WO2013058621A1 - Shuttlecock - Google Patents

Shuttlecock Download PDF

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Publication number
WO2013058621A1
WO2013058621A1 PCT/KR2012/008637 KR2012008637W WO2013058621A1 WO 2013058621 A1 WO2013058621 A1 WO 2013058621A1 KR 2012008637 W KR2012008637 W KR 2012008637W WO 2013058621 A1 WO2013058621 A1 WO 2013058621A1
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WO
WIPO (PCT)
Prior art keywords
flagpole
shuttlecock
hair
head
feather
Prior art date
Application number
PCT/KR2012/008637
Other languages
French (fr)
Korean (ko)
Inventor
김상웅
Original Assignee
Kim Sang-Woong
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from KR2020110009404U external-priority patent/KR200460073Y1/en
Priority claimed from KR2020110010694U external-priority patent/KR200461940Y1/en
Priority claimed from KR2020110010692U external-priority patent/KR200461941Y1/en
Application filed by Kim Sang-Woong filed Critical Kim Sang-Woong
Publication of WO2013058621A1 publication Critical patent/WO2013058621A1/en

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    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63BAPPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B69/00Training appliances or apparatus for special sports
    • A63B69/0017Training appliances or apparatus for special sports for badminton
    • 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
    • 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
    • A63B67/19Shuttlecocks with several feathers connected to each other

