EP3679315B1 - Vollmantel-sicherheitsgeschoss, insbesondere für mehrzweckanwendungen - Google Patents
Vollmantel-sicherheitsgeschoss, insbesondere für mehrzweckanwendungen Download PDFInfo
- Publication number
- EP3679315B1 EP3679315B1 EP18762548.8A EP18762548A EP3679315B1 EP 3679315 B1 EP3679315 B1 EP 3679315B1 EP 18762548 A EP18762548 A EP 18762548A EP 3679315 B1 EP3679315 B1 EP 3679315B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- full jacket
- projectile according
- safety projectile
- recess
- sided
- 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.)
- Active
Links
- 229910052751 metal Inorganic materials 0.000 title claims description 9
- 239000002184 metal Substances 0.000 title claims description 9
- 230000035515 penetration Effects 0.000 claims description 36
- 239000002360 explosive Substances 0.000 claims description 34
- 229910000831 Steel Inorganic materials 0.000 claims description 9
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 9
- 239000010959 steel Substances 0.000 claims description 9
- 239000010936 titanium Substances 0.000 claims description 8
- 229910052719 titanium Inorganic materials 0.000 claims description 8
- 238000004519 manufacturing process Methods 0.000 claims description 6
- 230000000149 penetrating effect Effects 0.000 claims description 5
- 230000000977 initiatory effect Effects 0.000 claims description 4
- 239000000203 mixture Substances 0.000 claims description 4
- 230000006835 compression Effects 0.000 claims description 3
- 238000007906 compression Methods 0.000 claims description 3
- LSSAUVYLDMOABJ-UHFFFAOYSA-N [Mg].[Co] Chemical compound [Mg].[Co] LSSAUVYLDMOABJ-UHFFFAOYSA-N 0.000 claims description 2
- 238000005065 mining Methods 0.000 claims description 2
- 239000000843 powder Substances 0.000 claims description 2
- 239000002994 raw material Substances 0.000 claims description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims 1
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims 1
- 239000000654 additive Substances 0.000 claims 1
- 230000000996 additive effect Effects 0.000 claims 1
- 229910052782 aluminium Inorganic materials 0.000 claims 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims 1
- 238000005516 engineering process Methods 0.000 claims 1
- 239000007924 injection Substances 0.000 claims 1
- 238000002347 injection Methods 0.000 claims 1
- 229910052749 magnesium Inorganic materials 0.000 claims 1
- 239000011777 magnesium Substances 0.000 claims 1
- 239000011159 matrix material Substances 0.000 claims 1
- 229920001643 poly(ether ketone) Polymers 0.000 claims 1
- 229920000642 polymer Polymers 0.000 claims 1
- 229910052726 zirconium Inorganic materials 0.000 claims 1
- 230000035939 shock Effects 0.000 description 14
- 230000015556 catabolic process Effects 0.000 description 9
- 230000000694 effects Effects 0.000 description 7
- 239000000463 material Substances 0.000 description 6
- 239000007787 solid Substances 0.000 description 5
- 238000010276 construction Methods 0.000 description 4
- 239000000700 radioactive tracer Substances 0.000 description 4
- 238000012360 testing method Methods 0.000 description 4
- 239000000126 substance Substances 0.000 description 3
- POCJOGNVFHPZNS-ZJUUUORDSA-N (6S,7R)-2-azaspiro[5.5]undecan-7-ol Chemical compound O[C@@H]1CCCC[C@]11CNCCC1 POCJOGNVFHPZNS-ZJUUUORDSA-N 0.000 description 2
- 229910000760 Hardened steel Inorganic materials 0.000 description 2
- BSPUVYFGURDFHE-UHFFFAOYSA-N Nitramine Natural products CC1C(O)CCC2CCCNC12 BSPUVYFGURDFHE-UHFFFAOYSA-N 0.000 description 2
- TZRXHJWUDPFEEY-UHFFFAOYSA-N Pentaerythritol Tetranitrate Chemical compound [O-][N+](=O)OCC(CO[N+]([O-])=O)(CO[N+]([O-])=O)CO[N+]([O-])=O TZRXHJWUDPFEEY-UHFFFAOYSA-N 0.000 description 2
- 206010041662 Splinter Diseases 0.000 description 2
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 2
- 238000004200 deflagration Methods 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- POCJOGNVFHPZNS-UHFFFAOYSA-N isonitramine Natural products OC1CCCCC11CNCCC1 POCJOGNVFHPZNS-UHFFFAOYSA-N 0.000 description 2
- 239000003550 marker Substances 0.000 description 2
- 150000002736 metal compounds Chemical class 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000004806 packaging method and process Methods 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 0.000 description 2
- 241000209035 Ilex Species 0.000 description 1
- NRTOMJZYCJJWKI-UHFFFAOYSA-N Titanium nitride Chemical compound [Ti]#N NRTOMJZYCJJWKI-UHFFFAOYSA-N 0.000 description 1
- 229910000994 Tombac Inorganic materials 0.000 description 1
- 239000004480 active ingredient Substances 0.000 description 1
- 230000001154 acute effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000009435 building construction Methods 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 230000002349 favourable effect Effects 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
- 239000000383 hazardous chemical Substances 0.000 description 1
- 238000007373 indentation Methods 0.000 description 1
