WO2022172706A1 - Shuttlecock - Google Patents

Shuttlecock Download PDF

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Publication number
WO2022172706A1
WO2022172706A1 PCT/JP2022/001740 JP2022001740W WO2022172706A1 WO 2022172706 A1 WO2022172706 A1 WO 2022172706A1 JP 2022001740 W JP2022001740 W JP 2022001740W WO 2022172706 A1 WO2022172706 A1 WO 2022172706A1
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Prior art keywords
shuttlecock
forming
base portion
lattice structure
forming portion
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PCT/JP2022/001740
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French (fr)
Japanese (ja)
Inventor
健一 中谷
謙介 田中
Original Assignee
ヨネックス株式会社
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Application filed by ヨネックス株式会社 filed Critical ヨネックス株式会社
Priority to CN202280013243.1A priority Critical patent/CN116801957A/en
Publication of WO2022172706A1 publication Critical patent/WO2022172706A1/en

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    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63BAPPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B67/00Sporting games or accessories therefor, not provided for in groups A63B1/00 - A63B65/00
    • A63B67/18Badminton or similar games with feathered missiles
    • A63B67/183Feathered missiles
    • A63B67/187Shuttlecocks

Definitions

  • the present invention relates to a shuttlecock hit by a sports racket.
  • shuttlecocks for badminton have been known in which wings (hereinafter also referred to as skirts) made of natural feathers or artificial feathers made of resin are provided on a generally hemispherical base (see Patent Document 1). ).
  • the base portion is formed by using natural cork, cork formed by solidifying cork particles, or by molding with synthetic resin.
  • a shuttlecock of one aspect of the present invention is a shuttlecock provided with a base portion that holds a skirt portion, wherein the base portion includes a holding portion that forms an area that holds the skirt portion and an area that is hit by a racket. and a core forming portion forming an inner region from the outer forming portion, wherein at least a part of the core forming portion is configured with a three-dimensional lattice structure. .
  • a three-dimensional lattice structure can secure a large space in which only air exists in the core forming portion of the base portion, and the amount of deformation of the base portion itself can be increased to lengthen the time required for deformation of the base portion. can do.
  • the impact at that time can be mitigated.
  • the shuttlecock is made heavier than the conventional shuttlecock in order to prevent the flight trajectory from being changed due to the influence of the wind outdoors, etc., the impact can be reduced.
  • FIG. 1 is a schematic perspective view of a shuttlecock according to an embodiment
  • FIG. It is a front view of the said shuttlecock.
  • 4 is an enlarged plan view of the base portion of the shuttlecock;
  • FIG. 4 is a cross-sectional view along AA in FIG. 3;
  • It is a schematic perspective view of the base part in the shuttlecock which concerns on a modification.
  • FIG. 11 is a schematic perspective view of a base portion of a shuttlecock according to another modified example;
  • FIG. 1 is a schematic perspective view of a shuttlecock according to an embodiment.
  • FIG. 2 is a front view of the shuttlecock.
  • FIG. 3 is an enlarged plan view of the base portion of the shuttlecock.
  • the shuttlecock 1 includes a base portion 2 and a skirt portion 4 (not shown in FIG. 3) held by the base portion 2. As shown in FIG. The shuttlecock 1 flies by being hit by a racket (not shown) for racket sports such as badminton.
  • racket for racket sports such as badminton.
  • the side of the shuttlecock 1 on which the base portion 2 is provided is the front side, and the opposite side (skirt portion 4 side) is the rear side.
  • the base portion 2 has an outer forming portion 21 that is arranged along the outer peripheral surface of the base portion 2 and forms an area that is hit by the racket.
  • the outer forming portion 21 has a region along a hemispherical curved surface on the front side and a region along a cylindrical curved surface connected to the curved surface on the rear side.
  • the base portion 2 also includes a core forming portion 22 that forms a thick portion (core portion) of the base portion 2 that is an inner region of the outer forming portion 21 .
  • the base portion 2 is made of a synthetic resin that can be elastically deformed by hitting with a racket. A specific configuration of the base portion 2 including the outer forming portion 21 and the core forming portion 22 will be described later.
  • the skirt portion 4 is provided on the rear side of the base portion 2 and is formed of an integrally molded product made of synthetic resin (for example, nylon resin).
  • synthetic resin for example, nylon resin
  • the skirt portion 4 shown in the figure is just an example, and various configurations can be adopted as long as it is playable, such as being configured with natural feathers or resin artificial feathers, or using synthetic resin in a form different from the configuration shown in the figure. can.
  • a plurality of skirt portions 4 are provided so as to be arranged in an annular shape at the rear end of the base portion 2 . and a grid portion 42 provided in the rear region. Adjacent rachis 41 are connected to each other by the lattice portion 42 .
  • FIG. 4 is a cross-sectional view along AA in FIG. 3.
  • the base portion 2 has a holding portion 24 serving as an inner forming portion that forms a region for holding the skirt portion 4 therein.
  • the holding portion 24 has a shape in which the rear portion of the base portion 2 is recessed forward, and is provided so as to be fitted to the front end side of the skirt portion 4 to maintain the connection state with the skirt portion 4 .
  • the holding portion 24 has a base portion 26 to which the rear ends of the outer forming portion 21 and the core forming portion 22 are connected, and an opening 26a formed in the center of the base portion 26. It is provided with the 1st accommodating part 27 along.
  • the holding portion 24 also includes a second housing portion 28 that is formed in a dome shape so as to cover the front of the first housing portion 27 , and the diameter of the rear end side of the second housing portion 28 is the same as that of the first housing portion 27 . is formed larger than the inner diameter of the A stepped portion is formed at the front end of the first housing portion 27 so that a later-described hook portion 45 of the skirt portion 4 is fitted.
  • the skirt portion 4 further includes fitting portions 43 provided in front of the plurality of rachis 41 .
  • the fitting portion 43 includes a columnar insertion portion 44 extending forward from the front ends of the plurality of rachis 41 and a hook portion 45 formed in a flange shape having a larger diameter than the insertion portion 44 at the front end of the insertion portion 44 .
