WO2014013197A2 - Badminton shuttlecock - Google Patents

Badminton shuttlecock Download PDF

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Publication number
WO2014013197A2
WO2014013197A2 PCT/FR2013/051720 FR2013051720W WO2014013197A2 WO 2014013197 A2 WO2014013197 A2 WO 2014013197A2 FR 2013051720 W FR2013051720 W FR 2013051720W WO 2014013197 A2 WO2014013197 A2 WO 2014013197A2
Authority
WO
WIPO (PCT)
Prior art keywords
wing
rods
plate
badminton
steering wheel
Prior art date
Application number
PCT/FR2013/051720
Other languages
French (fr)
Other versions
WO2014013197A3 (en
Inventor
Patrick Doby
Joël TRIBOULT
Original Assignee
Decathlon
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
Application filed by Decathlon filed Critical Decathlon
Priority to CN201390000753.1U priority Critical patent/CN204972945U/en
Priority to GB1500691.9A priority patent/GB2519687B/en
Publication of WO2014013197A2 publication Critical patent/WO2014013197A2/en
Publication of WO2014013197A3 publication Critical patent/WO2014013197A3/en

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Classifications

    • 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
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63BAPPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B2209/00Characteristics of used materials
    • A63B2209/02Characteristics of used materials with reinforcing fibres, e.g. carbon, polyamide fibres