Definitions

  • the present invention relates to a shuttlecock, and more particularly, to improve the productivity while allowing the production of a shuttlecock of uniform dimensions, and the lifespan of the shuttlecock long by preventing the flagpole bending and breaking of the fixed line portion when the shuttlecock strikes It is related to the shuttle cock to improve the feel feel while improving the hitting feeling, flight speed, trajectory and distance does not change, and when the artificial feather having a hair on the sheet does not cause tangling of the hair when hitting.
  • a general badminton competition shuttlecock is a bird feather 20 inserted into a head 10 made of a hemispherical cork, as shown in FIG.
  • cork diameter is 25mm ⁇ 28mm
  • the number of feathers should be 16 pieces
  • the length from the tip of the feather to the top of the head should be 64mm ⁇ 70mm
  • the diameter of the feather is 58mm ⁇ 68mm
  • head ( The upper surface of 10) and the outer circumferential surface of the feather 20 have an angle of about 65 ° to 75 °
  • the maximum speed is 320km / h
  • the feather of the natural bird is that the feather branch extends to both sides and the hair is formed on both ends of the flagpole, with the flagpole being excessively bent or its thickness does not reach a certain degree, but in many cases it cannot be used.
  • many parts except the flagpole that is, the state of the flagpole and the hair are in good condition, but if the flagpole is not satisfied, it can not be used and discarded.
  • the prior art 1 has a problem that the angle and spacing of the flagpole is not exactly matched to form the flagpole to which the feather is attached one by one separately, so as to fit in the head, the prior art 2 is the angle of the feather branch and hair Because it is not formed separately for each flagpole, it is formed into a barrel, so that the flight of air is not able to perform a flight motion suitable for the competition standards because it does not receive the resistance of air and the hair of a known natural shuttlecock in flight.
  • the flagpole's elasticity is very important in order to prevent damage of the shuttlecock.
  • the flagpoles of the prior arts 1 and 2 described above are produced by injection without any detailed description of the flagpole's structure. From the base material, it was not possible to secure a space for absorbing the impact on the end face, which could cause damage.
  • the conventional artificial shuttlecock has a problem that the flagpole is formed at 0 degrees with respect to the tangent of the circle connecting the end of the flagpole, so that when the hair is attached, it is impossible to obtain a rotational force such as natural feathers.
  • a fixing line 20b for fixing the spacing and the angle of the flagpole is installed on the flagpole 20, which is fixed to the flagpole 20 lifespan.
  • seawater is a very important factor.
  • the fixed line 20b is usually injection molded integrally with the flagpole, the fixed line and the flagpole have the same strength, and the inward face of the fixed line is formed in a plane.
  • the shuttlecock does not absorb the shock caused by the collision with the racket 60, as shown in FIG. 3, and thus the desired flight trajectory, speed, and distance cannot be obtained, Problems such as breaking occur.
  • the headpiece 10 when hitting with a racket during high clearing or smashing, the headpiece 10 is not fitted from the head, but the flagpole 20 and the hair, especially from the tip of the hair, which causes the flagpole 20 to swing back and forth, left and right,
  • the flagpole may not absorb the flow of the flagpole, and as shown in FIG. 3, the flagpole may be broken or broken at the fixed line portion.
  • the flight direction does not have a distance from the desired flight curve, such as shaking.
  • the flagpole 20 should be as light as possible, when the fixing line 20b is thinly formed, the elasticity in the inner / outer direction of the shuttle ball is lowered, so as to be crushed as shown in FIG. This takes a flight distance and speed and trajectory is not satisfactory, there was also a problem falling shot.
  • shuttlecocks using artificial feathers are mostly made of nonwoven fabrics or resins.
  • An object of the present invention is to provide a shuttlecock that can use a portion of the feather that was not available due to the flagpole problem of the conventional natural feathers while improving the problem of bad feel during use due to bad elasticity of the artificial shuttlecock.
  • the fixed line that plays an important role in the flight trajectory, distance and speed is light and excellent in elasticity so that the life of the shuttlecock is long and has excellent quality, and the conventional artificial feathers
  • Another purpose is to prevent hair entanglement so that flight speed, trajectory and distance are satisfactory at the time of hitting.
  • the base, the flagpole is integrally extended to have a predetermined angle from the centerline of the head with a plurality of bases having a predetermined distance to the base coupled to the head; Shuttlecock composed of hair attached to the end of the flagpole.
  • the injection molding is formed so as to form a groove along the longitudinal direction in the center of the inner surface of the flagpole, the fixing band is integrally injection molded in the center of the flagpole, the flagpole with respect to the tangent of the circle connecting the end of the flagpole from the center of the shuttlecock It is formed to have an angle of 0-30 degrees.
  • the feather branches are formed to be spaced apart from each other in an symmetrical inclination on the upper left and right sides of the flagpole corresponding to the hair, and a ring is formed at the end of the feather branch.
  • the hair is used either by thermally fusion-molding microfibers in a fibrous form, by foaming, or by terminating portions of natural feathers, that is, terminating portions of feather feathers.
  • the present invention is characterized in that the fixing line formed integrally with the flagpole in order to fix the spacing and angle of the flagpole, the groove is formed on the inner side in the longitudinal direction and has a shape protruding outward.
  • the thickness is moderate but the weight is reduced.
  • the flagpole is thinner and more elastic than the thickness of the flagpole to improve hitting feeling, reduce weight, and collide with the racket.
  • the center line and branch lines connected to the flagpole are further compressed to secure the elasticity and form stability of the hair, and the thickness of the hair is gradually thinned outward from the center line, resulting in dullness. It helps to reduce the weight and give a good feeling.
  • the fixed line becomes lighter, and thus the whole shuttlecock becomes lighter, so that the impact when the impact is transferred to the elbow of the user does not occur, and the impact of the artificial feather hits the racket. Since it has sufficient elasticity and has excellent elasticity, the flagpole's flagpole is not broken or broken so that the life of the shuttlecock is prolonged and flight trajectory and distance speed are not reduced.
  • the shuttlecock using the artificial feather is not tangled with each other when the hair on the sheet is not entangled with each other, so that the flight to the unwanted place due to shaking during flight.
  • FIG. 1 is a perspective view showing a general shuttle cock
  • FIG. 2 is a front view showing a conventional artificial shuttlecock
  • 3 and 4 is a view showing the change of shuttlecock when the shuttlecock hit
  • FIG. 5 is a view showing a hair tangled structure of a conventional artificial shuttlecock
  • FIG. 6 is a front view showing a shuttle cock according to a first embodiment of the present invention.
  • FIG. 7 is a cross-sectional view of FIG. 6
  • FIG. 8 is a cross-sectional view showing the flagpole and the head according to the first embodiment of the present invention.
  • FIG. 9 is a cross-sectional view of the flagpole of FIG.
  • FIG. 10 is a view showing an installation angle of the flagpole according to the first embodiment of the present invention.
  • FIG. 11 is a plan view showing the hair according to the first embodiment of the present invention.
  • FIG. 12 is a cross-sectional view of FIG.
  • FIG. 13 is a cross-sectional view illustrating attaching hair to a flagpole according to a first embodiment of the present invention.
  • FIG. 14 is a cross-sectional view showing the attachment of natural hair to the flagpole according to the first embodiment of the present invention
  • 15 is a cross-sectional view showing a shuttle cock according to a third embodiment of the present invention.
  • FIG. 16 is an enlarged view of the hair of FIG.
  • 17 is a cross-sectional view taken along the line A-A of FIG.
  • FIG. 18 is a cross-sectional view showing a fixed line structure of the present invention.
  • the shuttle cock is integrally formed to have a constant angle from the centerline of the head 30 while having a plurality of regular intervals in the base 42 is coupled to the head 30 as shown in FIGS.
  • Each cross section has a triangular shape
  • the injection-molded flagpole 40 the yarn is formed in the form of a sheet to form a groove 46 in the longitudinal direction in the center of the inward surface of the shuttlecock, respectively bonded to the end of the flagpole 40
  • the hairline 50 includes a centerline 55 coupled to the flagpole 40, a feather branch 52, and a comb line 53.
  • the fixing band 48 is integrally formed and the fixing band 48 prevents the flagpole 40 from being separated from inside, outside and left and right when being hit by the racket.
  • the reason for fixing the flagpole 40 in this way is that if the spacing of the flagpole 40 is changed and the angle is changed, the shuttlecock is shaken to travel as much as the desired course and distance.
  • the fixing band 48 is formed to a certain dimension through the injection molding, the length in the horizontal direction with the center line of the shuttlecock is molded into 0.5 ⁇ 3mm, the length in the vertical direction is 0.2 ⁇ 2mm, the fixing belt 48 ) Is thicker than the range, the feeling of hitting falls, it is difficult to control the weight. This is because it is good to hit with the flagpole when it is high clear or smashed.
  • the flagpole 40 is formed to be twisted from 0 to 30 ° from the tangent along the circumference of the shuttle cock as shown in Figure 10 can be reduced or increased the angle to increase the number of revolutions according to the wind, which is determined during the molding process It is molded at an angle, but not deformed during use.
  • the flagpole 40 has a cross-section, including an isosceles triangle shape or an isosceles triangle shape or arc shape, is symmetrically formed with respect to the center, and the portion corresponding to the racket in the shuttlecock is the flagpole 40 and the hair 50. Therefore, the flagpole 40 is preferably an isosceles triangle shape in which the outer two sides of the shuttlecock are isosceles, as shown in FIG. 9, and when formed in this way, the flagpole can be prevented from inside, outside, left and right twisting, and elasticity is generated.
  • the end diameter of the flagpole is preferably 6 to 7 cm.
  • the base 42 is formed so that the fastener 41 is integrally protruded to the bottom in contact with the head 30 to be plugged into the head 30, the fastener 41 is cylindrical to the bottom And a fixing protrusion 41b protruding outwardly from the lower end of the protruding wall 41a and protruding wall 41 to which the fastener 41 is fastened.
  • An insertion groove 46 having a shape corresponding to the 41a is formed, so that the protruding wall 41a is inserted into the insertion groove 46 to be fixed by the fixing protrusion 41b at the end.
  • the material for forming the hair 50 in the above can be used any material that makes a yarn as a yarn, such as polyester, nylon, silk, cotton, etc.
  • Shuttlecock hair should be very light, so low denier (5 denier) Using less than 20 ⁇ 100g per 1m2, and light and have some strength, so heat the thinly coated yarn so that it will not be distracted by fusion.
  • the yarn in the case of the yarn that is not easily dissolved in heat, the yarn is thinly disposed in a sheet form, and then laminated or coated with a heat-bondable material such as bond, latex, and vinyl on one or both surfaces thereof, and then molded.
  • a heat-bondable material such as bond, latex, and vinyl on one or both surfaces thereof, and then molded.
  • further fusion of latex, vinyl and the like may be applied to a yarn that can be heat-sealed to give a desired hardness.
  • the hair 50 formed by heat-sealing has a horizontal longest length of 1 to 2.5 cm, a vertical longest length of 2.5 to 5 cm, and a thickness of 0.5 to 1.5 mm as shown in FIGS. 11 and 12. Shaped so as to become thinner, the center line 55 constituting the hair 50 is 0.2 to 0.5mm thinner than the maximum thickness of the hair 50, while the center line 55 width of the surface combined with the flagpole 40 The centerline 55 of the surface is formed to the size that can accommodate the width of the flagpole 40 and is not coupled to the flagpole 40 is formed narrower than the width of the flagpole 40, the flagpole 52 is the hair 50 It is formed 0.2 ⁇ 0.5mm thinner than the maximum thickness, and the comb line 53 extending again from the feather branch 52 is formed 0.1 ⁇ 0.2mm thinner than the maximum thickness of the hair 50, the shape of the hair 50 Make a mold for thermal fusion to fit.
  • the mold presses the sheet for 0.5-5 seconds at 120 to 250 ° C.
  • the hair 50 formed of a sheet-like yarn may be bonded to the flagpole 40 which is injection molded integrally as described above, but as shown in Fig. 14, the flagpole 55a of natural feathers.
  • the natural hair 50 cut into a certain shape can be bonded to the flagpole 40 which is injection molded integrally as described above.
  • the hair may be foam-molded with polypropylene (PP), polyethylene (PE), urethane, or the like and adhered to the flagpole.
  • PP polypropylene
  • PE polyethylene
  • urethane or the like
  • the shuttlecock is composed of a head 30, a flag pole 40 engaged with the head 30, and a hair 50 formed on the upper left and right sides of the flag pole 40, as shown in Figs.
  • the flagpole 40 is integrally formed to have a predetermined angle from the centerline of the head 30 while having a plurality of flagpoles 40 at regular intervals on the cylindrical base 42.
  • the cross section of each of the flagpoles 40 formed as described above is injection-molded so that the grooves 46 are formed along the longitudinal direction at the center of the inward surface of the shuttlecock in a triangular shape.
  • the flagpole 40 is further formed to be spaced apart from each other to be symmetrically inclined symmetrically to the upper left and right sides of the flagpole 40 corresponding to the hair 50 is formed with a groove (47a) in the center, the end of the ring 48 is formed.
  • the fixed line 49 integrally formed with the flagpole 40 is bent the center in the longitudinal direction, as shown in FIG. It is formed to have a shape that is formed and protrudes outward.
  • the fixed line 49 has a longitudinal length of 0.3 to 3mm, a transverse length of 0.3 to 3mm, and can be used by adjusting the horizontal and vertical lengths according to a desired hitting feel.
  • the strength is weak and soft, and in the opposite case, the strength is high and rigid.
  • the hair 50 is formed in a sheet shape and adhered to the end of the flagpole 40 of the flagpole 40 and has a centerline (not shown) at a thickness thinner than other portions in the center to facilitate engagement with the flagpole 40. ).
  • the ring 48 of the flagpole 40 to hold the feather branch 47 of the adjacent flagpole 40 so that the arrangement position of the hair 50 is mixed or changed with each other inside and outside It is possible to prevent the hair 50 from being entangled by not happening, and thus, when the hair 50 is prevented from being entangled, a desired flight curve and a distance can be obtained.
  • the natural feathers are separated one by one, so no big problem occurs.
  • the normal artificial feather is formed in the shape of a hair sheet, the tangled feathers do not have a distance from the desired flight curve, such as severe shaking during flight and flight direction. There is a problem.
  • Flagpole 40 is shaken back and forth, left and right, the fixed line 49 is formed thinly by the groove (49a) has elasticity and has the necessary strength due to the ' ⁇ ' shaped cross-section shuttle shuttle when hitting As soon as it is returned to its original position, the flagpole is not broken or broken.

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  • Physical Education & Sports Medicine (AREA)
  • Injection Moulding Of Plastics Or The Like (AREA)

Abstract

The present invention relates to a shuttlecock and a method for manufacturing same, and more specifically, to a shuttle cock and a method for manufacturing same, which can allow manufacturing of the shuttlecock having a uniform size and superior quality while improving productivity, extending the life of the shuttle cock by preventing bending or breaking of the rachis of the feather around a fixing line portion when hitting the shuttlecock, improving hitting sensation, maintain a constant flight velocity, trajectory, and distance, prevent tangling of the feathers when using artificial feathers having feathers on a sheet, and improving the hitting sensation.

