WO2007000983A1 - Darts tip, darts shaft, and darts - Google Patents

Darts tip, darts shaft, and darts Download PDF

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Publication number
WO2007000983A1
WO2007000983A1 PCT/JP2006/312759 JP2006312759W WO2007000983A1 WO 2007000983 A1 WO2007000983 A1 WO 2007000983A1 JP 2006312759 W JP2006312759 W JP 2006312759W WO 2007000983 A1 WO2007000983 A1 WO 2007000983A1
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WO
WIPO (PCT)
Prior art keywords
shaft
flight
dart
tip
board
Prior art date
Application number
PCT/JP2006/312759
Other languages
French (fr)
Japanese (ja)
Inventor
Jun Nakamura
Original Assignee
Ron Corporation
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from JP2005009781U external-priority patent/JP3118732U/en
Application filed by Ron Corporation filed Critical Ron Corporation
Priority to JP2007523942A priority Critical patent/JPWO2007000983A1/en
Publication of WO2007000983A1 publication Critical patent/WO2007000983A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B6/00Projectiles or missiles specially adapted for projection without use of explosive or combustible propellant charge, e.g. for blow guns, bows or crossbows, hand-held spring or air guns
    • F42B6/003Darts

Definitions

  • the present invention relates to a duck, a dart chip (or a point) which is a component thereof, and a dull shaft.
  • the dart is composed of a tip, a barrel, a shaft, and a fly from the leading end side. Also, the dart has a metal needle at the tip, a hard dart to play by throwing it on a board compressed with hemp, and a plastic with a countless hole formed at the tip.
  • a soft darts that are thrown toward the board made of greaves. Soft darts have been widely used in recent years because they are made of plastic at the tip and are therefore very safe and can be played easily.
  • FIG. 9 shows an example of a conventional soft dart chip (or point).
  • the tip 300 has a narrow tip 302, and a middle portion 306 is provided with a node 306 having a large diameter.
  • the node 306 is provided so as not to go too far into the hole in the board, and may be provided as necessary.
  • the other end 304 is a screw part that can be attached to and detached from the end of the barrel (not shown).
  • the duck is stuck.
  • the cross section is almost circular as shown in FIG. 9 (B).
  • the circular shape here includes not only perfect circles but also those that are slightly elliptical due to manufacturing errors (such as precision when cutting the mold)!
  • the shaft is a body of V, a dull dart, and when the barrel and the flight are connected and thrown, in most cases, the shaft has a barrel. It has become.
  • the flight is attached by inserting a part of the flight into a substantially cross-shaped slit formed on the tip side of the shaft.
  • the shaft is provided with a slit that penetrates in a direction substantially perpendicular to the axial direction of the shaft. However, it may be attached through a flight folded flat in the slit.
  • Patent Document 1 Japanese Unexamined Patent Application Publication No. 2004-242937
  • the background art as described above has the following disadvantages.
  • the cross-sectional shape of the chip 300 is substantially circular, a strong force is required when pulling out a dart having a large contact area with the hole in the board.
  • the chip 300 currently in use is weak in durability and is bent or broken immediately, so the replacement frequency is very high. For this reason, it is convenient for a player to be as hard and durable as possible and to be able to use chips.
  • the dart base hurts and the durable life is reduced. The number of tournaments is increasing!
  • the fixed range of the flight is narrow or there are few fixed points, so the flight may easily lose its shaft force.
  • the method of passing the flight through the slit that penetrates the shaft also has the disadvantage that the flight does not open firmly in a cruciform shape and tends to be crushed, so that the stability when flying a dart is lacking.
  • the present invention focuses on the above points, and its purpose is to improve the durability without using a hard material and to remove the board from the board immediately and without damaging the board. Is to provide a chip.
  • Another object is to provide a dull shaft that does not easily disengage the flight from the shaft and that can maintain a flight shape suitable for stable flight.
  • Yet another objective is that a subsequent duck is played by a duck that is already stuck. It is to provide a dart that can alleviate.
  • the dart chip of the present invention is a chip in which the tip side is fitted into a hole provided in the board and the other end side is detachable from the duck body,
  • the cross section of the portion that contacts the hole has a shape other than a circle.
  • the main form is that at least one groove is provided along the longitudinal direction on the surface of the portion that contacts the hole of the board, or at least one or more is provided on the surface of the portion that contacts the hole of the board. It is characterized by providing a hole or a depression.
  • a dart of the present invention is characterized in that the dart chip according to any one of claims 1 to 3 is provided at a tip.
  • the dart shaft of the present invention is a dart shaft to which a flight is detachably attached, and is formed in the axial direction of the duck shaft, and all surfaces of the flight composed of a plurality of blade pieces are disposed on the flight surface. It is characterized by having a plurality of grooves or notches that can be fixed over a wide range in the axial direction.
  • a dart shaft of another invention is a dart shaft to which a flight is detachably attached, and is formed in the axial direction of the duck shaft, and all the surfaces of the flight composed of a plurality of blade pieces are all over the surface.
  • a plurality of groove notches that can be fixed over a wide range in the axial direction of the flight, and a detachable provided at the end of the dart shaft, and closing the ends of the plurality of grooves or notches It is characterized by that.
  • One of the main forms is characterized in that the plurality of grooves or notches have a step for determining a fixed position of the flight.
  • the dart of another invention is a dart composed of a flight and a part that can be divided into a plurality of parts in the axial direction, and has flexibility in at least one part between the divided parts.
  • the squeezing member is detachably provided.
  • One of the main forms is characterized in that the stagnation member is formed of rubber.
  • Another embodiment is characterized in that it also serves as a weight for adjusting the squeezing member force and weight.
  • the dart of another invention is characterized in that it is formed of a material softer than at least a part of the force part of the shaft part to which the flight is attached.
  • the tip of the dart chip that is, the cross section of the contact portion with the board
  • the burden applied to one point is reduced and the durability is improved.
  • the durability of the chip is enhanced, which reduces the burden on the dart board that does not require the use of hard materials, and improves the durability of the board.
  • the contact area with the boat is small, it is possible to pull out the dart without requiring a strong force.
  • a flexible squeeze member is detachably attached to at least any portion of the force between the divided parts in a dart composed of parts that can be divided into a plurality of parts in the axial direction. Or, at least a part of the shaft part to which the flight is attached was made of a softer material than the other parts. For this reason, even when a subsequent dart hits a dart that is being stabbed, at least a part of the dart that is stabbing will be played, so that the subsequent dart can be played and stable play can be performed. .
  • FIG. 1 is a diagram showing Example 1 of the present invention
  • (A) is a perspective view showing the appearance of a chip of this example
  • (B) is a chip of this example.
  • (C) is a cross-sectional view of (A) cut along line # A— # A and viewed in the direction of the arrow.
  • FIG. 2 is a view showing a modification of the chip of the first embodiment, (A) is a plan view, and (B) to (D) are sectional views.
  • FIG. 3 is a diagram showing another embodiment of the present invention
  • (A) is a perspective view showing the appearance of the chip of Example 2
  • (B) shows the appearance of the chip of Example 3.
  • a plan view, (C) is a sectional view of (B) cut along line # B- # B and viewed in the direction of the arrow.
  • FIG. 4 is a view showing Example 4 of the present invention
  • A is an external perspective view of a dart using the shaft of this example
  • B is an external perspective view of the shaft
  • C shows the mounting part of the shaft.
  • D is a perspective view showing a state before connection between the mounting portion and the connecting portion of the shaft
  • E is a perspective view showing (A) with different angular forces.
  • FIG. 5 is a view showing Example 5 of the present invention
  • A is an external perspective view of a dart using the shaft of this example
  • B is an external perspective view of the shaft
  • C is a perspective view in which the shaft is unfolded and the inner force is seen
  • D is a perspective view in which the shaft is unfolded and the outer force is also seen.
  • FIG. 6 is a diagram showing Example 6 of this example, (A) is an external perspective view of a duck using the shaft of this example, (B) is an external perspective view of the shaft, (C)-(E) is the perspective view which also looked at the angle force different from said (A) and (B), and the mode that a flight was attached to the said shaft.
  • FIG. 7 is an external perspective view showing Example 7 of the present invention.
  • FIG. 8 is a view showing Example 8 of the present invention
  • (A) is an external perspective view of the duck of this example
  • (B) is an exploded perspective view of the duck
  • (C) is a book. It is a disassembled perspective view which shows the modification of an Example.
  • FIG. 9 is a diagram showing an example of the background art
  • (A) is a perspective view showing the appearance
  • (B) is the above (A) cut along line # C # C, and in the direction of the arrow FIG.
  • A-122D Feather pieces
  • a ⁇ 150D Slit
  • a soft dart generally has a tip formed of plastic (salley, sardine) at the tip.
  • the dart chip of the present invention is applied.
  • Fig. 1 (A) is a perspective view showing the external appearance of the chip (or no point) of this embodiment
  • Fig. 1 (B) is an external perspective view of a duck using the chip of this embodiment
  • Fig. 1 (C) is an external perspective view of a duck using the chip of this embodiment
  • Fig. 3 is a cross-sectional view of Fig. 1 (A) taken along line # A- # A and viewed in the direction of the arrow.
  • FIG. 2 is a view showing a modification of the chip of this embodiment
  • FIG. 1 (A) is a perspective view showing the external appearance of the chip (or no point) of this embodiment
  • Fig. 1 (B) is an external perspective view of a duck using the chip of this embodiment
  • Fig. 1 (C) is a cross-sectional view
  • FIG. 2 (A) is a plan view
  • FIGS. 2 (B) to 2 (D) are sectional views.
  • the dart 50 is composed of a tip (or point) 10 that is a tip portion that fits into a hole in the board, a barrel 52, a shaft 54, and a flight 56.
  • the tip 10 shown in FIG. 1 (A) has a narrow tip 12 side, and a node 16 having a large diameter is provided in the middle portion. Section 16 may be provided as necessary.
  • the other end portion 14 is formed with a screw portion so as to be detachable from the end portion of the barrel 52.
  • a plurality of grooves 18 are formed on the surface of the chip 10 along the longitudinal direction from the tip 12 to the other end 14 side. As shown in the cross-sectional view of FIG. 1 (C), in this embodiment, four grooves 18 are formed, so that the cross section on the tip side of the chip 10 has a shape other than a circle. The area of contact with holes on the board not shown is decreasing.
  • the circle in the present invention includes not only a perfect circle but also a circle that is slightly elliptical due to a manufacturing error.
  • the groove 18 is provided to increase the durability of the chip 10 and to make it easier to remove the board force.
  • the groove 18 is provided between the tip 12 and the node 16. May be provided only. In other words, it is only necessary to be provided at least in a portion that contacts the hole of the board.
  • materials for forming the chips 10 and 10A various known hard plastic materials can be used so as not to damage the board.
  • Such a chip 10 (or 10A) is connected to the barrel 52 and, together with the shaft 54 and the flight 56, constitutes the duck 50.
  • the dart 50 Throw the dart 50 with the tip 10 (or 10A) at the tip toward a board (not shown), and if the tip 12 side fits into one of the numerous holes provided on the board, the dart 50 is targeted. It becomes stabbed. At this time, since the groove 18 is provided on the surface of the chip 10, it shrinks at the moment of being stabbed into the board, and after it is stabbed, a force to spread is applied, so that it falls out. On the other hand, when removing from the board Since the contact area with the board is reduced by the formation of the groove 18, it can be easily removed from the board without requiring a strong force.
  • FIGS. 2B to 2D show cross sections of modified examples of the present embodiment. These cross-sectional views correspond to the cross section of FIG.
  • a chip 10B shown in FIG. 2 (B) is an example in which a groove 18B deeper than the chip 10 is formed.
  • the chip 10C shown in FIG. 2 (C) is an example in which a relatively large number of relatively shallow grooves 18C are uniformly provided on the entire surface.
  • the chip 10D shown in FIG. 2 (D) has a substantially hexagonal cross section. In any of the chips 10B to 10D, the basic operation and effect are the same as those of the chips 10 to 10A shown in FIG. 1 or 2A described above.
  • FIG. 3A is a perspective view showing the appearance of the chip of this example.
  • a plurality of substantially linear grooves are provided in the longitudinal direction from one end of the chip to the other end.
  • the tip 22 is connected to the other end.
  • a plurality of grooves 28 are formed in a spiral manner over 24.