Definitions

  • the present invention relates to the field of jdminton wheels.
  • a badminton shuttlecock is a projectile that is used in the sports of racket called "badminton".
  • the steering wheel has the general shape of an open truncated cone with a significant aerodynamic wind.
  • Badminton shuttlecocks can be classified in two categories: first category consists of the wheels having a wing in urns. These have a good flight quality. Indeed, the flight ajectory is parachute type: the steering wheel can achieve a: itude important while having a trajectory of descent> rupte. This type of steering wheel, however, has the disadvantage of having a life expectancy reduced because of the fragility of the feathers.
  • the second category consists of flying nthetic material, especially plastic. These last have a great duration; life but have the disadvantage of poor flying qualities. Indeed, the trajectory is of the parabolic type: the altitude reached is more ible than in a parachute trajectory and presents a softer trajectory of iscent. This second type of trajectory is less interesting r the steering wheel is then more easily overtaken by the opponent.
  • WO-2008/038040 discloses a steering wheel belonging to the second category; it is composed of a front part carrying the end piece and a rear part constituting the canopy, the front and rear parts being made of two different synthetic materials and are connected to each other by portions of annular ends. .
  • This wheel sometimes has the disadvantage of sometimes breaking in two during the game.
  • GB-2 333 970 discloses a two-material badminton steering wheel in which the rods and the plate are formed by injection, the wings are stamped and each wing is attached to a corresponding rod by gluing, welding or by means mechanical.
  • An object of the present invention is to provide a dminton steering wheel having the dynamic behavior of a feather wheel while i having a longer life.
  • the invention achieves its goal by the fact that the steering wheel comprises:
  • a body comprising a plate which has a periphery and carries a tip, and a plurality of rods molded in one piece with the plate, each of the rods having:
  • the body structure which is composed of a one-piece plate with the plurality of rods, provides stiffness to the steering wheel, while the thin and flexible wing allows the steering wheel to exhibit aerodynamic behavior close to that of the steering wheel. a feathered steering wheel without the fragility.
  • the body has between 12 and 16 stems.
  • the sail is a single piece of frustoconical shape.
  • the thickness of the wing is between 0.1 mm and 0.3 mm.
  • the attachment portions preferably extend from the second ends of the opposite rods to the first ends.
  • the wing is arranged around the plurality of rods and has an inner surface attached to the rod attachment portions.
  • the wing thus surrounds the assembly constituted by the plurality of rods.
  • the wing is disposed within the volume defined by the plurality of rods.
  • the assembly consisting of the plurality of rods is arranged around the blade.
  • the rods are embedded in the wing.
  • the wing is attached, which means that the wing is a separate part of the body before attachment to the rods.
  • An interest is to be able to achieve the steering wheel in two materials having different rigidities.
  • the wing will preferably be made of a softer material than the material constituting the body.
  • the wing is fixed to the fixing portions by overmolding, welding or gluing.
  • the steering wheel is made by bi-injection, the body being formed during a first injection, while the wing is obtained by overmolding.
  • An overmoulding advantage is to allow the automated obtaining of a steering wheel having good adhesion between the body and the wing. As mentioned above, this technique also makes it easy to make a badminton shuttlecock made of two different materials.
  • the material of the rods has a hardness lower than that of the rod of a feather to make the rods less brittle during impacts, which increases the life of the steering wheel.
  • At least some of the attachment portions of the rods are fixed to the wing on at least a quarter of the length of the wing. At least some of the attachment portions, preferably at least half, have a length at least equal to one quarter of the length of the wing.
  • the length of the wing means the length of its lateral surface. This is usually the length of the wings constituting the wing.
  • the area of attachment of the rods to the wing extends over a length corresponding to at least one third of the length of the wing.
  • each of the attachment portions has a length greater than one third of the length of the wing.
  • the wing covers the rods which extend within the volume defined by the wing over a length corresponding to at least one third of the length of the wing.
  • Each of the rods has a portion not covered by the wing. This uncovered portion is at least 25% of the length of the stem.
  • the bearing surface of the wing that is to say the external or lateral surface of the wing, has a determined texture or a specific surface condition, for example a roughness, to modify the flow of the airfoil. air on it.
  • the wing can also have a bearing surface with specific patterns, for example geometric patterns, also to change the flow of air on it.
  • the choice of a determined texture, a determined surface state and / or a determined pattern for the airfoil of the wing can modify the aerodynamic behavior of the steering wheel, for example the braking or the speed of rotation of the steering wheel. .
  • the blade has a plurality of fins connected to each other by their longitudinal edges, while being inclined relative to each other.
  • This conformation which mimics the shape of a skirt of a feathered steering wheel, contributes to obtain an aerodynamic behavior comparable to that of a feathered steering wheel.
  • the fins are connected to each other by their longitudinal edges over all or part of the length of the fins.
  • the blade has a large base and a small base, the small base being located between the large base and the plate, and the wing has a decreasing thickness between its small base and its large base.
  • the rods advantageously have second ends opposite to the first ends, and the fixing portions of the rods have a decreasing thickness towards the second ends of the rods.
  • the thickness of the attachment portions is less than that of the rest of the rod.
  • the wing has a large base and a small base, the small base being located between the large base and platinum, and in that the small and / or large base has a zigzag-shaped peripheral cutout.
  • the body advantageously comprises at least one stiffening ring secured to the rods which is disposed between the wing and the plate.
  • this stiffening ring is molded in one piece with the rods.
  • the wing further comprises at least one stiffening ring.
  • the stiffening ring is disposed at the end of the wing forming the small base of the wing.
  • the wing and / or the body may be provided with a stiffening ring. These rings extend in planes parallel to the plate.
  • the rods have a cross section in the shape of "U".
  • An interest is to lighten the stems while maintaining their rigidity.
  • the U-shaped cross section opens into the volume defined by the plurality of rods.
  • the fixing portions of the rods comprise notches filled with material constituting the wing.
  • the wing comprises notches filled with constituent material of the rods.
  • An interest is to achieve a mechanical catch between the rods and the wing, to enhance the chemical grip between the constituent materials of the body and the wing.
  • the body is made of fiber filled polyamide, while the wing is made of unfilled polyamide.
  • the plate further comprises a fastening portion of the tip, said fixing portion protruding from a face of the plate.
  • the plate has the form of a solid disc.
  • the plate forms a disk that has a central opening, and the end of the fixing portion opposite the plate has a closing wall parallel to the plate in order to close off the end of the fixing portion.
  • An interest is to move the center of gravity of the steering wheel forward, in order to adjust the aerodynamic behavior of the steering wheel.
  • the attachment portion is in the form of one or more harpoons having a cylindrical shape.
  • the harpoon (s) are inserted into the mouthpiece to make it integral with the body.
  • the invention furthermore relates to a method of manufacturing a badminton shuttlecock according to the invention in which the body is first made by injection molding, and in which the wing is then overmolded onto the fastening portions of the invention. rods.
  • Such a method is easily automated and makes it possible to easily achieve a bi-material badminton steering wheel which has a better impact resistance than that of the prior art, while having a very flexible wing to present an aerodynamic behavior close to that of a feathered steering wheel.
  • the invention also relates to an alternative method of manufacturing a badminton shuttlecock according to the invention wherein the body is made by molding, the blade is thermoformed, and the body is overmolded on said wing.
  • the tip is made by foaming.
  • FIG. 1 is a perspective front view of the badminton shuttlecock according to the invention.
  • FIG. 1 is a rear perspective view of the steering wheel of Figure 1;
