JP2010510400A - Buffer layer for strings - Google Patents
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- JP2010510400A JP2010510400A JP2009537390A JP2009537390A JP2010510400A JP 2010510400 A JP2010510400 A JP 2010510400A JP 2009537390 A JP2009537390 A JP 2009537390A JP 2009537390 A JP2009537390 A JP 2009537390A JP 2010510400 A JP2010510400 A JP 2010510400A
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- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
- A63B51/00—Stringing tennis, badminton or like rackets; Strings therefor; Maintenance of racket strings
- A63B51/02—Strings; String substitutes; Products applied on strings, e.g. for protection against humidity or wear
-
- D—TEXTILES; PAPER
- D07—ROPES; CABLES OTHER THAN ELECTRIC
- D07B—ROPES OR CABLES IN GENERAL
- D07B1/00—Constructional features of ropes or cables
- D07B1/02—Ropes built-up from fibrous or filamentary material, e.g. of vegetable origin, of animal origin, regenerated cellulose, plastics
-
- D—TEXTILES; PAPER
- D07—ROPES; CABLES OTHER THAN ELECTRIC
- D07B—ROPES OR CABLES IN GENERAL
- D07B1/00—Constructional features of ropes or cables
- D07B1/16—Ropes or cables with an enveloping sheathing or inlays of rubber or plastics
- D07B1/162—Ropes or cables with an enveloping sheathing or inlays of rubber or plastics characterised by a plastic or rubber enveloping sheathing
-
- D—TEXTILES; PAPER
- D07—ROPES; CABLES OTHER THAN ELECTRIC
- D07B—ROPES OR CABLES IN GENERAL
- D07B1/00—Constructional features of ropes or cables
- D07B1/16—Ropes or cables with an enveloping sheathing or inlays of rubber or plastics
- D07B1/165—Ropes or cables with an enveloping sheathing or inlays of rubber or plastics characterised by a plastic or rubber inlay
-
- G—PHYSICS
- G10—MUSICAL INSTRUMENTS; ACOUSTICS
- G10D—STRINGED MUSICAL INSTRUMENTS; WIND MUSICAL INSTRUMENTS; ACCORDIONS OR CONCERTINAS; PERCUSSION MUSICAL INSTRUMENTS; AEOLIAN HARPS; SINGING-FLAME MUSICAL INSTRUMENTS; MUSICAL INSTRUMENTS NOT OTHERWISE PROVIDED FOR
- G10D3/00—Details of, or accessories for, stringed musical instruments, e.g. slide-bars
- G10D3/10—Strings
-
- D—TEXTILES; PAPER
- D07—ROPES; CABLES OTHER THAN ELECTRIC
- D07B—ROPES OR CABLES IN GENERAL
- D07B2201/00—Ropes or cables
- D07B2201/10—Rope or cable structures
- D07B2201/1028—Rope or cable structures characterised by the number of strands
- D07B2201/1036—Rope or cable structures characterised by the number of strands nine or more strands respectively forming multiple layers
-
- D—TEXTILES; PAPER
- D07—ROPES; CABLES OTHER THAN ELECTRIC
- D07B—ROPES OR CABLES IN GENERAL
- D07B2201/00—Ropes or cables
- D07B2201/20—Rope or cable components
- D07B2201/2071—Spacers
- D07B2201/2074—Spacers in radial direction
-
- D—TEXTILES; PAPER
- D07—ROPES; CABLES OTHER THAN ELECTRIC
- D07B—ROPES OR CABLES IN GENERAL
- D07B2201/00—Ropes or cables
- D07B2201/20—Rope or cable components
- D07B2201/2083—Jackets or coverings
- D07B2201/2087—Jackets or coverings being of the coated type
-
- D—TEXTILES; PAPER
- D07—ROPES; CABLES OTHER THAN ELECTRIC
- D07B—ROPES OR CABLES IN GENERAL
- D07B2205/00—Rope or cable materials
- D07B2205/10—Natural organic materials
-
- D—TEXTILES; PAPER
- D07—ROPES; CABLES OTHER THAN ELECTRIC
- D07B—ROPES OR CABLES IN GENERAL
- D07B2205/00—Rope or cable materials
- D07B2205/20—Organic high polymers
- D07B2205/2046—Polyamides, e.g. nylons
-
- D—TEXTILES; PAPER
- D07—ROPES; CABLES OTHER THAN ELECTRIC
- D07B—ROPES OR CABLES IN GENERAL
- D07B2205/00—Rope or cable materials
- D07B2205/30—Inorganic materials
- D07B2205/3007—Carbon
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
- Y10T428/2913—Rod, strand, filament or fiber
- Y10T428/2933—Coated or with bond, impregnation or core