  • all of the outer forming portion 21 and all of the core forming portion 22 are configured with a three-dimensional lattice structure. Further, all of the first accommodating portions 27 and all of the second accommodating portions 28 of the holding portion 24 in the base portion 2 are also configured with a three-dimensional lattice structure.
  • the three-dimensional lattice structure of the present embodiment is configured by three-dimensionally connecting a plurality of strips 31 to form a three-dimensional mesh. More specifically, in order to construct the three-dimensional lattice structure, the outer forming portion 21 is formed by connecting a plurality of strips 31 to form a substantially triangular peripheral opening 32 (see FIGS. 1 and 3) as a base. A single layer structure is formed by arranging a plurality of them along the outer peripheral surface of the portion 2 .
  • the outer peripheral opening 32 is formed in a substantially equilateral triangular shape in the region along the curved hemispherical surface on the front side, and in a substantially right isosceles triangular shape in the region along the cylindrical curved surface on the rear side. formed (see FIG. 2).
  • the holding portion 24 has a single layer structure that is generally parallel to the outer forming portion 21 inside the outer forming portion 21 .
  • the holding portion 24 forms substantially triangular inner peripheral openings 34 side by side by connecting a plurality of strips 31 .
  • 4 is a cross-sectional view at a position where the strip 31 extends linearly in the front-rear direction in the first housing portion 27 of the holding portion 27, and the inner peripheral opening 34 appears at the cross-sectional position.
  • An inner peripheral opening 34 is formed in the first accommodating portion 27 only by not opening.
  • the core forming portion 22 has a single layered portion 35 formed between the outer forming portion 21 and the holding portion 24 so as to form a three-dimensional lattice structure of the base portion 2 .
  • the layered portion 35 is spaced apart from both the outer forming portion 21 and the holding portion 24 by a predetermined distance and is arranged substantially parallel thereto.
  • the core forming portion 22 also includes a plurality of connecting portions 36 made up of strips 31 that connect the layered portion 35 and the outer forming portion 21 or connect the layered portion 35 and the holding portion 24 .
  • a plurality of connecting portions 36 position the layered portion 35 between the outer forming portion 21 and the retaining portion 24 .
  • the layered portion 35 is formed by connecting a plurality of strips 31 in the same manner as the outer forming portion 21 and the holding portion 24 .
  • a plurality of substantially triangular internal openings 37 are formed in the layered portion 35 in the same manner as the outer peripheral opening 32 and the inner peripheral opening 34 .
  • the core forming portion 22 also has a plurality of inner openings 38 surrounded by the connecting portion 36 and the strips 31 forming the outer forming portion 21 , the retaining portion 24 and the layered portion 35 .
  • the openings 32, 34, 37, and 38 described above form a single ventilating region in the base portion 2, including the outer forming portion 21 and the core forming portion 22, which are connected to each other without being independent of each other.
  • a single ventilation region is formed in adjacent openings 32 , 34 , 37 , 38 in such a manner that the spaces passing through and straddling the respective openings 32 , 34 , 37 , 38 are connected.
  • the outer peripheral opening 32 allows ventilation inside and outside the base portion 2 , and the air passing through the outer peripheral opening 32 also flows through the inner openings 37 and 38 .
  • the base portion 2 is configured to have a three-dimensional lattice structure as described above, a large space is secured in the core forming portion 22 in which the strips 31 do not exist and only air exists. be able to.
  • the deformation of the base portion 2 itself can be increased by securing the space in the base portion 2, and the time required for the deformation can be extended. can do.
  • the impact can be absorbed and mitigated by the deformation of the three-dimensional lattice structure.
  • the strip 31 is made of the same specific gravity as the cork or foamed resin that constitutes the base of the conventional shuttlecock, the strip 31 has a higher density than the conventional base made of cork or foamed resin.
  • the specific gravity of the base portion 2 is smaller, and the weight of the base portion 2 is also smaller. Therefore, in order to reduce the influence of the wind during play, it is necessary to increase the weight of the shuttlecock 1 of this embodiment.
  • the weight of the shuttlecock 1 is increased.
  • the weight of the shuttlecock 1 is increased.
  • the shuttlecock 1 may be made lighter than the conventional shuttlecock by not adopting a configuration that increases the weight of the shuttlecock 1 .
  • each opening 32, 34, 37, 38 is preferably 1 mm or more, and the thickness of each strip 31 is 0.5 mm or more at the thinnest point. preferably.
  • the three-dimensional lattice structure of the base portion 2 forms a single ventilation area in the base portion 2, so that air can flow inside and outside the base portion 2 through each of the openings 32, 34, 37, 38 when the shuttlecock 1 is in flight. becomes easier to flow. As a result, even if the wind is blowing outdoors, the wind passes through the base portion 2, which also suppresses changes in the flight trajectory, making it easier to enjoy the game.
  • the base portion 2 has a multi-layered three-dimensional lattice structure composed of the outer forming portion 21, the holding portion 24, and the layered portion 35 of the core forming portion 22. Therefore, the racket can be deformed to absorb shock while realizing deformation. It can demonstrate the rigidity and durability that can withstand the impact of . Furthermore, it is possible to adopt a design that can exhibit good repulsion against the ball-striking surface of the racket when the shuttlecock 1 is hit.
  • the base part 2 has been described as having a three-dimensional lattice structure in which all of the outer forming part 21 and all of the core forming part 22 have a three-dimensional lattice structure, it is not limited to this.
  • the present invention can adopt various configurations as long as at least part of the core forming portion 22 has a three-dimensional lattice structure.
  • a configuration in which the predetermined thickness region surrounding the holding portion 24, which is a partial region of the core forming portion 22, is solidly formed with a constant thickness instead of a three-dimensional lattice structure can be cited.
  • the layered portions 35 of the outer forming portion 21, the holding portion 24, and the core forming portion 22 (hereinafter referred to as the outer forming portion 21, etc.), which constitute a multi-layered three-dimensional lattice structure, are formed by a plurality of strips 31 and each opening 32. , 34, 37.
  • the outer forming portion 21 and the like may be formed of a layered body having a constant thickness, and a plurality of holes may be arranged in the layered body to form the respective openings 32, 34, and 37.