  • FIG. 3 is a view of the steering wheel in longitudinal section along the plane A of Figure 1;
  • - Figure 4 is a view of the steering wheel of Figure 1 in cross section along the plane B of Figure 1;
  • - Figure 5 is a side view of the body of the steering wheel of Figure i;
  • FIG. 6 is a semi-exploded perspective view of a variant of the badminton shuttlecock according to the invention.
  • FIG. 1 An exemplary embodiment of a badminton wheel 10 according to the invention is shown in Figures 1 to 5.
  • This wheel 10 has a rear portion 10a consists of a skirt 12 of generally frustoconical shape and a front portion 10b comprising a mouthpiece 14.
  • the flywheel has an axis of symmetry X.
  • the flywheel 10 considered in the axial direction of the frustoconical skirt 12, has a convergent shape from the rear portion 10a to the front portion 10b.
  • the skirt 12 comprises in particular a canopy 16 of frustoconical shape which will be described in more detail below.
  • the badminton shuttlecock 10 comprises a body 18 which comprises a plate 20 to which the tip 14 is fixed, as well as a plurality of rods 22 which extend from the periphery 20a of the plate 20.
  • the skirt is the assembly consisting of the plurality of rods and the wing.
  • the rods 22 are angularly spaced from each other so as to define a frustoconical volume.
  • the rods 22 are molded in one piece with the plate 20.
  • the plate has a circular shape, and more specifically a disc shape.
  • This plate 20 is perpendicular to the X axis of the flywheel 10. As will be seen below, the disk-shaped plate 20 may be full or, according to a variant which will be described below, have a central orifice.
  • the body 18 comprises sixteen rods 22. This number is however not limiting, the steering wheel may have a number of rods of between twelve and sixteen or more.
  • each of the rods 22 has a first end 22a integral with the plate 20: in other words, the end 22a of the rod 22 constitutes the connection zone between the rod 22 and the plate 20.
  • Each of the rods 22 further comprises a second end 22b opposite the first end 22a.
  • each of the rods 22 has a cross section S shaped "U".
  • the "U" shape opens towards the inside of the skirt 12.
  • This "U" -shaped cross section S extends over at least half the length L of the rod 22. specifies here that the rods 22 are substantially rectilinear; we will call longitudinal direction of the rod 22 the direction in which extends each of the rods.
  • Each of the rods 22 therefore has a longitudinal groove 22d which extends along the length L of the rod 22.
  • this groove 22d extends for each of the rods 22 from the first end 22a to a position 22c set back from the second end 22b.
  • the groove 22d extends over more than half the length of the rod 22.
  • the rods 22 are interconnected by means of a stiffening ring 24 which is perpendicular to the X axis and which is also molded in one piece with the rods 22.
  • the stiffening ring 24 is disposed between the plate 20 and the wing 16.
  • the body 18 further includes a fastening portion 26 for fastening the tip 14 to the plate 20.
  • the fixing portion 26 has the shape of a cylindrical harpoon extending from the face 20b of the plate 20 which is opposite the face 20c from which the rods 22 extend.
  • the fastening portion 26 is engaged in the material constituting the endpiece to make it integral with the plate 20.
  • the plate forms a solid disk and the end 26a of the fixing portion 26 which is remote from the plate is open.
  • the fixing portion 26 is preferably molded in one piece with the rest of the body 18.
  • the plate 20 ' is not full unlike the plate 20 of the example described above; it comprises a central orifice 21 'of circular shape so as to open the end of the fixing portion 26' which is connected to the plate 20 '.
  • the end 26'a of the fixing portion 26 'which is opposite the plate 20' has a closure wall 23 'parallel to the plate 20' to close the end 26'a of the fixing portion 26 '.
  • An interest of this variant is to move the center of gravity of the steering wheel forward to modify the aerodynamic behavior.
  • the frustoconically shaped wing 18 is made of a flexible material and has a thickness of between 0.1 mm and 0.3 mm. Therefore, the wing 16 is thin and flexible.
  • the wing 16 is an insert which consists of a single piece of frustoconical shape and which is arranged around the plurality of rods 22. In other words, the wing 16 extends around the assembly constituted by the rods 22.
  • each of the rods 22 further comprises an attachment portion 28 which is located opposite the first end 22a.
  • This fixing portion 28 extends along a fraction of the length L of the rod 22.
  • the end portion 28 extends from the second end 22b to the first end 22a.
  • the length I of the end portion 28 is strictly less than the length L of the corresponding rod 22.
  • the wing 16 is fixed to the rods along the fastening portion 28 of each of the rods 22.
  • the fixing portion 28 extends from the second end 22b of the rod.
  • the attachment portion thus comprises a first end 28a, and a second end 28b coincides with the second end 22b of the rod.
  • the length I of the attachment portion 28 along which the wing is fixed is at least equal to 1/5 of the length L of the rod 22.
  • the length L of the rod extends from the distance between the first end 22a and the second end 22b.
  • the wing 16 is disposed around the plurality of rods 22 and has an internal surface 17 which is fixed to the fixing portions of the rods 22.
  • the fastening portions 28 of the rods 22 extend inside the volume defined by the wing 16.
  • a small base 16a and a large base 16b of the wing can be defined, these bases being perpendicular to the axis X.
  • the fixing portions of the rods 22 are fixed to the wing 16 over at least a quarter of the length h of the wing. More specifically, the rods 22 extend inside the volume defined by the wing 16 from the small base 16a over a length that is at least equal to a quarter of the length h of the wing 16. It is specified here that the length h corresponds to the length of the lateral surface of the truncated cone defined by the wing 16.
  • the wing 16 is fixed to the fastening portions 28 by overmolding. It could however be fixed by welding or gluing. We will return below on the manufacturing process of this steering wheel.
  • the bearing surface of the wing 16 that is to say the outer surface of the wing, may have a determined texture or a specific surface condition, for example a roughness, to modify the flow of air on it.
  • the wing 16 may also have a bearing surface comprising specific patterns, for example geometric patterns, which also makes it possible to modify the flow of air thereon. It is then possible to modify the aerodynamic behavior of the steering wheel, for example the braking or the speed of rotation of the steering wheel.
  • the wing 16 has a plurality of fins 30 which are connected to each other by their longitudinal edges 30a.
  • the length of the fins corresponds substantially to the length of the wing.
  • the fins are inclined relative to each other so as to mimic the arrangement of a feather wing.
  • the wing 16 has a decreasing thickness between its small base 16a and its large base 16b.
  • the fins 30 have a decreasing thickness between the small base 16a and the large base 16b of the wing 16.
  • Another interest is to move the center of gravity of the steering wheel to its front portion 10b.
  • the large base 16b and the small base 16a each have a zigzag-shaped peripheral cut 32, 34 to improve the aerodynamic behavior.
  • the catch is primarily of a chemical nature between the constituent materials of the body 18 and the wing 16.
  • the fixing portions 28 of the rods comprise notches 29 which are initially empty and which are intended to be filled with the constituent material of the blade 16 at the time of overmolding.
  • One or more notches 29 may be provided next to one another in the fastening portion 28 of the rods.
  • the wing 16 also comprises notches (not shown here) which are initially empty and which are filled with constituent material of the rods at the time of the overmolding operation, which makes it possible to further improve the breaking resistance of the steering wheel 10.
  • the body 18 is firstly produced by injection molding so as to form the rods 22, the plate 20 and the fixing part 26, as well as the stiffening ring 24.
  • wing 16 is then overmolded on the fastening portions 28 of the rods.
  • overmolding is performed outside the volume defined by the plurality of rods.
  • the body 18 is made by molding.
  • the wing is thermoformed by known methods and then the body 18 is overmolded on said wing 16.

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  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Physical Education & Sports Medicine (AREA)
  • Toys (AREA)
  • Injection Moulding Of Plastics Or The Like (AREA)
  • Steering Controls (AREA)
  • Food-Manufacturing Devices (AREA)

Abstract

The invention relates to a badminton shuttlecock comprising: a body comprising a base plate (20) which has a rim and a tip (14), and a plurality of rods (22) moulded into one single part with the base plate (20), each of the rods having: o a first end (22a) rigidly connected to the base plate, and o a fastening part (28) located opposite the first end and which extends along a fraction of the length of the rod; a thin, flexible truncated blade (16) which is attached along the fastening part (28) of each of the rods (22).

