EP3312546A1 - Multi-purpose projectile - Google Patents
Multi-purpose projectile Download PDFInfo
- Publication number
- EP3312546A1 EP3312546A1 EP16405018.9A EP16405018A EP3312546A1 EP 3312546 A1 EP3312546 A1 EP 3312546A1 EP 16405018 A EP16405018 A EP 16405018A EP 3312546 A1 EP3312546 A1 EP 3312546A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- projectile according
- purpose projectile
- solid
- core
- front part
- 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
- 239000002360 explosive Substances 0.000 claims abstract description 18
- 230000015556 catabolic process Effects 0.000 claims abstract description 17
- 239000000203 mixture Substances 0.000 claims abstract description 9
- 239000007787 solid Substances 0.000 claims description 22
- 230000035515 penetration Effects 0.000 claims description 19
- 230000000694 effects Effects 0.000 claims description 6
- 229910052751 metal Inorganic materials 0.000 claims description 6
- 239000002184 metal Substances 0.000 claims description 6
- 239000011159 matrix material Substances 0.000 claims description 5
- 229920000642 polymer Polymers 0.000 claims description 5
- XTFIVUDBNACUBN-UHFFFAOYSA-N 1,3,5-trinitro-1,3,5-triazinane Chemical compound [O-][N+](=O)N1CN([N+]([O-])=O)CN([N+]([O-])=O)C1 XTFIVUDBNACUBN-UHFFFAOYSA-N 0.000 claims description 4
- 239000000843 powder Substances 0.000 claims description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 3
- 229910052802 copper Inorganic materials 0.000 claims description 3
- 239000010949 copper Substances 0.000 claims description 3
- 239000002086 nanomaterial Substances 0.000 claims description 3
- 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 claims description 2
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims description 2
- 229910000994 Tombac Inorganic materials 0.000 claims description 2
- 229920001643 poly(ether ketone) Polymers 0.000 claims description 2
- 239000010936 titanium Substances 0.000 claims description 2
- 229910052719 titanium Inorganic materials 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
- 239000000956 alloy Substances 0.000 claims 1
- 229910045601 alloy Inorganic materials 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
- 238000005253 cladding Methods 0.000 claims 1
- 229910052749 magnesium Inorganic materials 0.000 claims 1
- 239000011777 magnesium Substances 0.000 claims 1
- 150000002739 metals Chemical class 0.000 claims 1
- 238000007747 plating Methods 0.000 claims 1
- 229920002959 polymer blend Polymers 0.000 claims 1
- 229910052726 zirconium Inorganic materials 0.000 claims 1
- 239000002131 composite material Substances 0.000 abstract description 10
- 206010041662 Splinter Diseases 0.000 abstract description 4
- 238000001514 detection method Methods 0.000 abstract description 2
- 239000003550 marker Substances 0.000 abstract 1
- 230000002349 favourable effect Effects 0.000 description 4
- 239000000463 material Substances 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 238000013467 fragmentation Methods 0.000 description 2
- 238000006062 fragmentation reaction Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000000149 penetrating effect Effects 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- 239000003380 propellant Substances 0.000 description 2
- 238000003860 storage Methods 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- 238000007078 Treibs oxidation reaction Methods 0.000 description 1
- 230000002730 additional effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000005553 drilling Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000007373 indentation Methods 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000001746 injection moulding Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 210000002381 plasma Anatomy 0.000 description 1
Images
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
- F42B12/04—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
- F42B12/02—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
- F42B12/208—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 a plurality of charges within a single high explosive warhead
-
- 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
- F42B12/44—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 incendiary type
Definitions
- the present invention relates to a multi-purpose projectile according to the preamble of the claim.
- Incendiary shell is from the U.S. Patent 3,208,385 which initiates a font-based set of fire when serving on a hard target.
- a behind it, hollow projectile body is filled with another set of fire and contains a predetermined breaking point, so that when it penetrates into the target both incendiary acts.
- This type of ammunition was used from the 60s as a Panzerbrandgeunter.
