EP0604658A1 - Volant ayant divers usages - Google Patents

Volant ayant divers usages Download PDF

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Publication number
EP0604658A1
EP0604658A1 EP93911511A EP93911511A EP0604658A1 EP 0604658 A1 EP0604658 A1 EP 0604658A1 EP 93911511 A EP93911511 A EP 93911511A EP 93911511 A EP93911511 A EP 93911511A EP 0604658 A1 EP0604658 A1 EP 0604658A1
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EP
European Patent Office
Prior art keywords
elements
image
degrees
cavity
various
Prior art date
Legal status (The legal status 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 status listed.)
Pending
Application number
EP93911511A
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German (de)
English (en)
Inventor
Antonio Asensio Chapapria
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Individual
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Individual
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 Individual filed Critical Individual
Publication of EP0604658A1 publication Critical patent/EP0604658A1/fr
Pending legal-status Critical Current

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Classifications

    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B43/00—Balls with special arrangements
    • A63B43/007—Arrangements on balls for connecting lines or cords
    • A—HUMAN NECESSITIES
    • A63—SPORTS; GAMES; AMUSEMENTS
    • A63B—APPARATUS FOR PHYSICAL TRAINING, GYMNASTICS, SWIMMING, CLIMBING, OR FENCING; BALL GAMES; TRAINING EQUIPMENT
    • A63B67/00—Sporting games or accessories therefor, not provided for in groups A63B1/00 - A63B65/00
    • A63B67/18—Badminton or similar games with feathered missiles
    • A63B67/183—Feathered missiles

