing by the polishing apparatus 8, fine adjustment is performed to finally finish the surface of the laminate 2 smoothly.

その後、滑らかにした積層体2の表面に塗装を施して、図7に例示するような表面に塗料層4を有するシャフト1が完成する。このシャフト1では、硬化させた積層体2の最外周の第3編組層2cのみが実質的に除去されて、研磨残りがほぼない状態になっているので、製造したシャフト1の品質(性能)に悪影響が生じることがない。   Then, the surface of the smoothed laminate 2 is painted, and the shaft 1 having the paint layer 4 on the surface as illustrated in FIG. 7 is completed. In this shaft 1, only the outermost third braided layer 2c of the laminated body 2 is substantially removed and there is almost no polishing residue, so the quality (performance) of the manufactured shaft 1 Will not be adversely affected.

このように、本発明によれば、研磨対象となる第3編組層2cを設定どおり過不足なく研磨することが容易になり、硬化させた積層体2の表面を軸方向全長にわたって必要以上に研磨したり、必要以上に研磨残りが生じたりすることが回避できるので生産性と品質の向上を図ることができる。   Thus, according to the present invention, it becomes easy to polish the third braided layer 2c to be polished without excess or deficiency as set, and the surface of the cured laminate 2 is polished more than necessary over the entire axial length. Therefore, it is possible to avoid the occurrence of polishing residue more than necessary, so that productivity and quality can be improved.

研磨対象となる第3編組層2cを過不足なく研磨し易くするために、第3編組層2cの最大層厚と最小層厚との差は、できるだけ小さくすることが好ましく、0.1mm以下、特に好ましくは0.05mm以下にする。   In order to easily polish the third braided layer 2c to be polished without excess or deficiency, the difference between the maximum layer thickness and the minimum layer thickness of the third braided layer 2c is preferably as small as possible, 0.1 mm or less, Particularly preferably, it is 0.05 mm or less.

また、基材繊維3の配向角度aを変化させる範囲は、例えば、10°〜70°程度、或いは20°〜60°程度にする。配向角度aは一様に変化させるだけでなく、なるべく第3編組層2cの層厚を均一にするように、成形する積層体2のテーパ具合(軸方向での外径の変化具合)に応じて変化させるとよい。   The range in which the orientation angle a of the base fiber 3 is changed is, for example, about 10 ° to 70 °, or about 20 ° to 60 °. The orientation angle “a” is not only changed uniformly, but also according to the taper degree (change degree of the outer diameter in the axial direction) of the laminate 2 to be molded so as to make the layer thickness of the third braided layer 2c as uniform as possible. To change.

基材繊維3の配向角度aを変化させるのは、研磨対象となる編組層であればよく、具体的には、少なくとも最外周の第3編組層2cであればよいが、その他の編組層2a、2bの基材繊維3の配向角度aを同様に変化させてもよい。   The orientation angle a of the base fiber 3 may be changed in the braided layer to be polished, specifically, at least the third outermost braided layer 2c, but the other braided layer 2a. The orientation angle a of the base fiber 3 of 2b may be changed similarly.

上記実施形態では、第1編組層2a、第2編組層2b、第3編組層2cの3層を積層して積層体2を形成しているが、要求性能等に応じて適切な積層数が設定される。例えば、編組層を4、5、6層程度積層することもできる。編組層を5層積層して積層体2を形成した場合には、少なくとも最外周の第5編組層を研磨対象とする。また、それぞれの編組層における基材繊維3の本数についても適切な本数が設定される。   In the above embodiment, the laminated body 2 is formed by laminating three layers of the first braided layer 2a, the second braided layer 2b, and the third braided layer 2c. Is set. For example, about 4, 5, or 6 braided layers can be laminated. When the laminated body 2 is formed by laminating five braided layers, at least the outermost fifth braided layer is an object to be polished. Moreover, an appropriate number is set also about the number of the base fiber 3 in each braided layer.