- Another explosive fire is from the DE-OS-2 323 798 known, this contains a sub-caliber, central core made of carbide, which is surrounded by a pyrotechnic mass.
- the puncture core is placed on a caliber equal rear part, which acts as a sabot and is separated in the target via a predetermined breaking point.
- the penetration core is preceded by a fire rate, which also serves as a hit mark.
- Analogous explosive fire projectiles were later multipurpose projectiles ( DE-A1 27 27 970 ; U.S. Patent 4,444,112 ; EP-A3-0 531 697 ) called.
- the obtained hole should have a low flow resistance for the plasmas of the incendiary.
- the aerodynamic properties of the projectile should be excellent, in particular, the impact speed in the target must be high. This on the one hand to ensure a safe initiation of the ignition charge, even with soft targets and on the other hand to give the breakdown core the required kinetic impulse.
- the projectile construction should be inexpensive and precise to produce from a few parts, and also have a good inner ballistics in the projectile barrel. In particular, running-friendly properties are desired. Last but not least, the projectile should also be producible in large series using conventional means and procedures.
- the piercing core mentioned here is preferably one-piece for reasons of production, but may also be multi-part.
- the transition region between the front part and the actual punch-through part is designed as a predetermined breaking point, so that a fragmentation effect arises when penetrating into the target. This allows the penetration part with the full kinetic energy to penetrate even massive plates.
- the pyrotechnic charge stored in the top of the projectile shell causes a flash of light when it hits the target and ignites the following high-performance explosive. As a result, the above-mentioned fragmentation effect is generated.
- This relatively large pyrotechnic charge is optimal because it ignites easily even with not very hard targets and generates a bright flash of light, which is important for a safe hit tracking.
- a highly compressed high-performance explosive can fit accurately in the front part of the penetration core.
- the storage of the breakdown core as such, in the solid shell, is mechanically very advantageous, but it results from the exact centric storage and the space between the front and rear contact points remains elastic, which on the one hand reduces friction in the projectile barrel and on the other hand, the launching speed and the kinetic impact energy increased in the target, claim 6.
- the gap formed according to claim 6 is according to claim 7 by a composite material - another pyrotechnic Mixture - filled, which causes an increase in the amount of fire rate without losing the desired elasticity of the Vollmantels.
- the subject invention easily allows the rear-side installation of an additional pyrotechnic Markierladung for trajectory tracking, claim 8.
- At least its tip is hardened. But it can also be hardened the whole front part of the puncture core and / or made of a hard material, such as titanium. Likewise, the front part and the actual penetration core may consist of two materials that are fitted accurately; see. Claim 9 and 10.
- the penetration core can also be formed as a point but also as a concave recess, the latter resulting in an additional effect in the manner of a punch, due to its sharp edges - after splitting the front part.
- FIG. 1 is on a multipurpose projectile whose full coat 1 is designated; This projectile is launched in a usual run (not shown) in the direction of flight F.
- the solid shell 1 has a flattened tip 2 in order to achieve a reliable ignition of a stored in the projectile tip pyrotechnic mixture 3 at the impact.
- a breakdown core 6 with its front cylindrical cavity 5 in the form of a bore, which receives a high-performance explosive 5 '.
- the naturalschlagskern 6 is integrally formed and centered inside the Vollmantels front side in the area 8 and the rear side in the area 10 positively.
- a composite material 4 is incorporated, which contains in a polymer matrix a metal powder, which also ignites in the target.
- Fig. 1 Analogous to Fig. 1 is the embodiment after Fig. 2 configured; In addition, it contains in a rear-side bore 13 a marking charge 14 (also called flare), which is initiated by a squib 12 when firing the projectile. - This allows tracing the trajectory to the target.
- the pyrotechnic mixture 3 generates a flash of light upon impact with the target, which ensures reliable detection of the impact in the target.
- the front part of the breakdown core 6 penetrates the impact on the target, where the high-performance explosive 5 'detonates and the cylindrical recess 6' separated at the predetermined breaking points and splinters.