- 238000011089 mechanical engineering Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000008520 organization Effects 0.000 description 1
- 210000002381 plasma Anatomy 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000003716 rejuvenation Effects 0.000 description 1
- 238000011076 safety test Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- UONOETXJSWQNOL-UHFFFAOYSA-N tungsten carbide Chemical compound [W+]#[C-] UONOETXJSWQNOL-UHFFFAOYSA-N 0.000 description 1
- 230000003313 weakening effect Effects 0.000 description 1
- 238000005303 weighing Methods 0.000 description 1
Images
Classifications
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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
- F42B12/04—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
-
- 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
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/207—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type characterised by the explosive material or the construction of the high explosive warhead, e.g. insensitive ammunition
-
- 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 present invention relates to a full jacket security bullet according to the preamble of the patent claim.
- a security projectile is a projectile that contains only a minimal amount of explosives and can still be used as a pure penetrating projectile, multi-purpose projectile, explosive projectile or incendiary projectile.
- Small amounts of small caliber ammunition should also be sent more often by air freight at short notice, for reasons of time and for other reasons, for local protection and defense tasks, but also for test purposes.
- safety regulations namely regulations and transport classifications for dangerous goods of the IATA (International Air Transport Association) and the ICAO-TI (special organization of the UN for international civil aviation). Compliance with and monitoring of all regulations is the responsibility of the transporters and especially the members of the IATA and the airport and customs authorities.
- a successful safety test of the transport facility according to UN recommendations is required necessary so that these dangerous goods receive a transport classification, for example according to the classification code 1.4 S (UN 0012, among other things, cartridges for small arms).
- the packaging is described in detail and the maximum amount (number of pieces) of ammunition to be transported is specified.
- the dangerous goods are also limited to a total net weight of max. 25 kg.
- the total weight of the transport equipment must not exceed 50 kg, so that there are also relatively narrow limits for protective measures (transport packaging, etc.).
- incendiary bullet is out of the DE-OS- 2 323 798 known, this contains a sub-caliber, central penetration core made of hard metal, which is encased by an incendiary material.
- the penetration core is placed on a stern part of the same caliber, which acts as a sabot and is separated at the target via a predetermined breaking point.
- An incendiary device is placed in front of the penetration core, which also serves as a hit marker.
- the projectile should also be executable as tracer ammunition.
- the penetration performance for example of a multi-purpose bullet, should both in relation to the penetration depth and the penetration diameter compared to the EP application no. 16405018.9 at least be the same or even better.
- the hole in the target should only represent a low flow resistance for the plasmas of the incendiary devices.
- the internal and external ballistics of the projectile and the target accuracy should also be at least the same.
- the projectile structure should be inexpensive and precise to manufacture from a few parts and be able to be produced in large series using conventional means and processes. It must also be possible to manufacture the projectile for use in rifle cartridges. - In smaller numbers, the bullets should also be approved for air transport.
- the punch-through core mentioned here is preferably in one piece for manufacturing and dynamic reasons, but it can also be made up of several parts.
- the transition area between the front part and the actual penetration part is designed to guide the resulting shock waves, so that when the target penetrates, a phlegmatized explosive is initiated without further aids (such as detonating chains, sensitive explosives, etc.).
- the resulting splintering effect in the front part of the penetration core allows it to penetrate massive plates with full kinetic energy.
- the mass of explosive can basically be reduced; the dangerous nitropenta, which is often used today, can also be dispensed with.
- the different transit times of the opposing shock waves are in the range of microseconds, so that as a result of the inertia of the explosive, its extremely high compression and thus reliable initiation take place immediately.