Definitions

  • the invention is a flying object comprised of an elastic body, as a rule, where it is possible to fit several directional elements together, and according to them, its use may vary.
  • This invention is a flying object comprised of a normally elastic body, with the possibility to fit several different pieces or directionnal elements together to help and influence its flight and direction, during the flight these pieces are always at the rear, there is no danger of impact injuries (as it is elastic) its use can vary depending on these elements, such as a tuft of ribbons, threads etc. a string to launch like a sling or fly like a kite, with feathers, wings, etc. it may be punched and handlaunched with racquets, etc. it may be handlaunched and picked up with nothing but the feathers tuft and it may be used by one or several persons. It may have various possible uses either as a game, a toy or a sport.
  • the elastic body may have multiple possibilities of shapes and sizes in order to reach functional and commercial purposes and advertising messages, all sorts of publicity, not only with the mark but also with the possibility to adopt the shape and similarity of the product itself or the advertized object, thanks to the adaptability of its material.
  • the Shuttlecock Launcher is made of an elastic body (with one body or various bodies integrated in one body) preferably with an aerodynamic design that may vary in height and width according to its use, density of materials, distribution of weights, etc. it may also change into different shapes, such as a sphere, etc. It is elastic and resistant like rubber, foam rubber or foam. Its cavity may have variable sizes and goes through it totaly or partialy enabling to couple to directional elements (designed) with a support part, which may be a cylinder, ( plastic or similar) encircled by projection/s ( the shape of parallel rings) at suitable gaps.
  • the support part is crossed over longitudinaly (total or partialy) by a cavity, preferably conic-trunk or cylinder shaped etc., its border fits into the support part.
  • This support part couples and holds the elastic body as well as the various directional elements designed thanks to its projections or rings and to the pressure practiced by the elasticity and the strength of the material itself when enlarged by the piece, adjusting the sizes ( of both the piece and the cavity ).
  • This support part is able to carry and hold several directional elements (which cooperate and influence its flight and direction ), as the cavity may have multiple shapes and/ or diameters, it is possible to vary the elements coupled thereto and the uses, according to the shape of the cavity and to the position of the body.
  • the hollow support part whenever the hollow support part is introduced into the cavity of the elastic body, its shape becomes a conic-trunk, the largest opening faces the exterior, the conic shape decreasing towards the exterior shall act as a top in order to stop the flexible parts or elements from falling out , such as ribbons, threads, etc sticking to it with the help of a simple knot or a washer..,a size bigger than the way-out hole, forming a tuft that acts like a tail.
  • one end encircles and holds both the neck of the body and the support part introduced in it or the flying thread is joint to the tuft or ribbons into the hole, coming out either together from the same opening or separately from each of the opposite openings ( the body is crossed by the cavity ). It is possible to hold this thread by the opposite end and, with a rotation, launch it like a sling or fly it like a kite, with the tuft and the thread acting as a tail.
  • this thread it is possible to fix and hold an hollow part , with or without a cover, to a central orifice ( in order to launch it accurately ); the opposite end, where the thread is introduced with a knot, bigger than this orifice and smaller than the hollow part , so that nothing prevents it from rotating, fastens and is able to rotate on itself.
  • the tuft of ribbons or the launching thread may be used on its own and may be launched or hold back with the hands.
  • the cone decreasing towards the inside shall enable the insertion of : a) all sort of suitable directional elements such as wings, feathers, etc. which will fit and hold together according to a greater penetration into this cone; b) directional elements generally designed with projections (the last ring held by the smaller opening, or not ). So, it may be launched or hit with the hands, racquets, etc.
  • the hollow part may be crossed from one end to the other enabling to use the external part of the smaller opening as a fastening top.
  • the tuft knot and the launching thread that might also be used as described, with the smallest opening towards the exterior.
  • the tuft and/or the thread knot/s, clip/s etc. can also be fixed into the hollow of the support part ,( that could be crossed from one end to the other or partially and have different shapes such as cylinder or conic-trunk etc. and have a fastening piece): by its shape,with different diameters, etc.
  • the tuft and/or the thread knot/s may be placed directly into the body hollow part and firmly held: by its shape, with different diameters, etc.; by one or various of the possible bodies comprised in the body with an orifice etc.; or by the pressure of the body material in/ against this fastening knot and a support wedge part (with possible projections, hole, etc) or without it.
  • 4 elements with a coupler of 90 degrees ( similar or not ) coupled into 4 intervening elements with an angle of 90 degrees or 3 intervening elements with 90 degrees and 3 wedges of 30 degrees inserted which become biped in the couple space or without the biped part and with another piece fastening the couplers or with or not an angle of 120 degrees and enabling the spaces to fasten the 3 elements with coupler with 90 degrees, or not with 120 degrees to appear from the body etc.
