AU2005241136A1 - Lead-free projectile - Google Patents
Lead-free projectile Download PDFInfo
- Publication number
- AU2005241136A1 AU2005241136A1 AU2005241136A AU2005241136A AU2005241136A1 AU 2005241136 A1 AU2005241136 A1 AU 2005241136A1 AU 2005241136 A AU2005241136 A AU 2005241136A AU 2005241136 A AU2005241136 A AU 2005241136A AU 2005241136 A1 AU2005241136 A1 AU 2005241136A1
- Authority
- AU
- Australia
- Prior art keywords
- jacket
- core
- hollow space
- small
- projectile
- 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
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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
- F42B12/72—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
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
- F42B12/06—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with hard or heavy core; Kinetic energy penetrators
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- 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
- F42B12/34—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect expanding before or on impact, i.e. of dumdum or mushroom type
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Thermal Sciences (AREA)
- Physics & Mathematics (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Glass Compositions (AREA)
- Electrotherapy Devices (AREA)
- Powder Metallurgy (AREA)
- Fixed Capacitors And Capacitor Manufacturing Machines (AREA)
- Dental Preparations (AREA)
- Earth Drilling (AREA)
- Electron Sources, Ion Sources (AREA)
- Elimination Of Static Electricity (AREA)
- Vibration Dampers (AREA)
- Walking Sticks, Umbrellas, And Fans (AREA)
- Vessels And Coating Films For Discharge Lamps (AREA)
- Led Device Packages (AREA)
Abstract
Disclosed is a small-bore projectile (100) comprising an outer jacket (5) made of tombac, a hard core (4) made of hardened steel, and a hollow jacket core (8) that is also made of tombac. The kinetic energy is substantially transmitted to the hard core (4) when a target (Z) is hit such that said hard core (4) penetrates the target (Z). The ductile jacket (5) is supported by the jacket core (8) that is located on the inside and mushrooms up into a deformed jacket (5') without fragmenting. The inventive projectile (100) is provided with a good flying behavior and a great final ballistic performance and can be produced in an entirely lead-free manner.
Description
Verification of Translation I, Dr. Hana Frauenknecht of Grepperstrasse 53 in CH-6403 Ktssnacht am Rigi, Switzerland, hereby declare that I am conversant with the German and the English languages and certify that to the best of my knowl edge and belief the following is a true and correct trans lation of the German publication WO 2005/108908 Al (RUAG AMMOTEC) Place and date .. ... . Signature WO 2005/108908 Lead-free Projectile Description The present invention relates to a lead-free small-bore jacketed projectile. Such ammunition is known in various designs. It may be divided into those with hard cores made of steel, into those with hard cores made from dense sintered material and those with a medium additional to the hard core such as lead, aluminium and/or air. Together with this commercially available ammunition is a steel jacket, generally configured as a full jacket, i.e. a plated steel jacket or a jacket made from a copper/zinc alloy (tombac jacket). In this connection, the jacket receives one or more cores and further media and encloses said cores and media at least in a liquid-tight manner. Small arms ammunition and the manufacturing process thereof is known from EP-A2-0 106 411. The correspondingly optimised projectiles principally serve as live ammunition for infantry and already have good aerodynamic properties. This ammunition, however, does not have the required high final ballistic energy required by marksmen, which is necessary for penetrating armour plating. A further drawback is the large amount of hard lead (98% Pb + 2% Sn) in the core, which has a toxic effect on the environment both in blank ammunition and live ammunition and therefore is undesirable nowadays or even prohibited in some countries. A jacketed projectile (WO 99/10703) of increased penetration performance and target accuracy has a hard core made of tungsten carbide and, as an additional medium, a soft core made of lead (Pb/Sn WO 2005/108908 2 60/40) which are held with an interference fit in a gastight manner via a brass disc in the jacket. Thus the escape of heavy metals and/or vapour when firing is prevented; a toxic effect is, however, still present in the target area. Additionally, the manufacture of such a projectile is costly and too expensive for mass use (infantry ammunition). A further jacketed projectile for 9 mm bore pistols is marketed under the reference SWISS P SELF 9 mm Luger (RUAG Ammotec, Thun/Switzerland, formerly RUAG Ammunition Thun/Switzerland). In this case, the projectile consists of two sleeves pushed inside one another, the inner sleeve sealed at the tail and open upwards, enclosing a large air space with the outer sleeve. This projectile is, however, only designed for soft targets and, in this case, is able to perforate smoothly; it may be manufactured as lead-free. It is therefore the object of the invention to provide a small-bore projectile (small-bore = bore less than 0.5") suitable for hard targets, which may be manufactured economically, has a high penetration performance and target accuracy and does not release heavy metals on firing or in the target area. The projectile to be provided is intended, in particular, to contain no lead in the core. The projectile according to Claim 1 may be easily manufactured and in a hard target (sheet metal) etc. transmits almost the entire kinetic energy to the hard core which penetrates the target. In this connection, the mass remains preserved at 100%; at the bullet hole a mushroom-shaped collar is formed by the tombac jacket which corresponds to the original weight of the jacket.
