GB2068755A - Dart shafts - Google Patents

Dart shafts Download PDF

Info

Publication number
GB2068755A
GB2068755A GB8104560A GB8104560A GB2068755A GB 2068755 A GB2068755 A GB 2068755A GB 8104560 A GB8104560 A GB 8104560A GB 8104560 A GB8104560 A GB 8104560A GB 2068755 A GB2068755 A GB 2068755A
Authority
GB
United Kingdom
Prior art keywords
shaft
dart
magnesium
portions
barrel
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.)
Withdrawn
Application number
GB8104560A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
MY DART Ltd
Original Assignee
MY DART Ltd
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 MY DART Ltd filed Critical MY DART Ltd
Priority to GB8104560A priority Critical patent/GB2068755A/en
Publication of GB2068755A publication Critical patent/GB2068755A/en
Withdrawn legal-status Critical Current

Links

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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Forging (AREA)

Abstract

A dart shaft has at one end a portion (12) provided with a cruciform slot (13) forming a dart flight holder and at the other end a portion (14) having means, usually a screw thread (15), for connecting it to one end of a dart barrel, the two portions (12 and 14) being interconnected by a central shaft portion (11) of smaller diameter, wherein at least one of the portions (11, 12 or 14) is composed of magnesium or an alloy thereof containing at least 50% magnesium. If the end portions (12 and 14) are formed integrally with the central shaft portion (11), the shaft may be formed by a cold heading or cold forming process, such as rolling, and composed of the same or another metal or alloy. <IMAGE>

Description

SPECIFICATION Dart shafts This invention relates to dart shafts which form part of the construction of a dart used for playing the game of darts, and is concerned, more particularly, with dart shafts of the type having at one end a portion provided with a cruciform slot forming a dart flight holder and at the other end a portion having means, usually a screw thread, for connecting it to one end of a barrel having at its other end a dart point, the two end portions being interconnected by a central shaft portion of smaller diameter.
It is an object of the present invention to provide an improved dart shaft.
The present invention consists in a dart shaft of bthe type indicated, wherein at least one of the portions is composed of magnesium or an alloy thereof containing at least 50% magnesium.
- The invention further consists in a dart shaft having a smaller diameter central shaft portion formed integrally with enlarged portions at each end, one portion serving as a flight holder and the other portion having means for connecting the shaft to a dart barrel, wherein the shaft is composed of metal and formed by a cold heading or cold forming process such as rolling.
In carrying the invention into effect according to one convenient mode by way of example, the accompanying drawing shows a dart shaft having a smaller diameter central portion 11, say between .07 and .09 inches in diameter, formed integrally with enlarged portions at each end, say between .2 and .3 inches in diameter, one portion 12 having a cruciform slot 13 to form a flight holder and the other portion 14 having a screw thread 15 by means of which the shaft may be connected to a dart barrel (not shown).
The shaft is composed of magnesium or an alloy containing at least 50% magnesium. The shaft is manufactured from a length of stock material by means of a cold heading process in which axial pressure is applied to wire to cause its ends to be increased to the desired diameter and shape, the enlarged end portion 12 then being slitto provide the cruciform slot 13. Using such a process the grain structure more closely follows the profile of the shaft resulting in increased strength in the finished shafts.
Also the forming process causes work-hardening of the metal and this effect is greatest at the ends where most needed. Alternatively, the shaft may be manufactured by rolling a thicker wire to reduce its diameter to give the final desired shape.
The enlarged end portion 14 is provided with a screw thread 15, such as a 2BA or 14ft BSF thread. It is customary to provide an undercut adjacent to the shoulder at the base of the thread washer which provides a retaining effect when the shaft is screwed into the barrel. However, this creates a stress con centration in the shoulder region, which can prom ote local fracture, and it is preferred to dispense with the undercut.The thread is preferably formed by rol ling between hardened thread rolls or fiat dies instead of being cut, so that a stronger and smoother thread is produced in which the grain structure fol lows the profile, and the threaded portion is slit lon- gitudinallythrough its axis, as at 16, the two parts thus created being forced slightly apart by means of a wedge so asto exert radial pressure when screwed into the barrel thereby providing a self-jamming or locking effect to give a secure fixing.
Itis preferredthatthe shaft should be work- hardened or further work-hardened, for example by ball-burnishing.
Various modifications may be made within the scope of the present invention.
For example, one or both of the enlarged end portions may be connected to the central shaft portion instead of being formed integrally with it, in which case it may be of advantage to form only one or two ofthethree portions from magnesium or magnesium alloy, the other portion or portions being composed, for example, ofanother metal or plastics.
Alternatively, where the three portions are formed integrally by a cold heading or cold forming process, a metal other than magnesium or magnesium alloy may be used, such as aluminium or an aluminium alloy.
1. A dart shaft of the type indicated, wherein at least one of the portions is composed of magnesium or an alloy thereof containing at least 50% magnesium.
2. A dart shaft as claimed in claim 1, wherein the end portions are formed integrally with the central shaft portion.
3. A dart shaft having a smaller diameter central shaft portion formed integrally with enlarged portions at each end, one portion serving as a flight holder and the other having means for connecting the shaft to a dart barrel, wherein the shaft is composed of metal and formed by a cold heading or cold forming process.
4. A dart shaft as claimed in claim 3, wherein the said metal is magnesium organ alloy thereof containing at least 50% magnesium.
5. A dart shaft as claimed in any one of claims 1 to 4, wherein the shaft is work-hardened or further work-hardened.
6. A dart shaft as claimed in any one of claims 1 to 5, wherein the means for connecting the shaft to a shaft barrel includesathreaded portion having longitudinal slits.
7. A dart shaft substantially as described with reference to the accompanying drawings.
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (7)