Description

셔틀콕Shuttlecock
본 발명은 셔틀콕에 관한 것으로, 보다 상세하게는 균일한 치수의 셔틀콕을 제조할 수 있도록 하면서 생산성이 향상되도록 하고, 셔틀콕의 타격시 고정선 부분의 깃대 절곡 및 부러짐이 발생하지 않도록 하여 셔틀콕의 수명이 길어지도록 하면서 타구감이 개선되고 비행속도, 궤적 및 거리가 달라지지 않도록 하며, 시트 상의 털을 갖는 인공 깃털을 사용하는 경우 타격시 털의 엉킴이 발생하지 않도록 하면서, 타구감이 개선되도록 하는 셔틀콕에 관한 것이다.The present invention relates to a shuttlecock, and more particularly, to improve the productivity while allowing the production of a shuttlecock of uniform dimensions, and the lifespan of the shuttlecock long by preventing the flagpole bending and breaking of the fixed line portion when the shuttlecock strikes It is related to the shuttle cock to improve the feel feel while improving the hitting feeling, flight speed, trajectory and distance does not change, and when the artificial feather having a hair on the sheet does not cause tangling of the hair when hitting.
셔틀콕을 이용한 경기로는 배드민턴, 테크민턴 등이 있으며, 일반적인 배드민턴 경기용 셔틀콕은 도 1에 나타내는 바와 같이 반구상의 코르크로 이루어진 헤드(10)에 새의 깃털(20)을 꽂은 것으로, 셔틀콕의 총 무게는 4.5∼5.5g이고, 코르크의 지름은 25mm∼28mm이며, 깃털의 수는 16장, 깃털 끝에서 헤드 상부면까지의 길이는 64mm∼70mm여야 하며, 깃털 끝의 지름은 58mm~68mm, 헤드(10)의 상부면과 깃털(20)의 외주면은 65°~75°정도의 각을 갖게 되고, 최고속도는 320km/h이며, 경기자가 코트의 한쪽 끝에서 언더핸드로 쳐서 반대편 백바운더리 라인 안쪽의 53~99cm 사이에 떨어져야 한다.As a game using a shuttlecock, there are badminton, techminton, and the like. A general badminton competition shuttlecock is a bird feather 20 inserted into a head 10 made of a hemispherical cork, as shown in FIG. Is 4.5 ~ 5.5g, cork diameter is 25mm ~ 28mm, the number of feathers should be 16 pieces, the length from the tip of the feather to the top of the head should be 64mm ~ 70mm, the diameter of the feather is 58mm ~ 68mm, head ( The upper surface of 10) and the outer circumferential surface of the feather 20 have an angle of about 65 ° to 75 °, the maximum speed is 320km / h, and the player hits the underhand at one end of the court to the inner back boundary line. It should fall between 53 and 99 cm.
그리고, 테크민턴은 본원의 출원인이 개발하여 운영하고 있는 경기로서 대한민국 특허출원 10-2009-0065628호에 그 내용이 상세하게 개시되어 있으며, 라켓, 코트, 셔틀콕 모두를 배트민턴 보다 작게 형성하여 좁은 실내공간에서도 경기가 가능하도록 한 것이다.Techminton is a game developed and operated by the applicant of the present application, and its contents are disclosed in detail in Korean Patent Application No. 10-2009-0065628. It is possible to play in the space.
그런데 이러한 배트민턴 또는 테크민턴용 셔틀콕은 새의 깃털을 사용하지만, 일정한 크기와 중량 및 각도를 갖는 깃털을 고르는 것이 용이하지 않으며, 통상 오리 1마리에 좋은 털은 4~6개밖에 쓸 수가 없어서 우수한 셔틀콕 생산에 문제가 있고, 이와 같이 여러 개의 깃털 중 셔틀콕에 사용가능한 깃털을 고르고 정리하는 작업은 일일이 수작업을 거쳐야 하므로 생산성이 저하되며, 생산된 제품 역시 동일한 질량과 동일한 각도로 휘어진 깃털을 사용하기가 용이하지 않으므로 특징이 균일하지 않고 오차를 가지게 되는 등, 품질이 일정하지 않은 문제점이 있었다.By the way, such badminton or techminton shuttlecocks use bird feathers, but it is not easy to select feathers having a certain size, weight and angle, and usually only one or four good feathers for one duck are excellent. There is a problem in the production of shuttlecocks, and thus, selecting and arranging feathers that can be used for shuttlecocks among several feathers requires manual labor and productivity is reduced, and it is difficult to use feathers that are curved at the same mass and at the same angle. Since it is not easy, there is a problem that the quality is not constant, such as the characteristics are not uniform and have an error.
또한, 천연 새의 깃털은 중심의 깃대를 중심으로 깃대의 종단부에 깃가지가 양측으로 뻗어있고 상기 깃가지에 털이 형성된 것으로, 깃대가 지나치게 휘거나 굵기가 일정한 정도에 미치지 못하여 사용할 수 없는 경우가 많았으나 이러한 깃털의 경우에도 깃대를 제외한 부분 즉 깃가지와 털의 상태가 양호한 경우가 많이 있지만 깃대가 만족되지 않으면 사용을 할 수 없어서 폐기되었다.In addition, the feather of the natural bird is that the feather branch extends to both sides and the hair is formed on both ends of the flagpole, with the flagpole being excessively bent or its thickness does not reach a certain degree, but in many cases it cannot be used. In the case of such feathers, many parts except the flagpole, that is, the state of the flagpole and the hair are in good condition, but if the flagpole is not satisfied, it can not be used and discarded.
이러한 천연 깃털을 사용한 셔틀콕의 문제점을 해소하기 위하여 인조깃털을 사용한 셔틀콕에 대한 기술이 공개실용신안 20-2009-0002547(선행기술 1), 공개특허 10-2007-0121416(선행기술 2)등에 제시되고 있다.In order to solve the problem of the shuttlecock using natural feathers, a technique for shuttlecock using artificial feathers is disclosed in Korean Utility Model Publication No. 20-2009-0002547 (prior art 1), and Patent No. 10-2007-0121416 (prior art 2). have.
그러나, 상기 선행기술 1은 깃털이 부착되는 깃대를 하나하나 별개로 형성하여 헤드에 끼워넣도록 하고 있어서 깃대의 각도와 간격이 정확하게 일치되지 않는 문제점이 있으며, 선행기술 2는 깃가지와 털 부분을 각 깃대별로 별개로 형성하지 않고 통으로 형성하므로 비행과정에서 공지의 천연 셔틀콕의 깃가지와 털이 받는 공기의 저항을 받지 못하므로 경기 기준에 적합한 비행운동을 할 수 없게 되는 문제점이 있었다.However, the prior art 1 has a problem that the angle and spacing of the flagpole is not exactly matched to form the flagpole to which the feather is attached one by one separately, so as to fit in the head, the prior art 2 is the angle of the feather branch and hair Because it is not formed separately for each flagpole, it is formed into a barrel, so that the flight of air is not able to perform a flight motion suitable for the competition standards because it does not receive the resistance of air and the hair of a known natural shuttlecock in flight.
또한, 셔틀콕은 라켓과 충돌하기 때문에 셔틀콕의 파손을 방지하기 위해서는 깃대의 탄성이 매우 중요하지만 상기한 종래의 선행기술 1 및 2의 깃대는 모두 깃대의 구조에 대한 구체적인 설명이 없고 사출에 의하여 생산한다는 기재로 보아 단면에 충격을 흡수할만한 공간을 확보하지 못하고 있어서 파손의 우려가 있었다.In addition, since the shuttlecock collides with the racket, the flagpole's elasticity is very important in order to prevent damage of the shuttlecock. However, the flagpoles of the prior arts 1 and 2 described above are produced by injection without any detailed description of the flagpole's structure. From the base material, it was not possible to secure a space for absorbing the impact on the end face, which could cause damage.
아울러, 통상의 인조 셔틀콕은 깃대 종단을 연결하는 원의 접선에 대하여 깃대가 0°로 형성되어 있어서 털의 부착시에 천연깃털과 같은 회전력을 얻지 못하게 되는 문제점이 있었다.In addition, the conventional artificial shuttlecock has a problem that the flagpole is formed at 0 degrees with respect to the tangent of the circle connecting the end of the flagpole, so that when the hair is attached, it is impossible to obtain a rotational force such as natural feathers.
한편, 상기한 천연 혹은 인조 셔틀콕에는 도 2에 나타내는 바와 같이 깃대의 간격 및 각도를 고정하기 위한 고정선(20b)이 깃대(20)에 설치되는데, 상기한 고정선(20b)은 깃대(20) 수명과 셔틀콕의 탄력성 및 타구감을 좋게 해수는 아주 중용한 요소이다. On the other hand, in the above-mentioned natural or artificial shuttlecock, as shown in Fig. 2, a fixing line 20b for fixing the spacing and the angle of the flagpole is installed on the flagpole 20, which is fixed to the flagpole 20 lifespan. To make the shuttlecock more resilient and feel better, seawater is a very important factor.
이러한 고정선(20b)은 통상 깃대와 일체로 사출성형하게 되므로 고정선과 깃대는 동일한 강도를 가지게 되고, 상기 고정선 내향면은 평면으로 형성되는데, 이와 같이 내향면이 평면으로 형성되는 경우에는 강도가 세어서 탄력을 조절하기가 힘들어 셔틀콕이 도 3에 나타내는 바와 같이 라켓(60)과의 충돌로 인한 충격을 흡수하지 못하게 되어 원하는 비행궤적, 속도, 거리를 얻을 수 없게 되고, 셔틀콕의 일부 특히 깃대가 꺽이거나 부러지는 등의 문제점이 발생된다.Since the fixed line 20b is usually injection molded integrally with the flagpole, the fixed line and the flagpole have the same strength, and the inward face of the fixed line is formed in a plane. As it is difficult to adjust the elasticity, the shuttlecock does not absorb the shock caused by the collision with the racket 60, as shown in FIG. 3, and thus the desired flight trajectory, speed, and distance cannot be obtained, Problems such as breaking occur.