- Y10T428/2936—Wound or wrapped core or coating [i.e., spiral or helical]
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- Multimedia (AREA)
- Health & Medical Sciences (AREA)
- Physical Education & Sports Medicine (AREA)
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Acoustics & Sound (AREA)
- General Health & Medical Sciences (AREA)
- Chemical Or Physical Treatment Of Fibers (AREA)
- Treatments For Attaching Organic Compounds To Fibrous Goods (AREA)
- Extrusion Moulding Of Plastics Or The Like (AREA)
- Ropes Or Cables (AREA)
- Paints Or Removers (AREA)
- Carbon And Carbon Compounds (AREA)
- Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
- Compositions Of Macromolecular Compounds (AREA)
Abstract
Description
本発明は、ストリングのためのバッファ層に関している。 The present invention relates to a buffer layer for strings.
本願は米国仮出願第60/866,199号の優先権を主張し、これは参照によりこれによって組み込まれる。 This application claims priority of US Provisional Application No. 60 / 866,199, which is hereby incorporated by reference.
スポーツ用品(例えばテニスラケット)、または楽器で用いられるストリングは一般的に、その耐久性、回転、触感などを改善するために一番外側の表面に薄い層が被覆される。ポリアミド(ナイロン)、ポリエステル、及び他のポリマーがストリングを被覆するために用いられている。純ナイロン6よりも良好な物理的特性を有している、クレイ及びカーボンナノチューブ強化ナイロン6ナノ複合材料のようなナノ複合材料は、他の機能性を有する高く耐久力のあるストリング被覆材料となる潜在能力がある。高いアスペクト比を有するナノサイズのクレイ粒子を用いる前記強化高分子複合材料は、1980年代から研究されている(特許文献1を参照)。ストリングは一般的に、コアフィラメント、前記コアフィラメント上のラッピングフィラメント、及び被覆材の多層構造を有するポリマー材料である。多層構造を有する前記ストリングに対して、被覆材料は、基材を調和させ、及び前記ラッピングフィラメントの間のギャップにそれらが浸透することを可能にするために、所定の温度で良好な溶融流れ特性を有することが必要とされる。ナノ複合材料の粘度は、同一の温度で純ナイロン6より高い。このようにして、前記ナノ複合材料は、前記ラップフィラメント間の前記ギャップに容易には浸透し得ない。図1はラッピングフィラメント上に被覆されたナイロン6/クレイナノ複合材料の断面図のSEM画像を示している。前記ナノ複合材料は、前記ギャップを連続的に充填していないことがわかる。多くの欠陥が前記ストリング上に残っており、これは前記ストリングの許されない耐久性をもたらすだろう。前記ギャップは、ボールがヒットする高いインパクトの間に、被覆物の欠落または許されない耐久性をもたらすだろう。さらに、前記ギャップの生成に起因して、被覆物は同様に、前記ストリングの前記コア材料上に前記フィラメントを固定できない。図2は、前記ストリングの高インパクト試験の後のフィラメント及び被覆から欠落した材料を示している。 Strings used in sports equipment (eg, tennis rackets) or musical instruments are typically coated with a thin layer on the outermost surface to improve their durability, rotation, feel, etc. Polyamide (nylon), polyester, and other polymers have been used to coat the strings. Nanocomposites, such as clay and carbon nanotube reinforced nylon 6 nanocomposites, which have better physical properties than pure nylon 6, are highly durable string coating materials with other functionalities. There is potential. The reinforced polymer composite material using nano-sized clay particles having a high aspect ratio has been studied since the 1980s (see Patent Document 1). The string is generally a polymer material having a multi-layer structure of core filaments, wrapping filaments on the core filaments, and a covering material. For the strings having a multilayer structure, the coating material has good melt flow properties at a given temperature in order to harmonize the substrate and allow them to penetrate the gaps between the wrapping filaments. It is required to have The viscosity of the nanocomposite is higher than pure nylon 6 at the same temperature. In this way, the nanocomposite material cannot easily penetrate the gap between the wrap filaments. FIG. 1 shows an SEM image of a cross-sectional view of a nylon 6 / clay nanocomposite coated on a wrapping filament. It can be seen that the nanocomposite material does not continuously fill the gap. Many defects remain on the string, which will result in unacceptable durability of the string. The gap will result in missing coatings or unacceptable durability during high impact when the ball is hit. Furthermore, due to the creation of the gap, the coating cannot similarly fix the filament on the core material of the string. FIG. 2 shows the material missing from the filament and coating after high impact testing of the string.