**WARNING** start of CLMS field may overlap end of DESC **. SPECIFICATION Dart shafts This invention relates to dart shafts which form part of the construction of a dart used for playing the game of darts, and is concerned, more particularly, with dart shafts of the type having at one end a portion provided with a cruciform slot forming a dart flight holder and at the other end a portion having means, usually a screw thread, for connecting it to one end of a barrel having at its other end a dart point, the two end portions being interconnected by a central shaft portion of smaller diameter. It is an object of the present invention to provide an improved dart shaft. The present invention consists in a dart shaft of bthe type indicated, wherein at least one of the portions is composed of magnesium or an alloy thereof containing at least 50% magnesium. - The invention further consists in a dart shaft having a smaller diameter central shaft portion formed integrally with enlarged portions at each end, one portion serving as a flight holder and the other portion having means for connecting the shaft to a dart barrel, wherein the shaft is composed of metal and formed by a cold heading or cold forming process such as rolling. In carrying the invention into effect according to one convenient mode by way of example, the accompanying drawing shows a dart shaft having a smaller diameter central portion 11, say between .07 and .09 inches in diameter, formed integrally with enlarged portions at each end, say between .2 and .3 inches in diameter, one portion 12 having a cruciform slot 13 to form a flight holder and the other portion 14 having a screw thread 15 by means of which the shaft may be connected to a dart barrel (not shown). The shaft is composed of magnesium or an alloy containing at least 50% magnesium. The shaft is manufactured from a length of stock material by means of a cold heading process in which axial pressure is applied to wire to cause its ends to be increased to the desired diameter and shape, the enlarged end portion 12 then being slitto provide the cruciform slot 13. Using such a process the grain structure more closely follows the profile of the shaft resulting in increased strength in the finished shafts. Also the forming process causes work-hardening of the metal and this effect is greatest at the ends where most needed. Alternatively, the shaft may be manufactured by rolling a thicker wire to reduce its diameter to give the final desired shape. The enlarged end portion 14 is provided with a screw thread 15, such as a 2BA or 14ft BSF thread. It is customary to provide an undercut adjacent to the shoulder at the base of the thread washer which provides a retaining effect when the shaft is screwed into the barrel. However, this creates a stress con centration in the shoulder region, which can prom ote local fracture, and it is preferred to dispense with the undercut.The thread is preferably formed by rol ling between hardened thread rolls or fiat dies instead of being cut, so that a stronger and smoother thread is produced in which the grain structure fol lows the profile, and the threaded portion is slit lon- gitudinallythrough its axis, as at 16, the two parts thus created being forced slightly apart by means of a wedge so asto exert radial pressure when screwed into the barrel thereby providing a self-jamming or locking effect to give a secure fixing. Itis preferredthatthe shaft should be work- hardened or further work-hardened, for example by ball-burnishing. Various modifications may be made within the scope of the present invention. For example, one or both of the enlarged end portions may be connected to the central shaft portion instead of being formed integrally with it, in which case it may be of advantage to form only one or two ofthethree portions from magnesium or magnesium alloy, the other portion or portions being composed, for example, ofanother metal or plastics. Alternatively, where the three portions are formed integrally by a cold heading or cold forming process, a metal other than magnesium or magnesium alloy may be used, such as aluminium or an aluminium alloy. CLAIMS
1. A dart shaft of the type indicated, wherein at least one of the portions is composed of magnesium or an alloy thereof containing at least 50% magnesium.
2. A dart shaft as claimed in claim 1, wherein the end portions are formed integrally with the central shaft portion.
3. A dart shaft having a smaller diameter central shaft portion formed integrally with enlarged portions at each end, one portion serving as a flight holder and the other having means for connecting the shaft to a dart barrel, wherein the shaft is composed of metal and formed by a cold heading or cold forming process.
4. A dart shaft as claimed in claim 3, wherein the said metal is magnesium organ alloy thereof containing at least 50% magnesium.
5. A dart shaft as claimed in any one of claims 1 to 4, wherein the shaft is work-hardened or further work-hardened.
6. A dart shaft as claimed in any one of claims 1 to 5, wherein the means for connecting the shaft to a shaft barrel includesathreaded portion having longitudinal slits.
7. A dart shaft substantially as described with reference to the accompanying drawings.
GB8104560A 1980-02-13 1981-02-13 Dart shafts Withdrawn GB2068755A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8104560A GB2068755A (en) 1980-02-13 1981-02-13 Dart shafts