  • the holding part 24 may be formed in layers having a predetermined thickness without forming the internal opening 37 instead of the three-dimensional lattice structure.
  • the holding portion 24 is composed only of the base portion 26, and the skirt portion 4 is fixed to the base portion 26 by adhesion or the like.
  • the holding portion 24 may be formed with a region for holding the skirt portion 4.
  • the holding portion 24 may be configured to have a small hole formed in a visible state, and the skirt portion 4 may be provided with a pin that can be inserted into the hole and fixed. good too.
  • the shapes of the openings 32, 34, and 37 can adopt various shapes such as a polygonal shape other than a triangular shape, a circular shape, an elliptical shape, or a polygonal shape with partially curved sides.
  • a polygonal shape other than a triangular shape a circular shape, an elliptical shape, or a polygonal shape with partially curved sides.
  • FIGS. 5 and 6 the configuration of the base portion 2 shown in FIGS. 5 and 6 can be mentioned.
  • FIG. 5 is a schematic perspective view of a base portion of a shuttlecock according to a modification.
  • FIG. 6 is a schematic perspective view of a base portion of a shuttlecock according to another modification.
  • the base portion 2 of the modified example of FIG. 5 has a configuration in which the outer peripheral opening 32 is mainly formed in a hexagonal shape, and other polygonal outer peripheral openings 32 such as pentagons are mixed depending on the location.
  • the base portion 2 of the modified example of FIG. 6 is configured such that the outer peripheral opening 32 is mainly formed in a hexagonal or rhombic shape, and other polygonal outer peripheral openings 32 such as pentagons are mixed depending on the location.
  • the present invention relates to a shuttlecock that can reduce the impact of the wind on play and reduce the impact when it hits a player or a racket in flight.

Abstract

Provided is a shuttlecock that is capable of mitigating impact when caused to fly and collide with a player or racket, while suppressing the effect of wind on the play. The shuttlecock (1) comprises a base section (2) that holds a skirt section (4). The base section comprises: a holding part (24) forming an area that holds the skirt section; an outer forming part (21) forming an area to be hit by a racket; and a core forming part (22) forming an area more inward than the outer forming part. At least a portion of the core forming part is configured by a three-dimensional lattice structure.

Description

シャトルコックshuttlecock
 本発明は、スポーツ用のラケットにて打撃されるシャトルコックに関する。 The present invention relates to a shuttlecock hit by a sports racket.
 従来、バドミントン用のシャトルコックとして、概ね半球状のベース部に天然羽毛や樹脂製の人工羽根からなる翼部(以下、スカート部ともいう)を設けたものが知られている(特許文献1参照)。ベース部は、天然のコルクや、コルク粒子を固めて形成したコルクを用いたり、合成樹脂によって成形したりすることで形成されている。 BACKGROUND ART Conventionally, shuttlecocks for badminton have been known in which wings (hereinafter also referred to as skirts) made of natural feathers or artificial feathers made of resin are provided on a generally hemispherical base (see Patent Document 1). ). The base portion is formed by using natural cork, cork formed by solidifying cork particles, or by molding with synthetic resin.
特開2010-200890号公報Japanese Patent Application Laid-Open No. 2010-200890
 バドミントンにあっては、屋内だけでなく屋外でもプレーを楽しみたいとのニーズがある。しかし、屋外でのバドミントンのプレーは、風の影響によってシャトルコックの飛行軌道が変化し易くなり、風の強さによってはプレーを楽しみ難くなる、という問題がある。 In badminton, there is a need to enjoy playing outdoors as well as indoors. However, when playing badminton outdoors, there is a problem that the flight trajectory of the shuttlecock is likely to change due to the influence of the wind, making it difficult to enjoy playing depending on the strength of the wind.
 かかる問題を解消するため、シャトルコックを高重量化することを検討したが、飛行したシャトルコックがプレーヤやラケットに衝突すると衝撃が大きくなる、という問題が発生する。このように、シャトルコックでの風による影響の低減作用と、衝突時の衝撃抑制作用とはトレードオフの関係となるが、本発明者は鋭意検討を行うことで、それら2つの作用両方を同時に得ることができる発明を案出したものである。 In order to solve this problem, we considered increasing the weight of the shuttlecock, but the problem arises that when the shuttlecock in flight collides with the player or the racket, the impact will increase. In this way, there is a trade-off relationship between the effect of reducing the effect of the wind on the shuttlecock and the effect of suppressing the impact at the time of collision. I have devised an invention that can be obtained.
 本発明は、かかる点に鑑みてなされたものであり、風によるプレーへの影響を抑制しつつ飛行してプレーヤやラケットに衝突した際の衝撃を緩和することができるシャトルコックを提供することを目的とする。 SUMMARY OF THE INVENTION It is an object of the present invention to provide a shuttlecock capable of suppressing the influence of wind on play and mitigating the impact when it hits a player or a racket in flight. aim.
 本発明における一態様のシャトルコックは、スカート部を保持するベース部を備えたシャトルコックにおいて、前記ベース部は、前記スカート部を保持する領域を形成する保持部と、ラケットによって打撃される領域を形成する外側形成部と、前記外側形成部より内方領域を形成する芯形成部とを備え、前記芯形成部の少なくとも一部は、立体的な格子構造によって構成されていることを特徴とする。 A shuttlecock of one aspect of the present invention is a shuttlecock provided with a base portion that holds a skirt portion, wherein the base portion includes a holding portion that forms an area that holds the skirt portion and an area that is hit by a racket. and a core forming portion forming an inner region from the outer forming portion, wherein at least a part of the core forming portion is configured with a three-dimensional lattice structure. .