즉, 하이클리어나 스메싱을 할 때 라켓으로 타격하면 헤드부(10)부터 맞는게 아니라 깃대(20)와 털 특히 털 끝부분부터 맞게 되고 이로 인하여 깃대(20)가 앞뒤, 좌우로 흔들리게 되는데, 이 과정에서 고정선이 강도가 강한 경우 깃대의 유동을 흡수하지 못하여 도 3에 나타내는 바와 같이 깃대가 고정선 부위에서 꺽이거나 부러지는 문제점이 발생되고, 이와 같이 깃대가 꺽이거나 부러질 경우 비행 중 흔들림이 심하고 비행방향이 흔들리는 등 원하는 비행곡선과 거리를 가지지 못하게 되는 문제점이 있다.In other words, when hitting with a racket during high clearing or smashing, the headpiece 10 is not fitted from the head, but the flagpole 20 and the hair, especially from the tip of the hair, which causes the flagpole 20 to swing back and forth, left and right, In this process, if the fixed line has a strong strength, the flagpole may not absorb the flow of the flagpole, and as shown in FIG. 3, the flagpole may be broken or broken at the fixed line portion. There is a problem in that the flight direction does not have a distance from the desired flight curve, such as shaking.
아울러, 깃대(20)는 최대한 가벼워야 하므로 상기 고정선(20b)을 얇게 형성할 경우 셔틀곡의 내/외측 방향으로의 탄력성이 떨어지므로 타격시 도 4에 나타내는바와 같이 찌그러졌다 원상태로 돌아오는 데 시간이 걸리고 이로 인하여 비행거리와 속도 및 궤적이 만족스럽지 못하고, 타구감 역시 떨어지는 문제점이 있었다.In addition, since the flagpole 20 should be as light as possible, when the fixing line 20b is thinly formed, the elasticity in the inner / outer direction of the shuttle ball is lowered, so as to be crushed as shown in FIG. This takes a flight distance and speed and trajectory is not satisfactory, there was also a problem falling shot.
한편, 인조깃털을 사용한 셔틀콕들은 대부분 털을 부직포나 수지 등을 사용하여 제조하고 있다.Meanwhile, shuttlecocks using artificial feathers are mostly made of nonwoven fabrics or resins.
그러나, 이러한 인조 깃털들은 털(W)이 하나의 판으로 이루어져 있으므로 도 5에 나타내는 바와 같이 털(W)이 엉키는 일이 발생하게 되는데, 이는 하이클리어나 스메싱을 할 때 라켓으로 타격하면 헤드(10)부부터 맞는게 아니라 깃대(20)와 털(W)부터 맞게 되고 이로 인하여 깃대(20)가 앞뒤, 좌우로 흔들리기 때문에 털(W)이 엉키게 되고, 이와 같이 털(W)이 엉키는 경우 천연깃털은 털이 하나하나 분리되므로 큰 문제가 발생하지 않지만 통상의 인조 깃털은 털(W)이 시트형상으로 한판으로 형성되므로 엉킬 경우 비행 중 흔들림이 심하고 비행방향이 흔들리는 등 원하는 비행곡선과 거리를 가지지 못하게 되는 문제점이 있다.However, since these artificial feathers are composed of a single plate of hair W, the hair W is tangled as shown in FIG. 5, which is caused by hitting the racket when high clearing or smashing the head 10. ) Since the flagpole 20 and the hair (W) is not fitted from the first part, and the flagpole 20 is swayed back and forth and left and right because of this, the hair (W) is tangled, and thus the hair (W) is tangled Natural feathers do not cause a big problem because the hairs are separated one by one, but the normal artificial feathers are formed in a sheet-like sheet of hair (W), so if the tangled, they do not have a desired flight curve and distance such as severe shaking during flight and flight direction shaking. There is a problem that can not be.
본 발명은 인조 셔틀콕의 깃대가 탄력성이 나빠서 사용 중 타구감이 나쁜 문제점을 개선하면서 종래 천연깃털 중 깃대문제로 인하여 사용할 수 없었던 깃털의 일부를 사용할 수 있도록 하는 셔틀콕을 제공하는 데 목적이 있다.An object of the present invention is to provide a shuttlecock that can use a portion of the feather that was not available due to the flagpole problem of the conventional natural feathers while improving the problem of bad feel during use due to bad elasticity of the artificial shuttlecock.
아울러, 셔틀콕의 타격시 셔틀콕의 파손을 방지하면서 비행궤적과 거리 및 속도에 중요한 역할을 하는 고정선을 가벼우면서 탄력성이 우수하도록 하여 셔틀콕의 수명이 길어지도록 하면서 우수한 품질을 갖도록 하고, 종래 인조깃털이 갖는 털 엉킴 현상을 방지하여 타격시 비행속도, 궤적 및 거리가 만족스럽도록 하는 데 다른 목적이 있다.In addition, while preventing the damage of the shuttlecock during the strike of the shuttlecock, the fixed line that plays an important role in the flight trajectory, distance and speed is light and excellent in elasticity so that the life of the shuttlecock is long and has excellent quality, and the conventional artificial feathers Another purpose is to prevent hair entanglement so that flight speed, trajectory and distance are satisfactory at the time of hitting.
상기한 목적을 달성하기 위한 본 발명의 특징은, 헤드, 상기 헤드와 결합되는 베이스에 다수개가 일정한 간격을 가지면서 헤드의 중심선으로부터 일정한 각도를 갖도록 일체로 연장형성된 깃대; 상기 깃대의 종단에 부착되는 털로 구성되는 셔틀콕에 있다.Features of the present invention for achieving the above object, the base, the flagpole is integrally extended to have a predetermined angle from the centerline of the head with a plurality of bases having a predetermined distance to the base coupled to the head; Shuttlecock composed of hair attached to the end of the flagpole.
상기에서 깃대의 내향면 중심에 길이방향을 따라 홈이 형성되도록 사출성형되고, 깃대의 중심에 고정띠가 일체로 사출성형되며, 상기 깃대는 셔틀콕의 중심으로부터 깃대 종단을 연결하는 원의 접선에 대하여 0-30°각도를 갖도록 형성된다.The injection molding is formed so as to form a groove along the longitudinal direction in the center of the inner surface of the flagpole, the fixing band is integrally injection molded in the center of the flagpole, the flagpole with respect to the tangent of the circle connecting the end of the flagpole from the center of the shuttlecock It is formed to have an angle of 0-30 degrees.
그리고, 상기 털과 대응되는 깃대의 상부 좌우측에 깃가지를 대칭으로 경사지게 서로 이격되도록 형성하고, 상기 깃가지 종단에 고리를 형성한 것을 특징으로 한다.Further, the feather branches are formed to be spaced apart from each other in an symmetrical inclination on the upper left and right sides of the flagpole corresponding to the hair, and a ring is formed at the end of the feather branch.
또한, 털은 미세원사를 섬유상으로 열융착 성형한 것이나, 발포하여 형성한 것 혹은 천연 깃털의 종단부 즉 깃털의 깃대를 절단한 종단부 중에서 택일하여 사용한다.In addition, the hair is used either by thermally fusion-molding microfibers in a fibrous form, by foaming, or by terminating portions of natural feathers, that is, terminating portions of feather feathers.
아울러, 본 발명은 상기 깃대의 간격과 각도를 고정하기 위하여 깃대와 일체로 형성되는 고정선을 길이방향으로 내측에는 홈이 형성되고 외측으로 돌출된 모양을 갖도록 형성하는 것을 특징으로 한다.In addition, the present invention is characterized in that the fixing line formed integrally with the flagpole in order to fix the spacing and angle of the flagpole, the groove is formed on the inner side in the longitudinal direction and has a shape protruding outward.
상기한 바와 같은 구성을 갖는 본 발명에 의하면, 셔틀콕에서 가장 중요한 무게, 깃대 간격, 원지름, 각도, 탄력조건이 모두 우수한 셔틀콕을 제공할 수 있게 된다.According to the present invention having the configuration as described above, it is possible to provide a shuttlecock excellent in all the most important weight, flagpole spacing, diameter, angle, elasticity conditions in the shuttlecock.
그리고 깃대의 셔틀콕 내향면 즉 털과 접착되는 면으로 홈을 파서 굵기는 적당하되 무게를 적게 나가게 함으로, 깃대 굵기에 비해 깃대가 얇으면서 탄성이 생기도록 함으로서 타구감을 개선하고 무게를 감소시키며 라켓과 충돌시 파손율을 감소시킬 수 있고, 상기 깃대에 홈을 형성함으로서 종래 깃대문제로 사용할 수 없었던 깃털의 깃가지와 털부분만을 절단하여 접착하여 사용할 수 있으므로, 깃털 활용도를 높일 수 있게 되는 효과가 있다.In addition, by making grooves into the shuttlecock inward plane of the flagpole, that is, the surface that is bonded to the hair, the thickness is moderate but the weight is reduced.The flagpole is thinner and more elastic than the thickness of the flagpole to improve hitting feeling, reduce weight, and collide with the racket. When the damage rate can be reduced, and by forming a groove in the flagpole can be used to cut and glue only the feather branch and hair portion of the feather that could not be used in the conventional flagpole problem, there is an effect that can increase the utilization of the feather.
아울러, 깃대를 고정띠를 포함하여 하나로 사출 성형함으로서 깃대, 각도, 원지름까지 정확한 셔틀콕을 제공할 수 있게 되어 정확한 거리로 비행을 할 수 있게 된다.In addition, by injection molding the flagpole into a single one, including a fixed belt, it is possible to provide an accurate shuttlecock to the flagpole, angle, and diameter to fly at the correct distance.
그리고, 털을 원사를 압착하여 시트형으로 형성할 때 깃대와 연결되는 중심선, 가지선을 더 압착하여 털의 탄력성 및 형태안정성을 확보하고, 털의 두께는 중심선을 중심으로 해서 밖으로 점점 얇게 하여, 둔탁함을 줄이고 좋은 느낌을 주는데 도움을 준다.When the yarn is formed into a sheet form by compressing the yarn, the center line and branch lines connected to the flagpole are further compressed to secure the elasticity and form stability of the hair, and the thickness of the hair is gradually thinned outward from the center line, resulting in dullness. It helps to reduce the weight and give a good feeling.
또한, 고정선에 홈이 형성되면서 고정선이 가벼워져서 셔틀콕 전체가 가벼워지게 됨으로 인하여 타격시 충격이 사용자의 팔꿈치 등으로 전가되는 테니스엘보 등이 발생하지 않게 되고, 상기한 인조 깃털이 라켓과의 타격시 충격을 충분히 흡수하면서 우수한 탄성을 가지므로 셔틀콕의 깃대 꺽임이나 부러짐이 발생하지 않아서 셔틀콕의 수명이 길어지고 비행궤적, 거리 속도가 저하되는 일이 발생하지 않게되는 효과가 있다.In addition, as the groove is formed in the fixed line, the fixed line becomes lighter, and thus the whole shuttlecock becomes lighter, so that the impact when the impact is transferred to the elbow of the user does not occur, and the impact of the artificial feather hits the racket. Since it has sufficient elasticity and has excellent elasticity, the flagpole's flagpole is not broken or broken so that the life of the shuttlecock is prolonged and flight trajectory and distance speed are not reduced.