高分子ナノ複合材料は、純高分子材料よりも高い物理的/機械的特性を有しているにも関わらず、それらは通常的に、押出成形または被覆工程の間に高い粘度または溶融流れを有している。この問題を解決するために、薄いバッファ層は、多重フィラメントで包まれたストリングを被覆するために用いられ、前記ギャップを満たす。前記バッファ層被覆物のポリマーは、前記フィラメントの間の前記ギャップを満たすための被覆工程の間に高い溶融流れ(低い粘度)を有しており、及び前記フィラメントは被覆によって基礎のコア材料上に固定される。 Although polymer nanocomposites have higher physical / mechanical properties than pure polymer materials, they typically have a higher viscosity or melt flow during the extrusion or coating process. Have. To solve this problem, a thin buffer layer is used to cover the multifilament wrapped string to fill the gap. The polymer of the buffer layer coating has a high melt flow (low viscosity) during the coating process to fill the gap between the filaments, and the filaments are coated onto the underlying core material. Fixed.
(実施例1)ナイロン6バッファ層を有する被覆システム
図3Aは、小径マルチフィラメント302で包まれた一つのモノフィラメントコア301からなる被覆対象のストリングの断面を図示している。UBE Industries Inc.から得られうる(製品名:UBE SF 1018A)のような純ナイロン6ペレットが溶融される。前記バッファ層被覆物303は220℃から270℃の範囲の温度で押出成形工程によって塗布される。前記バッファ層303の厚さは10から100マイクロメートルでありうる。前記マルチフィラメント302の間の前記ギャップは、前記純ナイロン6被覆によって完全に満たされる。
Example 1 Coating System with Nylon 6 Buffer Layer FIG. 3A illustrates a cross-section of a string to be coated consisting of a single monofilament core 301 wrapped with a small diameter multifilament 302. UBE Industries Inc. Pure nylon 6 pellets such as (product name: UBE SF 1018A) which can be obtained from The buffer layer coating 303 is applied by an extrusion process at a temperature in the range of 220 ° C. to 270 ° C. The buffer layer 303 may have a thickness of 10 to 100 micrometers. The gap between the multifilaments 302 is completely filled with the pure nylon 6 coating.
耐摩耗性被覆304はそれから、240℃から280℃の範囲の温度で押出成形工程によって被覆される(図3C)。ナイロン6/クレイまたはナイロン6/カーボンナノチューブナノ複合材料は、前記耐磨耗性被覆材料304として用いられうる。その場重合で作られた前記ナイロン6ナノ複合材料は4%のナノクレイ充填物を含有しうる。溶融混合工程によって作り出された他のナイロン6ナノ複合材料は同様に、前記耐磨耗被覆304のために利用されうる。前記クレイを除くと、カーボンナノチューブ、SiO2及びAl2O3のようなセラミック粒子、またはガラス粒子は、ナイロン6ナノ複合材料を作るために利用されうる。前記ナイロン6ナノ複合材料は、柔軟性と耐久性を強化するためにゴム重合調整剤によって修飾されうる。前記耐摩耗性被覆の前記厚さは、1から100マイクロメートルでありうる。 The abrasion resistant coating 304 is then coated by an extrusion process at a temperature in the range of 240 ° C. to 280 ° C. (FIG. 3C). Nylon 6 / clay or nylon 6 / carbon nanotube nanocomposites can be used as the abrasion resistant coating material 304. The nylon 6 nanocomposite made by in situ polymerization may contain 4% nanoclay filler. Other nylon 6 nanocomposites created by the melt mixing process can also be utilized for the wear resistant coating 304. With the exception of the clay, carbon nanotubes, ceramic particles such as SiO 2 and Al 2 O 3 , or glass particles can be utilized to make nylon 6 nanocomposites. The nylon 6 nanocomposite can be modified with a rubber polymerization modifier to enhance flexibility and durability. The thickness of the wear resistant coating may be 1 to 100 micrometers.