 本発明によれば、立体的な格子構造にてベース部の芯形成部に空気だけが存在する空間を大きく確保でき、ベース部自体の変形量増大を図ってベース部の変形に要する時間を長くすることができる。これにより、シャトルコックが飛行してベース部がプレーヤやラケットに衝突しても、その際の衝撃を緩和することができる。これにより、屋外等での風の影響によって飛行軌道を変化し難くすべく従来のシャトルコックより重くしても、衝撃緩和を図ることができる。このように、立体的な格子構造を採用することで、トレードオフの関係にある風による影響の低減作用と、衝突時の衝撃緩和作用とを同時に得ることができる。 According to the present invention, a three-dimensional lattice structure can secure a large space in which only air exists in the core forming portion of the base portion, and the amount of deformation of the base portion itself can be increased to lengthen the time required for deformation of the base portion. can do. As a result, even if the shuttlecock flies and the base portion collides with the player or the racket, the impact at that time can be mitigated. As a result, even if the shuttlecock is made heavier than the conventional shuttlecock in order to prevent the flight trajectory from being changed due to the influence of the wind outdoors, etc., the impact can be reduced. In this way, by adopting a three-dimensional lattice structure, it is possible to simultaneously obtain an effect of reducing the effect of the wind and an effect of mitigating the impact at the time of collision, which are in a trade-off relationship.
実施の形態に係るシャトルコックの概略斜視図である。1 is a schematic perspective view of a shuttlecock according to an embodiment; FIG. 前記シャトルコックの正面図である。It is a front view of the said shuttlecock. 前記シャトルコックのベース部の拡大平面図である。4 is an enlarged plan view of the base portion of the shuttlecock; FIG. 図3のA-Aに沿う断面図である。FIG. 4 is a cross-sectional view along AA in FIG. 3; 変形例に係るシャトルコックにおけるベース部の概略斜視図である。It is a schematic perspective view of the base part in the shuttlecock which concerns on a modification. 他の変形例に係るシャトルコックにおけるベース部の概略斜視図である。FIG. 11 is a schematic perspective view of a base portion of a shuttlecock according to another modified example;
 以下、本発明の実施の形態について図面を参照しながら具体的に説明する。図1は、実施の形態に係るシャトルコックの概略斜視図である。図2は、前記シャトルコックの正面図である。図3は、前記シャトルコックのベース部の拡大平面図である。 Hereinafter, embodiments of the present invention will be specifically described with reference to the drawings. FIG. 1 is a schematic perspective view of a shuttlecock according to an embodiment. FIG. 2 is a front view of the shuttlecock. FIG. 3 is an enlarged plan view of the base portion of the shuttlecock.
 図1から図3に示すように、シャトルコック1は、ベース部2と、ベース部2に保持されるスカート部4(図3では不図示)とを備えている。シャトルコック1は、バドミントン等のラケットスポーツのラケット(不図示)によって打撃されることで飛行される。以下の説明において、シャトルコック1のうちベース部2が設けられた側を前側とし、その反対側(スカート部4の側)を後側とする。 As shown in FIGS. 1 to 3, the shuttlecock 1 includes a base portion 2 and a skirt portion 4 (not shown in FIG. 3) held by the base portion 2. As shown in FIG. The shuttlecock 1 flies by being hit by a racket (not shown) for racket sports such as badminton. In the following description, the side of the shuttlecock 1 on which the base portion 2 is provided is the front side, and the opposite side (skirt portion 4 side) is the rear side.
 ベース部2は、該ベース部2の外周面に沿って配設されてラケットによって打撃される領域を形成する外側形成部21を備えている。外側形成部21は、前側に半球状の曲面に沿う領域と、後側に該曲面に連なる円柱状の曲面に沿う領域とを有している。また、ベース部2は、外側形成部21より内方領域となるベース部2の肉厚部分(芯部分)を形成する芯形成部22とを備えている。ベース部2は、ラケットの打撃によって弾性変形可能な合成樹脂によって構成されている。外側形成部21及び芯形成部22を含むベース部2の具体的な構成については後述する。 The base portion 2 has an outer forming portion 21 that is arranged along the outer peripheral surface of the base portion 2 and forms an area that is hit by the racket. The outer forming portion 21 has a region along a hemispherical curved surface on the front side and a region along a cylindrical curved surface connected to the curved surface on the rear side. The base portion 2 also includes a core forming portion 22 that forms a thick portion (core portion) of the base portion 2 that is an inner region of the outer forming portion 21 . The base portion 2 is made of a synthetic resin that can be elastically deformed by hitting with a racket. A specific configuration of the base portion 2 including the outer forming portion 21 and the core forming portion 22 will be described later.
 スカート部4は、ベース部2の後側に設けられており、合成樹脂(例えばナイロン樹脂)による一体成形品によって形成されている。なお、図示のスカート部4は一例であり、天然羽毛や樹脂製の人工羽根によって構成したり、合成樹脂にて図示した構成とは異なる形態にしたりする等、プレーできる限りにおいて種々の構成を採用できる。 The skirt portion 4 is provided on the rear side of the base portion 2 and is formed of an integrally molded product made of synthetic resin (for example, nylon resin). The skirt portion 4 shown in the figure is just an example, and various configurations can be adopted as long as it is playable, such as being configured with natural feathers or resin artificial feathers, or using synthetic resin in a form different from the configuration shown in the figure. can.
 スカート部4は、本実施の形態では、ベース部2の後端にて円環状に並ぶように複数設けられ、ベース部2から離れるにつれて互いの間隔が広くなる羽軸41と、羽軸41の後方領域に設けられる格子部42とを備えている。格子部42によって、隣接する羽軸41同士が繋がるようになっている。 In the present embodiment, a plurality of skirt portions 4 are provided so as to be arranged in an annular shape at the rear end of the base portion 2 . and a grid portion 42 provided in the rear region. Adjacent rachis 41 are connected to each other by the lattice portion 42 .
 続いて、ベース部2の具体的構成と、ベース部2及びスカート部4の連結部分の具体的な構成について、図4を加えて説明する。図4は、図3のA-Aに沿う断面図である。図4にも示すように、ベース部2は、その内側にスカート部4を保持する領域を形成する内側形成部となる保持部24を備えている。保持部24は、ベース部2の後部を前方に陥没させた形状を備え、スカート部4の前端側と嵌合してスカート部4との接続状態を維持可能に設けられている。 Next, the specific configuration of the base portion 2 and the specific configuration of the connection portion between the base portion 2 and the skirt portion 4 will be described with reference to FIG. 4 is a cross-sectional view along AA in FIG. 3. FIG. As also shown in FIG. 4, the base portion 2 has a holding portion 24 serving as an inner forming portion that forms a region for holding the skirt portion 4 therein. The holding portion 24 has a shape in which the rear portion of the base portion 2 is recessed forward, and is provided so as to be fitted to the front end side of the skirt portion 4 to maintain the connection state with the skirt portion 4 .