  • the functions and effects of the present embodiment are the same as those of the first embodiment described above.
  • the groove 28 may be provided only between the node 26 and the tip 22 as in the first embodiment.
  • Fig. 3 (B) is a plan view showing the appearance of this embodiment
  • Fig. 3 (C) is a cross-sectional view of Fig. 3 (B) taken along line # B- # B and viewed in the direction of the arrow. is there.
  • the tip 30 of this embodiment is hung from the tip 32 to the node 36.
  • a plurality of depressions 38 are provided at appropriate intervals.
  • a continuous groove from the tip force of the tip to the other end side is formed. Even if the recess 38 or the hole is provided, the same effect as in the first embodiment can be obtained.
  • the recess 38 may be provided from the node 36 to the end 34 side.
  • FIG. 4 (A) is an external perspective view of a dart using the shaft of this embodiment
  • Fig. 4 (B) is an external perspective view of the shaft
  • Fig. 4 (C) is an enlarged view of the mounting portion of the shaft.
  • FIG. FIG. 4 (D) is a perspective view showing a state before connection between the mounting portion and the connecting portion of the shaft
  • FIG. 4 (E) is a perspective view showing the angular force different from (A).
  • the shaft 100 of the present embodiment is for detachably attaching a fly 122 in which four blade pieces 122A to 122D are opened in a substantially cross shape, and a mounting portion 112 to which the flight 122 is attached. And a connecting portion 124 for connecting the mounting portion 112 to the barrel 180.
  • the shaft 100 has a substantially cylindrical shape as a whole.
  • the mounting portion 112 is such that the holding pieces 112A to 112D each having a shape obtained by dividing the cylinder into four in the axial direction open in a substantially cross shape with the one end portion 114 as the center. It becomes.
  • the other end portions 118A to 118D of these sandwiching pieces 112A to 112D are formed narrower than the end portion 114 side, and when the sandwiching pieces 112A to 112D are closed, as shown in FIG.
  • the end portion 118 is detachably connected to one end portion 126 of the connecting portion 124.
  • the mounting portion 112 and the coupling portion 124 are connected by fitting the convex end portion 118 and the concave end portion 126, but they are connected by various other known mechanisms. It's okay.
  • the sandwiching pieces 112A to 112D are set so as to be substantially the same as or slightly longer than the axial length of the partial force flight 122 excluding the end portions 118A to 118D, and the surfaces 115 and 116 that are substantially orthogonal to each other.
  • the surface of the flight 122 is sandwiched and fixed by these surfaces.
  • the other end 128 of the connecting portion 124 is attached to and detached from the end 182 of the barrel 180. Connected to the expression.
  • the shaft 100 and the barrel 180 are connected by, for example, screwing of the screw portions formed at the respective end portions 128 and 182 as shown in the figure. .
  • the convex end portion 118 for connecting to the connecting portion 124 and the groove 120 for sandwiching the surface of the flight 122 (see FIG. 4 (B)) Is formed.
  • the blade piece 122A is fixed from both surfaces by the sandwiching pieces 112A and 112D
  • the blade piece 122B is fixed from both surfaces by the sandwiching pieces 112A and 112B.
  • the other blade pieces 122C and 122D are similarly fixed from both sides.
  • the center of the flight 122 is aligned with the center of the mounting portion 112 (that is, the end portion 114) opened in a substantially cross shape. Then, the sandwiching pieces 112A to 112D are closed, and the blade pieces 122A to 122D are sandwiched from both sides to fix the flight 122.
  • the end portion 118 of the mounting portion 112 and the end portion 126 of the connecting portion 124 are connected, and finally, as shown in FIG.
  • the part 182 is connected to the other end 128 of the connecting part 124.
  • a tip 184 shown in FIG. 4 (A) is connected in advance to the tip of the barrel 180.
  • FIG. 5A is an external perspective view of a duck using the shaft of this embodiment
  • FIG. 5B is an external perspective view of the shaft
  • Fig. 5 (C) shows the state where the shaft is expanded inside
  • Fig. 5 (D) is a perspective view of the shaft in an unfolded state as seen from the outside force.
  • the shaft 130 of the present embodiment is substantially cylindrical as in the fourth embodiment, and the cylinder is divided into four in the axial direction as shown in Figs. 5 (C) and (D).
  • the sandwiching pieces 130A to 130D having the above shapes are configured to open in a substantially cross shape with the one end portion 132 as the center.
  • the end portions 138 8 to 1380 of these sandwiching pieces 1308 to 1300 are formed narrower than the end portion 132 side, and when the sandwiching pieces 130A to 130D are closed, the end portion 138 becomes the end portion of the barrel 180A.
  • Removably connected to 182A In the example shown in the figure, the connection is made by fitting the convex end 138 and the concave end 182A.
  • the sandwiching pieces 130A to 130D have portions except for the end portions 138A to 138D longer than the axial length of the flight 122, so that an appropriate interval is provided from the end portion 138 to the flight 122. It has become. That is, the partial force from the end portion 138 to the flight 122 corresponds to the connecting portion 124 of the fourth embodiment described above.
  • the sandwiching pieces 130A to 130D have surfaces 134A and 136A that are substantially orthogonal to each other, and the surface of the flight 122 is fixed by these surfaces.
  • steps 140A to 140D are formed in the sandwiching pieces 130A to 130D. These steps 140A to 140D change the thickness of the grooves 142 and 144 shown in FIG. 5 (B) when the sandwiching pieces 130A to 130D are closed, and position the flight 122 based on the difference in thickness. Is.
  • the force at which the flight 122 is moved toward the end 132 side of the shaft 130 can change the fixing position of the flight 122 by changing the positions of the steps 140A to 140D as necessary.
  • an effect that the fixed position of the flight 122 can be changed is obtained.
  • the shaft 130 does not have to be a two-part configuration including a mounting portion and a connecting portion, the number of parts is reduced, and manufacturing and assembly are facilitated.
  • FIG. 6A is an external perspective view of a dart using the shaft of this embodiment
  • FIG. 6B is an external perspective view of the shaft
  • FIGS. 6 (C) to 6 (E) are perspective views showing how the flight is attached to the shaft, and show a state seen from an angle different from FIGS. 6 (A) and 6 (B).
  • the groove provided on the shaft is formed with the barrel side force directed toward the tip.
  • the embodiment is an example in which the groove is formed by directing the tip end of the shaft toward the barrel side.
  • the shaft 150 of the present embodiment is substantially cylindrical, and as shown in FIG. 6 (C), four slits 150A to 150D force along the axial direction from one end 154 side to the vicinity of the center. Is formed. These slits 150A to 150D are formed in a substantially cross shape so as to divide the end portion 154 side of the shaft 150 into four, and a flight 122 is inserted therein. A cap 156 having a fitting portion 158 and a head portion 160 is detachably provided in the opening on the end portion 154 side. The other end of the shaft 150 can be attached to the other end of the shaft 150, or the end of the nore 180 can be attached or detached. The functions and effects of the present embodiment are the same as those of the fourth embodiment described above, but the fixing position of the flight 122 can also be adjusted by adjusting the depths of the slits 150 to 150D.
  • FIGS. 7A and 7B are external perspective views showing the shaft of this embodiment.
  • the shaft 170 is formed from the end 174 side of one of the four slits 170A to 170D along the axial direction to the vicinity of the center, as in the sixth embodiment.
  • Slits 170C and 170D are not shown.
  • These slits are formed in a substantially cross shape so as to divide the end portion 174 side into four, and the flight 122 is inserted therein.
  • a ring 176 formed of, for example, rubber on the outer peripheral surface on the end 174 side, the flight 122 is prevented from being detached.
  • a spring 178 may be attached to the outer peripheral surface on the end portion 174 side to prevent the flight 122 from coming off.
  • FIG. 8 (A) is an external perspective view of the duck of this embodiment
  • FIG. 8 (B) is an exploded perspective view of this embodiment
  • FIG. 8 (C) is an exploded perspective view of a modification of this embodiment.
  • the dart 200 of this embodiment is provided between the shaft 204 and the nozzle 206, the force of the fly 202, the shaft 204, the nozzle 206, and the tip 208.
  • the stagnation member 210 is formed.
  • FIG. 8 (A) is an external perspective view of the duck of this embodiment
  • FIG. 8 (B) is an exploded perspective view of this embodiment
  • FIG. 8 (C) is an exploded perspective view of a modification of this embodiment.
  • the dart 200 of this embodiment is provided between the shaft 204 and the nozzle 206, the force of the fly 202, the shaft 204, the nozzle 206, and the tip 208.
  • the stagnation member 210 is formed.
  • the squeeze member 210 is connected to both ends of an elastic body 212 such as rubber, for example, a connecting portion 214 detachably connected to the end portion 204A of the shaft 204, and the barrel 206. Removable on end 206A A connecting portion 216 to be connected is provided.
  • the connecting portions 214 and 216 are formed of, for example, a synthetic resin or a metal, but the entire stagnation member 210 may be integrally formed of, for example, rubber or other flexible material. It should be noted that the squeezing member 210, the shaft 204, and the parallel 206 are attached and detached in the example shown in the figure by force fitting by screwing of the threaded portion or by other known mechanisms. ,.
  • the tip 208 is a soft dart or a hard duck, and a force in which plastic or metal is used.
  • the shaft 204 and the barrel 206 are made of metal or the like. If you throw a dart without wearing the kneading member 210, the shaft 204 or barrel 206 will not work if it hits a duck that has already been stabbed. Sometimes. However, by providing the stagnation member 210 between the shaft 204 and the barrel 206, the shaft 204 can be moved relative to the barrel 206 by the flexibility of the elastic body 212 even when the subsequent duck 200 hits. As a result, it is less likely to play the subsequent dart 200, and stable play can be achieved. Further, as shown in FIG.
  • the stagnation member 210 may be mounted so as to be sandwiched between the end portion 206 B of the barrel 206 and the end portion 208 A of the chip 208. This portion may be provided with a weight (or weight) for weight adjustment depending on the player, but the weight of the duck 200 may be adjusted by the kneading member 210.
  • the stagnation member 210 as a whole or the elastic body 212 can be made of heavy rubber, or metal can be used for the connecting portions 214 and 216.
  • the squeezing member 210 made of the elastic body 212 is detachably mounted between the shaft 204 and the nozzle 206 or between the nozzle 206 and the tip 208, it is already stuck. Even when a subsequent duck hits the duck 200, the elastic body 212 is bent, so that it is possible to reduce the bounce of the subsequent duck.
  • the cross-sectional shape of the tip portion of the chip may be a shape other than a circle, such as a polygon, such as a triangle, a rectangle, or an octagon, as well as a star or an ellipse, in addition to the above-described Examples 1 to 3. That's fine.
  • a shape that is slightly elliptical due to a manufacturing error is not included in the shape other than the circle in the present invention.
  • the shaft and barrel are substantially cylindrical, but a shape having a polygonal or elliptical cross section may be used.
  • Embodiments 4 to 7 are also examples, and may be appropriately changed as necessary, such as providing nodes.
  • Examples 4 to 7 are applied to a force with a structure in which the shaft and the barrel are detachable, or a dart having a structure in which the shaft, the barrel, and the chip are integrated. You can do it.
  • the cap 156 of the sixth embodiment, the ring 176 and the spring 178 of the seventh embodiment are examples, and the design may be changed as appropriate so as to achieve the same effect.
  • the kneading member 210 is provided at any one of the duck 200, but it is mounted between the shaft 204 and the norrel 206, and between the barrel 206 and the tip 208. You may make it. Further, in the eighth embodiment, the squeezing member 210 is not prevented from being mounted separately by the force that also serves as the weight adjusting weight. Of course, the squeezing member 210 can be applied to a dart having a structure in which a shaft and a barrel are integrated or a chip and a barrel are integrated. In addition, the material constituting the stagnation member 210 is You may use the raw material which has well-known various softness
  • connection method between the shaft and barrel, the connection method between the barrel and the tip, or the connection method between the rubbing member 210 and the shaft, barrel, and tip shown in the above embodiment is also an example, and the same effect is achieved. As described above, various known connection methods may be used.
  • the tip part of the dart chip that is, the cross section of the contact part with the board has a shape other than a circle, thereby improving the durability of the chip without using a hard material, It can be applied to soft dart applications using plastic chips because it does not damage the board as soon as it is removed from the board.
  • a flexible squeeze member is detachably attached to at least any portion of the force between the divided parts in a dart formed of parts that can be divided into a plurality of parts in the axial direction. Or, at least a part of the shaft part to which the flight is attached was made of a softer material than the other parts. For this reason, even when a subsequent duck hits a duck that has already been stabbed, it is less likely to play the subsequent duck, so it can be applied to the use of a dart for stable play.