WO 2005/108908 3 Thus it is proved that no heavy metals and/or metal vapour are released. The same may be detected for the subject of the invention according to Claim 2. This exhibits a high final ballistic performance, despite there not being a hard core over the entire surface in cross-section, in practical tests no fragmentation was detected at the target. Advantageous developments of the subject of the invention are disclosed in the dependent claims. A projectile with an ogive-like outer shape and an air space according to Claim 3 is particularly advantageous with regard to ballistics. It has been shown, that the necessary pressing-in of the hard core may be carried out accurately and with relatively low forces. Additionally, the pulse transmission of the core, after a short displacement path, allows a penetration of the jacket with lower energy losses. The embodiment according to Claim 4 is very advantageous for the central pulse transfer from the jacket core to the hard core. To a considerable extent, the flying behaviour of the projectile is provided by the position of the centre of gravity, Claim 5. The centre of gravity may be optimised by the constructive design and dimensioning of the hard core and, in particular, of the hollow space (bore) in the jacket core. Alloy tool steels are well suited to the hard core and may be machined and surface-treated by conventional means. Claim 6. Identical materials for the outer jacket and the jacket core according to Claim 7 have proved to be very economical and also expedient with regard to the density, the assembly and the thermal expansion. A constriction according to Claim 8 improves the connection to the cartridge sleeve and allows the simple assembly thereof.
WO 2005/108908 4 The thickening of the jacket in its front region described in Claim 9 reduces ricochets during acute angle firing at hard targets and also serves to determine the centre of gravity. The aforementioned embodiments of the projectile appear to be particularly suitable for the bore and projectile types cited in Claim 10. The current demand for lead-free projectiles is ensured with the choice of material revealed in the claims; see Claim 11. Standard filling material made of heavy metal in conventional projectiles may also be dispensed with, as the position of the centre of gravity may be optimally adjusted by the dimensioning of the individual components and hollow spaces. The invention is disclosed hereinafter with reference to the embodiments and drawings, in which: Figure 1 is a projectile according to the invention, fitted into a cartridge sleeve known per se, Figure 2 is a sectional view through a preferred embodiment of the projectile in Figure 1, Figure 3 is a sectional view of an alternative solution of a lead-free projectile, Figure 4a is a conventional projectile (according to the prior art) when striking the target Figure 4b is a projectile according to Figure 2 when striking the target and Figure 4c is a projectile according to Figure 3 when striking the target.
WO 2005/108908 5 The tip of a projectile 100 is denoted in Figure 1 by 1. A flange 21 is inserted into the reduced diameter of a peripheral constriction 6, and which is a component of a cartridge 20 known per se. A standard explosive 24 is located in the cartridge 20, which acts as a propellant for the projectile 100. An impact fuse 23 (SINTOX, trademark of the firm RUAG Ammotec GmbH, FUrth, DE) is inserted in a base 22 of the cartridge 20. The preferred rotationally symmetrical projectile 100 is visible in Figure 2 in an enlarged sectional view. The actual tip 1 is imaginary; in reality it is a tip in the shape of a spherical cup 2. A small air space 3 is located inside the projectile 100, which is formed between a hard core 4 and an outer jacket 5, as a result of the different radii. A jacket core 8 is attached to the hard core 4 with form fit, and which has a central hollow space 10 in the form of a blind hole. The centre of gravity 7 of the projectile is located in the upper part of said hollow space. An outer peripheral annular groove 6 is located thereover, which is illustrated here, portrayed as a diameter; see Figure 1. At the tail, the end of the jacket 5 is conically tapered and terminates in a stepped portion at an angle a of 300, which stepped portion merges with a terminal flange 9 and holds the two cores 4 and 8 together with an interference fit. The diameter of the projectile 100 denoted by K, the bore, in the present case is 5.56 mm and is of the SS 109 type. The diameter 6 of the constriction is 5.45 mm. The hard core 4 weighs 4 g and is made of hardened tool steel (material according to DIN 1.5511) and has been phosphatised after carburizing (penetration depth = 0.3 - 0.5 mm). The surface hardness is 570 HV1. In this embodiment, the hard core 4 has a lower conical tip of 900 which rests positively in a corresponding recess (countersink) in the upper part of the jacket core 8. This configuration may be varied at will; a similar form of central centering action is, however, advantageous, which facilitates the insertion or pressing-in of the core and ensures the rotational symmetry of the projectile.