- the further composite 4 was layered in the solid shell by injection molding peripherally accurate. Accordingly, it burns down at the target with a further slight time delay, thus increasing the total firing effect on breakdown. This will increase the total burn time and extend the hit mark time.
- blind holes may be present at the rear part of the puncture core, which allow together with radial holes the pressing of the peripheral composite material 4. This results, by the choice of the pressure curve during the pressing of the composite material 4, the advantage of a precise adjustment of the elasticity (friction in the barrel) of the solid shell. 1
- FIG. 3 shows the penetration core 6 with its front part 6 ', with the conical bottom with a conical tip 7', with a cone angle ⁇ of 60 °.
- the variant after Fig. 4 In place of a pointed cone contains a recess with a concave bottom in the front part 6 ", with a cone angle of 120 °.
- Fig. 5 contains in addition to the representation after Fig. 3 , twelve longitudinal notches 15 in the front part 6 "', whereby the notches 15 secure a secure splitting of the front part of the puncture core 6"' even with a soft target.
- Fig. 6 is a view of the front part 6 "', wherein the notches 15, easily recognizes as predetermined breaking points.
- an ogive tip 7 is favorable to prevent a rebound of the projectile at its oblique incidence on the target.
- the variants of Examples 3 to 5 are favorable in terms of manufacturing technology.
- the notches 15, Fig. 5 and Fig. 6 are drawn larger for purposes of illustration; As high notch factors, it is known to satisfy tip indentations of a few tenths of a millimeter, which can easily be produced by poking (broaching).
- pyrotechnic mixture 3 are composites in which a metal powder is embedded in a polymer matrix.
- a metal powder is embedded in a polymer matrix.
- This type of composite can be injected in layers into the top of the full jacket 1 - over the rear hole - before the following components are inserted and the bottom is crimped.
- the subject invention is an open construction, i. it can be modified in a variety of ways, combined with different materials and adapted to the intended, specific application, such as. also by means of inserts of metal splinters.
- To increase the breakdown power of the cylindrical shaft of the breakdown core 6 may also be designed ogivenförmig.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
- Toys (AREA)
Abstract
Ein Mehrzweckgeschoss mit erhöhter Durchschlags- und Brandleistung weist einen zentralen Durchschlagskern (6,6'), auf der in seinem Fronteil (6') eine Ausnehmung (5) enthält die mit einem Hochleistungssprengstoff (5') gefüllt ist und beim Eindringen in ein Ziel splittert. Initiiert wird das Geschoss durch ein in der Spitze seines Vollmantels eingelagerter Pyrotechnische Mischung (3), der beim Auftreffen am Ziel zur Treffererkennung einen Lichtblitz erzeugt. Weitere Ladungen sind ein Verbundwerkstoff (4) und eine heckseitige Markierladung (14), welche der Flugbahnverfolgung dient.A multi-purpose projectile with increased breakdown and fire power has a central piercing core (6,6 ') on which in its front part (6') contains a recess (5) which is filled with a high-performance explosive (5 ') and penetrates into a target splinter. The projectile is initiated by a pyrotechnic mixture (3) embedded in the tip of his full coat, which generates a flash of light when it hits the target for hit detection. Further charges are a composite material (4) and a rear marker load (14), which serves trajectory tracking.
Description
Die vorliegende Erfindung bezieht sich auf ein Mehrzweckgeschoss nach dem Oberbegriff des Patentanspruchs.The present invention relates to a multi-purpose projectile according to the preamble of the claim.
Ein sogenanntes Sprengbrandgeschoss (engl. Incendiary shell) ist aus der
Ein weiteres Sprengbrandgeschoss, ist aus der
Analog wirkende Sprengbrandgeschosse wurden später Mehrzweckgeschosse (
Alle oben aufgeführten Geschosse haben eine unbefriedigende Durchschlagsleistung und/oder der erzielte Durchmesser der Durchschlagsbohrung stellt einen zu grossen hydraulischen Widerstand dar, so dass der Brandsatz den Innenbereich des Ziels nicht wirksam erreicht.All of the projectiles listed above have unsatisfactory breakdown performance and / or the diameter of the breakdown bore achieved represents too great a hydraulic resistance, so that the fire rate does not effectively reach the interior of the target.