Abstract

A darts enabling an increase in the durability of a darts tip without using a hard material and the easy extraction thereof from a board and preventing the board from being damaged and the tip of the darts. Four grooves (18) are formed in the surface of the tip (10) along the longitudinal direction from its tip (12) up to its other end (14), and the cross section thereof is formed in a shape other than circular shapes. The tip (12) is fitted to a board hole, and the other end (14) is formed detachable from the end of a barrel not shown. Since the cross section of the contact portion of the tip with the board is formed in a shape other than circular shapes by forming the grooves (18) therein, a load applied to one point is reduced and the durability of the tip (10) can be increased. Since the durability of the tip (10) is increased depending on the shape thereof, the hard material must not be used for the tip, the load on the darts board is reduced, and the durability of the board can be increased. Furthermore, since the contact area of the tip with the board is reduced, the darts tip can be easily extracted from the board.

Description

明 細 書  Specification
ダーッチップ,ダーッシャフト,ダーッ  Dart chip, dart shaft, dart
技術分野  Technical field
[0001] 本発明は、ダーッ及びその構成部品であるダーッチップ (な 、しポイント) ,ダーッ シャフトに関するものである。  TECHNICAL FIELD [0001] The present invention relates to a duck, a dart chip (or a point) which is a component thereof, and a dull shaft.
背景技術  Background art
[0002] ダーッは、的に刺さる先端側から、チップ (な 、しポイント) ,バレル,シャフト,フライ トにより構成されている。また、ダーッには、先端部が金属製の針となっており、麻を 圧縮したボードに投げて競技するハードダーッと、先端部がプラスチックで形成され ており、無数の穴が設けられたプラスチック製 (榭脂製)のボードに向かって投げるソ フトダーッの 2種類がある。ソフトダーッは、先端がプラスチック製であることから安全 性に優れ、また、気軽に競技できることから、近年、広く普及し始めている。  [0002] The dart is composed of a tip, a barrel, a shaft, and a fly from the leading end side. Also, the dart has a metal needle at the tip, a hard dart to play by throwing it on a board compressed with hemp, and a plastic with a countless hole formed at the tip. There are two types of soft darts that are thrown toward the board made of greaves. Soft darts have been widely used in recent years because they are made of plastic at the tip and are therefore very safe and can be played easily.
[0003] 図 9には、従来のソフトダーッのチップ(ないしポイント)の一例が示されている。図 9 (A)の斜視図に示すように、チップ 300は、先端 302側が細くなつており、中間部分に はやゃ径が大きい節 306が設けられている。なお、節 306は、ボードの穴に入り込み 過ぎないように設けられているものであり、必要に応じて設けるようにすればよい。他 方の端部 304は、図示しないバレルの端部に対して着脱可能なネジ部となっている。 前記先端 302側が、ボードの穴に嵌ると、ダーッが的に刺さった状態となる。このよう なチップ 300を、 # C—# C線に沿って切断し矢印方向に見ると、その断面は、図 9( B)に示すように、ほぼ円形となっている。なお、ここでいう円形とは、真円のみならず、 製造上の誤差 (金型を削るときの精度など)により若干楕円形状などになったものも 含まれることは言うまでもな!/、。  FIG. 9 shows an example of a conventional soft dart chip (or point). As shown in the perspective view of FIG. 9 (A), the tip 300 has a narrow tip 302, and a middle portion 306 is provided with a node 306 having a large diameter. The node 306 is provided so as not to go too far into the hole in the board, and may be provided as necessary. The other end 304 is a screw part that can be attached to and detached from the end of the barrel (not shown). When the tip 302 side is fitted into the hole of the board, the duck is stuck. When such a chip 300 is cut along the # C- # C line and viewed in the direction of the arrow, the cross section is almost circular as shown in FIG. 9 (B). Needless to say, the circular shape here includes not only perfect circles but also those that are slightly elliptical due to manufacturing errors (such as precision when cutting the mold)!
[0004] ところで、上述したダーッ全般にお 、て、前記シャフトは、 V、わゆるダーッの本体で あって、前記バレルとフライトをつなぎ、投げるときには、多くの場合はバレルを持つ のが基本となっている。通常、フライトは、以下の特許文献 1に示すように、シャフトの 先端側に形成された略十字状のスリットにフライトの一部を差し込んで取り付けられる 。あるいは、シャフトに、該シャフトの軸方向と略直交する方向に貫通するスリットを設 け、そのスリットに平面状にたたんだフライトを通して取り付ける場合もある。 [0004] By the way, in the above-mentioned darts in general, the shaft is a body of V, a dull dart, and when the barrel and the flight are connected and thrown, in most cases, the shaft has a barrel. It has become. Usually, as shown in Patent Document 1 below, the flight is attached by inserting a part of the flight into a substantially cross-shaped slit formed on the tip side of the shaft. Alternatively, the shaft is provided with a slit that penetrates in a direction substantially perpendicular to the axial direction of the shaft. However, it may be attached through a flight folded flat in the slit.
特許文献 1:特開 2004— 242937公報  Patent Document 1: Japanese Unexamined Patent Application Publication No. 2004-242937
発明の開示  Disclosure of the invention
発明が解決しょうとする課題  Problems to be solved by the invention
[0005] し力しながら、以上のような背景技術には次のような不都合がある。まず、ソフトダー ッに関しては、前記チップ 300の断面形状が略円形であるため、ボードの穴との接触 面積が多ぐダーッを抜く際に強い力が必要となる。また、現在使用されているチップ 300は、耐久性が弱ぐすぐに曲がったり折れたりして交換頻度が非常に高い。この ためプレーヤとしては、できるだけ硬く耐久性が高 、チップを使用できれば都合がよ い。し力しながら、ダーツマシンを設置している店舗側では、硬いチップを使用される と、ダーッ台が痛み、耐久年数が減ってしまうという不都合があるため、硬いチップを 使用禁止にする店舗や大会が増えてきて 、ると!/、う状況である。  [0005] However, the background art as described above has the following disadvantages. First, regarding the soft dart, since the cross-sectional shape of the chip 300 is substantially circular, a strong force is required when pulling out a dart having a large contact area with the hole in the board. In addition, the chip 300 currently in use is weak in durability and is bent or broken immediately, so the replacement frequency is very high. For this reason, it is convenient for a player to be as hard and durable as possible and to be able to use chips. However, at stores where dart machines are installed, if hard chips are used, there is a disadvantage that the dart base hurts and the durable life is reduced. The number of tournaments is increasing!
[0006] 一方、ダーッ全般のフライトに関しては、上述した背景技術では、いずれの場合も フライトの固定範囲が狭い,あるいは、固定箇所が少ないために、フライトがシャフト 力もすぐに外れてしまうことがある。また、シャフトを貫通するスリットにフライトを通す 方法の場合は、フライトがしっかりと十字状に開かず潰れた形状になりやすいため、 ダーッを飛ばすときの安定性に欠けるという不都合もある。  [0006] On the other hand, with regard to the Dart flight in general, in the background art described above, in either case, the fixed range of the flight is narrow or there are few fixed points, so the flight may easily lose its shaft force. . In addition, the method of passing the flight through the slit that penetrates the shaft also has the disadvantage that the flight does not open firmly in a cruciform shape and tends to be crushed, so that the stability when flying a dart is lacking.
[0007] 更に、以上のようなダーッは、通常のプレーでは、 3本投げて 1スローとされ、一人 のプレーヤが 3本全て投げ終わるまでは、先に投げたダーッは的に刺さったままにさ れる。従って、既に刺さっているダーッによって、後続のダーッが弾かれやすくなると いう不都合がある。これを回避するためには、フライトがシャフトに対して回転するよう なダーッが用いられることもある力 十分な効果が得られて 、な 、のが現状である。  [0007] Further, in the normal play, the darts as described above are thrown to 1 throw, and until one player finishes throwing all 3 darts, the dart thrown first remains stuck. It is done. Therefore, there is an inconvenience that the duck that has already been stabbed is likely to play the subsequent duck. In order to avoid this, a dart that may cause the flight to rotate with respect to the shaft may be used.
[0008] 本発明は、以上の点に着目したもので、その目的は、硬い素材を使用することなく 耐久性を向上させるとともに、ボードから抜きやすぐかつ、ボードを痛めることがない ダーッ及びそのチップを提供することである。  [0008] The present invention focuses on the above points, and its purpose is to improve the durability without using a hard material and to remove the board from the board immediately and without damaging the board. Is to provide a chip.
[0009] 他の目的は、フライトがシャフトから容易に外れることがなぐかつ、安定した飛行に 適したフライト形状を維持することができるダーッシャフトを提供することである。  [0009] Another object is to provide a dull shaft that does not easily disengage the flight from the shaft and that can maintain a flight shape suitable for stable flight.
[0010] 更に他の目的は、既に的に刺さっているダーッによって、後続のダーッが弾かれる のを軽減することができるダーッを提供することである。 [0010] Yet another objective is that a subsequent duck is played by a duck that is already stuck. It is to provide a dart that can alleviate.
課題を解決するための手段  Means for solving the problem
[0011] 前記目的を達成するため、本発明のダーッチップは、ボードに設けられた穴に先端 側が嵌るとともに、他端側はダーッ本体に対して着脱可能なチップであって、前記ボ ードの穴と接触する部分の断面を、円以外の形状としたことを特徴とする。主要な形 態は、前記ボードの穴と接触する部分の表面に、長手方向に沿って少なくとも一つ 以上の溝を設ける,あるいは、前記ボードの穴と接触する部分の表面に、少なくとも 一つ以上の穴ないし窪みを設けることを特徴とする。  [0011] In order to achieve the above object, the dart chip of the present invention is a chip in which the tip side is fitted into a hole provided in the board and the other end side is detachable from the duck body, The cross section of the portion that contacts the hole has a shape other than a circle. The main form is that at least one groove is provided along the longitudinal direction on the surface of the portion that contacts the hole of the board, or at least one or more is provided on the surface of the portion that contacts the hole of the board. It is characterized by providing a hole or a depression.
[0012] 本発明のダーッは、請求項 1〜3のいずれかに記載のダーッチップが先端に設けら れたことを特徴とする。  [0012] A dart of the present invention is characterized in that the dart chip according to any one of claims 1 to 3 is provided at a tip.
[0013] 本発明のダーッシャフトは、フライトが着脱可能に取り付けられるダーッシャフトであ つて、該ダーッシャフトの軸方向に形成されており、複数の羽根片からなるフライトの 全ての面を、該フライトの軸方向の広範囲にわたって固定可能な複数の溝ないし切 れ込み,を備えたことを特徴とする。  [0013] The dart shaft of the present invention is a dart shaft to which a flight is detachably attached, and is formed in the axial direction of the duck shaft, and all surfaces of the flight composed of a plurality of blade pieces are disposed on the flight surface. It is characterized by having a plurality of grooves or notches that can be fixed over a wide range in the axial direction.
[0014] 他の発明のダーッシャフトは、フライトが着脱可能に取り付けられるダーッシャフトで あって、該ダーッシャフトの軸方向に形成されており、複数の羽根片からなるフライト の全ての面を、前記フライトの軸方向の広範囲にわたって固定可能な複数の溝ない し切れ込み,前記ダーッシャフトの端部に着脱可能に設けられており、前記複数の 溝ないし切れ込みの端部を閉塞する留め具,を備えたことを特徴とする。主要な形態 の一つは、前記複数の溝ないし切れ込みが、前記フライトの固定位置を決めるため の段差を有することを特徴とする。  [0014] A dart shaft of another invention is a dart shaft to which a flight is detachably attached, and is formed in the axial direction of the duck shaft, and all the surfaces of the flight composed of a plurality of blade pieces are all over the surface. A plurality of groove notches that can be fixed over a wide range in the axial direction of the flight, and a detachable provided at the end of the dart shaft, and closing the ends of the plurality of grooves or notches It is characterized by that. One of the main forms is characterized in that the plurality of grooves or notches have a step for determining a fixed position of the flight.