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8004818 1980-02-13
GB8104560A GB2068755A (en) 1980-02-13 1981-02-13 Dart shafts

Publications (1)

Publication Number Publication Date
GB2068755A true GB2068755A (en) 1981-08-19

Family

ID=26274477

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8104560A Withdrawn GB2068755A (en) 1980-02-13 1981-02-13 Dart shafts

Country Status (1)

Country Link
GB (1) GB2068755A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5573251A (en) * 1994-05-04 1996-11-12 Target Sports Limited Dart flight stem
GB2622634A (en) * 2022-09-23 2024-03-27 Gravity Brands Ltd Dart point

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5573251A (en) * 1994-05-04 1996-11-12 Target Sports Limited Dart flight stem
GB2622634A (en) * 2022-09-23 2024-03-27 Gravity Brands Ltd Dart point

Similar Documents

Publication Publication Date Title
US4826347A (en) Force-fitted connection of a circular metal tube in an oval housing
US4376604A (en) Blind fastener for composite materials
US3685135A (en) Method of fitting a golf club shaft to a head
EP1131564B1 (en) Screw connection
DE102009043928A1 (en) Cylinder sleeve, cylinder block and method for producing a cylinder liner
US2838000A (en) Projectile and method of making the same
US3076208A (en) Method of making setscrew with mutilated threads
US5209622A (en) Bolt having spherically tipped thread free cylindrical column
DE3991343C1 (en) Deformation bullet, ammunition equipped therewith, and method for the production of the bullet
US4620825A (en) Pull-type blind-riveting assemblies
GB8431667D0 (en) Extrusion dies
EP0312491A1 (en) Fragmentation case for a metallic explosive warhead, and method for manufacturing it
EP0323484B1 (en) Liner for a warhead
US4520521A (en) Process of manufacturing a sleeve and wedge for an anchor bolt
US4622842A (en) Die for extruding toothed helical members
US4381594A (en) Method of cold forming coupling shell
GB2068755A (en) Dart shafts
US5150981A (en) Ball joint assembly having an extended ball surface
EP0403730B1 (en) Sabot
DE4108771A1 (en) CHIPBOARD SCREW
IL30632A (en) Process for forming a self-locking nut
DE19730968B4 (en) Method for producing a projectile and projectile
EP0902249B1 (en) Dart
US3162938A (en) Spacer applying tool
US2250043A (en) Method of fabricating centering bolts and the like

Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)