WO 2005/108908 6 A hard core 4 made from tombac has also proved expedient; surprisingly, this produces a similar final ballistic performance. The projectiles may be manufactured by standard production devices and substantially by deep drawing and pressing. The hard core may also be made from other materials, for example from sintered materials such as tungsten carbide. Other projectile jackets are also conceivable, which have a similar ductility to tombac. The jacket core may also consist of other materials which have a similar or greater density. In all alloys, however, consideration has to be given to the deposition of heavy metal during firing and at the target. In Figure 3 a variant of the aforementioned projectile is shown, in this connection the same functional parts are provided with the same reference numerals. In contrast to the subject according to Figure 2, in this case, the hard core is dispensed with. A single jacket core 8' similarly fills up the space of the hard core 4, in Figure 2. The associated hollow space 10' is shortened relative to the hollow space 10 and has a smaller diameter. As a result, the mass of the entire projectile 100' is increased, so that approximately the same final ballistic performance and effect is achieved at the target. On the front face, the hollow space 10' tapers and is at least almost closed so that, together with the front part of the outer jacket 5, a compact tip is produced when striking the target. In both variants, measuring results, theoretical observations and comparisons with other projectiles (prior art) show exceptionally good results: The hollow space 10 and/or 10' allows a transverse contraction in the gun barrel (rifle) which, relative to solid projectiles, leads to a reduction in wear (abrasion), in particular in the rifling grooves. At the same time, the firing velocity vo of the projectile 100 and/or 100' at the muzzle is greater than with projectiles without a hollow space 10 and/or 10'.
WO 2005/108908 7 The low drag coefficient Cd of a 5.56 mm projectile (SS 109 type) according to the invention, after a 570 m flight distance (NATO target), still lead to an impact velocity of 470 m/s; the steel plate used was Stanag 4172 of 3.5 mm thickness with 55-70 HRB hardness (400N/mm 2 ) and was perforated smoothly. The precise spin stabilisation acts positively on the stability and reproducibility of the flight path, even with side wind. As a result of the choice of materials and the high firing velocity, the kinetic energy is greater than with comparable projectiles, as tests also showed. The precision of a standard weapon may be increased with the subject of the invention. Thus, for example, all fired shots (repeated fire) at a target distance of 25 m were located in a dispersion circle with a diameter < 50 mm. At a firing distance of 300 m, a standard deviation SD < 35 mm could be detected. In practice, this means that of 20 fired shots, of which 18 are located in a circular surface with a diameter of 110 mm, only two projectiles struck approximately 80 mm offset from the centre (target). As tests in firing against soap have shown, the requirements of the ICRC (International Committee of the Red Cross) are also completely fulfilled, with regard to wound ballistics, in contrast with numerous other projectiles according to the prior art. Figure 4a shows a conventional hard core projectile 200 (prior art) before and during impact on the target Z (steel). The steel jacket 50 explodes at the target Z, a hard core 40 consisting of tungsten or steel penetrates the target Z, whilst, due to the high kinetic energy, the lead core 30 which follows behind is partially liquefied and even partially vaporised by sublimation on impact. This may be seen by a vapour cloud 30' which, after the condensation thereof, also leaves traces of lead at the target. A combination of elastic and plastic impact with high deformability takes place in the projectile 200 (fragmentation of material on all sides). The material of the projectile 200 which is splintered at the target Z and which may still be detected, no longer corresponds to its initial weight at the muzzle.