[0015] 他の発明のダーッは、フライトと、軸方向に複数に分割可能なパーツにより構成さ れているダーッであって、分割されたパーツ間の少なくともいずれかの部分に、柔軟 性を有する橈み部材を着脱可能に設けたことを特徴とする。主要な形態の一つは、 前記橈み部材が、ゴムにより形成されていることを特徴とする。他の形態は、前記橈 み部材力 重量調節用のおもりを兼ねることを特徴とする。  [0015] The dart of another invention is a dart composed of a flight and a part that can be divided into a plurality of parts in the axial direction, and has flexibility in at least one part between the divided parts. The squeezing member is detachably provided. One of the main forms is characterized in that the stagnation member is formed of rubber. Another embodiment is characterized in that it also serves as a weight for adjusting the squeezing member force and weight.
[0016] 更に他の発明のダーッは、フライトを取り付ける軸部の少なくとも一部力 他の部分 よりも柔らかい素材により形成されていることを特徴とする。本発明の前記及び他の 目的,特徴,利点は、以下の詳細な説明及び添付図面力 明瞭になろう。 [0016] Further, the dart of another invention is characterized in that it is formed of a material softer than at least a part of the force part of the shaft part to which the flight is attached. The above and other aspects of the invention The purpose, features, and advantages will be clear from the following detailed description and accompanying drawings.
発明の効果  The invention's effect
[0017] 本発明は、ダーッのチップの先端部分,すなわち、ボードとの接触部分の断面を円 以外の形状としたので、一点に力かる負担が軽減し、耐久性が向上する。また、チッ プの形状により耐久性を高めているため硬い素材を利用する必要がなぐダーッボ ードへの負担が軽減し、ボードの耐久性も向上する。更に、ボートとの接触面積が少 ないため、強い力を要することなくダーッを抜くことが可能となる。  [0017] In the present invention, since the tip of the dart chip, that is, the cross section of the contact portion with the board, has a shape other than a circle, the burden applied to one point is reduced and the durability is improved. In addition, the durability of the chip is enhanced, which reduces the burden on the dart board that does not require the use of hard materials, and improves the durability of the board. Furthermore, since the contact area with the boat is small, it is possible to pull out the dart without requiring a strong force.
[0018] また、シャフトの軸方向に設けた複数の溝ないし切れ込みによって、フライトの全て の面を、該フライトの軸方向の広範囲にわたって固定することとしたので、フライトがシ ャフトから外れに《なるとともに、フライト形状を安定した飛行に適した形状に保つこ とができると!、う効果が得られる。  [0018] In addition, since all the planes of the flight are fixed over a wide range in the axial direction of the flight by a plurality of grooves or notches provided in the axial direction of the shaft, the flight is detached from the shaft. At the same time, if the flight shape can be maintained in a shape suitable for stable flight!
[0019] 更に、軸方向に複数に分割可能なパーツにより構成されているダーッに、前記分 割されたパーツ間の少なくともいずれ力の部分に、柔軟性を有する橈み部材を着脱 可能に装着する,あるいは、フライトを取り付ける軸部の少なくとも一部を、他の部分 よりも柔らかい素材で形成することした。このため、的に刺さっているダーッに後続の ダーッが当たったときでも、的に刺さっているダーッの少なくとも一部がしなるため、 後続ダーッを弾きに《なり、安定したプレーを行うことができる。  [0019] Further, a flexible squeeze member is detachably attached to at least any portion of the force between the divided parts in a dart composed of parts that can be divided into a plurality of parts in the axial direction. Or, at least a part of the shaft part to which the flight is attached was made of a softer material than the other parts. For this reason, even when a subsequent dart hits a dart that is being stabbed, at least a part of the dart that is stabbing will be played, so that the subsequent dart can be played and stable play can be performed. .
図面の簡単な説明  Brief Description of Drawings
[0020] [図 1]図 1は、本発明の実施例 1を示す図であり、(A)は本実施例のチップの外観を示 す斜視図,(B)は本実施例のチップを用いたダーッの外観斜視図,(C)は前記 (A)を # A— # A線に沿って切断し矢印方向に見た断面図である。  FIG. 1 is a diagram showing Example 1 of the present invention, (A) is a perspective view showing the appearance of a chip of this example, and (B) is a chip of this example. A perspective view of the appearance of the dart used, (C) is a cross-sectional view of (A) cut along line # A— # A and viewed in the direction of the arrow.
[図 2]図 2は、前記実施例 1のチップの変形例を示す図であり、(A)は平面図,(B)〜(D )は断面図である。  FIG. 2 is a view showing a modification of the chip of the first embodiment, (A) is a plan view, and (B) to (D) are sectional views.
[図 3]図 3は、本発明の他の実施例を示す図であり、(A)は実施例 2のチップの外観を 示す斜視図,(B)は実施例 3のチップの外観を示す平面図,(C)は前記 (B)を # B— # B線に沿って切断し矢印方向に見た断面図である。  FIG. 3 is a diagram showing another embodiment of the present invention, (A) is a perspective view showing the appearance of the chip of Example 2, and (B) shows the appearance of the chip of Example 3. A plan view, (C) is a sectional view of (B) cut along line # B- # B and viewed in the direction of the arrow.
[図 4]図 4は、本発明の実施例 4を示す図であり、(A)は本実施例のシャフトを用いたダ ーッの外観斜視図,(B)は前記シャフトの外観斜視図,(C)は前記シャフトの装着部を 広げた状態を示す斜視図,(D)は前記シャフトの装着部と連結部の接続前の状態を 示す斜視図,(E)は前記 (A)を異なる角度力もみた斜視図である。 FIG. 4 is a view showing Example 4 of the present invention, (A) is an external perspective view of a dart using the shaft of this example, (B) is an external perspective view of the shaft, (C) shows the mounting part of the shaft. (D) is a perspective view showing a state before connection between the mounting portion and the connecting portion of the shaft, and (E) is a perspective view showing (A) with different angular forces.
 Yes
[図 5]図 5は、本発明の実施例 5を示す図であり、(A)は本実施例のシャフトを用いたダ ーッの外観斜視図,(B)は前記シャフトの外観斜視図,(C)は前記シャフトを広げた状 態を内側力も見た斜視図,(D)は前記シャフトを広げた状態を外側力も見た斜視図で ある。  FIG. 5 is a view showing Example 5 of the present invention, (A) is an external perspective view of a dart using the shaft of this example, (B) is an external perspective view of the shaft, (C) is a perspective view in which the shaft is unfolded and the inner force is seen, and (D) is a perspective view in which the shaft is unfolded and the outer force is also seen.
[図 6]図 6は、本実施例の実施例 6を示す図であり、(A)は本実施例のシャフトを用い たダーッの外観斜視図,(B)は前記シャフトの外観斜視図,(C)〜(E)は前記シャフトに フライトを取り付ける様子を、前記 (A)及び (B)とは異なる角度力も見た斜視図である。  FIG. 6 is a diagram showing Example 6 of this example, (A) is an external perspective view of a duck using the shaft of this example, (B) is an external perspective view of the shaft, (C)-(E) is the perspective view which also looked at the angle force different from said (A) and (B), and the mode that a flight was attached to the said shaft.
[図 7]図 7は、本発明の実施例 7を示す外観斜視図である。 FIG. 7 is an external perspective view showing Example 7 of the present invention.
[図 8]図 8は、本発明の実施例 8を示す図であり、(A)は本実施例のダーッの外観斜視 図,(B)は前記ダーッの分解斜視図,(C)は本実施例の変形例を示す分解斜視図で ある。  FIG. 8 is a view showing Example 8 of the present invention, (A) is an external perspective view of the duck of this example, (B) is an exploded perspective view of the duck, and (C) is a book. It is a disassembled perspective view which shows the modification of an Example.
[図 9]図 9は、背景技術の一例を示す図であり、 (A)は外観を示す斜視図,(B)は前記( A)を # C # C線に沿って切断し、矢印方向に見た断面図である。  [FIG. 9] FIG. 9 is a diagram showing an example of the background art, (A) is a perspective view showing the appearance, (B) is the above (A) cut along line # C # C, and in the direction of the arrow FIG.
符号の説明 Explanation of symbols
10A〜: L0D:チップ(な!/、しポイント)  10A ~: L0D: Chip (N! /, Shi point)
12 : :先端  12:: Tip
14 : :端部  14:: End
16 : :節  16:: clause
18, 18B, 18C :溝  18, 18B, 18C: Groove
20 : :チップ  20:: Chip
22 : :先端  22:: Tip
24 : :端部  24:: End
26 : :節  26:: clause
28 : :溝  28:: Groove
30 : :チップ  30:: Chip
32 : :先端 :端部32:: Tip :edge
:節 :section
:窪み : Depression
:ダーッ : Dar
:ノ レノレ  : Norenore
:シャフト(ダーッシャフト) :フライト  : Shaft (Dar shaft): Flight
:シャフト(ダーッシャフト) :装着部 : Shaft (Dar shaft): Mounting part
A〜112D:挟持片A-112D: clamping piece
, 118, 118A〜118D:端部, 116:面, 118, 118A-118D: end, 116: surface
:溝:groove
:フライト:Flight
A〜122D:羽根片A-122D: Feather pieces
:連結部: Connecting part
, 128:端部, 128: End
:シャフト:shaft
A〜130D:挟持片A ~ 130D: clamping piece
, 138, 138A〜138D:端部A, 136A:面, 138, 138A to 138D: Edge A, 136A: Surface
A〜140D:段差A ~ 140D: Step
, 144:溝, 144: Groove
:シャフト:shaft
A〜150D:スリットA ~ 150D: Slit
, 154:端部, 154: End
:キャップ:cap
:嵌合部 160:頭部 :Fitting portion 160: head
170:シャフト  170: Shaft
170A, 170B:スリット  170A, 170B: Slit
172, 174:端部  172, 174: end
176:リング  176: Ring
178:スプリング  178: Spring
180, 180A:バレル  180, 180A: barrel
182, 182A:端部  182, 182A: End
184:チップ  184: chip
200:ダーッ  200: Dart
202:フライト  202: Flight
204:シャフト  204: Shaft
204A, 206A, 206B, 208A:端部  204A, 206A, 206B, 208A: End
206:バレノレ  206: Valenore
208:チップ  208: Chip
210:橈み部材  210: Rubbing member
212:弾性体  212: Elastic body
214, 216:連結部  214, 216: Connection part
300:チップ  300: chip
302:先端  302: Tip
304.·端部  304..End
306:節  Section 306:
発明を実施するための最良の形態  BEST MODE FOR CARRYING OUT THE INVENTION
[0022] この発明には数多くの実施形態が有り得るが、ここでは適切な数の実施例を示し、 詳細に説明する。 [0022] Although there may be many embodiments of the present invention, an appropriate number of examples are shown and described in detail herein.
実施例 1  Example 1
[0023] 最初に、図 1及び図 2を参照しながら、本発明の実施例 1を説明する。本実施例は、 プラスチック (なレ、し榭脂)で形成されたチップを先端に有するソフトダーッ一般に対 して、本発明のダーッチップを適用した例である。図 1(A)は、本実施例のチップ (な いしポイント)の外観を示す斜視図,図 1(B)は、本実施例のチップを用いたダーッの 外観斜視図,図 1(C)は、前記図 1(A)を #A— # A線に沿って切断し、矢印方向に見 た断面図である。図 2は、本実施例のチップの変形例を示す図であり、図 2(A)は平面 図,図 2(B)〜(D)は断面図である。図 1(B)に示すように、ダーッ 50は、ボードの穴に 嵌る先端部分であるチップ (ないしポイント) 10と、バレル 52,シャフト 54,フライト 56 により構成されている。 First, Embodiment 1 of the present invention will be described with reference to FIG. 1 and FIG. In this example, a soft dart generally has a tip formed of plastic (salley, sardine) at the tip. In this example, the dart chip of the present invention is applied. Fig. 1 (A) is a perspective view showing the external appearance of the chip (or no point) of this embodiment, Fig. 1 (B) is an external perspective view of a duck using the chip of this embodiment, and Fig. 1 (C). Fig. 3 is a cross-sectional view of Fig. 1 (A) taken along line # A- # A and viewed in the direction of the arrow. FIG. 2 is a view showing a modification of the chip of this embodiment, FIG. 2 (A) is a plan view, and FIGS. 2 (B) to 2 (D) are sectional views. As shown in FIG. 1 (B), the dart 50 is composed of a tip (or point) 10 that is a tip portion that fits into a hole in the board, a barrel 52, a shaft 54, and a flight 56.