아울러, 인조 깃털을 이용한 셔틀콕에서 시트 상의 털이 타격시 서로 엉키지 않게 되어 비행 중 흔들림 등으로 인하여 원치 않은 곳으로 비행하는 일이 발생하지 않게 된다.In addition, the shuttlecock using the artificial feather is not tangled with each other when the hair on the sheet is not entangled with each other, so that the flight to the unwanted place due to shaking during flight.
도 1은 일반적인 셔틀콕을 나타내는 사시도1 is a perspective view showing a general shuttle cock
도 2는 종래의 인조 셔틀콕을 나타내는 정면도2 is a front view showing a conventional artificial shuttlecock
도 3 및 도 4는 셔틀콕 타격시 셔틀콕 변화를 나타내는 도면3 and 4 is a view showing the change of shuttlecock when the shuttlecock hit
도 5는 종래 인조셔틀콕의 털엉킴 구조를 나타내는 도면5 is a view showing a hair tangled structure of a conventional artificial shuttlecock
도 6은 본 발명의 제 1실시예에 따른 셔틀콕을 나타내는 정면도6 is a front view showing a shuttle cock according to a first embodiment of the present invention;
도 7은 도 6의 횡단면도7 is a cross-sectional view of FIG. 6
도 8은 본 발명의 제 1실시예에 따른 깃대와 헤드를 나타내는 단면도8 is a cross-sectional view showing the flagpole and the head according to the first embodiment of the present invention.
도 9는 도 8의 깃대 단면도9 is a cross-sectional view of the flagpole of FIG.
도 10은 본 발명의 제 1실시예에 따른 깃대의 설치각도를 나타내는 도면10 is a view showing an installation angle of the flagpole according to the first embodiment of the present invention
도 11은 본 발명의 제 1실시예에 따른 털을 나타내는 평면도11 is a plan view showing the hair according to the first embodiment of the present invention
도 12는 도 11의 단면도12 is a cross-sectional view of FIG.
도 13은 본 발명의 제 1실시예에 따른 털을 깃대에 부착하는 것을 나타내는 단면도FIG. 13 is a cross-sectional view illustrating attaching hair to a flagpole according to a first embodiment of the present invention. FIG.
도 14는 본 발명의 제 1실시예에 따른 깃대에 천연 털을 부착하는 것을 나타내는 단면도14 is a cross-sectional view showing the attachment of natural hair to the flagpole according to the first embodiment of the present invention
도 15는 본 발명의 제 3실시예에 따른 셔틀콕을 나타내는 단면도15 is a cross-sectional view showing a shuttle cock according to a third embodiment of the present invention.
도 16은 도 15의 털 확대 도면16 is an enlarged view of the hair of FIG.
도 17은 도 16의 A-A선 단면도17 is a cross-sectional view taken along the line A-A of FIG.
도 18은 본 발명의 고정선 구조를 나타내는 단면도18 is a cross-sectional view showing a fixed line structure of the present invention.
*도면의 주요부분에 대한 부호의 설명** Description of the symbols for the main parts of the drawings *
10 : 헤드 20 : 깃대부10 head 20 flagpole
50 : 털50: fur
이하 본 발명의 실시 예를 하기에서 첨부된 도면을 참조하여 살펴본다.Hereinafter, an embodiment of the present invention will be described with reference to the accompanying drawings.
제 1실시예First embodiment
본 발명에 따른 셔틀콕은 도 6 내지 도 11에 나타내는 바와 같이 헤드(30)와 결합되는 베이스(42)에 다수개가 일정한 간격을 가지면서 헤드(30)의 중심선으로부터 일정한 각도를 갖도록 일체로 연장형성하고 각각의 단면은 삼각형 모양으로 셔틀콕의 내향면 중심에 길이방향을 따라 홈(46)이 형성되도록 사출성형된 깃대(40), 원사를 시트 상으로 형성하여 상기 깃대(40)의 종단에 각각 접착되며 상기 깃대(40)와 결합되는 중심선(55), 깃가지(52), 빗살선(53)을 포함하는 털(50)을 포함하여 구성된다.6 to 11, the shuttle cock is integrally formed to have a constant angle from the centerline of the head 30 while having a plurality of regular intervals in the base 42 is coupled to the head 30 as shown in FIGS. Each cross section has a triangular shape, the injection-molded flagpole 40, the yarn is formed in the form of a sheet to form a groove 46 in the longitudinal direction in the center of the inward surface of the shuttlecock, respectively bonded to the end of the flagpole 40 The hairline 50 includes a centerline 55 coupled to the flagpole 40, a feather branch 52, and a comb line 53.
상기에서, 깃대(40)의 중간에는 고정띠(48)가 일체로 사출형성되며 상기 고정띠(48)는 라켓으로 타격했을 때 깃대(40)가 안,밖 및 좌우로 이탈되는 것을 방지하고 고정시키는 역할을 하는데, 이와 같이 깃대(40)를 고정하는 이유는 깃대(40) 간격이 달라지고 각도가 달라지면 셔틀콕이 흔들려서 원하는 진로와 거리만큼 주행을 할 수 없게 되기 때문이다.In the above, in the middle of the flagpole 40, the fixing band 48 is integrally formed and the fixing band 48 prevents the flagpole 40 from being separated from inside, outside and left and right when being hit by the racket. The reason for fixing the flagpole 40 in this way is that if the spacing of the flagpole 40 is changed and the angle is changed, the shuttlecock is shaken to travel as much as the desired course and distance.
이에 따라 고정띠(48)는 사출성형을 통하여 일정한 치수로 형성하며, 셔틀콕의 중심선과 수평한 방향의 길이는 0.5~3mm, 수직한 방향의 길이는 0.2~2mm로 성형하는데, 상기 고정띠(48)가 범위보다 굵으면 타구감이 떨어지고, 무게 조절하기 힘들고, 범위보다 가늘면 탄성이 떨어지고 변형이 일어난다. 왜냐하면 하이클리어나 스매쉬를 했을 때 깃대부터 맞기 때문에 깃대의 탄력성이 있어야 타구감이 좋기 때문이다.Accordingly, the fixing band 48 is formed to a certain dimension through the injection molding, the length in the horizontal direction with the center line of the shuttlecock is molded into 0.5 ~ 3mm, the length in the vertical direction is 0.2 ~ 2mm, the fixing belt 48 ) Is thicker than the range, the feeling of hitting falls, it is difficult to control the weight. This is because it is good to hit with the flagpole when it is high clear or smashed.
그리고, 깃대(40)는 도 10에 나타내는 바와 같이 셔틀콕의 원주를 따른 접선으로부터 0~30°로 비틀어지게 형성되어 바람에 따라 회전수를 늘리기 위해 각도를 줄이거나 늘릴 수 있으며, 이는 성형과정에서 결정된 각도로 성형되는 것일 뿐 사용중 변형되는 것은 아니다.And, the flagpole 40 is formed to be twisted from 0 to 30 ° from the tangent along the circumference of the shuttle cock as shown in Figure 10 can be reduced or increased the angle to increase the number of revolutions according to the wind, which is determined during the molding process It is molded at an angle, but not deformed during use.
그리고, 상기 깃대(40)는 그 단면이, 이등변 삼각형 모양 또는 이등변사각형모양 또는 호모양을 포함하여 중심을 기준으로 대칭형성되는데, 셔틀콕에서 라켓에 맞는 부분이 깃대(40)와 털(50)이기 때문에 깃대(40)는 도 9에 나타내는 바와 같이 삼각형 특히 셔틀콕의 외측 두면이 이등변인 이등변 삼각형 모양이 바람직하며, 이와 같이 삼각형으로 형성할 경우 안팎, 좌우 뒤틀어짐을 막을 수 있고, 탄력이 생긴다.In addition, the flagpole 40 has a cross-section, including an isosceles triangle shape or an isosceles triangle shape or arc shape, is symmetrically formed with respect to the center, and the portion corresponding to the racket in the shuttlecock is the flagpole 40 and the hair 50. Therefore, the flagpole 40 is preferably an isosceles triangle shape in which the outer two sides of the shuttlecock are isosceles, as shown in FIG. 9, and when formed in this way, the flagpole can be prevented from inside, outside, left and right twisting, and elasticity is generated.
그리고, 상기한 깃대의 종단 직경은 6~7cm가 적당하다.The end diameter of the flagpole is preferably 6 to 7 cm.
한편, 상기한 베이스(42)에는 헤드(30)와 접하는 면에 하부로 체결구(41)가 일체로 돌출형성되어 헤드(30)에 꽂히도록 한 것으로, 상기 체결구(41)는 하부로 원통형으로 돌출형성된 돌출벽(41a)과 상기한 돌출벽(41a)의 하종단에 외부로 돌출형성된 고정돌기(41b)로 구성되며, 상기한 체결구(41)가 체결되는 헤드(30)에는 돌출벽(41a)과 대응되는 형상의 삽입홈(46)이 형성되어, 돌출벽(41a)이 삽입홈(46)으로 삽입되어 종단의 고정돌기(41b)에 의하여 고정되도록 한다.On the other hand, the base 42 is formed so that the fastener 41 is integrally protruded to the bottom in contact with the head 30 to be plugged into the head 30, the fastener 41 is cylindrical to the bottom And a fixing protrusion 41b protruding outwardly from the lower end of the protruding wall 41a and protruding wall 41 to which the fastener 41 is fastened. An insertion groove 46 having a shape corresponding to the 41a is formed, so that the protruding wall 41a is inserted into the insertion groove 46 to be fixed by the fixing protrusion 41b at the end.
그리고, 상기에서 털(50)을 형성하는 재료는 폴리에스테르, 나일론, 실크, 면 등의 원사로서 실을 만드는 재료면 어떠한 것이든 사용가능하며, 셔틀콕의 털은 아주 가벼워야 하므로 저 데니어(5데니어 이하)를 사용하여 1㎡당 20~100g정도 되게 얇게 깔고, 가벼우면서 어느 정도 힘도 있어야 하므로 얇게 깐 원사에 열을 주어 원사가 융착에 의하여 흐트러지지 않도록 한다.And, the material for forming the hair 50 in the above can be used any material that makes a yarn as a yarn, such as polyester, nylon, silk, cotton, etc. Shuttlecock hair should be very light, so low denier (5 denier) Using less than 20 ~ 100g per 1㎡, and light and have some strength, so heat the thinly coated yarn so that it will not be distracted by fusion.