- the amount of explosive can be reduced considerably in the subject matter of the invention, as shown by reproducible shooting tests at various targets with a multi-purpose bullet of caliber 0.5, without duds, deflagrations or deflagrations.
- a simple steering of shock waves takes place according to claim 2 by circumferential notches on the solid jacket.
- a front surface that is the surface which causes and aligns the reflection of the shock waves towards the recess 5
- the upper wedge surface is preferably flat, planar and, in particular, frustoconical with respect to the axial direction (F) (weft direction).
- the upper wedge surface can be configured at least partially, preferably completely, convex, preferably parabolic (viewed from the outside of the penetration core), in order to focus the shock waves onto the explosive in the recess.
- the further lower surface of the wedge-shaped constriction can also be either flat, planar or convex, in particular parabolic.
- the alignment of the front surfaces on the breakdown core takes place in the simplest way, in that this is determined geometrically, by a center line leading to the Target point leads. - This is the predetermined point where shock wave initiation is most efficient; Claim 5.
- the double function of the first wedge-shaped constriction mentioned in claim 7 is very space-saving and has proven to be extremely effective.
- a hardened steel tip ensures a good penetration into the target, which is increased by inserting a titanium pin, like a pilot hole. This hard pin creates a high surface pressure on the target, so that there are hardly any ricochets; Claim 8.
- the embodiment according to claim 9 results in a highly effective, continuously burning marking charge and is therefore used as a tracer.
- the pyrotechnic mixture according to claim 10 results in a good target marking, as is particularly desired in the case of multi-purpose projectiles.
- the front part of the penetration core in particular a cup part with the front, blind hole-like recess for filling with explosive, and a central part of the penetration core are made, in particular rotated, from one piece, in particular a metal piece.
- the metal piece is preferably formed from simple steel without, in particular, having an addition of magnesium-cobalt.
- the middle and rear parts of the breakdown core are delimited from one another in the axial direction by the front part by the first constriction.
- a rear end face of the breakdown core has a planar or flat surface or, alternatively, a convex, preferably parabolic shape, in particular to reflect and align, preferably bundle, especially shock waves essentially in the axial direction through the breakdown core towards the recess in the front part .
- the measures according to the invention resulted in a significant manufacturing advantage in that, instead of the usual high-quality magnesium-cobalt-metal mixture, a simple steel material can be used in order to achieve the desired function of the security projectile.
- a simple steel material can be used in order to achieve the desired function of the security projectile.
- the wedge-shaped constriction or groove which separates the front part from the central part of the puncture core resulted in a concentration of the deformation forces.
- the design of the penetration core in the front part is particularly advantageous with regard to the shape of the recess which, due to the weakening of the material, serves as a desired crumple zone, which in particular makes it possible to use a simple steel material for the penetration core.
- circumferential weaknesses arranged in the region of the recess, in particular grooves or notches, are preferably provided, which can also be oriented axially or spirally.
- Figure 1 is on a penetrating bullet of caliber 0.5 whose full jacket is designated with 1; this projectile is shot in a normal run (not shown) in the direction of flight F.
- the full jacket 1 has a flattened tip 2.
- An ogive-shaped, hardened steel point 4 with a front, central titanium pin 3 is embedded in the projectile point.
- a one-piece penetration core 6 with a blind hole-shaped recess 5 is provided, the conical surfaces of which are denoted by 5a and the point by 5b.
- a highly phlegmatized explosive 5 ' is pressed into the recess 5.
- the front area 6 'of the breakdown core 6 has a first wedge-shaped constriction 10, a recess into which a socket 7 made of plastic protrudes, which surrounds the breakdown core 6 laterally in the middle part.
- the socket 7 is cut off at the rear and leaves an air space 8 free between the solid jacket 1 and the penetration core 6, which has a positive internal ballistic effect.
- a second analogous wedge-shaped constriction 11 is located in front of the rear region of the breakdown core 6, the upper wedge surface 11 'here forming a relatively small acute angle with respect to the horizontal.
- a taper 15 is provided which is useful for introducing the projectile into a conventional cartridge and at the same time is aerodynamically advantageous.
- the projectile is closed by a rear sealing washer 9, which is inserted at its notoriously known flanging 16.
- the solid jacket 1 has circumferential notches 1 '(indentations) in the front region 6' of the punch core 6.
- a customary fine-grain steel with a hardness of 57 HRC is suitable as the steel tip 4.
- titanium carbide or titanium nitride, so-called cermets are also suitable.
