EP3230681A1 - Geschoss mit reduzierter abprallergefährlichkeit - Google Patents
Geschoss mit reduzierter abprallergefährlichkeitInfo
- Publication number
- EP3230681A1 EP3230681A1 EP15807915.2A EP15807915A EP3230681A1 EP 3230681 A1 EP3230681 A1 EP 3230681A1 EP 15807915 A EP15807915 A EP 15807915A EP 3230681 A1 EP3230681 A1 EP 3230681A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- projectile
- receiving space
- core
- jacket
- casing
- 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
- 229910001369 Brass Inorganic materials 0.000 claims abstract description 10
- 239000010951 brass Substances 0.000 claims abstract description 10
- 239000000463 material Substances 0.000 claims abstract description 8
- 238000005192 partition Methods 0.000 claims description 22
- 230000006378 damage Effects 0.000 abstract description 2
- 239000000428 dust Substances 0.000 description 3
- 230000009172 bursting Effects 0.000 description 2
- 230000007613 environmental effect Effects 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000003628 erosive effect Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 238000013467 fragmentation Methods 0.000 description 1
- 238000006062 fragmentation reaction Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 238000009931 pascalization Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B8/00—Practice or training ammunition
- F42B8/12—Projectiles or missiles
- F42B8/14—Projectiles or missiles disintegrating in flight or upon impact
-
- 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
- F42B12/72—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
- F42B12/74—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the core or solid body
-
- 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
- F42B12/72—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material
- F42B12/76—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the casing
- F42B12/78—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the material of the casing of jackets for smallarm bullets ; Jacketed bullets or projectiles
Definitions
- the invention relates to a projectile, which consists partly of a frangible material, for a short-track munitions.
- Short-track ammunition has the purpose that larger caliber can be used even in smaller training areas.
- Structural measures generate a greater drop in speed. This can be implemented with a low bullet weight.
- Another possibility is a modification of the projectile outer geometry.
- GD spin stabilization
- a deliberate pressure reduction in the run during the firing process which the bullet is accelerated less.
- Frangible is a property of special projectiles and means that the bullet material is designed so that the bullets fragment into very small pieces when hitting hard targets.
- German means frangible breakable.
- the English term has also prevailed in German-speaking countries.
- FIG. 1 shows a cartridge with a frangible projectile 12 according to the prior art.
- the frangible projectile 12 is inserted in a jacket 13, with the ogive of the projectile 12 protruding from the jacket 13. After the impact of the frangible projectile 12 on, for example, a steel plate breaks the frangible projectile 12 to dust 14.
- the modified geometry can lead to considerable loss of precision.
- the invention has the object of developing a projectile according to the preamble of claim 1 so that the above-mentioned disadvantages are avoided.
- the projectile consists of a jacket made of brass, the jacket, viewed in the direction of flight, has a front cylindrical receiving space and a rear cylindrical receiving space, both receiving spaces arranged coaxially to the projectile longitudinal axis and separated by a partition wall, the partition the bottom of the front Recording space forms and in the front receiving space a core of a frangible material is used, the Core protrudes with its tip from the front receiving space and in the region of the partition at least one circumferential on the jacket predetermined breaking point is introduced into the mantle, it comes through the modified geometry to no loss of precision and the internal ballistic load is not so great that this destroys the Bullet leads.
- a groove or spiral formed in the front room can also have further predetermined breaking points.
- a flare is arranged in the rear receiving space.
- the rear recording room is suitable for this purpose and the flare moves the center of gravity even slightly desired backwards, whereby the trajectory is improved.
- the core is preferably glued or pressed into the front receiving space. Both are fixing methods that offer and lead to the desired anchorages.
- the core has chamfers or grooves running parallel to the projectile longitudinal axis on its outer surface from the rear end to the front end of the jacket.
- a bore connecting the front receiving space with the rear receiving space is arranged in the dividing wall. This also dissipates the compressed air.
- a blind hole may be introduced, which communicates with the front receiving space. This blind hole is used for pressure reduction.
- two predetermined breaking points circulating on the jacket are introduced into the jacket in the region of the partition wall, with a predetermined breaking point being introduced on the rear end of the partition seen in the direction of flight.
- the predetermined breaking points are preferably introduced at right angles to the projectile longitudinal axis and are formed in cross-section V-shaped or U-shaped. These predetermined breaking points improve the decomposition behavior.
- the inner wall of the front receiving groove has one or more notches parallel to the projectile axis or spiral-shaped notches. This improves the anchoring of the frangible core in the front receiving space.