(実施例2)ナイロン11バッファ層の被覆システム
図3Aを再度参照すると、被覆のための前記ストリングは、小径マルチフィラメント302で包まれた一つのモノフィラメントコア301である。純ナイロン11はARKEMA Inc.から得られうる。ナイロン11は220℃を越える温度で良好な溶融流れを有している。良好なインパクト強さ及びせん断強さは同様に、ナイロン11を良好なバッファ層材料とさせている。図3Bにおいて、前記バッファ層被覆303は190℃から270℃の範囲の温度で押出成形工程によって塗布される。
Example 2 Nylon 11 Buffer Layer Coating System Referring again to FIG. 3A, the string for coating is a single monofilament core 301 wrapped with small multifilaments 302. Pure nylon 11 is available from ARKEMA Inc. Can be obtained from Nylon 11 has a good melt flow at temperatures in excess of 220 ° C. Good impact strength and shear strength also make nylon 11 a good buffer layer material. In FIG. 3B, the buffer layer coating 303 is applied by an extrusion process at a temperature in the range of 190 ° C. to 270 ° C.
前記バッファ層303の前記厚さは、10から100マイクロメートルでありうる。前記マルチフィラメント302の間の前記ギャップは、前記純ナイロン11被覆で完全に満たされる。 The thickness of the buffer layer 303 may be 10 to 100 micrometers. The gap between the multifilaments 302 is completely filled with the pure nylon 11 coating.
図3Cを参照すると、耐磨耗被覆304はそれから、240℃から280℃の範囲の温度で押出成形工程によって被覆される。ナイロン6/クレイまたはナイロン6/カーボンナノチューブナノ複合材料は前記耐摩耗性被覆材料304として利用されうる。その場重合で作られた前記ナイロン6ナノ複合材料は、4%のナノクレイ充填物を含有しうる。溶融混合工程で作られた他のナイロン6ナノ複合材料は同様に、前記耐摩耗性被覆304のために利用されうる。前記ナイロン6ナノ複合材料は同様に、前記柔軟性及び耐久性を強化するためにゴム重合調整剤によって修飾されうる。前記耐摩耗性被覆304の前記厚さは、1から100マイクロメートルでありうる。 Referring to FIG. 3C, the wear resistant coating 304 is then coated by an extrusion process at a temperature in the range of 240 ° C. to 280 ° C. Nylon 6 / clay or nylon 6 / carbon nanotube nanocomposites can be used as the abrasion resistant coating material 304. The nylon 6 nanocomposite made by in-situ polymerization can contain 4% nanoclay filler. Other nylon 6 nanocomposites made from a melt mixing process can be utilized for the abrasion resistant coating 304 as well. The nylon 6 nanocomposite can also be modified with a rubber polymerization modifier to enhance the flexibility and durability. The thickness of the wear resistant coating 304 may be 1 to 100 micrometers.