WO 2005/108908 8 In contrast, on one projectile 100, in Figure 4b, the identical mass may also be detected at the target Z. In this connection, the hard core 4 (steel or tombac) also penetrates the target Z. The outer jacket 5 mushrooms up at the target Z into a deformed jacket 5' and transmits almost 100% of the kinetic energy to the hard core 4 via its similarly ductile jacket core 8; there is no fragmentation of material, either on the jacket 5 or on the jacket core 8. The pulse direction remains preserved. Figure 4c shows a similar view: the projectile 100' which is modified relative to Figure 4b is squashed at the target Z and penetrates with a tip l' which is now flattened. The pulse direction also remains preserved, the jacket core 8' is displaced on impact into the air space 3, compressed and squashed which is denoted here by 8".
WO 2005/108908 9 List of Reference Numerals 1 Tip (imaginary) 1' Flattened, squashed tip 2 Spherical cup 3 Air space (hollow space) 4 Hard core (hardened steel; tombac) 5 Outer jacket (tombac) 5' Deformed jacket 5 6 Constriction/diameter 7 Centre of gravity 8 Jacket core 8' Jacket core 8" Squashed jacket core 8' 9 Flange at 5 10 Hollow space in 8 10' Hollow space in 8' 20 Cartridge sleeve 21 Flange at 20 22 Base of 20 23 Impact fuse 24 Explosive/propellant 30 Lead core 30' Vapour cloud made up of Pb 40 Hard core (tungsten; steel) 40' Lead vapour (sublimated Pb) 50 Steel jacket 100, 100' Projectiles 200 Conventional hard core ammunition (projectile) WO 2005/108908 10 K Bore Z Target (steel plate) Ot Angle (base angle)
Claims (11)
1. Small-bore projectile (100) with an ogival or conical front region, a cylindrical central part and a conically extending tail region, consisting of - an outer jacket (5) made of a copper/zinc alloy, the jacket (5) enclosing an approximately cylindrical hollow space, - a hard core (4) made of steel or a sintered material inserted into the hollow space towards the tip, - a jacket core (8) made of a copper/zinc alloy attached with form fit to the hard core (4), - the hollow space (10) of the jacket core (8) being located in the centre and being open on one face, - the open face of the hollow space (10) resting against the hard core (4) and sealing said hard core, - the tail part of the jacket core (8) being held at least peripherally by the tail region of the jacket (5) with an interference fit.
2. Small-bore projectile (100') with an ogival or conical front region, a cylindrical central part and a conically extending tail region, consisting of - an outer jacket (5) made of a copper/zinc alloy, the jacket (5) enclosing an approximately cylindrical hollow space, - the hollow space of the jacket (5) solely containing a jacket core (8') with a hollow space (10') and an air space (3), WO 2005/108908 12 - the hollow space (10') comprising an aperture tapering on the front face, the inner edge regions thereof being at least partially in contact with one another, - the tail part of the jacket core (8') being held at least peripherally by the tail region of the jacket (5) with an interference fit.
3. Small-bore projectile according to Claim 1, with an ogive-like front region, the tip thereof being configured at least approximately in the shape of a spherical cup, - the cylindrical hollow space in the front inner region being defined in the shape of a spherical cup, - the hard core (4) at its tip also having the shape of a spherical cup, - the radius of the spherical cup of the hollow space being larger than the radius of the tip of the hard core, so that in the hollow space of the jacket, in the tip thereof, an air space (3) remains.
4. Small-bore projectile according to Claim 3, - the tail region of the hard core (4) being of conical configuration and - the conical tip protruding into the hollow space (10) of the jacket core (8).
5. Small-bore projectile according to one of Claims 1 to 4, - the centre of gravity (7) of the projectile being located in the longitudinal axis and in the region of the hollow space (10) of the jacket core (8).
6. Small-bore projectile according to Claim 1 or 3, WO 2005/108908 13 - the hard core (4) consisting of an alloyed tool steel or sintered material of high density, such as tungsten carbide.
7. Small-bore projectile according to Claim 1 or 2, - the outer jacket (5) and the jacket core (8) consisting of the identical copper/zinc alloy.