이때, 열에 쉽게 녹지 않는 원사의 경우 원사를 시트형으로 얇게 배치한 후 그 일면 혹은 양면에 본드, 라텍스, 비닐 등의 열에 의하여 융착 가능한 재료를 더 적층 혹은 도포하여 성형한다. 아울러, 이와 같이 라텍스, 비닐 등을 더 융착하는 것은 원하는 경도를 주기 위하여 열융착 가능한 원사에도 적용이 가능하다.In this case, in the case of the yarn that is not easily dissolved in heat, the yarn is thinly disposed in a sheet form, and then laminated or coated with a heat-bondable material such as bond, latex, and vinyl on one or both surfaces thereof, and then molded. In addition, further fusion of latex, vinyl and the like may be applied to a yarn that can be heat-sealed to give a desired hardness.
이와 같이 열 융착되어 형성된 털(50)은 도 11 및 도 12에 나타내는 바와 같이 가로 최장길이가 1~2.5cm, 세로 최장길이가 2.5~5cm로 하고 두께는 0.5~1.5mm가되도록 하며 중심에서 가장자리로 갈수록 얇아지도록 성형하며, 상기 털(50)을 구성하는 중심선(55)은 털(50) 최대 두께보다 0.2~0.5mm를 더 얇게 형성되면서 깃대(40)와 결합되는 면의 중심선(55) 폭은 깃대(40)의 폭을 수용할 수 있는 치수로 형성되고 깃대(40)와 결합되지 않는 면의 중심선(55)은 깃대(40)폭보다 좁게 형성하며, 깃가지(52)는 털(50) 최대 두께보다 0.2~0.5mm 더 얇게 형성되며, 깃가지(52)에서 다시 뻗어나가는 빗살선(53)은 털(50) 최대 두께보다 0.1~0.2mm더 얇게 형성하며, 이러한 털(50)의 형상에 맞도록 열 융착을 위한 금형을 제작한다.Thus, the hair 50 formed by heat-sealing has a horizontal longest length of 1 to 2.5 cm, a vertical longest length of 2.5 to 5 cm, and a thickness of 0.5 to 1.5 mm as shown in FIGS. 11 and 12. Shaped so as to become thinner, the center line 55 constituting the hair 50 is 0.2 to 0.5mm thinner than the maximum thickness of the hair 50, while the center line 55 width of the surface combined with the flagpole 40 The centerline 55 of the surface is formed to the size that can accommodate the width of the flagpole 40 and is not coupled to the flagpole 40 is formed narrower than the width of the flagpole 40, the flagpole 52 is the hair 50 It is formed 0.2 ~ 0.5mm thinner than the maximum thickness, and the comb line 53 extending again from the feather branch 52 is formed 0.1 ~ 0.2mm thinner than the maximum thickness of the hair 50, the shape of the hair 50 Make a mold for thermal fusion to fit.
상기에서 금형은 120~250℃로 0.5-5초 시트를 가압한다.The mold presses the sheet for 0.5-5 seconds at 120 to 250 ° C.
한편, 상기한 바와 같이 일체로 사출성형된 깃대(40)에 도 13에 나타내는 바와 같이 원사를 시트형으로 성형한 털(50)을 접착할 수도 있지만, 도 14에 나타내는 바와 같이 천연깃털의 깃대(55a) 종단을 일정한 모양으로 절단한 천연 털(50)을 상기와 같이 일체로 사출성형한 깃대(40)에 접착하여 사용할 수도 있다.On the other hand, as shown in Fig. 13, the hair 50 formed of a sheet-like yarn may be bonded to the flagpole 40 which is injection molded integrally as described above, but as shown in Fig. 14, the flagpole 55a of natural feathers. ) The natural hair 50 cut into a certain shape can be bonded to the flagpole 40 which is injection molded integrally as described above.
또한 상기한 털은 폴리프로필렌(PP), 폴리에틸렌(PE), 우레탄 등으로 발포 성형되어 깃대에 접착될 수도 있다.In addition, the hair may be foam-molded with polypropylene (PP), polyethylene (PE), urethane, or the like and adhered to the flagpole.
제 2실시예Second embodiment
셔틀콕은 도 15 내지 도 18에 나타내는 바와 같이 크게, 헤드(30), 헤드(30)와 결합되는 깃대(40), 상기 깃대(40)의 상부 좌우측에 형성되는 털(50)로 구성된다.The shuttlecock is composed of a head 30, a flag pole 40 engaged with the head 30, and a hair 50 formed on the upper left and right sides of the flag pole 40, as shown in Figs.
상기에서 깃대(40)는 도 15 내지 도 17에 나타내는 바와 같이 원통형의 베이스(42)에 다수개의 깃대(40)를 일정한 간격을 가지면서 헤드(30)의 중심선으로부터 일정한 각도를 갖도록 일체로 연장형성하고 이와 같이 연장형성된 깃대(40) 각각의 단면은 삼각형 모양으로 셔틀콕의 내향면 중심에 길이방향을 따라 홈(46)이 형성되도록 사출성형된다.15 and 17, the flagpole 40 is integrally formed to have a predetermined angle from the centerline of the head 30 while having a plurality of flagpoles 40 at regular intervals on the cylindrical base 42. The cross section of each of the flagpoles 40 formed as described above is injection-molded so that the grooves 46 are formed along the longitudinal direction at the center of the inward surface of the shuttlecock in a triangular shape.
그리고, 상기 깃대(40)에는 중심에 홈(47a)이 형성된 깃가지(47)가 털(50)과 대응되는 깃대(40)의 상부 좌우측에 대칭으로 경사지게 서로 이격되도록 더 형성되고, 그 종단에는 고리(48)가 형성된다.In addition, the flagpole 40 is further formed to be spaced apart from each other to be symmetrically inclined symmetrically to the upper left and right sides of the flagpole 40 corresponding to the hair 50 is formed with a groove (47a) in the center, the end of the ring 48 is formed.
또한, 상기 깃대(40)의 간격과 각도를 고정하기 위하여 깃대(40)와 일체로 형성되는 고정선(49)은 도 18에 나타내는 바와 같이 그 길이방향으로 중심을 절곡하여 내측으로 홈(49a)이 형성되고 외측으로 돌출된 모양을 갖도록 형성한다.Moreover, in order to fix the space | interval and angle of the said flagpole 40, the fixed line 49 integrally formed with the flagpole 40 is bent the center in the longitudinal direction, as shown in FIG. It is formed to have a shape that is formed and protrudes outward.
이러한 고정선(49)은 종방향 단면의 세로길이가 0.3~3mm, 가로길이가 0.3~3mm이며 원하는 타구감에 따라 그 가로 및 세로 길이를 조절하여 사용할 수 있다. The fixed line 49 has a longitudinal length of 0.3 to 3mm, a transverse length of 0.3 to 3mm, and can be used by adjusting the horizontal and vertical lengths according to a desired hitting feel.
그 예로서 세로길이가 길고 가로길이가 짧으면 강도가 약해서 부드러워지고, 반대의 경우 강도가 높아져서 단단해진다.For example, if the length is long and the length is short, the strength is weak and soft, and in the opposite case, the strength is high and rigid.
그리고, 상기 털(50)은 시트 상으로 형성하여 상기 깃대(40)의 깃대(40) 종단에 접착되고 깃대(40)와 결합을 용이하게 하기 위하여 중심에는 다른 부분보다 두께가 얇게 중심선(미도시)을 형성한다.In addition, the hair 50 is formed in a sheet shape and adhered to the end of the flagpole 40 of the flagpole 40 and has a centerline (not shown) at a thickness thinner than other portions in the center to facilitate engagement with the flagpole 40. ).
이와 같이 형성된 셔틀콕을 타격하는 경우, 상기한 깃대(40)의 고리(48)가 인접한 깃대(40)의 깃가지(47)를 잡아주어 털(50)의 배치위치가 내측과 외측이 서로 뒤섞이거나 바뀌는 일이 일어나지 않음으로 털(50)이 엉클어지는 것을 방지하게 되며, 이와 같이 털(50)의 엉클어짐이 방지될 경우 원하는 비행곡선과 거리를 얻을 수 있게 된다.In the case of hitting the shuttlecock formed in this way, the ring 48 of the flagpole 40 to hold the feather branch 47 of the adjacent flagpole 40 so that the arrangement position of the hair 50 is mixed or changed with each other inside and outside It is possible to prevent the hair 50 from being entangled by not happening, and thus, when the hair 50 is prevented from being entangled, a desired flight curve and a distance can be obtained.
이는 하이클리어나 스메싱을 할 때, 라켓으로 타격하면 헤드부(30)부터 맞는게 아니라 깃대(40)와 털(50)부터 맞게 되고 이로 인하여 깃대(40)가 앞뒤, 좌우로 흔들리기 때문에 털(50)의 털이 엉키게 된다.This is because when the high clearing or smashing, hitting the racket does not fit from the head portion 30, but from the flagpole 40 and the hair 50, and because of this the flagpole 40 is shaken back and forth, left and right, because the hair ( 50) hairs are tangled.
이와 같이 털이 엉키는 경우 천연깃털은 털이 하나하나 분리되므로 큰 문제가 발생하지 않지만 통상의 인조 깃털은 털이 시트형상으로 형성되므로 엉킬 경우 비행 중 흔들림이 심하고 비행방향이 흔들리는 등 원하는 비행곡선과 거리를 가지지 못하게 되는 문제점이 있다.In this way, if the hair is tangled, the natural feathers are separated one by one, so no big problem occurs. However, since the normal artificial feather is formed in the shape of a hair sheet, the tangled feathers do not have a distance from the desired flight curve, such as severe shaking during flight and flight direction. There is a problem.
또한, 하이클리어나 스메싱을 할 때, 라켓으로 타격하면 헤드부(30)부터 맞는게 아니라 깃대(40)와 털(50) 특히 깃대(40) 및 털(50)의 끝부분부터 맞게 되고 이로 인하여 깃대(40)가 앞뒤, 좌우로 흔들리게 되는데, 상기한 고정선(49)이 홈(49a)에 의하여 얇게 형성되어 탄성을 가지면서 '<'형 단면구조로 인하여 필요한 강도도 가지기 때문에 타격시 셔틀콕이 빨리 원위치로 회복되면서 깃대의 꺽임이나 부러짐이 발생하지 않게 된다.In addition, when high clearing or smashing, hitting with the racket does not fit from the head 30, but from the end of the flagpole 40 and the hair 50, especially the flagpole 40 and hair 50, Flagpole 40 is shaken back and forth, left and right, the fixed line 49 is formed thinly by the groove (49a) has elasticity and has the necessary strength due to the '<' shaped cross-section shuttle shuttle when hitting As soon as it is returned to its original position, the flagpole is not broken or broken.