  • the external part of these directional elements may adopt different shapes with one or more integrated elements. These coupled directional elements or some of them may be cast by injecting one single piece. Their external part has the following possibilities : a) To place 1,2,3,4, etc. directional elements. b) to adopt different shapes. c) to join by wings or by their axles, etc. ( sharing them or not ); they may also be coupled into the support part, with the help of a fastening piece, to the elastic body or directly into it, with the help of this support part or not.
  • the body may be fastened to the end of an elastic ribbon, the other end is fixed, drawing back when it is launched.
  • the body may be comprised of one or several bodies or parts fitting into each other, becoming one single body with different shapes ( or several shapes at once ) such as concentric layers or spherical sectors with possible fissure/s, hole/s, male/s and female/s with the following possibilities : a) increase or decrease the volume by changing them. b) change their external shape by changing the external piece/s. c) one or several of these bodies ( or parts ) becomes a support part, fastening the tuft knot perhaps with an orifice/s etc. etc..
  • IMAGE 1 - Shows an inferior, superior and raised plant view of the body in one of the possible shapes of aerodynamic drawing, in one single piece and its cavity.
  • IMAGE 2 - Shows an example of the inferior, superior and raised part of the support part to couple to the body.
  • IMAGE 3 - Shows an inferior, superior and section part view of the special piece fastened to the extreme of the launching thread, as well as the cover to be coupled.
  • IMAGE 4 - Shows a complete view of the longitudinal section , Image 3, with the fitted cover.
  • IMAGE 5 shows a side raised view of images 1 and 2, coupled, with the tuft of feathers, the ribbon and the launching thread, appearing from the smaller opening and fastened by the neck of the elastic body and, on the opposite end, by image 4.
  • IMAGE 6 - Shows a section view of Image 5, only now the launching thread is joint to the tuft and the design of the body changes into a more aerodynamic shape.
  • IMAGE 7 - Shows a section view of Image 5 without the launching thread.
  • IMAGE 8 - Shows a section view of Images 2 and 9 coupled, with the thread and the tuft joint, coming out separately.
  • IMAGE 9 - Shows a view of the upper and lower sections and raised of the body, Image 8, in one single spherical part, completely crossed by its cavity, with different diameters.
  • IMAGE 10 Shows a view of Images 1 and 2 coupled, with directional elements coupled on Image 2.
  • IMAGE 11 - Shows a section view of Image 2 coupled with the body, now spherical, where the smallest opening fastens the launching thread and the tuft with a knot.
  • IMAGE 12 - Shows a section view of Image 11, with the tuft of ribbons only.
  • IMAGE 13 - Shows a raised view of one of the designed parts with directional elements in the body.
  • IMAGE 14 - Shows a raised view of Image 13, males and females of the base and the axle with its wings.
  • IMAGE 15 - Shows another side raised view of Image 13, males, females of the base and the axle with its wings.
  • IMAGE 16 - Shows a raised view of Image 13 but now with reversed curvature of the central axle, with the two side wings (on its external part).
  • IMAGE 17 - Shows a cross section view of Images 13.14.15. 16 according to cutting line A-B with the angle of 90 degree, the male, their females and their ring parts.
  • IMAGE 18 - Shows a longitudinal section view of the piece, image 16, properly self coupled.
  • IMAGE 19 - Shows a longitudinal section view of the piece Image 13, properly coupled.
  • IMAGE 20 - Shows a cross section view of Image 18 , 19 and 26 according to cutting line A-B, with 4 elements coupled with an angle of 90 degrees, males and females forming a circle with ring.
  • IMAGE 23 - Shows a section view of Image 18, coupled to the piece of Image 2 with the body Image 1.
  • IMAGE 24 - Shows a longitudinal section view of Image 18 directly coupled to the body, Image 1.
  • IMAGE 25 - Shows a cross section view of cutting line C-D of Image 13, 14, 15. 16, 32, 33, 34, 35 as well as other views of shapes it might possibly adopt.
  • IMAGE 26 - Shows a longitudinal section view of Images 18, 19 now with its external wing like part.
  • IMAGE 27 - Shows a side view of an intervening element, coupled to work as the base of Images 32, 35.
  • IMAGE 28 - Shows a side view of the previous image, now with the possibility of a smaller length.
  • IMAGE 29 - Shows a cross section view according to cutting line E-L of Images 27, 28 with an angle of 90 degrees coupling males and females and its ring part.
  • IMAGE 30 - Shows a longitudinal section view of the part of Image 27, self coupled.
  • IMAGE 32 - Shows a side view of another possibility of part Image 13, now without its base , but with a coupler.
  • IMAGE 33 - Shows a raised view of Image 32, with the coupler and the central axle with its wings.
  • IMAGE 34 - Shows a raised view with the opposite face of Image 33.
  • IMAGE 35 - Shows a side raised view of Image 32, but now with its central axle curvature and the one formed with its side wings reversed.
  • IMAGE 36 - Shows a longitudinal section view of the part on Image 35, coupled on Image 30.
  • IMAGE 37 - Shows a longitudinal section view of the part on Image 32, coupled on Image 30.
  • IMAGE 38 - Shows a longitudinal section view of the part on Image 35, coupled now on Image 31.
