GB2123124A - Tracer projectile - Google Patents
Tracer projectile Download PDFInfo
- Publication number
- GB2123124A GB2123124A GB08317114A GB8317114A GB2123124A GB 2123124 A GB2123124 A GB 2123124A GB 08317114 A GB08317114 A GB 08317114A GB 8317114 A GB8317114 A GB 8317114A GB 2123124 A GB2123124 A GB 2123124A
- Authority
- GB
- United Kingdom
- Prior art keywords
- tracer
- projectile
- container
- punch
- penetrator
- 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.)
- Granted
Links
- 239000000700 radioactive tracer Substances 0.000 title claims abstract description 40
- 239000000463 material Substances 0.000 claims abstract description 28
- 239000011888 foil Substances 0.000 claims abstract description 11
- 230000002093 peripheral effect Effects 0.000 claims abstract description 7
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims description 6
- 229910052721 tungsten Inorganic materials 0.000 claims description 6
- 239000010937 tungsten Substances 0.000 claims description 6
- JFALSRSLKYAFGM-UHFFFAOYSA-N uranium(0) Chemical compound [U] JFALSRSLKYAFGM-UHFFFAOYSA-N 0.000 claims description 6
- 229910052770 Uranium Inorganic materials 0.000 claims description 2
- 239000000853 adhesive Substances 0.000 claims description 2
- 230000001070 adhesive effect Effects 0.000 claims description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 2
- 229910052782 aluminium Inorganic materials 0.000 claims description 2
- 238000002788 crimping Methods 0.000 claims description 2
- 230000001066 destructive effect Effects 0.000 claims description 2
- 238000005553 drilling Methods 0.000 claims description 2
- 239000007789 gas Substances 0.000 claims description 2
- 238000003754 machining Methods 0.000 claims description 2
- 238000000034 method Methods 0.000 claims description 2
- 239000003380 propellant Substances 0.000 claims description 2
- 239000000565 sealant Substances 0.000 claims description 2
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/38—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information of tracer type
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
Abstract
The projectile comprises a penetrator (10) having a peripheral groove (14) at a rearward end thereof; and a tracer cup or container (20) having a first, open end crimped to the groove (14) and an opposite end closed by a foil seal (37), the cup containing tracer igniting material (32) located adjacent the seal and tracer material (34,35) remote from the seal. <IMAGE>
Description
SPECIFICATION
Tracer projectile
This invention relates to the field of munitions, and more particularly to tracer projectiles.
In the field of small caliber ammunition it is known to equip projectiles with tracer material so that the trajectories of the projectiles may be followed visually. Heretofore it has been known to drill axial cavities at the rearward ends of the projectiles, load tracer material and tracer ignition material into the cavities, and seal the mouths of the cavities with foil to protect the charges.
This procedure has been satisfactory for use with penetrators of tungsten, which is reasonably machinable. Tungsten is very expensive, however, and is in somewhat short supply.
Accordingly, consideration has been given to forming penetrators of depleted uranium, which is in good supply, and more economical. However, the uranium is extremely hard and so destructive of drills that the boring of the necessary tracer cavities is impractical.
According to the present invention, there is provided a projectile comprising a penetrator having a peripheral groove and a rearward end thereof and a container having a first open end secured to said groove and an opposite end closed by a foil seal, said container containing tracer igniting material located adjacent said seal and tracer material remote from said seal.
An embodiment of the invention will now be described by way of example, with reference to the accompanying drawings, in which: Figure 1 is a diagrammatic side view, partly in section of a tracer projectile according to the present invention, and
Figures 2 to 6 show steps in the assembly of the projectile of Fig. 1.
Referring to Fig. 1, the projectile comprises a penetrator 10 symmetrical about an axis 11 and having a blunt forward end 1 2 equipped with a windscreen 13, as is well known for munitions of this type. The rearward end of penetrator 10 is formed, as by grinding or machining for example, with a peripheral groove 1 4 of diameter smaller than that of the
main body of the penetrator 10.
A tracer cup or container 20 is secured to the rearward end of penetrator 10 as by crimping 21 into groove 14. The nature of cup 20 is more clearly shown in Figs. 2 to 6.
Cup 20 comprises a metallic container 22
having an open top 23 and a bottom 24 with a large central aperture 25. To prepare cup 20 the bottom of a die 30 (Figs. 3 to 5) is closed by a male step punch 31, and container 22 is inserted into the die so that its bottom contacts punch 31, which projects through aperture 25. A charge of tracer igniting material 32 is now loaded into container 22 and consolidated with a female step punch 33, (Fig. 3). Punch 23 is removed and a charge 34 of tracer material is consolidated in the container using punch 33, (Fig. 4). That punch is again removed and a second charge 35 of tracer material is consolidated into a container with a flat punch 36, (Fig. 6). Die 30 and punch 31 are removed, and the bottom of container 22 may be closed with a foil seal 37 of aluminum or other suitable material, using an appropriate adhesive.