Es ist daher Aufgabe der Erfindung ein Mehrzweckgeschoss zu schaffen, dass eine grosse Durchschlagsleistung sowohl in Bezug auf die Durchschlagstiefe, als auch auf den Durchschlagsdurchmesser aufweist. Die erzielte Bohrung soll für die Plasmen der Brandsätze einen nur geringen Strömungswiderstand haben.It is therefore an object of the invention to provide a multi-purpose projectile that has a high penetration both in terms of penetration depth, as well as on the breakdown diameter. The obtained hole should have a low flow resistance for the plasmas of the incendiary.
Ebenfalls sollen die aerodynamischen Eigenschaften des Geschosses hervorragend sein, insbesondere muss die Auftreffgeschwindigkeit im Ziel hoch sein. Dies um einerseits eine sichere Initiierung des Anzündsatzes, auch bei weichen Zielen zu gewährleisten und anderseits dem Durchschlagskern den erforderlichen kinetischen Impuls zu verleihen. Die Geschosskonstruktion soll kostengünstig und präzise aus wenigen Teilen herstellbar sein, und auch eine gute Innenballistik im Geschosslauf aufweisen. Insbesondere sind laufschonende Eigenschaften gewünscht. Nicht zu Letzt soll das Geschoss auch mit konventionellen Mitteln und Verfahren in grossen Serien produzierbar sein.Also, the aerodynamic properties of the projectile should be excellent, in particular, the impact speed in the target must be high. This on the one hand to ensure a safe initiation of the ignition charge, even with soft targets and on the other hand to give the breakdown core the required kinetic impulse. The projectile construction should be inexpensive and precise to produce from a few parts, and also have a good inner ballistics in the projectile barrel. In particular, running-friendly properties are desired. Last but not least, the projectile should also be producible in large series using conventional means and procedures.
Diese Aufgabe ist durch die Merkmale des Patentanspruch 1 gelöst. Der hier genannte Durchschlagskern ist aus Fertigungsgründen vorzugsweise einstückig, kann aber auch mehrteilig sein. In jedem Fall ist der Übergangsbereich zwischen dem Frontteil und dem eigentlichen Durchschlagsteil als Sollbruchstelle ausgebildet, so dass beim Eindringen in das Ziel eine Splitterwirkung entsteht. Dies erlaubt dem Durchschlagsteil mit der vollen kinetischen Energie auch massive Platten zu durchdringen.This object is solved by the features of
In abhängigen Ansprüchen sind vorteilhafte Weiterbildungen des Erfindungsgegenstands beschrieben.In dependent claims advantageous developments of the subject invention are described.
Günstig sind kupferhaltige Vollmantel gemäss Anspruch 2, da diese im Geschosslauf gute Gleiteigenschaften aufweisen.Favorable are copper-containing solid shell according to
Besonders bewährt hat sich Tombak nach Anspruch 3.Tombak has proven particularly suitable according to
Die in der Spitze des Geschossmantels eingelagerte pyrotechnische Ladung bewirkt beim Aufprall auf das Ziel einen Lichtblitz und entzündet dabei den nachfolgenden Hochleistungssprengstoff. Dadurch wird die oben erwähnte Splitterwirkung erzeugt. Diese relativ grosse pyrotechnische Ladung ist optimal, weil sie sich auch bei nicht sehr harten Zielen leicht entzündet und einen hellen Lichtblitz erzeugt, was für eine sichere Trefferverfolgung wichtig ist.The pyrotechnic charge stored in the top of the projectile shell causes a flash of light when it hits the target and ignites the following high-performance explosive. As a result, the above-mentioned fragmentation effect is generated. This relatively large pyrotechnic charge is optimal because it ignites easily even with not very hard targets and generates a bright flash of light, which is important for a safe hit tracking.