前記ストリング上に被覆物を堆積するための前記押出成形工程を除いては、噴き付け、ディッピング、スピンコーティング、ブラッシング、塗布、及び浸漬工程が、ストリングの前記表面上に被覆物を堆積するために利用されうる。ナイロン6ナノ複合材料は、190℃より高い温度で溶融され、前記ストリング上に被覆物を堆積するために押出成形される。ナイロン6ナノ複合材料は、ギ酸のような溶媒で溶解され、及び室温で、または段階的な温度で、前記ストリング上に被覆物を堆積するために、噴き付けられ、ディッピングされ、スピンコーティングされ、ブラッシングされ、塗布され、または浸漬されうる。前記溶媒はそれから、蒸発法のような事後工程によって取り除かれる。 Except for the extrusion step for depositing a coating on the string, spraying, dipping, spin coating, brushing, coating, and dipping steps are used to deposit the coating on the surface of the string. Can be used. Nylon 6 nanocomposites are melted at temperatures above 190 ° C. and extruded to deposit a coating on the strings. Nylon 6 nanocomposites are dissolved in a solvent such as formic acid and sprayed, dipped, spin coated to deposit a coating on the string at room temperature or stepwise temperature, It can be brushed, applied or dipped. The solvent is then removed by a post process such as evaporation.
図4は、本発明の他の実施形態を図示している。本質的に、図3Cの前記被覆されたストリング構造はそれから、小径マルチフィラメント401で再び被覆される。層303と類似のバッファ層被覆物402が190℃から270℃の範囲の温度で押出成形によって塗布される。前記バッファ層402の厚さは、10から100マイクロメートルでありうる。前記マルチフィラメント401の間のギャップは、前記純ナイロン11被覆物によって完全に満たされる。耐磨耗被覆403はそれから、240℃から280℃の範囲の温度で押出成形工程によって被覆される。ナイロン6/クレイまたはナイロン6/カーボンナノチューブナノ複合材料は前記耐摩耗性被覆材料403として用いられうる。その場重合で作られた前記ナイロン6ナノ複合材料は、4%ナノクレイ充填物を含有しうる。溶融混合工程により作られた他のナイロン6ナノ複合材料は同様に、前記耐摩耗性被覆403のために利用されうる。前記ナイロン6ナノ複合材料は同様に、前記柔軟性と耐久性を強化させるためにゴム重合調整剤によって修飾されうる。前記耐摩耗性被覆403の前記厚さは、1から100マイクロメートルでありうる。 FIG. 4 illustrates another embodiment of the present invention. Essentially, the coated string structure of FIG. 3C is then recoated with a small diameter multifilament 401. A buffer layer coating 402 similar to layer 303 is applied by extrusion at a temperature in the range of 190 ° C to 270 ° C. The buffer layer 402 may have a thickness of 10 to 100 micrometers. The gap between the multifilaments 401 is completely filled with the pure nylon 11 coating. The wear resistant coating 403 is then coated by an extrusion process at a temperature in the range of 240 ° C to 280 ° C. Nylon 6 / clay or nylon 6 / carbon nanotube nanocomposites can be used as the wear resistant coating material 403. The nylon 6 nanocomposite made by in situ polymerization may contain 4% nanoclay filler. Other nylon 6 nanocomposites made by a melt mixing process can be utilized for the wear resistant coating 403 as well. The nylon 6 nanocomposite can also be modified with a rubber polymerization modifier to enhance the flexibility and durability. The thickness of the wear resistant coating 403 may be 1 to 100 micrometers.