[0024] まず、図 1(A)〜(: C)に示す例について説明する。図 1(A)に示すチップ 10は、先端 1 2側が細くなつており、中間部分にはやゃ径が大きい節 16が設けられている。なお、 節 16は、必要に応じて設ければよい。他方の端部 14には、前記バレル 52の端部に 対して着脱可能となるように、ネジ部が形成されている。また、チップ 10の表面には、 前記先端 12から他方の端部 14側まで、長手方向に沿って複数の溝 18が形成され ている。図 1(C)の断面図に示すように、本実施例では、 4つの溝 18が形成されており 、それによつて、チップ 10の先端側の断面が円以外の形状となり、チップ 10と図示し ないボードの穴が接触する面積が少なくなつている。なお、本発明でいう円とは、真 円のみならず、製造誤差によって若干楕円形となったようなものも含まれる。前記溝 1 8は、チップ 10の耐久性を高めるとともに、前記ボード力も抜きやすくするためのもの であって、図 2(A)のチップ 10Aに示すように、先端 12から節 16までの間にのみ設け るよう〖こしてもよい。すなわち、少なくとも、ボードの穴と接触する部分に設けられてい ればよい。なお、チップ 10及び 10Aを形成する材料としては、ボードを痛めることが ないよう、公知の各種の硬くないプラスチック素材が利用可能である。このようなチッ プ 10 (ないし 10A)は、バレル 52に接続され、シャフト 54及びフライト 56とともに、ダ ーッ 50を構成する。  First, the example shown in FIGS. 1A to 1C will be described. The tip 10 shown in FIG. 1 (A) has a narrow tip 12 side, and a node 16 having a large diameter is provided in the middle portion. Section 16 may be provided as necessary. The other end portion 14 is formed with a screw portion so as to be detachable from the end portion of the barrel 52. Further, a plurality of grooves 18 are formed on the surface of the chip 10 along the longitudinal direction from the tip 12 to the other end 14 side. As shown in the cross-sectional view of FIG. 1 (C), in this embodiment, four grooves 18 are formed, so that the cross section on the tip side of the chip 10 has a shape other than a circle. The area of contact with holes on the board not shown is decreasing. The circle in the present invention includes not only a perfect circle but also a circle that is slightly elliptical due to a manufacturing error. The groove 18 is provided to increase the durability of the chip 10 and to make it easier to remove the board force. As shown in the chip 10A in FIG. 2 (A), the groove 18 is provided between the tip 12 and the node 16. May be provided only. In other words, it is only necessary to be provided at least in a portion that contacts the hole of the board. As materials for forming the chips 10 and 10A, various known hard plastic materials can be used so as not to damage the board. Such a chip 10 (or 10A) is connected to the barrel 52 and, together with the shaft 54 and the flight 56, constitutes the duck 50.
[0025] 次に、本実施例の作用を説明する。前記チップ 10 (ないし 10A)を先端に備えたダ ーッ 50を、図示しないボードに向かって投げ、該ボードに設けられた無数の穴のい ずれかに先端 12側が嵌ると、ダーッ 50が的に刺さった状態となる。このとき、チップ 1 0の表面に溝 18が設けられているため、ボードに刺さる瞬間には縮まり、刺さった後 には広がろうとする力が働くため、抜け落ちに《なる。一方、ボードから抜くときには 、前記溝 18の形成によってボードとの接触面積が小さくなつているため、強い力を要 することなく容易にボードから抜くことが可能となる。 Next, the operation of the present embodiment will be described. Throw the dart 50 with the tip 10 (or 10A) at the tip toward a board (not shown), and if the tip 12 side fits into one of the numerous holes provided on the board, the dart 50 is targeted. It becomes stabbed. At this time, since the groove 18 is provided on the surface of the chip 10, it shrinks at the moment of being stabbed into the board, and after it is stabbed, a force to spread is applied, so that it falls out. On the other hand, when removing from the board Since the contact area with the board is reduced by the formation of the groove 18, it can be easily removed from the board without requiring a strong force.
[0026] このように、実施例 1によれば、チップ 10 (ないし 10A)の表面に長手方向に沿って 複数の溝 18を設けることとしたので、次のような効果がある。 Thus, according to the first embodiment, since the plurality of grooves 18 are provided along the longitudinal direction on the surface of the chip 10 (or 10A), the following effects are obtained.
(1)ボードとの接触部分の断面が、円以外の形状となるため、一点にかかる負担が軽 減し、チップ 10の耐久性が向上する。  (1) Since the cross section of the contact portion with the board has a shape other than a circle, the burden on one point is reduced and the durability of the chip 10 is improved.
(2)チップ 10の形状によって耐久性が向上するため、硬い素材を利用する必要がなく なり、ダーッボードへの負担が軽減し、ボードの耐久性も向上する。  (2) Since the durability is improved by the shape of the chip 10, it is not necessary to use a hard material, the burden on the duck board is reduced, and the durability of the board is also improved.
(3)ボードとの接触面積が少ないため、強い力を要することなぐダーッを抜くことがで きる。  (3) Since the contact area with the board is small, it is possible to pull out the dart without requiring a strong force.
[0027] <実施例 1の変形例 > · · ·図 2(B)〜(D)には、本実施例の変形例の断面が示されて いる。これら断面図は、前記図 1(C)の断面に相当するものである。図 2(B)に示すチッ プ 10Bは、前記チップ 10よりも深い溝 18Bが形成された例である。図 2(C)に示すチッ プ 10Cは、比較的浅い多数の溝 18C力 表面全体に均等に設けられた例である。図 2(D)に示すチップ 10Dは、断面が略六角形となっている。チップ 10B〜10Dのいず れも、基本的作用'効果は、上述した図 1又は図 2(A)に示すチップ 10ないし 10Aと同 様である。  <Modified Example of Embodiment 1> FIGS. 2B to 2D show cross sections of modified examples of the present embodiment. These cross-sectional views correspond to the cross section of FIG. A chip 10B shown in FIG. 2 (B) is an example in which a groove 18B deeper than the chip 10 is formed. The chip 10C shown in FIG. 2 (C) is an example in which a relatively large number of relatively shallow grooves 18C are uniformly provided on the entire surface. The chip 10D shown in FIG. 2 (D) has a substantially hexagonal cross section. In any of the chips 10B to 10D, the basic operation and effect are the same as those of the chips 10 to 10A shown in FIG. 1 or 2A described above.
実施例 2  Example 2
[0028] 次に、図 3(A)を参照しながら、本発明の実施例 2を説明する。図 3(A)は、本実施例 のチップの外観を示す斜視図である。上述した実施例 1では、チップの一端から他端 側にかけて、長手方向にほぼ直線状の溝を複数設けることとしたが、本実施例 2のチ ップ 20では、先端 22から他方の端部 24にかけて、螺旋状に複数の溝 28が形成され ている。本実施例の作用 ·効果は、上述した実施例 1と同様である。なお、溝 28は、 前記実施例 1と同様に、節 26と先端 22の間にのみ設けるようにしてもよい。  Next, Embodiment 2 of the present invention will be described with reference to FIG. 3 (A). FIG. 3A is a perspective view showing the appearance of the chip of this example. In the first embodiment described above, a plurality of substantially linear grooves are provided in the longitudinal direction from one end of the chip to the other end. However, in the chip 20 of the second embodiment, the tip 22 is connected to the other end. A plurality of grooves 28 are formed in a spiral manner over 24. The functions and effects of the present embodiment are the same as those of the first embodiment described above. The groove 28 may be provided only between the node 26 and the tip 22 as in the first embodiment.
実施例 3  Example 3
[0029] 次に、図 3(B)及び (C)を参照しながら、本発明の実施例 3を説明する。図 3(B)は、本 実施例の外観を示す平面図,図 3(C)は、前記図 3(B)を # B— # B線に沿って切断し 矢印方向に見た断面図である。本実施例のチップ 30は、先端 32から節 36に掛けて 、複数の窪み 38が適宜間隔で設けられている。上述した実施例 1及び 2では、チップ の先端力ゝら他端側まで連続した溝が形成されているが、本実施例のように、先端 32 力も節 36まで、適宜間隔をおいて複数の窪み 38ないし穴を設けるようにしても、上述 した実施例 1と同様の効果が得られる。もちろん、前記窪み 38は、節 36から端部 34 側まで設けるようにしてもょ ヽ。 Next, Embodiment 3 of the present invention will be described with reference to FIGS. 3 (B) and 3 (C). Fig. 3 (B) is a plan view showing the appearance of this embodiment, and Fig. 3 (C) is a cross-sectional view of Fig. 3 (B) taken along line # B- # B and viewed in the direction of the arrow. is there. The tip 30 of this embodiment is hung from the tip 32 to the node 36. A plurality of depressions 38 are provided at appropriate intervals. In Examples 1 and 2 described above, a continuous groove from the tip force of the tip to the other end side is formed. Even if the recess 38 or the hole is provided, the same effect as in the first embodiment can be obtained. Of course, the recess 38 may be provided from the node 36 to the end 34 side.
実施例 4  Example 4
[0030] 次に、図 4を参照しながら、本発明の実施例 4を説明する。本実施例は、ソフトダー ッに限らず、チップ (ないしポイント)とバレル,シャフト,フライトにより構成されるダー ッ一般に対して適用可能なものである。図 4(A)は、本実施例のシャフトを用いたダー ッの外観斜視図,図 4(B)は、前記シャフトの外観斜視図,図 4(C)は前記シャフトの装 着部を広げた状態を示す斜視図である。図 4(D)は、前記シャフトの装着部と連結部 の接続前の状態を示す斜視図,図 4(E)は前記 (A)を異なる角度力も見た斜視図であ る。  Next, Embodiment 4 of the present invention will be described with reference to FIG. The present embodiment is applicable not only to soft darts but also to darts generally composed of chips (or points), barrels, shafts, and flights. Fig. 4 (A) is an external perspective view of a dart using the shaft of this embodiment, Fig. 4 (B) is an external perspective view of the shaft, and Fig. 4 (C) is an enlarged view of the mounting portion of the shaft. FIG. FIG. 4 (D) is a perspective view showing a state before connection between the mounting portion and the connecting portion of the shaft, and FIG. 4 (E) is a perspective view showing the angular force different from (A).
[0031] 本実施例のシャフト 100は、 4つの羽根片 122A〜122Dが略十字状に開いたフラ イト 122を着脱可能に取り付けるためのものであって、前記フライト 122が取り付けら れる装着部 112と、該装着部 112をバレル 180に接続するための連結部 124により 構成される。該シャフト 100は、図 4(B)に示すように、全体が略円柱状となっている。 また、図 4(C)に示すように、前記装着部 112は、円柱を軸方向に 4分割した形状の挟 持片 112A〜112Dが、一方の端部 114を中心として略十字状に開くようになって ヽ る。これら挟持片 112A〜112Dの他方の端部 118A〜118Dは、前記端部 114側よ りも細く形成されており、挟持片 112A〜 112Dを閉じたときに、図 4(D)に示すように、 端部 118が連結部 124の一方の端部 126に着脱可能に接続される。図示の例では 、凸状の端部 118と凹状の端部 126の嵌合により、装着部 112と連結部 124が接続 される構成となっているが、他の公知の各種の機構により接続してよい。また、挟持片 112A〜112Dは、前記端部 118A〜 118Dを除いた部分力 フライト 122の軸方向 長さと略同一もしくは若干長くなるように設定されるとともに、それぞれが略直交する 面 115及び 116を有しており、これらの面によってフライト 122の表面を挟み込み固 定する。なお、前記連結部 124の他方の端部 128は、バレル 180の端部 182と着脱 式に接続される。シャフト 100とバレル 180の接続は、例えば図示のように、それぞれ の端部 128及び 182に形成されたネジ部の螺合により行われるが、凹凸形状の嵌合 により接続するようにしてもょ 、。 [0031] The shaft 100 of the present embodiment is for detachably attaching a fly 122 in which four blade pieces 122A to 122D are opened in a substantially cross shape, and a mounting portion 112 to which the flight 122 is attached. And a connecting portion 124 for connecting the mounting portion 112 to the barrel 180. As shown in FIG. 4B, the shaft 100 has a substantially cylindrical shape as a whole. In addition, as shown in FIG. 4C, the mounting portion 112 is such that the holding pieces 112A to 112D each having a shape obtained by dividing the cylinder into four in the axial direction open in a substantially cross shape with the one end portion 114 as the center. It becomes. The other end portions 118A to 118D of these sandwiching pieces 112A to 112D are formed narrower than the end portion 114 side, and when the sandwiching pieces 112A to 112D are closed, as shown in FIG. The end portion 118 is detachably connected to one end portion 126 of the connecting portion 124. In the example shown in the figure, the mounting portion 112 and the coupling portion 124 are connected by fitting the convex end portion 118 and the concave end portion 126, but they are connected by various other known mechanisms. It's okay. The sandwiching pieces 112A to 112D are set so as to be substantially the same as or slightly longer than the axial length of the partial force flight 122 excluding the end portions 118A to 118D, and the surfaces 115 and 116 that are substantially orthogonal to each other. The surface of the flight 122 is sandwiched and fixed by these surfaces. The other end 128 of the connecting portion 124 is attached to and detached from the end 182 of the barrel 180. Connected to the expression. The shaft 100 and the barrel 180 are connected by, for example, screwing of the screw portions formed at the respective end portions 128 and 182 as shown in the figure. .
[0032] 以上のような挟持片 112A〜112Dを閉じると、連結部 124と接続するための凸状 の端部 118と、フライト 122の表面を挟み込むための溝 120 (図 4(B)参照)が形成さ れる。そして、例えば、挟持片 112A及び 112Dによって羽根片 122Aが両面から固 定され、挟持片 112A及び 112Bによって羽根片 122Bが両面から固定される。他の 羽根片 122C及び 122Dについても同様に両面から固定される。  [0032] When the sandwiching pieces 112A to 112D as described above are closed, the convex end portion 118 for connecting to the connecting portion 124 and the groove 120 for sandwiching the surface of the flight 122 (see FIG. 4 (B)) Is formed. For example, the blade piece 122A is fixed from both surfaces by the sandwiching pieces 112A and 112D, and the blade piece 122B is fixed from both surfaces by the sandwiching pieces 112A and 112B. The other blade pieces 122C and 122D are similarly fixed from both sides.