  • IMAGE 39 - Shows a cross section view of the base of Images 30, 31, 36, 37, 38 according to the cutting plan E-L, with 4 coupled elements forming a circle with ring and its internal faces with angles of 90 degrees with males and females.
  • IMAGE 42 - Shows a cross section view according to cutting plan O-P of Images 36,37,38 as the example of Image 39 and the coupler of 90 degrees.
  • IMAGE 46 - Shows a longitudinal section view of Image 36 coupled in the part shown on Image 2 and in the body on Image 1.
  • IMAGE 47 - Shows a longitudinal section view of Image 37 directly coupled in the body on Image 1.
  • IMAGE 48 - Shows a longitudinal section view of Image 38 coupled in the body on Image 1.
  • IMAGE 49 - Shows a longitudinal section view of these coupled directional elements ( or some of them ) injected into a whole single part by its external side.
  • IMAGE 50 - Shows a longitudinal section view of the support part, acting as a base on Image 49.
  • IMAGE 51 - Shows a longitudinal section view of Image 49 coupled in Image 50, in part shown on Image 2 and in body , Image 1.
  • IMAGE 52 - Shows a longitudinal section view of Images 49 and 50 coupled in the body, Image 1.
  • IMAGE 53 shows a longitudinal section view of the body, Image 1, now in one of its possibilities, with its most aerodynamic design, and comprised of various parts, inserted and integrated and with an orifice for possible fastenings (the tuft , the knot, etc.)
  • the body (2) normally elastic may be formed by one (2) or several bodies or elements (48) inserted and integrated in one body (2), with an aerodynamic design ( Images 1,6, and 53 ) which may vary in width and height depending on the various possible uses, it may be more or less aerodynamic as well as the materials density and weight distribution and the fact that it may adopt various shapes , spherical, (see Images 8, 9, 11 and 12 ).
  • its neck sector (3) (Image 1) shall also vary in size, the same happens to its cavity (1) which may cross it partialy or completely as shown on Images 1 and 9; its measures fit together to couple tightly ( as fastening means in several directional elements, normally designed ), coupled between them or not and which cooperate and influence the flight and direction, they are always placed at the rear as parts (23), (24), (33), (35), (34), (17), (16),etc.
  • cylinder shaped etc. comprised of (5) a projection (spiral, ring, etc.) or fastening projections ( these examples are ring shape ) it is completely or partially crossed by the cavity (9) ( its axle may fit into the part or not ) its preferable shape is conic-trunk ( could be cylinder, with different diameters, etc. and have a support part ) it may fasten and be composed of several directional elements, such as (7), (16), (17), (20), (23), (24), (33), (34) some of its possibilities are : change of its cavity shape (9) , the coupling position in the body (2), the possibility to change the elements to be coupled and the uses.
  • this cone shape (9) decreasing towards the exterior, ( or the external face of the opening (6) ) may be used as a top, preventing the flexible elements from loosening, ribbon, threads, etc. (17) with the help of a knot, a clip, etc.
  • a tuft (17) wich acts as a tail ( Image 7) with the help of one or several ribbons or threads (16) , made of any sort of material or type, it may be launched as a sling, in different ways or possibilities such as : with the help of a rivet or clip (13) , one end tightly fasten by the neck (3) to the body (2) to the part introduced into it ( see Image 5); in another possibility this launching thread (16) is joint to the tuft (17) inside the cavity (9) by the knot (18) they may come out together , by the smallest opening(4) (Image 16) or separately, the thread (16) through the smallest (4); the tuft (17) through the biggest opening (6) (Image 8) .
  • the body (2) (spheric) is completely crossed by the cavity (1) (Image 9) to let them out. It is possible to fasten this launching thread (16) by the opposite end and, with rotating movements, make the body turn as a sling, it will fly, with a tail formed by the tuft of ribbons (17) and the thread (16).
  • the end/s of this thread (16) may be formed by a part/s (12), to hold (one), with or without a cover (10), hollow (14) with an orifice (11) situated at one end ( in order to launch accurately ) enabling the insertion of the thread (16) which self rotates as it is fastened by a simple knot (15) with a diameter bigger than the orifice (11) and smaller than the hollow (14) completely free to rotate.
  • a simple knot (15) with a diameter bigger than the orifice (11) and smaller than the hollow (14) completely free to rotate.
  • any other suitable part with an orifice (11) smaller than the knot (15) completely free to rotate (14) with a ring or similar with an orifice in the edge (11).
  • the tuft can be on its own (17) can be launched, picked up and hit with the hands or use the thread only (16).
  • Additional weight may be added to the cavity (9) of the support part (8) or underneath it, in the hollow part (1).
  • this hollow (9) conic-trunk part (8) faces the exterior, and once it is coupled in the body (2) (Images 10, 11, 12, 23, 46, 51 ) as shown on Image 10, decreasing towards the interior, it shall enable and easy the insertion of (20) directional elements of any sort, shape or suitable material, such as feathers, wings etc. that will couple and fasten more and more depending on a bigger penetration through this cone (9). If necessary, it may be fastened with some drops of a suitable sticking product. It may be hit, launched etc. with the hands, racquets, etc.