Description

VOLANT DE BADMINTON  BADMINTON BIRDIE
rière-plan de l'invention background of the invention
La présente invention concerne le domaine des volants de jdminton.  The present invention relates to the field of jdminton wheels.
De manière connue, un volant de badminton est un projectile qui ;t utilisé dans le sport de raquette dénommé « badminton ». Le volant ésente la forme générale d'un tronc de cône ouvert présentant une ainée aérodynamique importante.  In known manner, a badminton shuttlecock is a projectile that is used in the sports of racket called "badminton". The steering wheel has the general shape of an open truncated cone with a significant aerodynamic wind.
Les volants de badminton peuvent être classés en deux catégories: première catégorie est constituée par les volants ayant une voilure en urnes. Ces derniers présentent une bonne qualité de vol. En effet, la ajectoire de vol est de type parachute : le volant peut atteindre une :itude importante tout en présentant une trajectoire de descente >rupte. Ce type de volant présente toutefois l'inconvénient d'avoir une irée de vie réduite en raison de la fragilité des plumes.  Badminton shuttlecocks can be classified in two categories: first category consists of the wheels having a wing in urns. These have a good flight quality. Indeed, the flight ajectory is parachute type: the steering wheel can achieve a: itude important while having a trajectory of descent> rupte. This type of steering wheel, however, has the disadvantage of having a life expectancy reduced because of the fragility of the feathers.
La seconde catégorie est constituée par les volants en matière nthétique, notamment en plastique. Ces derniers ont une grande durée ; vie mais ont l'inconvénient de présenter de mauvaises qualités de vol. i effet, la trajectoire est du type parabolique : l'altitude atteinte est plus ible que dans une trajectoire parachute et présente une trajectoire de iscente plus douce. Ce second type de trajectoire est moins intéressant r le volant est alors plus facilement rattrapable par l'adversaire.  The second category consists of flying nthetic material, especially plastic. These last have a great duration; life but have the disadvantage of poor flying qualities. Indeed, the trajectory is of the parabolic type: the altitude reached is more ible than in a parachute trajectory and presents a softer trajectory of iscent. This second type of trajectory is less interesting r the steering wheel is then more easily overtaken by the opponent.
WO-2008/038040 divulgue un volant appartenant à la seconde tégorie ; il est composé d'une partie avant portant l'embout et d'une irtie arrière constituant la voilure, les parties avant et arrière étant alisées dans deux matières synthétiques différentes et sont reliées l'une l'autre par des portions d'extrémités annulaires. Ce volant présente utefois l'inconvénient parfois de se casser en deux pendant le jeu.  WO-2008/038040 discloses a steering wheel belonging to the second category; it is composed of a front part carrying the end piece and a rear part constituting the canopy, the front and rear parts being made of two different synthetic materials and are connected to each other by portions of annular ends. . This wheel sometimes has the disadvantage of sometimes breaking in two during the game.
GB-2 333 970 divulgue un volant de badminton bi-matière dans :juel : les tiges et la platine sont formées par injection, les voilures sont rmées par estampage et chaque voilure est fixée à une tige rrespondante par collage, soudure ou par des moyens mécaniques.  GB-2 333 970 discloses a two-material badminton steering wheel in which the rods and the plate are formed by injection, the wings are stamped and each wing is attached to a corresponding rod by gluing, welding or by means mechanical.
)iet et résumé de l'invention and a summary of the invention
Un but de la présente invention est de proposer un volant de dminton ayant le comportement dynamique d'un volant à plumes tout i présentant une meilleure durée de vie. L'invention atteint son but par le fait que le volant comporte : An object of the present invention is to provide a dminton steering wheel having the dynamic behavior of a feather wheel while i having a longer life. The invention achieves its goal by the fact that the steering wheel comprises:
• un corps comprenant une platine qui présente une périphérie et porte un embout, et une pluralité de tiges moulées en une seule pièce avec la platine, chacune des tiges présentant :  A body comprising a plate which has a periphery and carries a tip, and a plurality of rods molded in one piece with the plate, each of the rods having:
o une première extrémité solidaire de la platine, et o une portion de fixation située à l'opposé de la première extrémité et qui s'étend selon une fraction de la longueur de la tige ;  o a first end secured to the plate, and o an attachment portion located opposite the first end and which extends along a fraction of the length of the rod;
• une voilure fine et souple de forme tronconique qui est fixée le long de la portion de fixation de chacune des tiges.  • A thin and flexible frustoconical shape wing which is fixed along the fixing portion of each of the rods.
La structure du corps, qui est composé d'une platine formée d'une seule pièce avec la pluralité de tiges, fournit la rigidité au volant, tandis que la voilure fine et souple permet au volant de présenter un comportement aérodynamique proche de celui d'un volant à plumes sans en avoir la fragilité. De préférence, le corps comporte entre 12 et 16 tiges.  The body structure, which is composed of a one-piece plate with the plurality of rods, provides stiffness to the steering wheel, while the thin and flexible wing allows the steering wheel to exhibit aerodynamic behavior close to that of the steering wheel. a feathered steering wheel without the fragility. Preferably, the body has between 12 and 16 stems.
On comprend ainsi que la voilure constitue une seule et unique pièce de forme tronconique.  It is thus understood that the sail is a single piece of frustoconical shape.
De préférence, l'épaisseur de la voilure est comprise entre 0,1 mm et 0,3 mm.  Preferably, the thickness of the wing is between 0.1 mm and 0.3 mm.
Les portions de fixation s'étendent de préférence depuis les secondes extrémités des tiges opposées aux premières extrémités.  The attachment portions preferably extend from the second ends of the opposite rods to the first ends.
On comprend donc que l'accroche entre la voilure et les tiges se fait selon une zone de fixation s'étendant le long de chacune des portions de fixation des tiges.  It is therefore understood that the catch between the wing and the rods is in a fastening zone extending along each of the rod attachment portions.
Selon un mode de réalisation préférentiel, la voilure est disposée autour de la pluralité de tiges et présente une surface interne fixée aux portions de fixation des tiges.  According to a preferred embodiment, the wing is arranged around the plurality of rods and has an inner surface attached to the rod attachment portions.
La voilure entoure donc l'ensemble constitué par la pluralité de tiges.  The wing thus surrounds the assembly constituted by the plurality of rods.
Selon une variante, la voilure est disposée à l'intérieur du volume défini par la pluralité de tiges. Dans ce cas, l'ensemble constitué de la pluralité de tiges est disposé autour de la voilure.  Alternatively, the wing is disposed within the volume defined by the plurality of rods. In this case, the assembly consisting of the plurality of rods is arranged around the blade.
Selon une autre variante, les tiges sont noyées dans la voilure. According to another variant, the rods are embedded in the wing.
De préférence, la voilure est rapportée, ce qui signifie que la voilure constitue une pièce distincte du corps avant sa fixation aux tiges. Un intérêt est de pouvoir réaliser le volant en deux matières ayant des rigidités différentes. La voilure sera préférentiellement réalisée dans un matériau plus souple que le matériau constitutif du corps. Preferably, the wing is attached, which means that the wing is a separate part of the body before attachment to the rods. An interest is to be able to achieve the steering wheel in two materials having different rigidities. The wing will preferably be made of a softer material than the material constituting the body.
Avantageusement, la voilure est fixée aux portions de fixation par surmoulage, soudure ou collage.  Advantageously, the wing is fixed to the fixing portions by overmolding, welding or gluing.
De préférence, le volant est réalisé par bi-injection, le corps étant formé au cours d'une première injection, tandis que la voilure est obtenue par surmoulage.  Preferably, the steering wheel is made by bi-injection, the body being formed during a first injection, while the wing is obtained by overmolding.
Un intérêt du surmoulage est de permettre l'obtention automatisée d'un volant présentant une bonne adhérence entre le corps et la voilure. Comme mentionné précédemment, cette technique permet également de réaliser facilement un volant de badminton constitué de deux matières différentes.  An overmoulding advantage is to allow the automated obtaining of a steering wheel having good adhesion between the body and the wing. As mentioned above, this technique also makes it easy to make a badminton shuttlecock made of two different materials.
De préférence, le matériau constitutif des tiges présente une dureté inférieure à celle de la tige d'une plume afin de rendre les tiges moins cassantes lors des impacts, ce qui permet d'augmenter la durée de vie du volant.  Preferably, the material of the rods has a hardness lower than that of the rod of a feather to make the rods less brittle during impacts, which increases the life of the steering wheel.
Avantageusement, au moins certaines des portions de fixation des tiges sont fixées à la voilure sur au moins un quart de la longueur de la voilure. Au moins certaines des portions de fixation, de préférence au moins la moitié, présentent une longueur au moins égale au quart de la longueur de la voilure.  Advantageously, at least some of the attachment portions of the rods are fixed to the wing on at least a quarter of the length of the wing. At least some of the attachment portions, preferably at least half, have a length at least equal to one quarter of the length of the wing.
Par longueur de la voilure, on entend la longueur de sa surface latérale. Il s'agit le plus souvent de la longueur des ailettes constituant la voilure.  The length of the wing means the length of its lateral surface. This is usually the length of the wings constituting the wing.
Ainsi, la zone de fixation des tiges à la voilure s'étend sur une longueur correspondant à au moins un tiers de la longueur de la voilure.  Thus, the area of attachment of the rods to the wing extends over a length corresponding to at least one third of the length of the wing.
De préférence, chacune des portions de fixation présente une longueur supérieure au tiers de la longueur de la voilure.  Preferably, each of the attachment portions has a length greater than one third of the length of the wing.
Cela permet d'assurer la fixation de la voilure aux tiges tout en permettant à la voilure, une fois fixée au corps, de conserver sa souplesse.  This ensures the attachment of the wing to the rods while allowing the wing, once attached to the body, to maintain its flexibility.