 具体的には、保持部24は、外側形成部21及び芯形成部22の後端が連結される基部26と、基部26の中央に形成された開口26a周りから前方に向かう円筒内周形状に沿う第1収容部27とを備えている。また、保持部24は、第1収容部27の前方を覆うようにドーム状に形成された第2収容部28を備え、第2収容部28の後端側の径寸法は第1収容部27の内径より大きく形成されている。なお、第1収容部27の前端には、スカート部4の後述する引っ掛け部45が嵌り合う段部が形成される。 Specifically, the holding portion 24 has a base portion 26 to which the rear ends of the outer forming portion 21 and the core forming portion 22 are connected, and an opening 26a formed in the center of the base portion 26. It is provided with the 1st accommodating part 27 along. The holding portion 24 also includes a second housing portion 28 that is formed in a dome shape so as to cover the front of the first housing portion 27 , and the diameter of the rear end side of the second housing portion 28 is the same as that of the first housing portion 27 . is formed larger than the inner diameter of the A stepped portion is formed at the front end of the first housing portion 27 so that a later-described hook portion 45 of the skirt portion 4 is fitted.
 スカート部4は、複数の羽軸41の前方に設けられた嵌合部43を更に備えている。嵌合部43は、複数の羽軸41の前端から前方に延出する円柱状の挿入部44と、挿入部44の前端にて挿入部44より大径のフランジ状に形成される引っ掛け部45とを備えている。本実施の形態では、ベース部2にスカート部4を保持させる場合、保持部24及び嵌合部43の少なくとも一方を変形させつつ保持部24の内部に嵌合部43を押し込んで挿入する。そして、保持部24に嵌合部43を挿入した状態で、引っ掛け部45が第1収容部27の前端と嵌り合い、ベース部2にスカート部4が保持される。保持部24と嵌合部43との間には、必要に応じて接着剤等が設けられる。 The skirt portion 4 further includes fitting portions 43 provided in front of the plurality of rachis 41 . The fitting portion 43 includes a columnar insertion portion 44 extending forward from the front ends of the plurality of rachis 41 and a hook portion 45 formed in a flange shape having a larger diameter than the insertion portion 44 at the front end of the insertion portion 44 . and In the present embodiment, when the skirt portion 4 is held by the base portion 2 , at least one of the holding portion 24 and the fitting portion 43 is deformed and the fitting portion 43 is pushed into the holding portion 24 to be inserted. With the fitting portion 43 inserted into the holding portion 24 , the hook portion 45 is engaged with the front end of the first accommodating portion 27 , and the skirt portion 4 is held by the base portion 2 . An adhesive or the like is provided between the holding portion 24 and the fitting portion 43 as necessary.
 ベース部2にあっては、外側形成部21の全て及び芯形成部22の全てが立体的な格子構造によって構成されている。また、ベース部2における保持部24の第1収容部27の全て及び第2収容部28の全ても立体的な格子構造によって構成されている。 In the base portion 2, all of the outer forming portion 21 and all of the core forming portion 22 are configured with a three-dimensional lattice structure. Further, all of the first accommodating portions 27 and all of the second accommodating portions 28 of the holding portion 24 in the base portion 2 are also configured with a three-dimensional lattice structure.
 ここで、本実施の形態の立体的な格子構造は、複数のストリップ31を立体的に連結して構成され、立体的なメッシュ状に形成されている。より具体的に説明すると、該立体的な格子構造を構成すべく、外側形成部21は、複数のストリップ31を連結することで略三角形状の外周開口32(図1及び図3参照)をベース部2の外周面に沿って複数並べて形成した単一の層構造をなしている。外側形成部21にて、外周開口32は、前側の半球状の曲面に沿う領域にて概略正三角形状に形成され、後側の円柱状の曲面に沿う領域にて概略直角二等辺三角形状に形成される(図2参照)。 Here, the three-dimensional lattice structure of the present embodiment is configured by three-dimensionally connecting a plurality of strips 31 to form a three-dimensional mesh. More specifically, in order to construct the three-dimensional lattice structure, the outer forming portion 21 is formed by connecting a plurality of strips 31 to form a substantially triangular peripheral opening 32 (see FIGS. 1 and 3) as a base. A single layer structure is formed by arranging a plurality of them along the outer peripheral surface of the portion 2 . In the outer forming portion 21, the outer peripheral opening 32 is formed in a substantially equilateral triangular shape in the region along the curved hemispherical surface on the front side, and in a substantially right isosceles triangular shape in the region along the cylindrical curved surface on the rear side. formed (see FIG. 2).
 また、ベース部2の立体的な格子構造を構成すべく、保持部24は、外側形成部21より内側にて外側形成部21と概ね平行になる単一の層構造をなしている。また、保持部24は、複数のストリップ31を連結することで略三角形状の内周開口34を並べて形成している。なお、図4は、保持部27における第1収容部27にて、ストリップ31が前後方向に直線状に延出した位置にて断面視しており、断面視した位置で内周開口34が表れていないだけで第1収容部27に内周開口34が形成される。 In addition, in order to configure the three-dimensional lattice structure of the base portion 2 , the holding portion 24 has a single layer structure that is generally parallel to the outer forming portion 21 inside the outer forming portion 21 . In addition, the holding portion 24 forms substantially triangular inner peripheral openings 34 side by side by connecting a plurality of strips 31 . 4 is a cross-sectional view at a position where the strip 31 extends linearly in the front-rear direction in the first housing portion 27 of the holding portion 27, and the inner peripheral opening 34 appears at the cross-sectional position. An inner peripheral opening 34 is formed in the first accommodating portion 27 only by not opening.