本発明によって形成した先細円筒状の積層体を例示する平面図である。It is a top view which illustrates the tapered cylindrical laminated body formed by this invention. 図1のA−A断面図である。It is AA sectional drawing of FIG. 第3編組層の基材繊維の状態を模式的に示す図2のB−B半断面図である。It is a BB half sectional view of Drawing 2 showing the state of the substrate fiber of the 3rd braiding layer typically. 第3編組層の基材繊維の状態を模式的に示す図2のC−C半断面図である。It is CC sectional view taken on the line in FIG. 2 schematically showing the state of the base fiber of the third braided layer. 基材繊維を編組する工程を例示する説明図である。It is explanatory drawing which illustrates the process of braiding a base fiber. 硬化させた積層体の表面を研磨する工程を例示する説明図である。It is explanatory drawing which illustrates the process of grind | polishing the surface of the laminated body hardened | cured. 図2の第3編組層を研磨した後、塗料層を形成して完成したシャフトを例示する縦断面図である。FIG. 3 is a longitudinal sectional view illustrating a shaft completed by forming a paint layer after polishing the third braided layer of FIG. 2. 基材繊維の配向角度を一定にして形成した先細円筒状の積層体を例示する平面図である。It is a top view which illustrates the tapered cylindrical laminated body formed by making the orientation angle of a base fiber constant. 図8のD−D断面図である。It is DD sectional drawing of FIG. 第3編組層の基材繊維の状態を模式的に示す図9のE−E半断面図である。FIG. 10 is a half cross-sectional view taken along the line E-E in FIG. 9 schematically showing the state of the base fiber of the third braided layer. 第3編組層の基材繊維の状態を模式的に示す図9のF−F半断面図である。FIG. 10 is a FF half cross-sectional view of FIG. 9 schematically showing the state of the base fiber of the third braided layer.

符号の説明Explanation of symbols

1 シャフト
2 積層体
2a 第1編組層
2b 第2編組層
2c 第3編組層
3 基材繊維
4 塗料層
5 マンドレル
6 編組装置
6a 回転ベース
7 ボビン
8 研磨装置
8a 研磨体
DESCRIPTION OF SYMBOLS 1 Shaft 2 Laminated body 2a 1st braided layer 2b 2nd braided layer 2c 3rd braided layer 3 Base fiber 4 Paint layer 5 Mandrel 6 Braiding device 6a Rotating base 7 Bobbin 8 Polishing device 8a Polishing body

Claims (4)

樹脂材料を含浸させた基材繊維を、マンドレル外周上にマンドレル軸方向に対して所定の配向角度で編組することにより順次、先細円筒状の編組層を積層して先細円筒状の積層体を成形し、この積層体を加熱することにより基材繊維に含浸させた樹脂材料を硬化させ、次いで、硬化させた積層体の表面を研磨するゴルフクラブ用シャフトの製造方法において、前記積層した編組層のうち、少なくとも最外周の編組層を形成する際には、前記配向角度が軸方向先端側よりも後端側が大きくなるように変化させて基材繊維を編組するゴルフクラブ用シャフトの製造方法。   The base fiber impregnated with the resin material is braided on the outer periphery of the mandrel at a predetermined orientation angle with respect to the mandrel axial direction, and then a tapered cylindrical braided layer is laminated to form a tapered cylindrical laminate. In the method for manufacturing a golf club shaft, the resin material impregnated in the base fiber is cured by heating the laminate, and then the surface of the cured laminate is polished. Of these, when forming at least the outermost braided layer, the golf club shaft is produced by braiding the base fiber by changing the orientation angle so that the rear end side is larger than the front end side in the axial direction. 前記配向角度を変化させて形成した編組層の最大層厚と最小層厚との差を0.1mm以下にする請求項1に記載のゴルフクラブ用シャフトの製造方法。   The golf club shaft manufacturing method according to claim 1, wherein a difference between the maximum layer thickness and the minimum layer thickness of the braided layer formed by changing the orientation angle is 0.1 mm or less. 前記配向角度を変化させる範囲を10°〜70°にする請求項1または2に記載のゴルフクラブ用シャフトの製造方法。   The golf club shaft manufacturing method according to claim 1, wherein a range in which the orientation angle is changed is set to 10 ° to 70 °. 前記硬化させた積層体を、回転する研磨体の間を通過させることにより、表面を一定厚さ研磨する請求項1〜3のいずれかに記載のゴルフクラブ用シャフトの製造方法。   The method for producing a shaft for a golf club according to any one of claims 1 to 3, wherein the cured laminate is passed through a rotating abrasive body to polish the surface to a certain thickness.
JP2008316431A 2008-12-12 2008-12-12 Manufacturing method of shaft for golf club Expired - Fee Related JP5287200B2 (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101420832B1 (en) 2014-02-20 2014-07-17 최용현 The manufacturing methods of a pole which is using a braiding method
JP2014161429A (en) * 2013-02-22 2014-09-08 明 ▲吉▼田 Fiber-reinforced plastic shaft