- the socket 7 can perform several functions, especially if it is designed as a metal compound.
- the targeted addition of metal powder can also be useful for optimizing the center of gravity of the projectile.
- the notches 1 'and the wedge-shaped constrictions 10 act analogously to the subject matter of the invention European patent application No. 16405018.9 splinter-forming and increase the penetration capacity of the core 6. On the other hand, they also serve here to direct shock waves as follows in Fig. 2 will be shown.
- the titanium post is 3 in Fig. 2 not shown.
- the central shock wave front S1 that forms on impact with the target experiences a dispersion at the transition to the explosive 5 ', with the side waves being reflected at the notches 1' of the full jacket 1 as wave fronts S3 at the same time.
- the second wedge-shaped constriction 11 in the penetration core 6 reflects on its wedge surface 11 'lateral wavefronts S2' running towards the center, which overlap with the wavefronts S1 and act as pressure waves in the explosive 5 'through the first wedge-shaped constriction 10; see. Fig. 3 , an enlarged view in the front part 6 'of the breakdown core.
- the construction according to the invention enables the construction of new projectile types with specific effects in the target, as the following example indicates.
- a sleeve 14 made of tombac which is provided with a point, is inserted in a blind hole-like recess 12 at the rear of the penetration core 6.
- a marker charge 13 which is pressed into the case 14, is ignited when fired by the cartridge (not shown) via the rear seal 9 and via a small ignition charge 13 '.
- This thermally favorable construction is characterized by an even burn over the entire flight distance of the projectile and serves as a reliably acting tracer.
- the seal 9 is then inserted and the rear side of the entire floor is provided with a flange 16, see Fig. 6 .
- the subject matter of the invention represents an open construction, i.e. it can be modified in a wide variety of ways, combined with different materials and adapted to the intended, specific application, including by means of inserts made of metal splinters. According to the model laws, medium and large-caliber weapons should also be realizable in an analogous manner.
- the cylindrical shaft of the penetration core 6 can also be designed in the shape of an ogive.
- the subject matter of the invention is not limited to police and military applications: In mechanical engineering, mining, building construction and civil engineering, but also when exploring raw materials, breakthroughs and boreholes must be continuously made, which for safety and environmental reasons are only made with minimal use of explosives should.
- the use claims 13 to 17 outline these uses, but by no means exhaustive.
Landscapes
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Portable Nailing Machines And Staplers (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
- Powder Metallurgy (AREA)
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
- Buffer Packaging (AREA)
- Drilling And Exploitation, And Mining Machines And Methods (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
HRP20211681TT HRP20211681T1 (hr) | 2017-09-09 | 2018-09-10 | Sigurnosni metak s punom metalnom košuljicom, posebno za višenamjenske primjene |
SI201830461T SI3679315T1 (sl) | 2017-09-09 | 2018-09-10 | Popolnoma oplaščeni varnostni izstrelek, zlasti za večnamensko uporabo |
RS20211410A RS62590B1 (sr) | 2017-09-09 | 2018-09-10 | Sigurnosni projektil sa potpunom košuljicom, naročito za višenamensku primenu |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/IB2017/055447 WO2019048914A1 (de) | 2017-09-09 | 2017-09-09 | Vollmantel-sicherheitsgeschoss, insbesondere für mehrzweckanwendungen |
PCT/EP2018/074315 WO2019048678A1 (de) | 2017-09-09 | 2018-09-10 | Vollmantel-sicherheitsgeschoss, insbesondere für mehrzweckanwendungen |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3679315A1 EP3679315A1 (de) | 2020-07-15 |