 更に、ベース部2の立体的な格子構造を構成すべく、芯形成部22は、外側形成部21と保持部24との間に形成される単一の層状部35を備えている。言い換えると、層状部35は、外側形成部21及び保持部24の両方から所定間隔を隔て、それらと概ね平行に配設されている。また、芯形成部22は、層状部35と外側形成部21を連結したり層状部35と保持部24を連結したりするストリップ31からなる複数の接続部36を備えている。複数の接続部36によって、層状部35が外側形成部21と保持部24との間で位置決めされる。 Further, the core forming portion 22 has a single layered portion 35 formed between the outer forming portion 21 and the holding portion 24 so as to form a three-dimensional lattice structure of the base portion 2 . In other words, the layered portion 35 is spaced apart from both the outer forming portion 21 and the holding portion 24 by a predetermined distance and is arranged substantially parallel thereto. The core forming portion 22 also includes a plurality of connecting portions 36 made up of strips 31 that connect the layered portion 35 and the outer forming portion 21 or connect the layered portion 35 and the holding portion 24 . A plurality of connecting portions 36 position the layered portion 35 between the outer forming portion 21 and the retaining portion 24 .
 層状部35は、外側形成部21及び保持部24と同様に複数のストリップ31を連結して形成される。また、層状部35には、外周開口32及び内周開口34と同様に略三角形状の内部開口37が複数形成されている。また、芯形成部22においては、接続部36と、外側形成部21、保持部24及び層状部35を形成するストリップ31とによって囲われる内部開口38も複数形成される。 The layered portion 35 is formed by connecting a plurality of strips 31 in the same manner as the outer forming portion 21 and the holding portion 24 . A plurality of substantially triangular internal openings 37 are formed in the layered portion 35 in the same manner as the outer peripheral opening 32 and the inner peripheral opening 34 . The core forming portion 22 also has a plurality of inner openings 38 surrounded by the connecting portion 36 and the strips 31 forming the outer forming portion 21 , the retaining portion 24 and the layered portion 35 .
 上述した各開口32、34、37、38によって、外側形成部21及び芯形成部22を含むベース部2には、相互に独立せずに連なった状態となる単一の通気領域が形成される。単一の通気領域は、隣り合う開口32、34、37、38にて、それぞれの開口32、34、37、38を通過して跨ぐ空間が繋がった状態となって形成される。そして、外周開口32は、ベース部2の内外で通気することが可能となり、外周開口32を通過する空気は内部開口37、38にも流れるようになる。 The openings 32, 34, 37, and 38 described above form a single ventilating region in the base portion 2, including the outer forming portion 21 and the core forming portion 22, which are connected to each other without being independent of each other. . A single ventilation region is formed in adjacent openings 32 , 34 , 37 , 38 in such a manner that the spaces passing through and straddling the respective openings 32 , 34 , 37 , 38 are connected. The outer peripheral opening 32 allows ventilation inside and outside the base portion 2 , and the air passing through the outer peripheral opening 32 also flows through the inner openings 37 and 38 .
 このように本実施の形態では、上述のようにベース部2を立体的な格子構造により構成したので、芯形成部22にてストリップ31が存在せずに空気だけが存在する空間を大きく確保することができる。これにより、シャトルコック1が飛行してベース部2がプレーヤやラケットに衝突するときに、ベース部2に空間を確保した分、ベース部2自体の変形を大きくでき、該変形に掛かる時間を長くすることができる。この結果、ベース部2の衝突の際、立体的な格子構造の変形にて衝撃を吸収して緩和することができる。 As described above, in the present embodiment, since the base portion 2 is configured to have a three-dimensional lattice structure as described above, a large space is secured in the core forming portion 22 in which the strips 31 do not exist and only air exists. be able to. As a result, when the shuttlecock 1 flies and the base portion 2 collides with the player or the racket, the deformation of the base portion 2 itself can be increased by securing the space in the base portion 2, and the time required for the deformation can be extended. can do. As a result, when the base portion 2 collides, the impact can be absorbed and mitigated by the deformation of the three-dimensional lattice structure.
 また、立体的な格子構造における複数のストリップ31を用いることで、ベース部2に空気だけが存在する空間を大きく確保することが可能となる。これにより、従来のシャトルコックのベース部を構成するコルクや発泡樹脂と同じ比重の物をストリップ31に使った場合、従来のコルクや発泡樹脂を使用したベース部に比べて、本実施の形態の方がベース部2としての比重が小さくなり、ベース部2の重量も小さくなる。よって、プレー中の風の影響を減らすためには、本実施の形態のシャトルコック1にて重量を大きくする必要がある。このため、ストリップ31に従来のコルクや発泡樹脂より比重を大きくした素材を用いたり、ベース部2の任意の位置やストリップ31などに錘などの追加パーツをつけたり、スカート部4の厚みを厚くするなどして、シャトルコック1の重量を大きくする。このように重量を大きくすることで、屋外等での風によって飛行軌道を変化し難くしてプレーを楽しみ易くすることができる。以上のように、ベース部2に立体的な格子構造を採用することで、トレードオフの関係にある風による影響の低減作用と、上述した衝突時の衝撃緩和作用とを同時に得ることができる。なお、シャトルコック1に重量を大きくする構成を採用しないことで、従来のシャトルコックに比べて軽量化したシャトルコック1にしても良い。 Also, by using a plurality of strips 31 in a three-dimensional lattice structure, it is possible to secure a large space in which only air exists in the base portion 2 . As a result, when the strip 31 is made of the same specific gravity as the cork or foamed resin that constitutes the base of the conventional shuttlecock, the strip 31 has a higher density than the conventional base made of cork or foamed resin. The specific gravity of the base portion 2 is smaller, and the weight of the base portion 2 is also smaller. Therefore, in order to reduce the influence of the wind during play, it is necessary to increase the weight of the shuttlecock 1 of this embodiment. For this reason, a material having a higher specific gravity than conventional cork or foamed resin is used for the strip 31, an additional part such as a weight is attached to an arbitrary position of the base portion 2 or the strip 31, or the thickness of the skirt portion 4 is increased. For example, the weight of the shuttlecock 1 is increased. By increasing the weight in this way, it is possible to make it easier to enjoy playing by making it difficult for the flight trajectory to change due to the wind outdoors or the like. As described above, by adopting a three-dimensional lattice structure for the base portion 2, it is possible to simultaneously obtain the effect of reducing the effect of the wind, which is in a trade-off relationship, and the impact mitigating effect at the time of collision as described above. It should be noted that the shuttlecock 1 may be made lighter than the conventional shuttlecock by not adopting a configuration that increases the weight of the shuttlecock 1 .