Beim Eindringen des Geschosses in ein Ziel entsteht eine derart hohe Reibungsenergie, welche die periphere Ladung, Anspruch 4 entzündet.Upon penetration of the projectile into a target, such a high friction energy is generated, which ignites the peripheral charge, claim 4.
Gemäss Anspruch 5 lässt sich ein hochverdichteter Hochleistungssprengstoff passgenau im Frontteil des Durchschlagskerns einfügen.According to
Die Lagerung des Durchschlagskerns als solcher, im Vollmantel, ist mechanisch sehr vorteilhaft, ergibt sich doch daraus dessen genaue zentrische Lagerung und der Zwischenraum zwischen den frontseitigen und heckseitigen Kontaktstellen bleibt elastisch, was einerseits die Reibung im Geschosslauf verringert und anderseits die Abschussgeschwindigkeit und die kinetische Aufprallenergie im Ziel erhöht, Anspruch 6.The storage of the breakdown core as such, in the solid shell, is mechanically very advantageous, but it results from the exact centric storage and the space between the front and rear contact points remains elastic, which on the one hand reduces friction in the projectile barrel and on the other hand, the launching speed and the kinetic impact energy increased in the target, claim 6.
Der nach Anspruch 6 gebildete Zwischenraum wird nach Anspruch 7 durch einen Verbundwerkstoff - eine weitere pyrotechnische Mischung - ausgefüllt, was eine Erhöhung der Menge an Brandsatz bewirkt, ohne die gewünschte Elastizität des Vollmantels zu verlieren.The gap formed according to
Der Erfindungsgegenstand erlaubt problemlos den heckseitigen Einbau einer zusätzlichen pyrotechnischen Markierladung zur Flugbahnverfolgung, Anspruch 8.The subject invention easily allows the rear-side installation of an additional pyrotechnic Markierladung for trajectory tracking, claim 8.
Zur Erhöhung der Durchschlagsleistung ist zumindest dessen Spitze gehärtet. Es kann aber auch das ganze Frontteil des Durchschlagskerns gehärtet und/oder aus einem harten Material, beispielsweise Titan gefertigt sein. Ebenfalls können das Frontteil und der eigentliche Durchschlagskern aus zwei Werkstoffen bestehen, die passgenau gefügt sind; vgl. Anspruch 9 und 10.To increase the breakdown power, at least its tip is hardened. But it can also be hardened the whole front part of the puncture core and / or made of a hard material, such as titanium. Likewise, the front part and the actual penetration core may consist of two materials that are fitted accurately; see.
Ausgehend von einstückigen Durchschlagsgeschossen kann der Durchschlagskern als Spitze aber auch als konkave Ausnehmung ausgebildet sein, wobei letztere auf Grund ihrer scharfen Kanten - nach dem Splittern des Frontteils - eine zusätzliche Wirkung nach Art eines Lochstempels ergibt, Anspruch 11.Starting from one-piece penetrating bullets, the penetration core can also be formed as a point but also as a concave recess, the latter resulting in an additional effect in the manner of a punch, due to its sharp edges - after splitting the front part.
Durch longitudinale Kerben im Hohlraum des Frontteils des Durchschlagskerns, Anspruch 12, wird die notwendige Energie zur Splitterwirkung reduziert, was bei relativ weichen Zielen günstig ist.By longitudinal notches in the cavity of the front part of the breakdown core, claim 12, the necessary energy is reduced to splinter effect, which is favorable for relatively soft targets.
Als Hochleistungssprengstoff im Frontteil des Durchschlagskerns sind konventionelle Ladungen nach den im Anspruch 13 genannten Sprengstoffen einsetzbar.As a high-performance explosive in the front part of the breakdown core conventional charges can be used according to the explosives mentioned in
Eine extreme Leistungssteigerung kann durch den Einsatz von energetischen Nanomaterialien, Anspruch 14, erreicht werden.An extreme increase in performance can be achieved by the use of energetic nanomaterials, claim 14.