[0033] 次に、本実施例の組み立て手順について説明する。まず、図 4(C)に示すように略 十字状に開いた装着部 112の中心 (すなわち端部 114)に、フライト 122の中心を合 わせる。そして、挟持片 112A〜 112Dを閉じて、羽根片 122A〜122Dを両面から 挟み込み、フライト 122を固定する。次に、図 4(D)に示すように、装着部 112の端部 1 18と連結部 124の端部 126を接続し、最後に、図 4(E)に示すように、バレル 180の端 部 182を、連結部 124の他方の端部 128に接続する。なお、前記バレル 180の先端 には、図 4(A)に示すチップ 184が予め接続されている。フライト 122を交換するときは 、連結部 124を装着部 112から取り外したのちに、挟持片 112A〜 112Dを開いて交 換する。  Next, the assembly procedure of the present embodiment will be described. First, as shown in FIG. 4 (C), the center of the flight 122 is aligned with the center of the mounting portion 112 (that is, the end portion 114) opened in a substantially cross shape. Then, the sandwiching pieces 112A to 112D are closed, and the blade pieces 122A to 122D are sandwiched from both sides to fix the flight 122. Next, as shown in FIG. 4 (D), the end portion 118 of the mounting portion 112 and the end portion 126 of the connecting portion 124 are connected, and finally, as shown in FIG. The part 182 is connected to the other end 128 of the connecting part 124. A tip 184 shown in FIG. 4 (A) is connected in advance to the tip of the barrel 180. When exchanging the flight 122, after removing the connecting portion 124 from the mounting portion 112, the clamping pieces 112A to 112D are opened and replaced.
[0034] このように、実施例 4によれば、次のような効果がある。  Thus, according to Example 4, the following effects are obtained.
(1)挟持片 112A〜112Dによって、フライト 122の全ての面を、該フライト 122の軸方 向の全範囲にわたって固定することができるため、フライト 122がシャフト 100から外 れにくくなる。  (1) Since all the surfaces of the flight 122 can be fixed over the entire range in the axial direction of the flight 122 by the sandwiching pieces 112A to 112D, the flight 122 is not easily detached from the shaft 100.
(2)フライト 122の羽根片 122A〜 122Dを、略十字状に開!ヽた状態で保つことができ るため、ダーッの飛行時の安定性が増す。  (2) Since the blade pieces 122A to 122D of the flight 122 can be kept in a substantially cross-shaped open state, the stability during the flight of the duck is increased.
実施例 5  Example 5
[0035] 次に、図 5を参照しながら、本発明の実施例 5を説明する。なお、上述した実施例 4 と同一ないし対応する構成要素には同一の符号を用いることとする(以下の実施例に ついても同様)。図 5(A)は、本実施例のシャフトを用いたダーッの外観斜視図,図 5( B)は前記シャフトの外観斜視図である。図 5(C)は前記シャフトを広げた状態を内側か ら見た斜視図,図 5(D)は前記シャフトを広げた状態を外側力 見た斜視図である。 Next, Embodiment 5 of the present invention will be described with reference to FIG. Note that the same reference numerals are used for components that are the same as or correspond to those in the fourth embodiment described above (the same applies to the following embodiments). FIG. 5A is an external perspective view of a duck using the shaft of this embodiment, and FIG. 5B is an external perspective view of the shaft. Fig. 5 (C) shows the state where the shaft is expanded inside. Fig. 5 (D) is a perspective view of the shaft in an unfolded state as seen from the outside force.
[0036] 本実施例のシャフト 130は、前記実施例 4と同様に、全体が略円柱状となっており、 図 5(C)及び (D)に示すように、円柱を軸方向に 4分割した形状の挟持片 130A〜 130 Dが、一方の端部 132を中心として略十字状に開くようになつている。これら挟持片 1 30八〜1300の端部138八〜1380は、前記端部 132側よりも細く形成されており、 挟持片 130A〜130Dを閉じたときに、端部 138がバレル 180Aの端部 182Aに着脱 可能に接続される。図示の例では、凸状の端部 138と凹状の端部 182Aの嵌合によ り接続される構成となっている。本実施例では、前記挟持片 130A〜130Dは、前記 端部 138A〜138Dを除いた部分がフライト 122の軸方向長さよりも長くなつており、 端部 138からフライト 122まで適当な間隔が空くようになつている。すなわち、前記端 部 138からフライト 122までの部分力 上述した実施例 4の連結部 124に相当する。 また、前記挟持片 130A〜130Dは、それぞれが略直交する面 134A及び 136Aを 有しており、これらの面によってフライト 122の表面を固定する。 [0036] The shaft 130 of the present embodiment is substantially cylindrical as in the fourth embodiment, and the cylinder is divided into four in the axial direction as shown in Figs. 5 (C) and (D). The sandwiching pieces 130A to 130D having the above shapes are configured to open in a substantially cross shape with the one end portion 132 as the center. The end portions 138 8 to 1380 of these sandwiching pieces 1308 to 1300 are formed narrower than the end portion 132 side, and when the sandwiching pieces 130A to 130D are closed, the end portion 138 becomes the end portion of the barrel 180A. Removably connected to 182A. In the example shown in the figure, the connection is made by fitting the convex end 138 and the concave end 182A. In the present embodiment, the sandwiching pieces 130A to 130D have portions except for the end portions 138A to 138D longer than the axial length of the flight 122, so that an appropriate interval is provided from the end portion 138 to the flight 122. It has become. That is, the partial force from the end portion 138 to the flight 122 corresponds to the connecting portion 124 of the fourth embodiment described above. The sandwiching pieces 130A to 130D have surfaces 134A and 136A that are substantially orthogonal to each other, and the surface of the flight 122 is fixed by these surfaces.
[0037] 更に、本実施例では、前記挟持片 130A〜130Dに、段差 140A〜140Dが形成さ れている。これら段差 140A〜140Dは、挟持片 130A〜130Dを閉じたときに、図 5( B)に示す溝 142及び 144の厚みを変えて、その厚みの差により、フライト 122の位置 決めを行うためのものである。図示の例は、フライト 122をシャフト 130の端部 132側 に寄せたものである力 必要に応じて段差 140A〜140Dの位置を変えることにより、 フライト 122の固定位置を変更することができる。本実施例によれば、上述した実施 例 4の作用 '効果に加え、フライト 122の固定位置を変更できるという効果が得られる 。また、シャフト 130を装着部と連結部の 2部構成とする必要がないため、部品点数が 減り、製造や組み立てが容易となる。 [0037] Furthermore, in this embodiment, steps 140A to 140D are formed in the sandwiching pieces 130A to 130D. These steps 140A to 140D change the thickness of the grooves 142 and 144 shown in FIG. 5 (B) when the sandwiching pieces 130A to 130D are closed, and position the flight 122 based on the difference in thickness. Is. In the example shown in the drawing, the force at which the flight 122 is moved toward the end 132 side of the shaft 130 can change the fixing position of the flight 122 by changing the positions of the steps 140A to 140D as necessary. According to the present embodiment, in addition to the operation 'effect of the fourth embodiment described above, an effect that the fixed position of the flight 122 can be changed is obtained. Further, since the shaft 130 does not have to be a two-part configuration including a mounting portion and a connecting portion, the number of parts is reduced, and manufacturing and assembly are facilitated.
実施例 6  Example 6
[0038] 次に、図 6を参照しながら、本発明の実施例 6を説明する。図 6(A)は、本実施例の シャフトを利用したダーッの外観斜視図,図 6(B)は前記シャフトの外観斜視図である 。図 6(C)〜(E)は、前記シャフトにフライトを取り付ける様子を示す斜視図であって、前 記図 6(A)及び (B)とは異なる角度から見た状態を示す。上述した実施例 4及び 5は ヽ ずれも、シャフトに設ける溝をバレル側力も先端に向けて形成することとしたが、本実 施例は、前記溝をシャフトの先端力 バレル側に向力つて形成した例である。 Next, Embodiment 6 of the present invention will be described with reference to FIG. FIG. 6A is an external perspective view of a dart using the shaft of this embodiment, and FIG. 6B is an external perspective view of the shaft. FIGS. 6 (C) to 6 (E) are perspective views showing how the flight is attached to the shaft, and show a state seen from an angle different from FIGS. 6 (A) and 6 (B). In Examples 4 and 5 described above, the groove provided on the shaft is formed with the barrel side force directed toward the tip. The embodiment is an example in which the groove is formed by directing the tip end of the shaft toward the barrel side.
[0039] 本実施例のシャフト 150は、略円柱状であって、図 6(C)に示すように、軸方向に沿 つて 4つのスリット 150A〜 150D力 一方の端部 154側から中央付近まで形成されて いる。これらスリット 150A〜150Dは、前記シャフト 150の端部 154側を 4分割するよ うに、略十字状に形成されており、ここにフライト 122が差し込まれる。前記端部 154 側の開口部には、嵌合部 158と頭部 160を備えたキャップ 156が着脱可能に設けら れる。なお、シャフト 150の他方の端咅 152ίま、ノ レノレ 180の端咅 【こ着脱可會 【こ 取り付けられる。本実施例の作用 ·効果は、上述した実施例 4と同様であるが、スリット 150Α〜 150Dの深さを調節することにより、フライト 122の固定位置の調節も可能で ある。  [0039] The shaft 150 of the present embodiment is substantially cylindrical, and as shown in FIG. 6 (C), four slits 150A to 150D force along the axial direction from one end 154 side to the vicinity of the center. Is formed. These slits 150A to 150D are formed in a substantially cross shape so as to divide the end portion 154 side of the shaft 150 into four, and a flight 122 is inserted therein. A cap 156 having a fitting portion 158 and a head portion 160 is detachably provided in the opening on the end portion 154 side. The other end of the shaft 150 can be attached to the other end of the shaft 150, or the end of the nore 180 can be attached or detached. The functions and effects of the present embodiment are the same as those of the fourth embodiment described above, but the fixing position of the flight 122 can also be adjusted by adjusting the depths of the slits 150 to 150D.
実施例 7  Example 7
[0040] 次に、図 7を参照しながら、本発明の実施例 7を説明する。図 7(A)及び (Β)は、本実 施例のシャフトを示す外観斜視図である。まず、図 7(A)に示す例では、シャフト 170 は、前記実施例 6と同様に、軸方向に沿って 4つのスリット 170A〜170D力 一方の 端部 174側から中央付近まで形成されている (スリット 170C及び 170Dは図示せず) 。これらスリットは、前記端部 174側を 4分割するように、略十字状に形成されており、 ここにフライト 122が差し込まれる。そして、前記端部 174側の外周面に、例えば、ゴ ムなどで形成されたリング 176を嵌めることで、フライト 122が外れるのを防止する。あ るいは、図 7(B)に示す例のように、端部 174側の外周面にスプリング 178を装着して 、フライト 122が外れるのを防止するようにしてもよい。  Next, Embodiment 7 of the present invention will be described with reference to FIG. FIGS. 7A and 7B are external perspective views showing the shaft of this embodiment. First, in the example shown in FIG. 7 (A), the shaft 170 is formed from the end 174 side of one of the four slits 170A to 170D along the axial direction to the vicinity of the center, as in the sixth embodiment. (Slits 170C and 170D are not shown). These slits are formed in a substantially cross shape so as to divide the end portion 174 side into four, and the flight 122 is inserted therein. Then, by fitting a ring 176 formed of, for example, rubber on the outer peripheral surface on the end 174 side, the flight 122 is prevented from being detached. Alternatively, as in the example shown in FIG. 7B, a spring 178 may be attached to the outer peripheral surface on the end portion 174 side to prevent the flight 122 from coming off.
実施例 8  Example 8
[0041] 次に、図 8を参照しながら、本発明の実施例 8を説明する。図 8(A)は本実施例のダ ーッの外観斜視図,図 8(B)は本実施例の分解斜視図,図 8(C)は本実施例の変形例 の分解斜視図である。図 8(A)及び (B)に示すように、本実施例のダーッ 200は、フライ ト 202,シャフト 204,ノ レノレ 206,チップ 208のほ力、前記シャフト 204とノ レノレ 206 の間に設けられた橈み部材 210により構成されている。該橈み部材 210は、図 8(B) に示すように、例えばゴムなどの弾性体 212の両端に、前記シャフト 204の端部 204 Aと着脱可能に連結する連結部 214と、前記バレル 206の端部 206Aに着脱可能に 連結する連結部 216を備えている。これら連結部 214, 216は、例えば、合成樹脂や 金属などで形成されるが、橈み部材 210全体を、例えばゴムや、それ以外の柔軟な 素材で一体形成するようにしてもよい。なお、前記橈み部材 210と、シャフト 204,パ レル 206の着脱は、図示の例ではネジ部の螺合により行われる力 凹凸形状の嵌合 や他の公知の機構により着脱する構成としてもょ 、。 Next, Embodiment 8 of the present invention will be described with reference to FIG. FIG. 8 (A) is an external perspective view of the duck of this embodiment, FIG. 8 (B) is an exploded perspective view of this embodiment, and FIG. 8 (C) is an exploded perspective view of a modification of this embodiment. As shown in FIGS. 8 (A) and 8 (B), the dart 200 of this embodiment is provided between the shaft 204 and the nozzle 206, the force of the fly 202, the shaft 204, the nozzle 206, and the tip 208. The stagnation member 210 is formed. As shown in FIG. 8 (B), the squeeze member 210 is connected to both ends of an elastic body 212 such as rubber, for example, a connecting portion 214 detachably connected to the end portion 204A of the shaft 204, and the barrel 206. Removable on end 206A A connecting portion 216 to be connected is provided. The connecting portions 214 and 216 are formed of, for example, a synthetic resin or a metal, but the entire stagnation member 210 may be integrally formed of, for example, rubber or other flexible material. It should be noted that the squeezing member 210, the shaft 204, and the parallel 206 are attached and detached in the example shown in the figure by force fitting by screwing of the threaded portion or by other known mechanisms. ,.