 なお、特に限定されるものでないが、各開口32、34、37、38における最大幅としては1mm以上とすることが好ましく、それぞれのストリップ31の太さは、最も細い箇所で0.5mm以上とすることが好ましい。かかる数値範囲に設定することで、上述した風による影響の低減作用と、衝突時の衝撃緩和作用との両方をより良く発揮することができる。 Although not particularly limited, the maximum width of each opening 32, 34, 37, 38 is preferably 1 mm or more, and the thickness of each strip 31 is 0.5 mm or more at the thinnest point. preferably. By setting the value within such a numerical range, both the effect of reducing the effect of the wind and the effect of mitigating the impact at the time of collision can be exhibited better.
 更に、ベース部2の立体的な格子構造によってベース部2に単一の通気領域が形成されるので、シャトルコック1の飛行時に各開口32、34、37、38を通じてベース部2の内外で空気が流れ易くなる。これにより、屋外等で風が吹いていても、該風がベース部2を通過するようになり、これによっても飛行軌道の変化を抑制し、プレーをより楽しみ易くすることができる。 Furthermore, the three-dimensional lattice structure of the base portion 2 forms a single ventilation area in the base portion 2, so that air can flow inside and outside the base portion 2 through each of the openings 32, 34, 37, 38 when the shuttlecock 1 is in flight. becomes easier to flow. As a result, even if the wind is blowing outdoors, the wind passes through the base portion 2, which also suppresses changes in the flight trajectory, making it easier to enjoy the game.
 また、ベース部2は、外側形成部21と、保持部24と、芯形成部22の層状部35とによって多層な立体的な格子構造としたので、衝撃を吸収する変形を実現しつつ、ラケットの打撃に十分耐え得る剛性、耐久性を発揮できる。更には、シャトルコック1が打撃された際のラケットの打球面に対する反発性を良好に発揮できる設計を採用可能となる。 In addition, the base portion 2 has a multi-layered three-dimensional lattice structure composed of the outer forming portion 21, the holding portion 24, and the layered portion 35 of the core forming portion 22. Therefore, the racket can be deformed to absorb shock while realizing deformation. It can demonstrate the rigidity and durability that can withstand the impact of . Furthermore, it is possible to adopt a design that can exhibit good repulsion against the ball-striking surface of the racket when the shuttlecock 1 is hit.
 なお、本発明は上記実施の形態に限定されず、種々変更して実施することが可能である。上記実施の形態において、添付図面に図示されている大きさや形状、方向などについては、これに限定されず、本発明の効果を発揮する範囲内で適宜変更することが可能である。その他、本発明の目的の範囲を逸脱しない限りにおいて適宜変更して実施することが可能である。 It should be noted that the present invention is not limited to the above embodiments, and can be implemented with various modifications. In the above embodiments, the sizes, shapes, directions, etc. shown in the accompanying drawings are not limited to these, and can be changed as appropriate within the scope of exhibiting the effects of the present invention. In addition, it is possible to carry out by appropriately modifying the present invention as long as it does not deviate from the scope of the purpose of the present invention.
 ベース部2は、外側形成部21の全て及び芯形成部22の全てが立体的な格子構造となる構成を説明したが、これに限られるものでない。本発明は、芯形成部22の少なくとも一部が立体的な格子構造である限りにおいて、種々の構成を採用することができる。例としては、外側形成部21の全領域或いは一部領域となる平面視で半分領域が立体的な格子構造でなく一定の厚みの層状に形成される構成を挙げることができる。また、例として、芯形成部22の一部領域となる保持部24を囲う所定厚領域が立体的な格子構造でなく一定の厚みで中実に形成される構成も挙げることができる。 Although the base part 2 has been described as having a three-dimensional lattice structure in which all of the outer forming part 21 and all of the core forming part 22 have a three-dimensional lattice structure, it is not limited to this. The present invention can adopt various configurations as long as at least part of the core forming portion 22 has a three-dimensional lattice structure. As an example, it is possible to adopt a configuration in which a half region of the outer formation portion 21, which is the entire region or a partial region in a plan view, is formed in layers of a certain thickness instead of a three-dimensional lattice structure. Further, as an example, a configuration in which the predetermined thickness region surrounding the holding portion 24, which is a partial region of the core forming portion 22, is solidly formed with a constant thickness instead of a three-dimensional lattice structure can be cited.
 また、多層な立体的な格子構造を構成する外側形成部21、保持部24及び芯形成部22の層状部35(以下、外側形成部21等とする)は、複数のストリップ31で各開口32、34、37を形成することに限定されるものでない。例えば、外側形成部21等が一定の厚みの層状体により形成され、該層状体に複数の孔を並べて形成して各開口32、34、37としてもよい。 The layered portions 35 of the outer forming portion 21, the holding portion 24, and the core forming portion 22 (hereinafter referred to as the outer forming portion 21, etc.), which constitute a multi-layered three-dimensional lattice structure, are formed by a plurality of strips 31 and each opening 32. , 34, 37. For example, the outer forming portion 21 and the like may be formed of a layered body having a constant thickness, and a plurality of holes may be arranged in the layered body to form the respective openings 32, 34, and 37. FIG.