Besonders bewährt hat sich das in Anspruch 15 genannte Geschosskaliber, da dieses auch von leichten Waffen abfeuerbar ist.Has proven particularly useful in
Nachfolgend werden ah Hand von Zeichnungen Ausführungsbeispiele des Erfindungsgegenstands erläutert, wobei für gleichwirkende Teile gleiche Bezugszeichen verwendet sind.Hereinafter, embodiments of the subject invention will be explained by hand of drawings, wherein like reference numerals are used for like-acting parts.
Es zeigen, in vereinfachter Darstellung:
- Fig. 1
- ein Mehrzweckgeschoss mit Durchschlagskern und Brandsätzen,
- Fig. 2
- eine Variante eines Mehrzweckgeschosses mit heckseitiger Markierladung,
- Fig. 3
- den Durchschlagskern nach
Fig. 1 in einer einzelnen Schnittdarstellung, - Fig. 4
- eine Variante eines Durchschlagskerns,
- Fig. 5
- eine weitere Variante zum Durchschlagskern
Fig. 1 mit longitudinalen Kerben und - Fig. 6
- eine Frontalansicht auf die
zylindrische Ausnehmung 6"' des Durchschlagskerns nachFig. 5 .
- Fig. 1
- a multi-purpose bullet with penetration core and incendiary devices,
- Fig. 2
- a variant of a multi-purpose projectile with rear-side marking load,
- Fig. 3
- after the puncture core
Fig. 1 in a single sectional view, - Fig. 4
- a variant of a breakdown core,
- Fig. 5
- another variant to the breakdown core
Fig. 1 with longitudinal notches and - Fig. 6
- a frontal view of the
cylindrical recess 6 "'of the puncture coreFig. 5 ,
In
Der Vollmantel 1 weist eine abgeplattete Spitze 2 auf um beim Aufschlag am Ziel eine sichere Zündung eines in der Geschossspitze eingelagerten Pyrotechnische Mischung 3 zu erzielen. Anschliessend an den Pyrotechnische Mischung 3 befindet sich ein Durchschlagskern 6, mit seiner frontseitigen zylindrischen Hohlraum 5 in Form einer Bohrung, welche einen Hochleistungssprengstoff 5' aufnimmt. In den Sprengstoff 5' ragt aus dem kegelförmigen Boden eine ogive Spitze 7. Der Durchschlagskern 6 ist einstückig ausgebildet und im Innern des Vollmantels frontseitig im Bereich 8 und heckseitig im Bereich 10 formschlüssig zentriert. Zwischen dem Schaft des Durchschlagskerns 6 und seinem frontseitigen Bereich befinden sich scharfe Übergänge in Form einer umlaufenden Kante 9 welche beim Aufschlag des Geschosses als konzentrische Sollbruchstelle 11 wirkt.The
Peripher zum Schaft des Kerns 6 ist ein Verbundwerkstoff 4 eingelagert, der in eine Polymermatrix ein Metallpulver enthält, welches sich im Ziel ebenfalls entzündet.Peripherally to the shaft of the
Analog zu
Der weitere Verbundstoff 4 wurde schichtweise in den Vollmantel mittels Spritztechnik peripher formgenau angelagert. Er brennt dementsprechend mit einer nochmaligen geringfügigen zeitlichen Verzögerung im Ziel ab und erhöht damit die totale Brandwirkung beim Durchschlag. Dadurch wird die gesamte Leuchtdauer erhöht und damit die Treffermarkierungszeit verlängert.The
Alternativ können - hier nicht gezeichnet - am Heckteil des Durchschlagskerns 6 Sacklochbohrungen vorhanden sein, die zusammen mit radialen Bohrungen das Einpressen des peripheren Verbundwerkstoffs 4 ermöglichen. Dies ergibt, durch die Wahl des Druckverlaufs beim Einpressen des Verbundwerkstoffs 4 den Vorteil einer präzisen Einstellung der Elastizität (Reibung im Lauf) des Vollmantels 1.Alternatively - not shown here - 6 blind holes may be present at the rear part of the puncture core, which allow together with radial holes the pressing of the peripheral