[0042] 次に、本実施例の作用を説明する。チップ 208は、ソフトダーッかハードダーッかに より、プラスチック又は金属が用いられる力 通常、シャフト 204及びバレル 206は金 属などで形成されている。仮に、前記橈み部材 210を装着せずにダーッを投げると、 既に的に刺さっているダーッに当たった場合には、前記シャフト 204やバレル 206が しならないため、後続のダーッが弾かれてしまうことがある。し力しながら、前記橈み 部材 210をシャフト 204とバレル 206間に設けることにより、後続のダーッ 200が当た つた場合でも、前記弾性体 212の可撓性によりバレル 206に対してシャフト 204がし なる(曲がる)ため、後続ダーッ 200を弾くことが少なくなり、安定したプレーを行うこと ができる。また、前記橈み部材 210は、図 8(C)に示すように、バレル 206の端部 206 Bと、チップ 208の端部 208Aの間に挟んで装着するようにしてもよい。この部分には 、プレーヤに応じて重量調節用のウェイト (ないしおもり)が設けられることがあるが、 前記橈み部材 210により、前記ダーッ 200の重量の調節を行うようにしてもよい。この 場合は、例えば、前記橈み部材 210全体もしくは弾性体 212を重たいゴムで形成し たり、連結部 214, 216に金属を用いたりすることにより対応が可能である。  Next, the operation of the present embodiment will be described. The tip 208 is a soft dart or a hard duck, and a force in which plastic or metal is used. Usually, the shaft 204 and the barrel 206 are made of metal or the like. If you throw a dart without wearing the kneading member 210, the shaft 204 or barrel 206 will not work if it hits a duck that has already been stabbed. Sometimes. However, by providing the stagnation member 210 between the shaft 204 and the barrel 206, the shaft 204 can be moved relative to the barrel 206 by the flexibility of the elastic body 212 even when the subsequent duck 200 hits. As a result, it is less likely to play the subsequent dart 200, and stable play can be achieved. Further, as shown in FIG. 8C, the stagnation member 210 may be mounted so as to be sandwiched between the end portion 206 B of the barrel 206 and the end portion 208 A of the chip 208. This portion may be provided with a weight (or weight) for weight adjustment depending on the player, but the weight of the duck 200 may be adjusted by the kneading member 210. In this case, for example, the stagnation member 210 as a whole or the elastic body 212 can be made of heavy rubber, or metal can be used for the connecting portions 214 and 216.
[0043] このように、実施例 8によれば、次のような効果がある。  Thus, according to Example 8, there are the following effects.
(1)シャフト 204とノ レノレ 206の間、もしくは、前記ノ レノレ 206とチップ 208の間に、弾 性体 212からなる橈み部材 210を着脱可能に装着することとしたので、既に的に刺さ つているダーッ 200に後続のダーッが当たったときでも、前記弾性体 212がしなるた め、後続ダーッが弾かれるのを軽減することができる。  (1) Since the squeezing member 210 made of the elastic body 212 is detachably mounted between the shaft 204 and the nozzle 206 or between the nozzle 206 and the tip 208, it is already stuck. Even when a subsequent duck hits the duck 200, the elastic body 212 is bent, so that it is possible to reduce the bounce of the subsequent duck.
(2)重量調整用のウェイト(おもり)の替わりに、前記橈み部材 210を装着することによ り、一つの追加部品で、重量調節と後続ダーッの弾き飛ばし軽減を図ることができる  (2) By installing the kneading member 210 instead of the weight adjustment weight (weight), it is possible to reduce the weight adjustment and the subsequent dulling off with one additional part.
[0044] 本発明には数多くの実施形態があり、以上の開示に基づいて多様に改変すること が可能である。例えば、次のようなものも含まれる。 [0044] The present invention has many embodiments, and various modifications can be made based on the above disclosure. Is possible. For example, the following are included.
(1)前記実施例で示した形状,大きさ,材料は一例であり、必要に応じて適宜変更し てよい。例えば、チップの先端部分の断面形状は、上述した実施例 1〜3のほか、三 角形,四角形,八角形などの多角形のほか、星形や楕円形状とするなど、円以外の 形状であればよい。なお、上述した通り、製造誤差によって若干楕円形になったよう なものは、本発明でいう円以外の形状に含まれるものではない。また、例えば、前記 実施例では、シャフトやバレルを略円筒状としたが、断面が多角形や楕円形となるよ うな形状のものを用いてもょ 、。  (1) The shape, size, and material shown in the above embodiment are examples, and may be appropriately changed as necessary. For example, the cross-sectional shape of the tip portion of the chip may be a shape other than a circle, such as a polygon, such as a triangle, a rectangle, or an octagon, as well as a star or an ellipse, in addition to the above-described Examples 1 to 3. That's fine. In addition, as described above, a shape that is slightly elliptical due to a manufacturing error is not included in the shape other than the circle in the present invention. Further, for example, in the above-described embodiment, the shaft and barrel are substantially cylindrical, but a shape having a polygonal or elliptical cross section may be used.
[0045] (2)前記実施例 1〜3で示したチップに設ける溝 18, 28の本数や長さ、あるいは、窪 み 38の位置や個数なども一例であり、同様の効果を奏するように適宜変更してよぐ 更に、溝と窪みを組み合わせるようにしてもよい。  [0045] (2) The number and length of the grooves 18 and 28 provided in the chips shown in the above-described embodiments 1 to 3, or the position and number of the recesses 38 are examples, so that the same effects can be obtained. It may be changed as appropriate. Further, a groove and a recess may be combined.
(3)前記実施例 4〜7で示した溝やスリットは、フライト 122の全ての面を、軸方向の ほぼ全範囲にわたって固定するものである力 これも一例であり、フライト 122の各面 を、軸方向の広範囲にわたって固定できるものであれば、どのような形態で挟み込む ようにしてもよい。なお、広範囲とは、少なくとも羽根の軸方向長さの半分程度をいう。  (3) The grooves and slits shown in Examples 4 to 7 are forces that fix all surfaces of the flight 122 over almost the entire range in the axial direction. This is also an example. As long as it can be fixed over a wide range in the axial direction, it may be sandwiched in any form. The wide range means at least about half the axial length of the blade.
[0046] (4)前記実施例 4〜7におけるシャフトの上下部分 (フライト 122が取り付けられてい ない部分)も一例であり、節を設けるようにするなど、必要に応じて適宜変更してよい 。また、前記実施例 4〜7は、シャフトとバレルが着脱可能な構成とした力 シャフトと バレルが一体化したものや、シャフト,バレル,チップまでが一体化したような構成の ダーッに対して適用するようにしてもよ ヽ。  (4) The upper and lower portions of the shaft in Embodiments 4 to 7 (portions where the flight 122 is not attached) are also examples, and may be appropriately changed as necessary, such as providing nodes. In addition, Examples 4 to 7 are applied to a force with a structure in which the shaft and the barrel are detachable, or a dart having a structure in which the shaft, the barrel, and the chip are integrated. You can do it.
(5)前記実施例 6のキャップ 156や、実施例 7のリング 176及びスプリング 178も一例 であり、同様の効果を奏するように適宜設計変更してよい。  (5) The cap 156 of the sixth embodiment, the ring 176 and the spring 178 of the seventh embodiment are examples, and the design may be changed as appropriate so as to achieve the same effect.
[0047] (6)前記実施例 8では、橈み部材 210をダーッ 200のいずれか一箇所に設けることと したが、シャフト 204とノレル 206の間,バレル 206とチップ 208の間の双方に装着す るようにしてもよい。また、前記実施例 8では、橈み部材 210が重さ調整用のウェイト を兼ねることとした力 別個に装着することを妨げるものではない。むろん、シャフトと バレルが一体ィ匕したものや、チップとバレルが一体ィ匕したような構成のダーッに対し ても、前記橈み部材 210が適用可能である。また、橈み部材 210を構成する素材も、 ゴムに限定されるものではなぐ公知の各種の柔軟性を有する素材を用いてよい。更 に、シャフトからチップまでの軸部が一体形成されたようなダーッにおいて、その一部 を、他の部分よりも柔軟性がある素材で形成するようにしても、前記実施例 8と同様の 効果が得られる。 [0047] (6) In the eighth embodiment, the kneading member 210 is provided at any one of the duck 200, but it is mounted between the shaft 204 and the norrel 206, and between the barrel 206 and the tip 208. You may make it. Further, in the eighth embodiment, the squeezing member 210 is not prevented from being mounted separately by the force that also serves as the weight adjusting weight. Of course, the squeezing member 210 can be applied to a dart having a structure in which a shaft and a barrel are integrated or a chip and a barrel are integrated. In addition, the material constituting the stagnation member 210 is You may use the raw material which has well-known various softness | flexibility which is not limited to rubber | gum. Further, in the duck in which the shaft portion from the shaft to the tip is integrally formed, even if a part thereof is formed of a material that is more flexible than the other portions, the same as in the eighth embodiment. An effect is obtained.
(7)前記実施例で示したシャフトとバレルの接続方法や、バレルとチップの接続方法 、あるいは、橈み部材 210とシャフト,バレル,チップとの接続方法も一例であり、同様 の効果を奏するように公知の各種の接続方法を利用してよい。  (7) The connection method between the shaft and barrel, the connection method between the barrel and the tip, or the connection method between the rubbing member 210 and the shaft, barrel, and tip shown in the above embodiment is also an example, and the same effect is achieved. As described above, various known connection methods may be used.
産業上の利用可能性  Industrial applicability
[0048] 本発明によれば、ダーッチップの先端部分,すなわち、ボードとの接触部分の断面 を円以外の形状とすることで、硬い素材を使用することなくチップの耐久性を向上さ せるとともに、ボードから抜きやすぐかつ、ボードを痛めることがなくなるため、プラス チック製のチップを利用したソフトダーッの用途に適用できる。  [0048] According to the present invention, the tip part of the dart chip, that is, the cross section of the contact part with the board has a shape other than a circle, thereby improving the durability of the chip without using a hard material, It can be applied to soft dart applications using plastic chips because it does not damage the board as soon as it is removed from the board.
[0049] また、シャフトの軸方向に設けた複数の溝ないし切れ込みによって、フライトの全て の面を、軸方向の広範囲にわたって固定することとしたので、フライトがシャフトから外 れに《なるため、ダーッシャフトの用途に適用できる。特に、フライト形状を維持する ことができるため、安定した飛行を重視するダーッの用途に好適である。  [0049] In addition, since all the planes of the flight are fixed over a wide range in the axial direction by a plurality of grooves or notches provided in the axial direction of the shaft, the flight is detached from the shaft. Applicable to shaft applications. In particular, since the flight shape can be maintained, it is suitable for dart applications that place importance on stable flight.
[0050] 更に、軸方向に複数に分割可能なパーツにより構成されているダーッに、前記分 割されたパーツ間の少なくともいずれ力の部分に、柔軟性を有する橈み部材を着脱 可能に装着する,あるいは、フライトを取り付ける軸部の少なくとも一部を、他の部分 よりも柔らかい素材で形成することした。このため、既に的に刺さっているダーッに後 続のダーッが当たったときでも、後続ダーッを弾くことが少なくなるため、安定したプ レーを行うためのダーッの用途に適用できる。  [0050] Furthermore, a flexible squeeze member is detachably attached to at least any portion of the force between the divided parts in a dart formed of parts that can be divided into a plurality of parts in the axial direction. Or, at least a part of the shaft part to which the flight is attached was made of a softer material than the other parts. For this reason, even when a subsequent duck hits a duck that has already been stabbed, it is less likely to play the subsequent duck, so it can be applied to the use of a dart for stable play.