  • the external face of the smaller opening (4) may be used as a top, now inside the body (2) (Images 11 and 12 ), fastening the knot (18) joining the tuft (17) with the launching thread (16) ( with the part (12) of its opposite end ) enabling them to come out together through the bigger opening (6) (Image 11 ); or separately , now with the body (2) completely crossed by the cavity (1) (Image 9). It may be launched as a sling or with the tuft (17) only (Image 12) picked up and hit with the hands (Image 12 ); the thread (16) may also be used fastening the body (2) by the neck (3) as shown on Image 5 but with the bigger opening (6) facing the exterior, the thread may be used on its own as well (16).
  • the knot/s (18), clip/s, etc. of (16) and/or (17), etc. may be fastened to the cavity (9) (depending on its uses it may cross completely or partially the support part (8) it may have various shapes: cylinder, conic-trunk, etc. and place a fastening part etc.): according to its shape, with different diameters, etc.; by the external face of the opening, inside the body (2); by the pressure of the material of part (8) when expanded by it (18) as it tightly fits. And with a possible part with possible projection/s , orifice/s, etc. wedge like and / or fitted, etc.
  • the knot/s (18) may be situated and fastened in the cavity (1) by : its shape (1) with different diameters (Image 9) etc.; one or several (48) of the various bodies or elements (48) inserted into the body (2) with an orifice (46) (Image 53); or by the pressure of the body (2) material on this fastening knot (18) and on/against the support part ( with possible projections, orifice ) wedge like , or not.
  • the parts designed to couple between them may be coupled in the support part (8) just like (23), (24), (33), once they are coupled, they may be coupled to the body (2) as directional elements, with the possibility of coupling either in the part (8) to the body (2) cavity (1) shown on Image 23; or directly in this cavity (1), Image 24.
  • the directional elements (23),(24),...on their external side appearing from the body(2) Image 24, comprise a central axle (21) with a possible longitudinal flexible fissure ( fissures, projections, etc.) with aerodynamic wings (22) etc. with possible fissure/s and/or aerodynamic projection/s(41), Image 25, suitable curvatures, if necessary and for a better adaptation ,variable size, and depending on the sizes, shapes, design and weight of the body (2).
  • This axle is normally thicker than the base (28) or the coupling section, to introduce into the body (2), Image 24, comprised of projection/s (26) or fastening rings and of male and female (25) couplers (or not ) on their internal faces (27) ( or their hypothetical extension )which form an angle obtained dividing 360 degrees by the number of coupled elements, and according to the resulting degrees even fewer elements may be coupled ( or elements of any number of degrees) proportionaly reaching 360 degrees by inserting wedges between them, like 1,2,3,4,5, etc coupled elements: so, with an angle of 90 degrees (31) Image 17 , it is possible : to couple 4 identical or different elements (23), (24), (33) Image 20 ; or 3 with 3 wedges inserted of 30 degrees (30), Image 21; or 2 with 2 wedges of 90 degrees , with an angle of 120 degrees (32) it is possible to couple 3 elements (Image 22 ); or 2 with 2 wedges of 60 degrees, etc. with rings or similar circling the base(28), as brackets.
  • the external part of these directional elements (23), (24),(38), (39),etc. may have one or several directional elements inserted, as shown on Image 25, a cross section view of cutting line (41) of the aerodynamic design used as an example as well as other different views of examples of other possible aerodynamic shapes adopted by these directional elements, on their external part; with one or several axes (21) or nothing but a sort of curved membrane (42), with one or several wings (22).
  • This coupling and fastening system of the base in the body (2) is perfectly valid for different shapes of directional elements of any sort, type.
  • These directional elements coupled, or part of them, may be cast by injecting one single piece as (7), Images 49, 51, 52 ; their external part has the following possibilities: a) to place 1,2,3,4,..directional elements, etc. ; b) adopt different shapes as shown on Image 25, with one or several wings (22) one or several axes (21) or none (42); c) these may be joint by their wing (42) or wings (22) or by their axles (21) ; d) none of these parts may be used or shared (42), (22), (21) by one or several elements at once, they may also be coupled : by the exterior side of part (8) ( with a fastening piece in the cavity (9), an exterior bracket, etc.) ; or in its cavity (9)as (7) with the possible fastening piece (44), Image 50, or without it, with the base (28) now integrated, and part (8) in the body (2), Image 51; or couple directly in the body (2) , if it is without the base (28) with the help of these parts such as (
  • the body may be fastened to the end of an elastic ribbon, the opposite end is fix to make it draw back when launched.
  • the body (2) may be composed of a body (2) or several bodies (48) or parts, superposed and fitted between them, integrating into a single body (2) Image 53, with multiple shapes ( or various shapes at once ) in concentric layers as an onion, in spheric sectors as orange segments, with possible fissure/s, projection/s, orifice/s (46), males and females, with different possibilities for a) increase or decrease the volume only by changing them (48) (2); b) change the exterior shape only by changing the shape of the exterior part/s (2)(48) ; c) one or several of these bodies or parts work as support part, fastening the knot (18) with a possible orifice (46), Image 53, in it etc.