EP3679315B1 true EP3679315B1 (de) | 2021-08-18 |
Family
ID=59966800
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP18762548.8A Active EP3679315B1 (de) | 2017-09-09 | 2018-09-10 | Vollmantel-sicherheitsgeschoss, insbesondere für mehrzweckanwendungen |
Country Status (30)
Country | Link |
---|---|
US (1) | US10976143B2 (es) |
EP (1) | EP3679315B1 (es) |
JP (1) | JP7108685B2 (es) |
KR (1) | KR20200084325A (es) |
CN (1) | CN111433554B (es) |
AU (1) | AU2018328056B2 (es) |
BR (1) | BR112020004521B1 (es) |
CA (1) | CA3074896A1 (es) |
CL (1) | CL2020000590A1 (es) |
CO (1) | CO2020004185A2 (es) |
CR (1) | CR20200155A (es) |
DK (1) | DK3679315T3 (es) |
EA (1) | EA038243B1 (es) |
EC (1) | ECSP20021970A (es) |
HR (1) | HRP20211681T1 (es) |
HU (1) | HUE056480T2 (es) |
IL (1) | IL273134A (es) |
JO (1) | JOP20200051A1 (es) |
LT (1) | LT3679315T (es) |
MA (1) | MA50072A (es) |
MX (1) | MX2020002616A (es) |
PE (1) | PE20201127A1 (es) |
PH (1) | PH12020500449A1 (es) |
RS (1) | RS62590B1 (es) |
SA (1) | SA520411496B1 (es) |
SG (1) | SG11202002112WA (es) |
SI (1) | SI3679315T1 (es) |
UA (1) | UA125975C2 (es) |
WO (2) | WO2019048914A1 (es) |
ZA (1) | ZA202001711B (es) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102017106526A1 (de) * | 2017-03-27 | 2018-10-11 | Rheinmetall Waffe Munition Gmbh | Geschoss, insbesondere im Mittelkaliberbereich |
US11333472B1 (en) * | 2018-07-16 | 2022-05-17 | Vista Outdoor Operations Llc | Reduced stiffness barrel fired projectile |
DE102019135870A1 (de) * | 2019-12-30 | 2021-07-01 | Ruag Ammotec Ag | Projektil und Munition |
CN111595211B (zh) * | 2020-06-24 | 2024-06-04 | 湖南天合终极防务科技实业有限公司 | 一种高穿透子弹 |
EP4148413A4 (en) | 2020-07-08 | 2023-10-18 | LG Energy Solution, Ltd. | SYSTEM FOR DETECTING DEFECTIVE POROUS FILMS AND DETECTION METHOD |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1240760B (de) | 1962-12-24 | 1967-05-18 | Diehl Fa | Panzerbrandgeschoss |
NO137297C (no) * | 1976-07-01 | 1978-02-01 | Raufoss Ammunisjonsfabrikker | Prosjektil. |
US4444112A (en) | 1981-03-27 | 1984-04-24 | A/S Raufoss Ammunisjonsfabrikker | Multi-capability projectile and method of making same |
BE905373A (fr) * | 1986-09-04 | 1987-03-04 | Herstal Sa | Projectile a effets multiples. |
FR2615937B1 (fr) * | 1987-05-27 | 1989-09-08 | Ladriere Serge | Perfectionnements apportes aux projectiles perforants |
NO172865B1 (no) | 1991-08-01 | 1993-09-15 | Raufoss As | Flereffekt-prosjektil og fremgangsmate ved dets fremstilling |
DE19948710B4 (de) * | 1999-10-09 | 2006-03-02 | Rheinmetall W & M Gmbh | Flügelstabilisiertes Wuchtgeschoß |
EP1167914A1 (de) * | 2000-06-19 | 2002-01-02 | SM Schweizerische Munitionsunternehmung AG | Selbstangetriebenes Geschoss mit einem Durchschlagskern |
US20030140811A1 (en) * | 2001-12-14 | 2003-07-31 | General Dynamics Ordnance & Tactical Systems, Inc. | Medium caliber high explosive dual-purpose projectile with dual function fuze |
DE502005008143D1 (de) * | 2004-05-11 | 2009-10-29 | Ruag Ammotec | Bleifreies geschoss |
JP2006132874A (ja) * | 2004-11-08 | 2006-05-25 | Mitsubishi Heavy Ind Ltd | 弾丸 |
FR2910612B1 (fr) * | 2006-12-21 | 2009-10-02 | Ateliers Mecaniques De Pont Su | Bombe aerienne de penetration munie d'un revetement externe. |
US8056478B2 (en) * | 2008-04-25 | 2011-11-15 | Raytheon Company | Methods and apparatus for high-impulse fuze booster for insensitive munitions |
US9587918B1 (en) * | 2015-09-24 | 2017-03-07 | True Velocity, Inc. | Ammunition having a projectile made by metal injection molding |
-
2017
- 2017-09-09 WO PCT/IB2017/055447 patent/WO2019048914A1/de active Application Filing
-
2018
- 2018-09-10 CR CR20200155A patent/CR20200155A/es unknown
- 2018-09-10 MA MA050072A patent/MA50072A/fr unknown
- 2018-09-10 CA CA3074896A patent/CA3074896A1/en active Pending
- 2018-09-10 LT LTEPPCT/EP2018/074315T patent/LT3679315T/lt unknown
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