Claims

請求の範囲 The scope of the claims
[1] ボードに設けられた穴に先端側が嵌るとともに、他端側はダーッ本体に対して着脱 可能なチップであって、  [1] The tip is fitted into a hole provided in the board, and the other end is a chip that can be attached to and detached from the duck body.
前記ボードの穴と接触する部分の断面を、円以外の形状としたことを特徴とするダ ーッチップ。  A dart chip characterized in that a cross section of a portion in contact with the hole of the board has a shape other than a circle.
[2] 前記ボードの穴と接触する部分の表面に、長手方向に沿って少なくとも一つ以上の 溝を設けたことを特徴とする請求項 1記載のダーッチップ。  2. The dart chip according to claim 1, wherein at least one groove is provided along a longitudinal direction on a surface of a portion in contact with the hole of the board.
[3] 前記ボードの穴と接触する部分の表面に、少なくとも一つ以上の穴ないし窪みを設 けたことを特徴とする請求項 1記載のダーッチップ。 [3] The dart chip according to claim 1, wherein at least one or more holes or dents are provided on a surface of a portion in contact with the hole of the board.
[4] 請求項 1〜3の 、ずれに記載のダーッチップが先端に設けられたことを特徴とする ダーッ。 [4] A dart tip according to any one of claims 1 to 3, wherein the dart tip according to the deviation is provided at the tip.
[5] フライトが着脱可能に取り付けられるダーッシャフトであって、  [5] A dart shaft to which the flight is detachably attached,
該ダーッシャフトの軸方向に形成されており、複数の羽根片からなるフライトの全て の面を、該フライトの軸方向の広範囲にわたって固定可能な複数の溝ないし切れ込 み,  A plurality of grooves or notches formed in the axial direction of the dart shaft and capable of fixing all surfaces of the flight composed of a plurality of blade pieces over a wide range in the axial direction of the flight;
を備えたことを特徴とするダーッシャフト。  A dart shaft characterized by comprising.
[6] フライトが着脱可能に取り付けられるダーッシャフトであって、 [6] A dart shaft to which the flight is detachably attached,
該ダーッシャフトの軸方向に形成されており、複数の羽根片からなるフライトの全て の面を、前記フライトの軸方向の広範囲にわたって固定可能な複数の溝ないし切れ 込み,  A plurality of grooves or notches formed in the axial direction of the dull shaft, and capable of fixing all surfaces of the flight composed of a plurality of blade pieces over a wide range in the axial direction of the flight;
前記ダーッシャフトの端部に着脱可能に設けられており、前記複数の溝ないし切れ 込みの端部を閉塞する留め具,  A fastener that is detachably provided at an end of the dull shaft, and closes the ends of the plurality of grooves or cuts;
を備えたことを特徴とするダーッシャフト。  A dart shaft characterized by comprising.
[7] 前記複数の溝ないし切れ込みが、前記フライトの固定位置を決めるための段差を 有することを特徴とする請求項 5又は 6記載のダーッシャフト。 7. The dart shaft according to claim 5 or 6, wherein the plurality of grooves or notches have a step for determining a fixed position of the flight.
[8] フライトと、軸方向に複数に分割可能なパーツにより構成されているダーッであって 分割されたパーツ間の少なくともいずれかの部分に、柔軟性を有する橈み部材を 着脱可能に設けたことを特徴とするダーッ。 [8] A duck made up of a flight and a part that can be divided into multiple parts in the axial direction. Darts characterized by being detachable.
[9] 前記橈み部材が、ゴムにより形成されていることを特徴とする請求項 8記載のダーッ  [9] The duck according to claim 8, wherein the stagnation member is formed of rubber.
[10] 前記橈み部材が、重量調節用のおもりを兼ねることを特徴とする請求項 8又は 9記 載のダーッ。 [10] The duck according to claim 8 or 9, wherein the stagnation member also serves as a weight for weight adjustment.
[11] フライトを取り付ける軸部の少なくとも一部が、他の部分よりも柔らかい素材により形 成されて!/ヽることを特徴とするダーッ。  [11] Darts characterized in that at least a part of the shaft part to which the flight is attached is formed of a softer material than other parts!
PCT/JP2006/312759 2005-06-28 2006-06-26 Darts tip, darts shaft, and darts WO2007000983A1 (en)

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JP2005009781U JP3118732U (en) 2005-11-21 2005-11-21 Dart shaft
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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010004901A (en) * 2008-06-24 2010-01-14 Mgm Inc Dart barrel and dart
US8177668B2 (en) 2008-09-10 2012-05-15 Cosmo Precision Machine, Inc. Dart
JP2014068785A (en) * 2012-09-28 2014-04-21 Ferix Inc Dart
JP5976907B1 (en) * 2015-08-17 2016-08-24 株式会社コスモ精機 Badminton shuttle
KR20180118192A (en) * 2016-03-02 2018-10-30 진타 세리자와 Screw members, fastening members and darts
GB2584893A (en) * 2019-06-20 2020-12-23 Unicorn Products Ltd Dart point
US11920911B2 (en) 2019-11-19 2024-03-05 Cosmo Seiki Co., Ltd. Dart

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JPS5477675U (en) * 1977-11-11 1979-06-02
JP2004242937A (en) * 2003-02-14 2004-09-02 Bandai Co Ltd Dart

Patent Citations (2)

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Publication number Priority date Publication date Assignee Title
JPS5477675U (en) * 1977-11-11 1979-06-02
JP2004242937A (en) * 2003-02-14 2004-09-02 Bandai Co Ltd Dart

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010004901A (en) * 2008-06-24 2010-01-14 Mgm Inc Dart barrel and dart
US8177668B2 (en) 2008-09-10 2012-05-15 Cosmo Precision Machine, Inc. Dart
JP2014068785A (en) * 2012-09-28 2014-04-21 Ferix Inc Dart
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
KR20180118192A (en) * 2016-03-02 2018-10-30 진타 세리자와 Screw members, fastening members and darts
EP3425218A4 (en) * 2016-03-02 2019-09-11 Jinta Serizawa Threaded member, fastening member, and dart
US10663270B2 (en) 2016-03-02 2020-05-26 Jinta SERIZAWA Threaded member, fastening member, and dart
KR102261319B1 (en) 2016-03-02 2021-06-04 진타 세리자와 Thread members, fastening members and darts
GB2584893A (en) * 2019-06-20 2020-12-23 Unicorn Products Ltd Dart point
GB2584893B (en) * 2019-06-20 2022-03-09 Unicorn Products Ltd Dart point
US11920911B2 (en) 2019-11-19 2024-03-05 Cosmo Seiki Co., Ltd. Dart

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