The container is now removed from punch 36, the non-sealed end 21 being coated internally with a suitable sealant 40 before being positioned at the rearward reduced end of the penetrator 10 where it is crimped or swaged into place. The arrangement is useful with subcaliber or full caliber rounds, and the tracer is ignited through the foil seal by the hot propellant gases, just as before.
From the above it will be evident that the described projectile provides tracer capabilities where the projectile material is not practically drillable to form a tracer cavity. As a matter of fact, it has been found that the described projectile is cost effective, even with materials such as tungsten which are susceptible to drilling.
1. A projectile comprising a penetrator having a peripheral groove and a rearward end thereof and a container having a first open end secured to said groove and an opposite end closed by a foil seal, said container tracer igniting material located adjacent said seal and tracer material remote from said seal.
2. The projectile of Claim 1 in which said penetrator is of depleted uranium.
3. The projectile of Claim 1 or 2, wherein the first open end is crimped to said groove.
4. A projectile substantially as herein described with reference to the accompanying drawings.
5. The and each feature of the projectile described herein either taken alone or in combination.
**WARNING** end of DESC field may overlap start of CLMS **.
Claims (5)
1. A projectile comprising a penetrator having a peripheral groove and a rearward end thereof and a container having a first open end secured to said groove and an opposite end closed by a foil seal, said container tracer igniting material located adjacent said seal and tracer material remote from said seal.
2. The projectile of Claim 1 in which said penetrator is of depleted uranium.
3. The projectile of Claim 1 or 2, wherein the first open end is crimped to said groove.
4. A projectile substantially as herein described with reference to the accompanying drawings.
5. The and each feature of the projectile described herein either taken alone or in combination.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US39460982A | 1982-07-02 | 1982-07-02 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| GB8317114D0 GB8317114D0 (en) | 1983-07-27 |
| GB2123124A true GB2123124A (en) | 1984-01-25 |
| GB2123124B GB2123124B (en) | 1985-09-25 |
Family
ID=23559687
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB08317114A Expired GB2123124B (en) | 1982-07-02 | 1983-06-23 | Tracer projectile |
Country Status (2)
| Country | Link |
|---|---|
| CH (1) | CH660783A5 (en) |
| GB (1) | GB2123124B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4732086A (en) * | 1987-01-27 | 1988-03-22 | Honeywell Inc. | Fin stabilized armor-penetrating tracer projectile and method of manufacturing same |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102023125957A1 (en) * | 2023-09-25 | 2025-03-27 | Rws Gmbh | Tracer projectile with at least one color change |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1340238A (en) * | 1971-06-23 | 1973-12-12 | Karlsruhe Augsburg Iweka | Encased projectile |
| GB1562596A (en) * | 1975-11-12 | 1980-03-12 | Sarmac Sa | Explosive projectile |
| GB1601254A (en) * | 1977-07-21 | 1981-10-28 | Oerlikon Buehrle Ag | Sabot projectile |
| EP0072050A1 (en) * | 1981-08-05 | 1983-02-16 | Werkzeugmaschinenfabrik Oerlikon-Bührle AG | Process to fasten a tracer case in a hole at the rear of a projectile |
-
1983
- 1983-05-02 CH CH236483A patent/CH660783A5/en not_active IP Right Cessation
- 1983-06-23 GB GB08317114A patent/GB2123124B/en not_active Expired
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1340238A (en) * | 1971-06-23 | 1973-12-12 | Karlsruhe Augsburg Iweka | Encased projectile |
| GB1562596A (en) * | 1975-11-12 | 1980-03-12 | Sarmac Sa | Explosive projectile |
| GB1601254A (en) * | 1977-07-21 | 1981-10-28 | Oerlikon Buehrle Ag | Sabot projectile |
| EP0072050A1 (en) * | 1981-08-05 | 1983-02-16 | Werkzeugmaschinenfabrik Oerlikon-Bührle AG | Process to fasten a tracer case in a hole at the rear of a projectile |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4732086A (en) * | 1987-01-27 | 1988-03-22 | Honeywell Inc. | Fin stabilized armor-penetrating tracer projectile and method of manufacturing same |
| WO1988005522A1 (en) * | 1987-01-27 | 1988-07-28 | Honeywell Inc. | Fin stabilized armor-penetrating tracer projectile and method of manufacturing same |
Also Published As
| Publication number | Publication date |
|---|---|
| CH660783A5 (en) | 1987-06-15 |
| GB2123124B (en) | 1985-09-25 |
| GB8317114D0 (en) | 1983-07-27 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19940623 |