Selon le mode de réalisation préféré, la voilure recouvre les tiges qui s'étendent à l'intérieur du volume défini par la voilure sur une longueur correspondant à au moins un tiers de la longueur de la voilure. Chacune des tiges présente une portion non recouverte par la voilure. Cette portion découverte est au moins égale à 25% de la longueur de la tige. According to the preferred embodiment, the wing covers the rods which extend within the volume defined by the wing over a length corresponding to at least one third of the length of the wing. Each of the rods has a portion not covered by the wing. This uncovered portion is at least 25% of the length of the stem.
Avantageusement, la surface portante de la voilure, c'est-à-dire la surface externe ou latérale de la voilure, présente une texture déterminée ou un état de surface déterminé, par exemple une rugosité, permettant de modifier l'écoulement de l'air sur celle-ci. Par ailleurs, la voilure peut également présenter une surface portante comportant des motifs déterminés, par exemple des motifs géométriques, permettant également de modifier l'écoulement de l'air sur celle-ci.  Advantageously, the bearing surface of the wing, that is to say the external or lateral surface of the wing, has a determined texture or a specific surface condition, for example a roughness, to modify the flow of the airfoil. air on it. Furthermore, the wing can also have a bearing surface with specific patterns, for example geometric patterns, also to change the flow of air on it.
Le choix d'une texture déterminée, d'un état de surface déterminé et/ou d'un motif déterminé pour la surface portante de la voilure permet de modifier le comportement aérodynamique du volant, par exemple le freinage ou la vitesse de rotation du volant.  The choice of a determined texture, a determined surface state and / or a determined pattern for the airfoil of the wing can modify the aerodynamic behavior of the steering wheel, for example the braking or the speed of rotation of the steering wheel. .
Avantageusement, la voilure présente une pluralité d'ailettes reliées les unes aux autres par leurs bords longitudinaux, tout en étant inclinées les unes par rapport aux autres.  Advantageously, the blade has a plurality of fins connected to each other by their longitudinal edges, while being inclined relative to each other.
Cette conformation, qui imite la forme d'une jupe d'un volant à plumes, contribue à obtenir un comportement aérodynamique comparable à celui d'un volant à plumes.  This conformation, which mimics the shape of a skirt of a feathered steering wheel, contributes to obtain an aerodynamic behavior comparable to that of a feathered steering wheel.
De préférence, les ailettes sont reliées les unes aux autres par leurs bords longitudinaux sur toute ou partie de la longueur des ailettes.  Preferably, the fins are connected to each other by their longitudinal edges over all or part of the length of the fins.
Pour améliorer encore la souplesse de la jupe du volant, à savoir la partie arrière opposée à la partie avant portant l'embout, la voilure présente une grande base et une petite base, la petite base étant située entre la grande base et la platine, et la voilure présente une épaisseur décroissante entre sa petite base et sa grande base.  To further improve the flexibility of the skirt of the steering wheel, namely the rear portion opposite to the front portion carrying the tip, the blade has a large base and a small base, the small base being located between the large base and the plate, and the wing has a decreasing thickness between its small base and its large base.
Pour améliorer encore la souplesse du volant, les tiges présentent avantageusement des secondes extrémités opposées aux premières extrémités, et les portions de fixation des tiges présentent une épaisseur décroissante vers les secondes extrémités des tiges. De préférence, pour chacune des tiges, l'épaisseur des portions de fixation est inférieure à celle du reste de la tige. Un intérêt est d'améliorer encore la souplesse de la voilure.  To further improve the flexibility of the steering wheel, the rods advantageously have second ends opposite to the first ends, and the fixing portions of the rods have a decreasing thickness towards the second ends of the rods. Preferably, for each of the rods, the thickness of the attachment portions is less than that of the rest of the rod. An interest is to further improve the flexibility of the wing.
De préférence, mais pas exclusivement, la voilure présente une grande base et une petite base, la petite base étant située entre la grande base et la platine, et en ce que la petite et/ou la grande base présente une découpe périphérique en forme de zigzag. Preferably, but not exclusively, the wing has a large base and a small base, the small base being located between the large base and platinum, and in that the small and / or large base has a zigzag-shaped peripheral cutout.
Pour renforcer la rigidité du volant, le corps comporte avantageusement au moins un anneau de rigidification solidaire des tiges qui est disposé entre la voilure et la platine.  To enhance the rigidity of the steering wheel, the body advantageously comprises at least one stiffening ring secured to the rods which is disposed between the wing and the plate.
De préférence, cet anneau de rigidification est moulé en une seule pièce avec les tiges.  Preferably, this stiffening ring is molded in one piece with the rods.
Avantageusement, la voilure comporte en outre au moins un anneau de rigidification. De préférence, l'anneau de rigidification est disposé à l'extrémité de la voilure formant la petite base de la voilure.  Advantageously, the wing further comprises at least one stiffening ring. Preferably, the stiffening ring is disposed at the end of the wing forming the small base of the wing.
Ainsi, selon l'invention, la voilure et/ou le corps peuvent être munis d'un anneau de rigidification. Ces anneaux s'étendent dans des plans parallèles à la platine.  Thus, according to the invention, the wing and / or the body may be provided with a stiffening ring. These rings extend in planes parallel to the plate.
Avantageusement, les tiges présentent une section transversale en forme de « U ». Un intérêt est d'alléger les tiges tout en conservant leur rigidité.  Advantageously, the rods have a cross section in the shape of "U". An interest is to lighten the stems while maintaining their rigidity.
De préférence, la section transversale en forme de U débouche à l'intérieur du volume défini par la pluralité de tiges.  Preferably, the U-shaped cross section opens into the volume defined by the plurality of rods.
Avantageusement, les portions de fixation des tiges comprennent des encoches remplies de matière constitutive de la voilure.  Advantageously, the fixing portions of the rods comprise notches filled with material constituting the wing.
Alternativement, ou en combinaison avec la caractéristique précédente, la voilure comprend des encoches remplies de matière constitutive des tiges. Un intérêt est de réaliser une accroche mécanique entre les tiges et la voilure, afin de renforcer l'accroche chimique entre les matériaux constitutifs du corps et de la voilure.  Alternatively, or in combination with the preceding feature, the wing comprises notches filled with constituent material of the rods. An interest is to achieve a mechanical catch between the rods and the wing, to enhance the chemical grip between the constituent materials of the body and the wing.
Selon un mode de réalisation préféré, mais pas exclusif, le corps est réalisé en polyamide chargé en fibres, tandis que la voilure est réalisée en polyamide non chargé.  According to a preferred embodiment, but not exclusively, the body is made of fiber filled polyamide, while the wing is made of unfilled polyamide.
Les inventeurs ont constaté que ce choix de types de matériaux permet d'obtenir un corps rigide, ainsi qu'une voilure suffisamment souple pour se déformer lors de l'impact avec la raquette et résistant pour ne pas casser.  The inventors have found that this choice of types of materials makes it possible to obtain a rigid body, as well as a wing that is sufficiently flexible to deform upon impact with the racket and resistant so as not to break.
Avantageusement, la platine comporte en outre une partie de fixation de l'embout, ladite partie de fixation faisant saillie depuis une face de la platine.  Advantageously, the plate further comprises a fastening portion of the tip, said fixing portion protruding from a face of the plate.
De préférence, la platine présente la forme d'un disque plein. En variante, la platine forme un disque qui présente une ouverture centrale, et l'extrémité de la partie de fixation opposée à la platine présente une paroi d'obturation parallèle à la platine afin d'obturer l'extrémité de la partie de fixation. Un intérêt est de déplacer le centre de gravité du volant vers l'avant, et ce afin d'ajuster le comportement aérodynamique du volant. Preferably, the plate has the form of a solid disc. In a variant, the plate forms a disk that has a central opening, and the end of the fixing portion opposite the plate has a closing wall parallel to the plate in order to close off the end of the fixing portion. An interest is to move the center of gravity of the steering wheel forward, in order to adjust the aerodynamic behavior of the steering wheel.
De préférence, la partie de fixation présente la forme d'un ou plusieurs harpons ayant une forme cylindrique. Le ou les harpons sont enfoncés dans l'embout afin de le rendre solidaire du corps.  Preferably, the attachment portion is in the form of one or more harpoons having a cylindrical shape. The harpoon (s) are inserted into the mouthpiece to make it integral with the body.
L'invention porte en outre sur un procédé de fabrication d'un volant de badminton selon l'invention dans lequel le corps est tout d'abord réalisé par moulage par injection, et dans lequel la voilure est ensuite surmoulée sur les portions de fixation des tiges.  The invention furthermore relates to a method of manufacturing a badminton shuttlecock according to the invention in which the body is first made by injection molding, and in which the wing is then overmolded onto the fastening portions of the invention. rods.
Un tel procédé est facilement automatisable et permet de réaliser facilement un volant de badminton bi-matière qui présente une meilleure résistance aux impacts que celui de l'art antérieur, tout en ayant une voilure très souple afin de présenter un comportement aérodynamique proche de celui d'un volant à plumes.  Such a method is easily automated and makes it possible to easily achieve a bi-material badminton steering wheel which has a better impact resistance than that of the prior art, while having a very flexible wing to present an aerodynamic behavior close to that of a feathered steering wheel.
L'invention porte également sur une variante du procédé de fabrication d'un volant de badminton selon l'invention dans lequel le corps est réalisé par moulage, la voilure est thermoformée, et le corps est surmoulé sur ladite voilure.  The invention also relates to an alternative method of manufacturing a badminton shuttlecock according to the invention wherein the body is made by molding, the blade is thermoformed, and the body is overmolded on said wing.
De préférence, mais pas exclusivement, l'embout est réalisé par moussage.  Preferably, but not exclusively, the tip is made by foaming.