301 モノフィラメントコア
302 小径マルチフィラメント
303 バッファ層
401 小径マルチフィラメント
402 バッファ層被覆物
403 被覆
301 monofilament core 302 small-diameter multifilament 303 buffer layer 401 small-diameter multifilament 402 buffer layer coating 403 coating
Claims (19)
コアフィラメントであって、前記コアフィラメントより小径の複数のラッピングフィラメントで包まれたコアフィラメントと、
前記ラッピングフィラメントの間と、前記ラッピングフィラメントと前記コアフィラメントとの間のギャップを充填しているバッファ層被覆物と、
前記バッファ層被覆物、ラッピングフィラメント、及びコアフィラメントを覆う外部被覆物と、
を備えている被覆物。 A covering for the string,
A core filament, which is wrapped with a plurality of wrapping filaments having a smaller diameter than the core filament, and
A buffer layer coating filling a gap between the wrapping filaments and between the wrapping filaments and the core filaments;
An outer coating covering the buffer layer coating, the wrapping filament, and the core filament;
A coating comprising:
第1の直径を有しているコアフィラメントを、前記第1の直径より小さい第2の直径を有している一つ以上のラッピングフィラメントで包む段階と、
前記一つ以上のラッピングフィラメントの間のギャップ、及び前記ラッピングフィラメントと前記コアフィラメントの間のギャップ内に溶融ナイロンを押出成形させる段階と、
前記一つ以上のラッピングフィラメント及び前記ギャップ内の前記溶融ナイロンを被覆するように、前記ストリングの外周上に被覆物を押出成形させる段階と、
を備えている方法。 A method for coating a string, comprising:
Wrapping a core filament having a first diameter with one or more wrapping filaments having a second diameter smaller than the first diameter;
Extruding molten nylon into the gap between the one or more wrapping filaments and the gap between the wrapping filament and the core filament;
Extruding a coating on the outer circumference of the string to cover the one or more wrapping filaments and the molten nylon in the gap;
A method comprising:
前記外部被覆の周りに包まれた他の複数のラッピングフィラメントと、
前記他の複数のラッピングフィラメントの間のギャップを満たす他のバッファ層被覆物と、
前記他のバッファ層被覆物の一面を覆う他の外部被覆と、
をさらに備えている被覆。 The coating according to claim 1,
A plurality of other wrapping filaments wrapped around the outer coating;
Another buffer layer coating that fills a gap between the other plurality of wrapping filaments;
Another outer coating covering one surface of the other buffer layer coating;
Further comprising a coating.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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US86619906P | 2006-11-16 | 2006-11-16 | |
PCT/US2007/084973 WO2008061229A1 (en) | 2006-11-16 | 2007-11-16 | Buffer layer for strings |
Publications (2)
Publication Number | Publication Date |
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JP2010510400A true JP2010510400A (en) | 2010-04-02 |
JP2010510400A5 JP2010510400A5 (en) | 2012-08-02 |
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Application Number | Title | Priority Date | Filing Date |
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JP2009537390A Pending JP2010510400A (en) | 2006-11-16 | 2007-11-16 | Buffer layer for strings |
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US (1) | US20080124546A1 (en) |
EP (1) | EP2083928B1 (en) |
JP (1) | JP2010510400A (en) |
CN (1) | CN101534909A (en) |
AT (1) | ATE530230T1 (en) |
TW (1) | TW200840890A (en) |
WO (1) | WO2008061229A1 (en) |
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WO2020031529A1 (en) * | 2018-08-10 | 2020-02-13 | 株式会社ゴーセン | Racket string and method of manufacturing same |
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RU2500849C2 (en) * | 2008-08-15 | 2013-12-10 | Отис Элевэйтор Компани | Lifting system and method of its operation |
EP2704136A1 (en) * | 2012-09-04 | 2014-03-05 | Larsen Strings A/S | Damping and adhesive material for music strings |
CN104043233A (en) * | 2014-05-21 | 2014-09-17 | 安徽梦谷纤维材料科技有限公司 | Method for preparing badminton racket string |
JP6698317B2 (en) * | 2015-11-12 | 2020-05-27 | ヨネックス株式会社 | Racket string |
JP6812052B2 (en) * | 2016-04-18 | 2021-01-13 | ヨネックス株式会社 | Racket string |
PT3418433T (en) * | 2017-06-21 | 2020-03-23 | Speed France S A S | Monofilament string for a racket and process for manufacturing such a monofilament string |
EP3775365B1 (en) * | 2018-03-26 | 2024-06-19 | Bridon International Limited | Synthetic fiber rope |
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Also Published As
Publication number | Publication date |
---|---|
EP2083928B1 (en) | 2011-10-26 |
TW200840890A (en) | 2008-10-16 |
WO2008061229A1 (en) | 2008-05-22 |
EP2083928A1 (en) | 2009-08-05 |
ATE530230T1 (en) | 2011-11-15 |
WO2008061229A9 (en) | 2008-08-21 |
CN101534909A (en) | 2009-09-16 |
US20080124546A1 (en) | 2008-05-29 |
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