 更に、保持部24は、立体的な格子構造でなく、内部開口37を形成せずに所定の厚みを有する層状に形成してもよい。また、保持部24は、基部26だけの構成として該基部26に接着等によってスカート部4を固定し、各収容部27、28の形成領域を芯形成部22に変更して立体的な格子構造としてもよい。更に、保持部24は、スカート部4を保持する領域を形成すればよく、例えば、視認した状態で小さな穴を形成した構成とし、該穴に差し込んで固定可能なピンをスカート部4に設けてもよい。 Furthermore, the holding part 24 may be formed in layers having a predetermined thickness without forming the internal opening 37 instead of the three-dimensional lattice structure. In addition, the holding portion 24 is composed only of the base portion 26, and the skirt portion 4 is fixed to the base portion 26 by adhesion or the like. may be Further, the holding portion 24 may be formed with a region for holding the skirt portion 4. For example, the holding portion 24 may be configured to have a small hole formed in a visible state, and the skirt portion 4 may be provided with a pin that can be inserted into the hole and fixed. good too.
 また、各開口32、34、37の形状は、三角形以外の多角形状にしたり、円形や楕円形、一部の辺が湾曲した多角形状にする等、種々の形状を採用することができる。例を挙げると、図5及び図6に示すベース部2の構成を挙げることができる。図5は、変形例に係るシャトルコックにおけるベース部の概略斜視図である。図6は、他の変形例に係るシャトルコックにおけるベース部の概略斜視図である。 Also, the shapes of the openings 32, 34, and 37 can adopt various shapes such as a polygonal shape other than a triangular shape, a circular shape, an elliptical shape, or a polygonal shape with partially curved sides. For example, the configuration of the base portion 2 shown in FIGS. 5 and 6 can be mentioned. FIG. 5 is a schematic perspective view of a base portion of a shuttlecock according to a modification. FIG. 6 is a schematic perspective view of a base portion of a shuttlecock according to another modification.
 図5の変形例のベース部2は、外周開口32が主として六角形状に形成され、場所によって五角形等の他の多角形状の外周開口32が混在する構成となっている。図6の変形例のベース部2は、外周開口32が主として六角形状又は菱形状に形成され、場所によって五角形等の他の多角形状の外周開口32が混在する構成となっている。 The base portion 2 of the modified example of FIG. 5 has a configuration in which the outer peripheral opening 32 is mainly formed in a hexagonal shape, and other polygonal outer peripheral openings 32 such as pentagons are mixed depending on the location. The base portion 2 of the modified example of FIG. 6 is configured such that the outer peripheral opening 32 is mainly formed in a hexagonal or rhombic shape, and other polygonal outer peripheral openings 32 such as pentagons are mixed depending on the location.
 本発明は、風によるプレーへの影響を抑制しつつ飛行してプレーヤやラケットに衝突した際の衝撃を緩和することができるシャトルコックに関する。 The present invention relates to a shuttlecock that can reduce the impact of the wind on play and reduce the impact when it hits a player or a racket in flight.
 本出願は、2021年2月10日出願の特願2021-019785に基づく。この内容は、すべてここに含めておく。 This application is based on Japanese Patent Application No. 2021-019785 filed on February 10, 2021. All of this content is included here.

Claims (7)

  1.  スカート部を保持するベース部を備えたシャトルコックにおいて、
     前記ベース部は、前記スカート部を保持する領域を形成する保持部と、
     ラケットによって打撃される領域を形成する外側形成部と、
     前記外側形成部より内方領域を形成する芯形成部とを備え、
     前記芯形成部の少なくとも一部は、立体的な格子構造によって構成されていることを特徴とするシャトルコック。
    A shuttlecock having a base portion that holds a skirt portion,
    the base portion includes a holding portion forming a region for holding the skirt portion;
    an outer formation forming an area struck by the racquet;
    a core forming portion forming an inner region from the outer forming portion;
    A shuttlecock, wherein at least part of the core-forming portion has a three-dimensional lattice structure.
  2.  前記外側形成部の少なくとも一部は、立体的な格子構造によって構成されていることを特徴とする請求項1に記載のシャトルコック。 The shuttlecock according to claim 1, wherein at least part of the outer forming portion is configured with a three-dimensional lattice structure.
  3.  前記芯形成部の全て及び前記外側形成部の全てが立体的な格子構造によって構成されていることを特徴とする請求項2に記載のシャトルコック。 The shuttlecock according to claim 2, characterized in that all of said core forming parts and all of said outer forming parts are configured with a three-dimensional lattice structure.
  4.  前記立体的な格子構造は、複数のストリップを立体的に連結して前記芯形成部及び前記外側形成部に単一の通気領域を形成することを特徴とする請求項2に記載のシャトルコック。 The shuttlecock according to claim 2, wherein the three-dimensional lattice structure three-dimensionally connects a plurality of strips to form a single ventilation area in the core forming portion and the outer forming portion.
  5.  前記外側形成部は、前記ベース部の内外で通気可能な外周開口を備え、該外周開口は多角形状に形成されていることを特徴とする請求項2に記載のシャトルコック。 The shuttlecock according to claim 2, wherein the outer forming portion has an outer peripheral opening that allows air to pass through the inside and outside of the base portion, and the outer peripheral opening is formed in a polygonal shape.
  6.  前記芯形成部は、前記外側形成部と所定間隔を隔てて配設された層状部を備え、該層状部には通気可能な複数の内部開口が形成されていることを特徴とする請求項1に記載のシャトルコック。 2. The core-forming portion has a layered portion spaced apart from the outer forming portion by a predetermined distance, and the layered portion is formed with a plurality of ventilating internal openings. Shuttlecock described in .
  7.  前記ベース部は、前記ラケットの打撃によって弾性変形可能な合成樹脂によって構成されることを特徴とする請求項1に記載のシャトルコック。 The shuttlecock according to claim 1, wherein the base portion is made of a synthetic resin that is elastically deformable when hit by the racket.
PCT/JP2022/001740 2021-02-10 2022-01-19 Shuttlecock WO2022172706A1 (en)

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WO2023203991A1 (en) * 2022-04-21 2023-10-26 ヨネックス株式会社 Shuttlecock

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JPH1157096A (en) * 1997-08-19 1999-03-02 Goosen:Kk Shuttlecock
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JPH1157096A (en) * 1997-08-19 1999-03-02 Goosen:Kk Shuttlecock
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Publication number Priority date Publication date Assignee Title
WO2023203991A1 (en) * 2022-04-21 2023-10-26 ヨネックス株式会社 Shuttlecock

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JP2022122510A (en) 2022-08-23
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