Brève description des dessins  Brief description of the drawings
L'invention sera mieux comprise à la lecture de la description qui suit de modes de réalisation de l'invention donnés à titre d'exemples non limitatifs, en référence aux dessins annexés sur lesquels :  The invention will be better understood on reading the following description of embodiments of the invention given as non-limiting examples, with reference to the appended drawings, in which:
- la figure 1 est une vue avant en perspective du volant de badminton selon l'invention ;  - Figure 1 is a perspective front view of the badminton shuttlecock according to the invention;
- la figure 2 est une vue arrière en perspective du volant de la figure 1 ;  - Figure 2 is a rear perspective view of the steering wheel of Figure 1;
- la figure 3 est une vue du volant en coupe longitudinale selon le plan A de la figure 1;  - Figure 3 is a view of the steering wheel in longitudinal section along the plane A of Figure 1;
- la figure 4 est une vue du volant de la figure 1 en coupe transversale selon le plan B de la figure 1; - la figure 5 est une vue latérale du corps du volant de la figure i ; - Figure 4 is a view of the steering wheel of Figure 1 in cross section along the plane B of Figure 1; - Figure 5 is a side view of the body of the steering wheel of Figure i;
- la figure 6 est une vue en perspective semi-éclatée d'une variante du volant de badminton selon l'invention.  FIG. 6 is a semi-exploded perspective view of a variant of the badminton shuttlecock according to the invention.
Description détaillée de l'invention Detailed description of the invention
Un exemple de réalisation d'un volant de badminton 10 conforme à l'invention est représenté en figures 1 à 5. Ce volant 10 présente une partie arrière 10a constituée d'une jupe 12 de forme générale tronconique et une partie avant 10b comprenant un embout 14. Le volant présente un axe de symétrie X.  An exemplary embodiment of a badminton wheel 10 according to the invention is shown in Figures 1 to 5. This wheel 10 has a rear portion 10a consists of a skirt 12 of generally frustoconical shape and a front portion 10b comprising a mouthpiece 14. The flywheel has an axis of symmetry X.
De manière classique, le volant 10, considéré selon la direction axiale de la jupe tronconique 12, présente une forme convergente de la partie arrière 10a vers la partie avant 10b.  In a conventional manner, the flywheel 10, considered in the axial direction of the frustoconical skirt 12, has a convergent shape from the rear portion 10a to the front portion 10b.
La jupe 12 comporte notamment une voilure 16 de forme tronconique qui sera décrite plus en détail ci-après.  The skirt 12 comprises in particular a canopy 16 of frustoconical shape which will be described in more detail below.
Conformément à l'invention, le volant de badminton 10 comprend un corps 18 qui comporte une platine 20 à laquelle est fixé l'embout 14, ainsi qu'une pluralité de tiges 22 qui s'étendent depuis la périphérie 20a de la platine 20. La jupe est l'ensemble constitué de la pluralité de tiges et de la voilure.  According to the invention, the badminton shuttlecock 10 comprises a body 18 which comprises a plate 20 to which the tip 14 is fixed, as well as a plurality of rods 22 which extend from the periphery 20a of the plate 20. The skirt is the assembly consisting of the plurality of rods and the wing.
Comme on le constate sur la figure 2, les tiges 22 sont espacées angulairement les unes des autres de manière à définir un volume tronconique.  As can be seen in FIG. 2, the rods 22 are angularly spaced from each other so as to define a frustoconical volume.
Selon l'invention, les tiges 22 sont moulées en une seule pièce avec la platine 20. Dans cet exemple, la platine présente une forme circulaire, et plus précisément une forme de disque.  According to the invention, the rods 22 are molded in one piece with the plate 20. In this example, the plate has a circular shape, and more specifically a disc shape.
Cette platine 20 est perpendiculaire à l'axe X du volant 10. Comme on le verra ci-dessous, la platine en forme de disque 20 peut être pleine ou, selon une variante qui sera décrite ci-dessous, présenter un orifice central.  This plate 20 is perpendicular to the X axis of the flywheel 10. As will be seen below, the disk-shaped plate 20 may be full or, according to a variant which will be described below, have a central orifice.
Dans cet exemple, le corps 18 comprend seize tiges 22. Ce nombre n'est toutefois pas limitatif, le volant pouvant tout à fait comporter un nombre de tiges compris entre douze et seize, voire davantage.  In this example, the body 18 comprises sixteen rods 22. This number is however not limiting, the steering wheel may have a number of rods of between twelve and sixteen or more.
En se référant à la figure 3, on constate que chacune des tiges 22 présente une première extrémité 22a solidaire de la platine 20 : autrement dit, l'extrémité 22a de la tige 22 constitue la zone de connexion entre la tige 22 et la platine 20. Referring to FIG. 3, it can be seen that each of the rods 22 has a first end 22a integral with the plate 20: in other words, the end 22a of the rod 22 constitutes the connection zone between the rod 22 and the plate 20.
Chacune des tiges 22 comporte en outre une seconde extrémité 22b opposée à la première extrémité 22a.  Each of the rods 22 further comprises a second end 22b opposite the first end 22a.
Tel que représenté sur les figures 4 et 5, chacune des tiges 22 présente une section transversale S en forme de « U ». Dans cet exemple, la forme en « U » s'ouvre vers l'intérieur de la jupe 12. Cette section transversale S en forme de « U » s'étend sur au moins la moitié de la longueur L de la tige 22. On précise ici que les tiges 22 sont sensiblement rectilignes ; on appellera donc direction longitudinale de la tige 22 la direction selon laquelle s'étend chacune des tiges.  As shown in Figures 4 and 5, each of the rods 22 has a cross section S shaped "U". In this example, the "U" shape opens towards the inside of the skirt 12. This "U" -shaped cross section S extends over at least half the length L of the rod 22. specifies here that the rods 22 are substantially rectilinear; we will call longitudinal direction of the rod 22 the direction in which extends each of the rods.
Chacune des tiges 22 présente donc une rainure longitudinale 22d qui s'étend selon la longueur L de la tige 22.  Each of the rods 22 therefore has a longitudinal groove 22d which extends along the length L of the rod 22.
Comme on le voit sur la figure 4, les rainures 22d s'ouvrent vers l'intérieur de la jupe 12.  As seen in FIG. 4, the grooves 22d open towards the inside of the skirt 12.
Dans cet exemple, cette rainure 22d s'étend pour chacune des tiges 22 depuis la première extrémité 22a jusqu'à une position 22c disposée en retrait de la seconde extrémité 22b.  In this example, this groove 22d extends for each of the rods 22 from the first end 22a to a position 22c set back from the second end 22b.
Dans cet exemple, la rainure 22d s'étend sur plus de la moitié de la longueur de la tige 22.  In this example, the groove 22d extends over more than half the length of the rod 22.
Selon un autre aspect avantageux de l'invention, les tiges 22 sont reliées entre elles par le biais d'un anneau de rigidification 24 qui est perpendiculaire à l'axe X et qui est également moulé en une seule pièce avec les tiges 22. Dans cet exemple, l'anneau de rigidification 24 est disposé entre la platine 20 et la voilure 16.  According to another advantageous aspect of the invention, the rods 22 are interconnected by means of a stiffening ring 24 which is perpendicular to the X axis and which is also molded in one piece with the rods 22. this example, the stiffening ring 24 is disposed between the plate 20 and the wing 16.
En se référant à nouveau à la figure 3, on constate que le corps 18 comporte en outre une partie de fixation 26 permettant la fixation de l'embout 14 à la platine 20.  Referring again to FIG. 3, it can be seen that the body 18 further includes a fastening portion 26 for fastening the tip 14 to the plate 20.
Dans cet exemple, la partie de fixation 26 présente la forme d'un harpon cylindrique qui s'étend depuis la face 20b de la platine 20 qui est opposée à la face 20c d'où s'étendent les tiges 22.  In this example, the fixing portion 26 has the shape of a cylindrical harpoon extending from the face 20b of the plate 20 which is opposite the face 20c from which the rods 22 extend.
La partie de fixation 26 vient s'engager dans la matière constitutive de l'embout afin de le rendre solidaire de la platine 20.  The fastening portion 26 is engaged in the material constituting the endpiece to make it integral with the plate 20.
Dans cet exemple, la platine forme un disque plein et l'extrémité 26a de la partie de fixation 26 qui est distante de la platine est ouverte. La partie de fixation 26 est préférentiellement moulée en une seule pièce avec le reste du corps 18. In this example, the plate forms a solid disk and the end 26a of the fixing portion 26 which is remote from the plate is open. The fixing portion 26 is preferably molded in one piece with the rest of the body 18.
Dans la variante représentée sur la figure 6, la platine 20' n'est pas pleine contrairement à la platine 20 de l'exemple décrit précédemment ; elle comporte un orifice central 21' de forme circulaire de manière à ouvrir l'extrémité de la partie de fixation 26' qui est connectée à la platine 20'. Dans cette variante, l'extrémité 26'a de la partie de fixation 26' qui est opposée à la platine 20' présente une paroi d'obturation 23' parallèle à la platine 20' afin d'obturer l'extrémité 26'a de la partie de fixation 26'.  In the variant shown in Figure 6, the plate 20 'is not full unlike the plate 20 of the example described above; it comprises a central orifice 21 'of circular shape so as to open the end of the fixing portion 26' which is connected to the plate 20 '. In this embodiment, the end 26'a of the fixing portion 26 'which is opposite the plate 20' has a closure wall 23 'parallel to the plate 20' to close the end 26'a of the fixing portion 26 '.
Un intérêt de cette variante, est de déplacer le centre de gravité du volant vers l'avant afin d'en modifier le comportement aérodynamique.  An interest of this variant is to move the center of gravity of the steering wheel forward to modify the aerodynamic behavior.
A l'aide des figures 2 et 3, on va maintenant décrire plus en détail la voilure du volant de badminton 10 selon l'invention.  With the help of Figures 2 and 3, we will now describe in more detail the wing of the badminton shuttlecock 10 according to the invention.
Dans cet exemple, la voilure de forme tronconique 18 est réalisée dans un matériau souple et présente une épaisseur comprise entre 0,1 mm et 0,3 mm. Par conséquent, la voilure 16 est fine et souple.  In this example, the frustoconically shaped wing 18 is made of a flexible material and has a thickness of between 0.1 mm and 0.3 mm. Therefore, the wing 16 is thin and flexible.
La voilure 16 est une pièce rapportée qui est constituée d'une seule et unique pièce de forme tronconique et qui est disposée autour de la pluralité de tiges 22. En d'autres termes, la voilure 16 s'étend autour de l'ensemble constitué par les tiges 22.  The wing 16 is an insert which consists of a single piece of frustoconical shape and which is arranged around the plurality of rods 22. In other words, the wing 16 extends around the assembly constituted by the rods 22.