Claims (10)

  1. 셔틀콕에 있어서, In shuttlecock,
    헤드(30), Head 30,
    상기 헤드(30)와 결합되는 베이스(42)에 다수개의 깃대(40)가 일정한 간격을 가지면서 셔틀콕의 원주를 따른 접선으로부터 0~30°각도 비틀어지도록 일체로 연장형성된 깃대(40),Flagpole 40 which is integrally formed to be twisted at an angle of 0 ~ 30 ° from the tangent along the circumference of the shuttlecock while the plurality of flagpoles 40 are fixed to the base 42 coupled to the head 30,
    상기 깃대(40)의 깃대(40) 종단에 일체로 성형되거나 접착되는 털(50)로 구성되는 것을 특징으로 하는 셔틀콕.Shuttlecock, characterized in that consisting of a hair (50) integrally molded or bonded to the end of the flagpole (40) of the flagpole (40).
  2. 제 1항에 있어서, 상기 깃대(40)에는 셔틀콕의 내향면 중심에 길이방향을 따라 홈(46)이 형성되는 것을 특징으로 하는 셔틀콕.The shuttlecock according to claim 1, wherein the flagpole has a groove 46 formed in a longitudinal direction at the center of the inward surface of the shuttlecock.
  3. 제 1항에 있어서, 상기 깃대(40)의 단면은 이등변 삼각형 모양 또는 이등변사각형모양 또는 호모양을 포함하여 중심을 기준으로 대칭형성되는 것을 특징으로 하는 셔틀콕.The shuttlecock according to claim 1, wherein the cross section of the flagpole (40) is symmetrical about the center, including an isosceles triangle shape or an isosceles triangle shape or arc shape.
  4. 제 1항에 있어서, 상기 깃대(40)의 중간에는 고정띠(48)가 일체로 사출형성되는 것을 특징으로 하는 셔틀콕.The shuttlecock according to claim 1, wherein the fixing band is integrally formed in the middle of the flagpole.
  5. 제 1항에 있어서, 상기 털(50)은 5데니어 이하의 원사를 사용하여 1㎡당 20~100g되게 얇게 깔고, 깃대(40)와 결합되는 중심선(55), 깃가지(52), 빗살선(53) 및 털(50)의 형상에 대응되도록 열 융착에 의하여 시트상으로 형성되고 절단 성형되는 것을 접착하는 것을 특징으로 하는 셔틀콕.According to claim 1, wherein the hair 50 is thinned 20 to 100g per square meter using less than 5 denier yarn, the centerline 55, the feather 52, combined with the flagpole 40, comb line ( 53) and a shuttlecock characterized in that the adhesive is formed by cutting and forming a sheet by heat fusion so as to correspond to the shape of the hair (50).
  6. 제 1항에 있어서, 상기 털(50)은 발포 성형되어 접착되는 것을 특징으로 하는 셔틀콕.The shuttlecock according to claim 1, wherein the hair (50) is foam molded and bonded.
  7. 제 2항에 있어서, 상기 털(50)은 천연깃털의 깃대 종단을 절단성형하여 상기 깃대(40)의 종단에 접착되는 것을 특징으로 하는 배드민턴 셔틀콕.The badminton shuttlecock according to claim 2, wherein the hair (50) is formed by cutting and cutting the end of the flagpole of the natural feather to the end of the flagpole (40).
  8. 헤드에 일정한 간격과 각도로 꽂힌 깃대 상부에 털가 접착되는 셔틀콕에 있어서, Shuttlecock in which the hair is glued to the upper portion of the flagpole is inserted into the head at a constant interval and angle,
    상기 깃대와 일체로 형성되는 고정선을 길이방향 내측으로 홈이 형성되고 외측으로 돌출된 모양을 갖도록 형성하는 것을 특징으로 하는 셔틀콕.Shuttlecock, characterized in that the fixing line formed integrally with the flagpole to have a shape in which the groove is formed in the longitudinal direction and protruded outward.
  9. 헤드에 일정한 간격과 각도로 꽂힌 깃대의 상부에 털이 접착된 셔틀콕에 있어서,In the shuttlecock hair-bonded to the top of the flagpole inserted at regular intervals and angles to the head,
    상기 털과 대응되는 깃대의 상부 좌우측에 깃가지를 대칭으로 경사지게 서로 이격되도록 형성하고, 상기 깃가지 종단에 고리를 형성한 것을 특징으로 하는 셔틀콕.Shuttlecocks are formed on the upper left and right sides of the flagpole corresponding to the hair so as to be spaced apart from each other inclined symmetrically, and the end of the feather branch formed a ring.
  10. 제 9항에 있어서, The method of claim 9,
    상기 깃대와 일체로 형성되는 고정선을 길이방향 내측으로 홈이 형성되고 외측으로 돌출된 모양을 갖도록 형성하는 것을 특징으로 하는 셔틀콕.Shuttlecock, characterized in that the fixing line formed integrally with the flagpole to have a shape in which the groove is formed in the longitudinal direction and protruded outward.
PCT/KR2012/008637 2011-10-22 2012-10-22 Shuttlecock WO2013058621A1 (en)