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  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Physical Education & Sports Medicine (AREA)
  • Toys (AREA)

Abstract

Objet volant comprenant un corps (2) normalement élastique (avec un seul corps (2) ou plusieurs corps (48) intégrés en un seul corps (2) et pouvant rebondir ou non), présentant une configuration aérodynamique (figures (1, 6 et 53), de dimensions variables, et pouvant également adopter des formes multiples, et présentant une cavité (1) variable permettant la fixation d'éléments directionnels tels que (17, 23, 24) etc., (qui varient en fonction des utilisations recherchées, etc.), et présentant également une pièce porteuse (8), creuse (9), etc., pouvant porter des éléments directionnels tels que (17, 24, etc.), et en fonction de la forme du creux (9) et de la position de l'accouplement des éléments dans le corps (2), il est possible de varier lesdits éléments et par conséquent les utilisations. Avec une huppe (17) et un cordon (16) (ou seulement le cordon (16)) on peut le lancer comme une fronde, le faire voler comme un cerf-volant avec des éléments tels que (7, 24, etc.), on peut le lancer en le tapant avec les mains, ou avec des raquettes, etc., ou on peut l'utiliser uniquement avec la huppe (17), etc., comme un jeu, un jouet ou un sport. L'objet volant présente également des possibilités publicitaires, etc.
EP93911511A 1992-04-22 1993-04-22 Volant ayant divers usages Pending EP0604658A1 (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
ES9200851 1992-04-22
ES09200851A ES2076848B1 (es) 1992-04-22 1992-04-22 Nuevo objeto volador lanzable, con multiples posibilidades combinablesde realizacion y usos.
PCT/ES1993/000029 WO1993020902A1 (fr) 1992-04-22 1993-04-22 Volant ayant divers usages

Publications (1)

Publication Number Publication Date
EP0604658A1 true EP0604658A1 (fr) 1994-07-06

Family

ID=8276803

Family Applications (1)

Application Number Title Priority Date Filing Date
EP93911511A Pending EP0604658A1 (fr) 1992-04-22 1993-04-22 Volant ayant divers usages

Country Status (5)

Country Link
EP (1) EP0604658A1 (fr)
AU (1) AU4041493A (fr)
CA (1) CA2112668A1 (fr)
ES (1) ES2076848B1 (fr)
WO (1) WO1993020902A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5976907B1 (ja) * 2015-08-17 2016-08-24 株式会社コスモ精機 バドミントン用シャトル

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2312855B (en) * 1996-05-10 1999-12-01 William Charles Carlton An improved shuttlecock

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1035547B (de) * 1956-01-02 1958-07-31 Karlhans Krohn Handschlagfederball
US3934873A (en) * 1974-04-29 1976-01-27 Griffin Billy J Baseball batting aid
ES273574Y (es) * 1983-07-15 1984-07-01 Galan Rodriguez Jose R Cometa de juguete
CA1246627A (fr) * 1984-03-22 1988-12-13 Roy W. Buckland Volants de badminton
US4813686A (en) * 1988-01-19 1989-03-21 Miranda Gonzalo F Shuttlecock
FR2646356A1 (fr) * 1989-04-28 1990-11-02 Rizio Yves Volant notamment pour jeu de lancer
FR2650959B1 (fr) * 1989-08-21 1991-11-15 Astri Jean Jeu d'adresse analogue a une fronde ou comete compose d'au moins deux balles disposees a l'extremite d'un bout qui, apres tournoiement permet le jet en direction d'une cible

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO9320902A1 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5976907B1 (ja) * 2015-08-17 2016-08-24 株式会社コスモ精機 バドミントン用シャトル
JP2017038634A (ja) * 2015-08-17 2017-02-23 株式会社コスモ精機 バドミントン用シャトル

Also Published As

Publication number Publication date
ES2076848B1 (es) 1996-08-16
CA2112668A1 (fr) 1993-10-28
ES2076848A1 (es) 1995-11-01
AU4041493A (en) 1993-11-18
WO1993020902A1 (fr) 1993-10-28

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