Selon l'invention, chacune des tiges 22 comporte en outre une portion de fixation 28 qui est située à l'opposé de la première extrémité 22a. Cette portion de fixation 28 s'étend selon une fraction de la longueur L de la tige 22.  According to the invention, each of the rods 22 further comprises an attachment portion 28 which is located opposite the first end 22a. This fixing portion 28 extends along a fraction of the length L of the rod 22.
Comme on le constate sur la figure 2, la portion d'extrémité 28 s'étend depuis la seconde extrémité 22b vers la première extrémité 22a.  As seen in Figure 2, the end portion 28 extends from the second end 22b to the first end 22a.
La longueur I de la portion d'extrémité 28 est strictement inférieure à la longueur L de la tige 22 correspondante.  The length I of the end portion 28 is strictly less than the length L of the corresponding rod 22.
Selon l'invention, la voilure 16 est fixée aux tiges le long de la portion de fixation 28 de chacune des tiges 22.  According to the invention, the wing 16 is fixed to the rods along the fastening portion 28 of each of the rods 22.
Dans cet exemple, la portion de fixation 28 s'étend depuis la seconde extrémité 22b de la tige. La portion de fixation comprend donc une première extrémité 28a, et une seconde extrémité 28b confondue avec la seconde extrémité 22b de la tige.  In this example, the fixing portion 28 extends from the second end 22b of the rod. The attachment portion thus comprises a first end 28a, and a second end 28b coincides with the second end 22b of the rod.
De préférence, la longueur I de la portion de fixation 28 le long de laquelle est fixée la voilure, est au moins égale à 1/5 de la longueur L de la tige 22. On précise là encore que la longueur L de la tige s'étend de la distance entre la première extrémité 22a et la seconde extrémité 22b. Preferably, the length I of the attachment portion 28 along which the wing is fixed is at least equal to 1/5 of the length L of the rod 22. Here again it is specified that the length L of the rod extends from the distance between the first end 22a and the second end 22b.
Dans l'exemple de réalisation de la figure 2, la voilure 16 est disposée autour de la pluralité de tiges 22 et présente une surface interne 17 qui est fixée aux portions de fixation des tiges 22.  In the embodiment of FIG. 2, the wing 16 is disposed around the plurality of rods 22 and has an internal surface 17 which is fixed to the fixing portions of the rods 22.
En d'autres termes, dans cet exemple de réalisation, les portions de fixation 28 des tiges 22 s'étendent à l'intérieur du volume défini par la voilure 16.  In other words, in this embodiment, the fastening portions 28 of the rods 22 extend inside the volume defined by the wing 16.
Dans la mesure où la voilure 16 présente une forme tronconique, on peut définir une petite base 16a et une grande base 16b de la voilure, ces bases étant perpendiculaires à l'axe X.  Insofar as the wing 16 has a frustoconical shape, a small base 16a and a large base 16b of the wing can be defined, these bases being perpendicular to the axis X.
On comprend, à l'aide des figures 1 à 3, que les portions de fixation 28 des tiges 22 s'étendent à l'intérieur du volume défini par la voilure 16 entre la petite base 16a et la grande base 16b.  It will be understood from FIGS. 1 to 3 that the fastening portions 28 of the rods 22 extend inside the volume defined by the blade 16 between the small base 16a and the large base 16b.
De préférence, les portions de fixation des tiges 22 sont fixées à la voilure 16 sur au moins un quart de la longueur h de la voilure. Plus précisément, les tiges 22 s'étendent à l'intérieur du volume défini par la voilure 16 depuis la petite base 16a sur une longueur qui est au moins égale à un quart de la longueur h de la voilure 16. On précise ici que la longueur h correspond à la longueur de la surface latérale du tronc de cône défini par la voilure 16.  Preferably, the fixing portions of the rods 22 are fixed to the wing 16 over at least a quarter of the length h of the wing. More specifically, the rods 22 extend inside the volume defined by the wing 16 from the small base 16a over a length that is at least equal to a quarter of the length h of the wing 16. It is specified here that the length h corresponds to the length of the lateral surface of the truncated cone defined by the wing 16.
Dans cet exemple particulier, la voilure 16 est fixée aux portions de fixation 28 par surmoulage. Elle pourrait toutefois être fixée par soudure ou collage. On reviendra ci-dessous sur le procédé de fabrication de ce volant.  In this particular example, the wing 16 is fixed to the fastening portions 28 by overmolding. It could however be fixed by welding or gluing. We will return below on the manufacturing process of this steering wheel.
La surface portante de la voilure 16, c'est-à-dire la surface externe de la voilure, peut présenter une texture déterminée ou un état de surface déterminé, par exemple une rugosité, permettant de modifier l'écoulement de l'air sur celle-ci. La voilure 16 peut également présenter une surface portante comprenant des motifs déterminés, par exemple des motifs géométriques, permettant également de modifier l'écoulement de l'air sur celle-ci. Il est alors possible de modifier le comportement aérodynamique du volant, par exemple le freinage ou la vitesse de rotation du volant.  The bearing surface of the wing 16, that is to say the outer surface of the wing, may have a determined texture or a specific surface condition, for example a roughness, to modify the flow of air on it. The wing 16 may also have a bearing surface comprising specific patterns, for example geometric patterns, which also makes it possible to modify the flow of air thereon. It is then possible to modify the aerodynamic behavior of the steering wheel, for example the braking or the speed of rotation of the steering wheel.
Comme on le constate sur les figures 1 à 3 et 6, la voilure 16 présente une pluralité d'ailettes 30 qui sont reliées les unes aux autres par leurs bords longitudinaux 30a. La longueur des ailettes correspond sensiblement à la longueur de la voilure. As can be seen in FIGS. 1 to 3 and 6, the wing 16 has a plurality of fins 30 which are connected to each other by their longitudinal edges 30a. The length of the fins corresponds substantially to the length of the wing.
Dans cet exemple, les ailettes sont inclinées les unes par rapport aux autres de manière à imiter l'agencement d'une voilure à plumes.  In this example, the fins are inclined relative to each other so as to mimic the arrangement of a feather wing.
Dans cet exemple particulier, la voilure 16 présente une épaisseur décroissante entre sa petite base 16a et sa grande base 16b. En d'autres termes, les ailettes 30 présentent une épaisseur décroissante entre la petite base 16a et la grande base 16b de la voilure 16. Un intérêt, comme mentionné plus haut, est d'améliorer la souplesse et la légèreté de la voilure du volant 10.  In this particular example, the wing 16 has a decreasing thickness between its small base 16a and its large base 16b. In other words, the fins 30 have a decreasing thickness between the small base 16a and the large base 16b of the wing 16. An interest, as mentioned above, is to improve the flexibility and lightness of the wing of the steering wheel. 10.
Un autre intérêt est de déplacer le centre de gravité du volant vers sa partie avant 10b.  Another interest is to move the center of gravity of the steering wheel to its front portion 10b.
Comme on le voit sur la figure 3, dans cet exemple, la grande base 16b et la petite base 16a présentent chacune une découpe périphérique 32, 34 en forme de zigzag, afin d'améliorer le comportement aérodynamique.  As seen in Figure 3, in this example, the large base 16b and the small base 16a each have a zigzag-shaped peripheral cut 32, 34 to improve the aerodynamic behavior.
Dans la mesure où la voilure est surmoulée à la pluralité de tiges 22, on comprend que l'accroche est en premier lieu de nature chimique entre les matériaux constitutifs du corps 18 et de la voilure 16.  Insofar as the wing is overmolded to the plurality of rods 22, it is understood that the catch is primarily of a chemical nature between the constituent materials of the body 18 and the wing 16.
Pour améliorer cette accroche, on prévoit également une accroche mécanique. Pour ce faire, les portions de fixation 28 des tiges comprennent des encoches 29 qui sont initialement vides et qui sont destinées à venir se remplir de la matière constitutive de la voilure 16 au moment du surmoulage. On peut prévoir une ou plusieurs encoches 29 disposées les unes à côté des autres dans la portion de fixation 28 des tiges. Cette accroche mécanique qui vient compléter l'accroche chimique, permet d'augmenter sensiblement la résistance à la casse du volant selon l'invention.  To improve this grip, it also provides a mechanical catch. To do this, the fixing portions 28 of the rods comprise notches 29 which are initially empty and which are intended to be filled with the constituent material of the blade 16 at the time of overmolding. One or more notches 29 may be provided next to one another in the fastening portion 28 of the rods. This mechanical catch which completes the chemical grip, allows to significantly increase the breaking strength of the steering wheel according to the invention.
Dans ces exemples non limitatifs, la voilure 16 comprend également des encoches (non représentées ici) qui sont initialement vides et qui viennent se remplir de matière constitutive des tiges au moment de l'opération de surmoulage, ce qui permet d'améliorer encore davantage la résistance à la casse du volant 10.  In these nonlimiting examples, the wing 16 also comprises notches (not shown here) which are initially empty and which are filled with constituent material of the rods at the time of the overmolding operation, which makes it possible to further improve the breaking resistance of the steering wheel 10.
On va maintenant expliciter deux variantes de procédé de fabrication du volant selon l'invention. Selon un premier procédé de fabrication, le corps 18 est tout d'abord réalisé par moulage par injection de manière à former les tiges 22, la platine 20 et la partie de fixation 26, ainsi que l'anneau de rigidification 24. Puis, la voilure 16 est ensuite surmoulée sur les portions de fixation 28 des tiges. Dans cet exemple, le surmoulage est réalisé à l'extérieur du volume défini par la pluralité de tiges. We will now explain two variants of manufacturing method of the steering wheel according to the invention. According to a first manufacturing method, the body 18 is firstly produced by injection molding so as to form the rods 22, the plate 20 and the fixing part 26, as well as the stiffening ring 24. wing 16 is then overmolded on the fastening portions 28 of the rods. In this example, overmolding is performed outside the volume defined by the plurality of rods.
Selon un autre procédé de fabrication, le corps 18 est réalisé par moulage. La voilure est quant à elle thermoformée par des procédés connus puis, le corps 18 est surmoulé sur ladite voilure 16.  According to another manufacturing method, the body 18 is made by molding. The wing is thermoformed by known methods and then the body 18 is overmolded on said wing 16.