8. Small-bore projectile according to Claim 1, 2 or Claim 5, - the outer jacket (5) comprising a circumferential, peripheral constriction, on which the front end (21) of a cartridge sleeve (20) is flanged.
9. Small-bore projectile according to Claim 3, - the material of the jacket (5) in its front region, relative to its cylindrical region and its tail region having a thickening which is at least a factor of 2.
10. Small-bore projectile according to at least one of the preceding claims, - said projectile having a bore of 5.56 mm (0.223" or 0.224").
11. Small-bore projectile according to at least one of the preceding claims, - said projectile being lead-free.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US56987604P | 2004-05-11 | 2004-05-11 | |
US60/569,876 | 2004-05-11 | ||
PCT/CH2005/000257 WO2005108908A1 (en) | 2004-05-11 | 2005-05-09 | Lead-free projectile |
Publications (2)
Publication Number | Publication Date |
---|---|
AU2005241136A1 true AU2005241136A1 (en) | 2005-11-17 |
AU2005241136B2 AU2005241136B2 (en) | 2011-06-09 |
Family
ID=34965921
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AU2005241136A Ceased AU2005241136B2 (en) | 2004-05-11 | 2005-05-09 | Lead-free projectile |
Country Status (28)
Country | Link |
---|---|
EP (1) | EP1745260B1 (en) |
JP (1) | JP4713577B2 (en) |
KR (1) | KR101245289B1 (en) |
CN (1) | CN1950667A (en) |
AT (1) | ATE443242T1 (en) |
AU (1) | AU2005241136B2 (en) |
BR (1) | BRPI0511041B1 (en) |
CA (1) | CA2566450C (en) |
CY (1) | CY1109632T1 (en) |
DE (1) | DE502005008143D1 (en) |
DK (1) | DK1745260T3 (en) |
EA (1) | EA009142B1 (en) |
EG (1) | EG24497A (en) |
ES (1) | ES2333658T3 (en) |
HR (1) | HRP20090664T1 (en) |
IL (1) | IL178866A (en) |
MA (1) | MA28572B1 (en) |
MX (1) | MXPA06013084A (en) |
NO (1) | NO334506B1 (en) |
NZ (1) | NZ551194A (en) |
PL (1) | PL1745260T3 (en) |
PT (1) | PT1745260E (en) |
RS (1) | RS51099B (en) |
SI (1) | SI1745260T1 (en) |
TN (1) | TNSN06355A1 (en) |
UA (1) | UA90273C2 (en) |
WO (1) | WO2005108908A1 (en) |
ZA (1) | ZA200609185B (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
PL3105530T3 (en) * | 2014-02-10 | 2018-10-31 | Ruag Ammotec Gmbh | Fragmenting projectile having projectile cores made of pb or pb-free materials having fragmentation in steps |
CN105277078A (en) * | 2014-06-05 | 2016-01-27 | 赵颖 | High-efficiency killing bullet for gun |
DE102014019198A1 (en) * | 2014-12-19 | 2016-06-23 | Diehl Bgt Defence Gmbh & Co. Kg | bullet |
DE102014019197A1 (en) * | 2014-12-19 | 2016-06-23 | Diehl Bgt Defence Gmbh & Co. Kg | bullet |
KR101702955B1 (en) * | 2016-11-03 | 2017-02-09 | 주식회사 두레텍 | Bullet with Increased Effective Range |
DE102017112889A1 (en) * | 2017-06-12 | 2018-12-13 | Rheinmetall Waffe Munition Gmbh | Kleinkalibergschoss and small caliber ammunition with such a small caliber bullet |
KR101942448B1 (en) | 2017-07-11 | 2019-04-11 | 주식회사 풍산 | Armor piercing bullet and armor piercing cartridge with it |
WO2019048914A1 (en) * | 2017-09-09 | 2019-03-14 | Ruag Ammotec Ag | Full metal jacket safety bullet, in particular for multi-purpose applications |
DE102022205242B4 (en) | 2022-05-25 | 2024-02-15 | Metallwerk Elisenhütte GmbH | Bullet for a hard core handgun cartridge and method for producing same |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4384528A (en) * | 1980-04-07 | 1983-05-24 | The United States Of America As Represented By The Secretary Of The Navy | Duplex round |