Applications Claiming Priority (6)

Application Number Priority Date Filing Date Title
KR20-2011-0009404 2011-10-22
KR2020110009404U KR200460073Y1 (en) 2011-10-22 2011-10-22 Shuttlecock
KR20-2011-0010694 2011-12-01
KR2020110010694U KR200461940Y1 (en) 2011-12-01 2011-12-01 Shuttlecock
KR2020110010692U KR200461941Y1 (en) 2011-12-01 2011-12-01 Shuttlecock
KR20-2011-0010692 2011-12-01

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WO2013058621A1 true WO2013058621A1 (en) 2013-04-25

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104436595A (en) * 2014-12-27 2015-03-25 贵阳华合仁信息技术有限公司 Badminton ball
JP5976907B1 (en) * 2015-08-17 2016-08-24 株式会社コスモ精機 Badminton shuttle

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5926676U (en) * 1982-08-13 1984-02-18 西村 嘉信 Shuttlecock for badminton competition
KR20090121465A (en) * 2008-05-22 2009-11-26 이재성 Divisible and combinable badminton shuttlecock
EP2236176A1 (en) * 2008-01-08 2010-10-06 Mizuno Corporation Shuttlecock for badminton
KR20110040331A (en) * 2009-10-14 2011-04-20 김형주 Divisible and combinable badminton shuttlecock
KR20110052260A (en) * 2009-11-12 2011-05-18 김두림 Badminton shuttlecock

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5926676U (en) * 1982-08-13 1984-02-18 西村 嘉信 Shuttlecock for badminton competition
EP2236176A1 (en) * 2008-01-08 2010-10-06 Mizuno Corporation Shuttlecock for badminton
KR20090121465A (en) * 2008-05-22 2009-11-26 이재성 Divisible and combinable badminton shuttlecock
KR20110040331A (en) * 2009-10-14 2011-04-20 김형주 Divisible and combinable badminton shuttlecock
KR20110052260A (en) * 2009-11-12 2011-05-18 김두림 Badminton shuttlecock

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104436595A (en) * 2014-12-27 2015-03-25 贵阳华合仁信息技术有限公司 Badminton ball
JP5976907B1 (en) * 2015-08-17 2016-08-24 株式会社コスモ精機 Badminton shuttle
JP2017038634A (en) * 2015-08-17 2017-02-23 株式会社コスモ精機 Badminton shuttlecock

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