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0288088A (en) * 1988-09-26 1990-03-28 Ryobi Ltd Golf shaft and manufacture thereof
JPH0524068U (en) * 1991-09-20 1993-03-30 日立化成工業株式会社 Shaft for golf club
JPH0737231U (en) * 1993-12-24 1995-07-11 日立化成工業株式会社 Golf club shaft
JPH09277389A (en) * 1996-04-19 1997-10-28 Nippon Oil Co Ltd Tapered hollow shaft
JP2002177424A (en) * 2000-12-18 2002-06-25 Mizuno Corp Shaft for golf club
JP2002291951A (en) * 2001-01-23 2002-10-08 Nippon Shaft Co Ltd Shaft for golf club
JP2003275355A (en) * 2002-03-26 2003-09-30 Mizuno Corp Golf shaft
JP2004057731A (en) * 2002-07-31 2004-02-26 Mizuno Corp Golf club shaft made of fiber reinforced plastic
JP2005131838A (en) * 2003-10-28 2005-05-26 Sumitomo Rubber Ind Ltd Tubular body and its manufacturing method
JP2005270343A (en) * 2004-03-24 2005-10-06 Sumitomo Rubber Ind Ltd Golf club shaft and manufacturing method thereof
JP2008295940A (en) * 2007-06-04 2008-12-11 Mrc Composite Products Co Ltd Manufacturing method of golf club shaft and golf club shaft

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0288088A (en) * 1988-09-26 1990-03-28 Ryobi Ltd Golf shaft and manufacture thereof
JPH0524068U (en) * 1991-09-20 1993-03-30 日立化成工業株式会社 Shaft for golf club
JPH0737231U (en) * 1993-12-24 1995-07-11 日立化成工業株式会社 Golf club shaft
JPH09277389A (en) * 1996-04-19 1997-10-28 Nippon Oil Co Ltd Tapered hollow shaft
JP2002177424A (en) * 2000-12-18 2002-06-25 Mizuno Corp Shaft for golf club
JP2002291951A (en) * 2001-01-23 2002-10-08 Nippon Shaft Co Ltd Shaft for golf club
JP2003275355A (en) * 2002-03-26 2003-09-30 Mizuno Corp Golf shaft
JP2004057731A (en) * 2002-07-31 2004-02-26 Mizuno Corp Golf club shaft made of fiber reinforced plastic
JP2005131838A (en) * 2003-10-28 2005-05-26 Sumitomo Rubber Ind Ltd Tubular body and its manufacturing method
JP2005270343A (en) * 2004-03-24 2005-10-06 Sumitomo Rubber Ind Ltd Golf club shaft and manufacturing method thereof
JP2008295940A (en) * 2007-06-04 2008-12-11 Mrc Composite Products Co Ltd Manufacturing method of golf club shaft and golf club shaft

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2014161429A (en) * 2013-02-22 2014-09-08 明 ▲吉▼田 Fiber-reinforced plastic shaft
KR101420832B1 (en) 2014-02-20 2014-07-17 최용현 The manufacturing methods of a pole which is using a braiding method
WO2015126063A1 (en) * 2014-02-20 2015-08-27 최용현 Method for manufacturing pole using braiding method

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