EP0106411B1 (en) | 1982-10-18 | 1987-06-24 | Schweizerische Eidgenossenschaft vertreten durch die Eidg. Munitionsfabrik Thun der Gruppe für Rüstungsdienste | Small arms ammunition, and manufacturing process therefor |
EP0270527B1 (en) * | 1986-06-09 | 1990-05-09 | Royal Ordnance plc | Armour piercing projectile |
DE3840165A1 (en) * | 1988-06-06 | 1990-07-05 | Schirnecker Hans Ludwig | Multiple projectile |
US5621186A (en) * | 1995-09-20 | 1997-04-15 | Trophy Bonded Bullets, Inc. | Bullet |
DE19710113A1 (en) * | 1997-03-12 | 1998-09-17 | Elisenhuette Metallwerk | Cartridge for handguns, for high accuracy and penetration of armoured targets |
CZ290054B6 (en) * | 1997-08-26 | 2002-05-15 | Ruag Munition | Jacketed projectile comprising a hard core |
US6070532A (en) * | 1998-04-28 | 2000-06-06 | Olin Corporation | High accuracy projectile |
DE10042711A1 (en) * | 1999-09-08 | 2001-03-15 | Dynamit Nobel Ag | Bullet for hunting comprises core and mantle connected to it via deformation section |
WO2001020244A1 (en) * | 1999-09-10 | 2001-03-22 | Dynamit Nobel Gmbh Explosivstoff- Und Systemtechnik | Deformation projectile with a penetrator in the nose of the projectile |
-
2005
- 2005-05-09 DE DE502005008143T patent/DE502005008143D1/en active Active
- 2005-05-09 WO PCT/CH2005/000257 patent/WO2005108908A1/en active Application Filing
- 2005-05-09 DK DK05735953T patent/DK1745260T3/en active
- 2005-05-09 PT PT05735953T patent/PT1745260E/en unknown
- 2005-05-09 CN CNA2005800150116A patent/CN1950667A/en active Pending
- 2005-05-09 EA EA200601893A patent/EA009142B1/en not_active IP Right Cessation
- 2005-05-09 CA CA2566450A patent/CA2566450C/en not_active Expired - Fee Related
- 2005-05-09 BR BRPI0511041-6A patent/BRPI0511041B1/en not_active IP Right Cessation
- 2005-05-09 AU AU2005241136A patent/AU2005241136B2/en not_active Ceased
- 2005-05-09 RS RSP-2009/0495A patent/RS51099B/en unknown
- 2005-05-09 KR KR1020067023639A patent/KR101245289B1/en not_active IP Right Cessation
- 2005-05-09 JP JP2007511831A patent/JP4713577B2/en not_active Expired - Fee Related
- 2005-05-09 NZ NZ551194A patent/NZ551194A/en not_active IP Right Cessation
- 2005-05-09 MX MXPA06013084A patent/MXPA06013084A/en active IP Right Grant
- 2005-05-09 PL PL05735953T patent/PL1745260T3/en unknown
- 2005-05-09 AT AT05735953T patent/ATE443242T1/en active
- 2005-05-09 EP EP05735953A patent/EP1745260B1/en active Active
- 2005-05-09 ES ES05735953T patent/ES2333658T3/en active Active
- 2005-05-09 SI SI200530866T patent/SI1745260T1/en unknown
- 2005-09-05 UA UAA200613135A patent/UA90273C2/en unknown
-
2006
- 2006-10-26 IL IL178866A patent/IL178866A/en active IP Right Grant
- 2006-11-03 TN TNP2006000355A patent/TNSN06355A1/en unknown
- 2006-11-03 ZA ZA200609185A patent/ZA200609185B/en unknown
- 2006-11-08 MA MA29439A patent/MA28572B1/en unknown
- 2006-11-08 EG EGNA2006001063 patent/EG24497A/en active
- 2006-12-01 NO NO20065546A patent/NO334506B1/en unknown
-
2009
- 2009-11-20 CY CY20091101209T patent/CY1109632T1/en unknown
- 2009-12-14 HR HR20090664T patent/HRP20090664T1/en unknown
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FGA | Letters patent sealed or granted (standard patent) | ||
MK14 | Patent ceased section 143(a) (annual fees not paid) or expired |