- FIG. 1 shows the state of the art and is described above.
- FIG 2 shows an embodiment of a projectile according to the invention, consisting of a jacket 4 made of brass and a frangible core.
- the jacket 4 has, seen in the direction of flight 19, a front 4a and a rear cylindrical receiving space 4b in the projectile tail 1 1 on.
- the front receiving space 4 a was introduced from the front and the rear receiving space 4 b from behind in the jacket 4.
- Both receiving spaces 4a, 4b are arranged coaxially to the projectile longitudinal axis 15 of the projectile and are separated by a partition wall 16.
- the partition wall 16 forms the bottom of the receiving space 4a.
- In the front receiving space 4a of the frangible core is used, preferably via a press fit.
- the frangible core 1 protrudes with its front tip 17 from the front receiving space 4a, or the jacket 4 out.
- a flare (not shown in the figure) is introduced in the rear receiving space 4b.
- This predetermined breaking point 2 is introduced at right angles to the projectile longitudinal axis 15 and can, as shown, be rectangular in cross-section. However, a V-shaped predetermined breaking point 2, as shown in FIG. 4, is preferred.
- the outer geometry of the projectile thus consisting of a frangible core 1 and a jacket 4 and largely corresponds to a known and proven short-track munitions of the applicant.
- a core 1 is inserted into the jacket 4, which consists of frangible material.
- a frangible core is understood to mean a kernel that breaks down when hitting a hard target, for example into a dust.
- 1 1 predetermined breaking points 2 are attached to the projectile tail, so that the residual mass of the individual parts corresponds at most to the mass of a conventional small caliber projectile.
- the jacket 4 of the projectile is preferably made of brass. With brass as a shell, the bullet of the invention has largely decomposed on impact to dust. This was surprising and not predicted for the skilled person.
- the frangible core 1 is pressed into the jacket 4.
- the frangible core 1 produces a high hydrostatic pressure when pressed in abruptly (see the arrows 20 in FIG. 3). This causes a fragmentation of the majority of the projectile.
- the brass of the shell 4 behaves naturally brittle at such a short loading period. Also, the multiaxial load condition when bursting the frangible core 1 helps that the brass of the shell 4 behaves brittle. As a result, the impact energy is extremely reduced and almost destroyed.
- the frangible core 1 of the projectile is a subcaliber projectile, which is simply inserted into the front receiving space 4a.
- the attachment between shell 4 and frangible core 1 can be implemented by means of adhesive or interference fit. If a press fit is chosen, side chamfers on the core can drain the compressed air. Another possibility is the discharge of the compressed air when setting the projectile through a hole in the projectile longitudinal axis 15 through the partition 16 or through a blind hole in the partition, so that the pressure can be mininned.
- the tailstock 1 1 is still made of brass, as this is suitable for pressing light sets.
- FIG. 4 shows another embodiment of a projectile 5 according to the invention, consisting of a jacket 4 made of brass and a frangible core 1.
- the jacket 4 also has, seen in the direction of flight 19, a front 4a and a rear cylindrical receiving space 4b in the projectile tail 1 1 on.
- the front receiving space 4 a was introduced from the front and the rear receiving space 4 b from behind in the jacket 4.
- Both receiving spaces 4a, 4b are arranged coaxially to the projectile longitudinal axis 15 of the projectile and are separated by a partition wall 16.
- the partition 16 is substantially thicker in this embodiment than in the embodiment according to FIG. Again, the partition wall 16 forms the bottom of the receiving space 4a.
- the front receiving space 4a of the frangible core 1 is used, preferably via a press fit.
- the frangible core 1 protrudes here with its front tip 17 from the front receiving space 4a, and the jacket 4 out.
- a flare (not shown in the figure) may be introduced.
- a predetermined breaking point 2 b is introduced at the front portion of the partition wall 16 .