Claims

REVENDICATIONS
1. Volant de badminton (10) caractérisé en ce qu'il comporte : 1. Badminton steering wheel (10) characterized in that it comprises:
• un corps (18) comprenant une platine (20) qui présente une périphérie et porte un embout (14), et une pluralité de tiges (22) moulées en une seule pièce avec la platine (20), chacune des tiges présentant :  A body (18) comprising a plate (20) which has a periphery and carries a tip (14), and a plurality of rods (22) molded in one piece with the plate (20), each of the rods having:
o une première extrémité (22a) solidaire de la platine (20), et  a first end (22a) integral with the plate (20), and
o une portion de fixation (28) située à l'opposé de la première extrémité et qui s'étend selon une fraction de la longueur (L) de la tige ;  o an attachment portion (28) located opposite the first end and which extends along a fraction of the length (L) of the rod;
• une voilure (16) fine et souple de forme tronconique qui est fixée le long de la portion de fixation (28) de chacune des tiges (22).  • A thin and flexible frustoconical shape wing (16) which is fixed along the fastening portion (28) of each of the rods (22).
2. Volant de badminton selon la revendication 1, caractérisé en ce que la voilure est disposée autour de la pluralité de tiges (22) et présente une surface interne (16a) fixée aux portions de fixation (28) des tiges (22). 2. badminton shuttlecock according to claim 1, characterized in that the wing is arranged around the plurality of rods (22) and has an inner surface (16a) fixed to the fixing portions (28) of the rods (22).
3. Volant de badminton selon la revendication 1 ou 2, caractérisé en ce que la voilure (16) est fixée aux portions de fixation (28) par surmoulage, soudure ou collage. 3. badminton shuttlecock according to claim 1 or 2, characterized in that the wing (16) is fixed to the fastening portions (28) by overmolding, welding or gluing.
4. Volant de badminton selon l'une quelconque des revendications 1 à 4. Badminton steering wheel according to one of claims 1 to
3, caractérisé en ce qu'au moins certaines des portions de fixation (28) des tiges (22) sont fixées à la voilure (16) sur au moins un quart de la longueur (h) de la voilure (16).  3, characterized in that at least some of the fixing portions (28) of the rods (22) are fixed to the wing (16) over at least a quarter of the length (h) of the wing (16).
5. Volant de badminton selon l'une quelconque des revendications 1 à Badminton steering wheel according to one of claims 1 to
4, caractérisé en ce que la voilure (16) présente une pluralité d'ailettes reliées les unes aux autres par leurs bords longitudinaux, tout en étant inclinées les unes par rapport aux autres. 4, characterized in that the wing (16) has a plurality of fins connected to each other by their longitudinal edges, while being inclined relative to each other.
6. Volant de badminton selon l'une quelconque des revendications 1 àThe badminton steering wheel according to one of claims 1 to
5, caractérisé en ce que la voilure (16) présente une grande base (16c) et une petite base (16b), la petite base étant située entre la grande base et la platine, et en ce que la voilure (16) présente une épaisseur décroissante entre sa petite base (16b) et sa grande base (16c). 5, characterized in that the wing (16) has a large base (16c) and a small base (16b), the small base being located between the large base and the plate, and in that the wing (16) has a decreasing thickness between its small base (16b) and its large base (16c).
7. Volant de badminton selon l'une quelconque des revendications 1 à 7. Badminton shuttlecock according to one of claims 1 to
6, caractérisé en ce que la voilure (16) présente une grande base (16c) et une petite base (16b), la petite base étant située entre la grande base et la platine, et en ce que la petite et/ou la grande base présente une découpe périphérique en forme de zigzag.  6, characterized in that the wing (16) has a large base (16c) and a small base (16b), the small base being located between the large base and the plate, and in that the small and / or large base has a zigzag-shaped peripheral cut.
8. Volant de badminton selon l'une quelconque des revendications 1 à 8. Badminton shuttlecock according to any one of claims 1 to
7, caractérisé en ce que le corps (18) comporte en outre au moins un anneau de rigidification (24) solidaire des tiges qui est disposé entre la voilure et la platine.  7, characterized in that the body (18) further comprises at least one stiffening ring (24) integral with the rods which is disposed between the wing and the plate.
9. Volant de badminton selon l'une quelconque des revendications 1 à A badminton shuttlecock according to any one of claims 1 to
8, caractérisé en ce que la voilure (16) comporte en outre au moins un anneau de rigidification.  8, characterized in that the wing (16) further comprises at least one stiffening ring.
10. Volant de badminton selon l'une quelconque des revendications 1 à A badminton shuttlecock according to any one of claims 1 to
9, caractérisé en ce que les tiges (22) présentent une section transversale (22b) en forme de « U ».  9, characterized in that the rods (22) have a cross section (22b) shaped "U".
11. Volant de badminton selon l'une quelconque des revendications 1 à Badminton steering wheel according to one of claims 1 to
10, caractérisé en ce que les portions de fixation (28) des tiges comprennent des encoches (29) remplies de matière constitutive de la voilure.  10, characterized in that the fixing portions (28) of the rods comprise notches (29) filled with material constituting the wing.
12. Volant de badminton selon l'une quelconque des revendications 1 à 12. Badminton shuttlecock according to one of claims 1 to
11, caractérisé en ce que la voilure (16) comprend des encoches remplies de matière constitutive des tiges. 11, characterized in that the wing (16) comprises notches filled with constituent material of the rods.
13. Volant de badminton selon l'une quelconque des revendications 1 à13. Badminton steering wheel according to any one of claims 1 to
12, caractérisé en ce que les tiges (22) présentent des secondes extrémités (22b) opposées aux premières extrémités (22a), et en ce que les portions de fixation (28) des tiges présentent une épaisseur décroissante vers les secondes extrémités (22b) des tiges. 12, characterized in that the rods (22) have second ends (22b) opposite the first ends (22a), and in that the fastening portions (28) of the rods have a decreasing thickness towards the second ends (22b) stems.
14. Volant de badminton selon l'une quelconque des revendications 1 à 14. Badminton shuttlecock according to any one of claims 1 to
13, caractérisé en ce que le corps (18) est réalisé en polyamide chargé en fibres, tandis que la voilure est réalisé en polyamide non chargé.  13, characterized in that the body (18) is made of fiber filled polyamide, while the wing is made of unfilled polyamide.
15. Volant de badminton selon l'une quelconque des revendications 1 à 15. Badminton shuttlecock according to one of claims 1 to
14, caractérisé en ce que la platine présente la forme d'un disque plein (20).  14, characterized in that the plate has the form of a solid disc (20).
16. Volant de badminton selon l'une quelconque des revendications 1 à 16. Badminton steering wheel according to one of claims 1 to
14, caractérisé en ce que la platine (200 comporte en outre une partie de fixation (260 de l'embout, ladite partie de fixation faisant saillie depuis une face (20b') de la platine (20'), en ce que la platine présente la forme d'un disque présentant une ouverture centrale (217), et en ce que l'extrémité (26'a) de la partie (260 de fixation opposée à la platine présente une paroi d'obturation parallèle à la platine afin d'obturer l'extrémité (26'a) de la partie de fixation (260- 14, characterized in that the plate (200 further comprises a fixing portion (260 of the tip, said fixing portion protruding from a face (20b ') of the plate (20'), in that the plate has the shape of a disc having a central opening (21 7 ), and in that the end (26'a) of the portion (260 of attachment opposite the plate has a closure wall parallel to the plate so closing the end (26'a) of the fixing part (260-
17. Procédé de fabrication d'un volant de badminton selon l'une quelconque des revendications 1 à 16, dans lequel le corps (18) est tout d'abord réalisé par moulage par injection, et dans lequel la voilure est ensuite surmoulée sur les portions de fixation (28) des tiges. 17. A method of manufacturing a badminton shuttlecock according to any one of claims 1 to 16, wherein the body (18) is first made by injection molding, and wherein the wing is then overmolded on the fixing portions (28) of the rods.
18. Procédé de fabrication d'un volant de badminton selon l'une quelconque des revendications 1 à 16, dans lequel le corps (18) est réalisé par moulage, la voilure est thermoformée, et le corps (18) est surmoulé sur ladite voilure (16). 18. A method of manufacturing a badminton shuttlecock according to any one of claims 1 to 16, wherein the body (18) is made by molding, the wing is thermoformed, and the body (18) is overmolded on said wing (16).
PCT/FR2013/051720 2012-07-20 2013-07-17 Badminton shuttlecock WO2014013197A2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CN201390000753.1U CN204972945U (en) 2012-07-20 2013-07-17 Shuttlecock
GB1500691.9A GB2519687B (en) 2012-07-20 2013-07-17 A Badminton shuttlecock

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1257030A FR2993469B1 (en) 2012-07-20 2012-07-20 BADMINTON BIRDIE
FR1257030 2012-07-20

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WO2014013197A2 true WO2014013197A2 (en) 2014-01-23
WO2014013197A3 WO2014013197A3 (en) 2014-05-01

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FR (1) FR2993469B1 (en)
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WO (1) WO2014013197A2 (en)

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JP5976907B1 (en) * 2015-08-17 2016-08-24 株式会社コスモ精機 Badminton shuttle
CN107952226A (en) * 2017-11-24 2018-04-24 陈小侠 The badminton ball support and shuttlecock of a kind of replaceable feather wings

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Publication number Priority date Publication date Assignee Title
CN105536220B (en) * 2016-02-23 2019-01-25 南京狮鹏体育用品有限公司 A kind of shuttlecock of artificial feather
CN107569837A (en) * 2017-09-21 2018-01-12 林日馀 A kind of shuttlecock of replaceable feather
CN108525257B (en) * 2018-01-17 2024-02-20 安徽玩就玩吧新零售有限责任公司 Badminton with plug connector

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GB912365A (en) * 1957-12-03 1962-12-05 Yutaka Nakamura Improvements in or relating to shuttlecocks
GB2263412A (en) * 1992-01-25 1993-07-28 Peter Shu Chun Cheng Shuttlecock
GB2333970A (en) * 1998-02-10 1999-08-11 Dunlop Slazenger Group Ltd Shuttlecock
GB2441979A (en) * 2006-09-25 2008-03-26 Gordon Willis Improvements in shuttlecocks
KR20110040331A (en) * 2009-10-14 2011-04-20 김형주 Divisible and combinable badminton shuttlecock
KR200460073Y1 (en) * 2011-10-22 2012-05-02 김상웅 Shuttlecock

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WO2012023587A1 (en) * 2010-08-20 2012-02-23 ヨネックス株式会社 Artificial feathers for shuttlecocks, shuttlecock and method for producing artificial shuttlecock feathers

Cited By (4)

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Publication number Priority date Publication date Assignee Title
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
CN107952226A (en) * 2017-11-24 2018-04-24 陈小侠 The badminton ball support and shuttlecock of a kind of replaceable feather wings
CN107952226B (en) * 2017-11-24 2023-11-03 陈小侠 Badminton ball support with replaceable feather wings and badminton

Also Published As

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GB2519687B (en) 2016-03-23
GB201500691D0 (en) 2015-03-04
GB2519687A (en) 2015-04-29
WO2014013197A3 (en) 2014-05-01
FR2993469A1 (en) 2014-01-24
FR2993469B1 (en) 2015-09-18
CN204972945U (en) 2016-01-20

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