- These predetermined breaking points 2a, 2b are introduced at right angles to the projectile longitudinal axis 15 and are formed in cross-section V-shaped.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Catching Or Destruction (AREA)
- Medicines Containing Antibodies Or Antigens For Use As Internal Diagnostic Agents (AREA)
- Nitrogen And Oxygen Or Sulfur-Condensed Heterocyclic Ring Systems (AREA)
- Toys (AREA)
Abstract
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
HRP20190650TT HRP20190650T1 (hr) | 2014-12-11 | 2019-04-05 | Projektil sa smanjenim rizikom od rikošeta |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP14197363 | 2014-12-11 | ||
EP15171573 | 2015-06-11 | ||
PCT/EP2015/079198 WO2016091991A1 (de) | 2014-12-11 | 2015-12-10 | Geschoss mit reduzierter abprallergefährlichkeit |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3230681A1 true EP3230681A1 (de) | 2017-10-18 |
EP3230681B1 EP3230681B1 (de) | 2019-03-13 |
Family
ID=54843843
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP15807915.2A Active EP3230681B1 (de) | 2014-12-11 | 2015-12-10 | Geschoss mit reduzierter abprallergefährlichkeit |
Country Status (11)
Country | Link |
---|---|
US (1) | US9970739B2 (de) |
EP (1) | EP3230681B1 (de) |
AU (1) | AU2015359428B2 (de) |
BR (1) | BR112017012373B1 (de) |
CA (1) | CA2970505C (de) |
DK (1) | DK3230681T3 (de) |
HR (1) | HRP20190650T1 (de) |
HU (1) | HUE044969T2 (de) |
IL (1) | IL252823A0 (de) |
SG (1) | SG11201704809SA (de) |
WO (1) | WO2016091991A1 (de) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10436557B2 (en) * | 2016-04-18 | 2019-10-08 | Ammo Technologies, Inc. | Armor-piercing projectile |
US20190120603A1 (en) * | 2017-10-19 | 2019-04-25 | Richard C. Cole | Projectile with radial grooves |
US11486683B2 (en) * | 2021-04-06 | 2022-11-01 | Joseph Cziglenyi | Angled dual impact bullet |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10045009A1 (de) | 1999-09-11 | 2001-05-10 | Dynamit Nobel Ag | Jagdbüchsengeschoß mit zusätzlich gekapseltem Kern |
DE50101647D1 (de) | 2000-11-23 | 2004-04-15 | Contraves Pyrotec Ag | Treibspiegel-Geschoss mit Zerschell-Penetrator |
WO2003027602A1 (de) | 2001-09-22 | 2003-04-03 | Ruag Ammotec Gmbh | Sich zerlegendes jagdgeschoss |
DE102009011093A1 (de) | 2009-03-03 | 2010-09-09 | Brenneke Gmbh | Teilzerlegungsgeschoss für Jagdzwecke |
RU2631369C2 (ru) | 2011-12-01 | 2017-09-21 | Руаг Аммотек Гмбх | Частично или полностью разрушаемый снаряд с не содержащим свинца сердечником, с намеченными участками разрушения |
-
2015
- 2015-12-10 WO PCT/EP2015/079198 patent/WO2016091991A1/de active Application Filing
- 2015-12-10 EP EP15807915.2A patent/EP3230681B1/de active Active
- 2015-12-10 HU HUE15807915 patent/HUE044969T2/hu unknown
- 2015-12-10 DK DK15807915.2T patent/DK3230681T3/da active
- 2015-12-10 US US15/534,990 patent/US9970739B2/en active Active
- 2015-12-10 BR BR112017012373-8A patent/BR112017012373B1/pt active IP Right Grant
- 2015-12-10 SG SG11201704809SA patent/SG11201704809SA/en unknown
- 2015-12-10 AU AU2015359428A patent/AU2015359428B2/en active Active
- 2015-12-10 CA CA2970505A patent/CA2970505C/en active Active
-
2017
- 2017-06-11 IL IL252823A patent/IL252823A0/en unknown
-
2019
- 2019-04-05 HR HRP20190650TT patent/HRP20190650T1/hr unknown
Also Published As
Publication number | Publication date |
---|---|
BR112017012373B1 (pt) | 2021-06-01 |
EP3230681B1 (de) | 2019-03-13 |
CA2970505A1 (en) | 2016-06-16 |
US9970739B2 (en) | 2018-05-15 |
BR112017012373A2 (pt) | 2018-04-24 |
SG11201704809SA (en) | 2017-07-28 |
DK3230681T3 (da) | 2019-05-06 |
IL252823A0 (en) | 2017-08-31 |
HRP20190650T1 (hr) | 2019-05-31 |
CA2970505C (en) | 2020-08-18 |
HUE044969T2 (hu) | 2019-11-28 |
AU2015359428B2 (en) | 2020-06-25 |
WO2016091991A1 (de) | 2016-06-16 |
NZ733335A (en) | 2021-01-29 |
US20170336183A1 (en) | 2017-11-23 |
AU2015359428A1 (en) | 2017-07-20 |
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