Weitere Ausführungsbeispiele von Durchschlagskernen sind in
Die Ausgestaltung der Spitzen 7, 7' kann dem hauptsächlichen Einsatzzweck des Geschosses angepasst werden: So ist eine ogive Spitze 7 günstig um ein Abprallen des Geschosses bei dessen schiefwinkligen Auftreffen am Ziel zu verhindern. Die Varianten nach den Beispielen 3 bis 5 sind fertigungstechnisch günstig. Die Kerben 15,
Als Pyrotechnische Mischung 3 eignen sich Verbundstoffe bei denen ein Metallpulver in eine Polymermatrix eingelagert ist. Besonders bewährt hat sich als Polymermatrix Polyetherketon, wie in der
Als Hochleistungssprengstoff 5 eignen sich Penetrit (PETN), Hexogen (RDX), insbesondere aber Octastit 8 (nach
Besondere Erwartungen werden in die hochenergetischen Nano-Sprengstoffe gesetzt, deren Sprengwirkung ein mehrfaches bisheriger Hochleistungssgrengstoffe betragen soll. Derartige Nanomaterialien werden derzeit entwickelt und untersucht; sie dienen generell als Treibladungen und pyrotechnische Komponenten. Siehe dazu: www.isl.eu/de/forschung/neue-energetische-stoffe-undschutzmaterialien. Sowie "
Der Erfindungsgegenstand stellt eine offene Konstruktion dar, d.h. sie kann auf verschiedenste Art modifiziert, mit unterschiedlichen Materialien kombiniert und an den beabsichtigten, spezifischen Einsatzzweck angepasst werden, so u.a. auch mittels Einlagen aus Metallsplittern.The subject invention is an open construction, i. it can be modified in a variety of ways, combined with different materials and adapted to the intended, specific application, such as. also by means of inserts of metal splinters.
Zur Erhöhung der Durchschlagsleistung kann der zylindrische Schaft des Durchschlagskerns 6 ebenfalls ogivenförmig ausgestaltet sein.To increase the breakdown power of the cylindrical shaft of the
- 11
- Vollmantel (Mehrzweckgeschoss)Full coat (multipurpose storey)
- 22
- abgeplattete Spitzeflattened top
- 33
- Pyrotechnische Mischung (Ladung)Pyrotechnic mixture (charge)
- 44
- VerbundwerkstoffComposite material
- 55
- Hohlraumcavity
- 5'5 '
- HochleistungssprengstoffHigh power explosive
- 66
- Durchschlagskern, einstückigImpact core, one-piece
- 6'6 '
- zylindrisches Frontteil von 6 (mit kegelförmigem Boden)cylindrical front part of 6 (with conical bottom)
- 6"6 "
- zylindrisches Frontteil von 6 (mit konkavem Boden)cylindrical front part of 6 (with concave bottom)
- 6"'6 " '
- zylindrisches Frontteil von 6 mit zusätzlichen Kerbfaktorencylindrical front part of 6 with additional notch factors
- 77
- ogive Spitze an 6 (gehärtet)ogive tip to 6 (hardened)
- 7'7 '
- kegelförmige Spitze an 6 (gehärtet)conical tip at 6 (hardened)
- 88th
- frontseitiger Formschlussfront-side positive connection
- 99
- umlaufende scharfe Kantecircumferential sharp edge
- 1010
- heckseitiger Formschlussrear-sided positive connection
- 1111
- Sollbruchstellen (konzentrisch)Predetermined breaking points (concentric)
- 1212
- heckseitige ZündladungRear ignition charge
- 1313
- Bohrungdrilling
- 1414
- MarkierladungMarkierladung
- 1515
- Kerben (longitudinal)Notches (longitudinal)
- FF
- Flugrichtungflight direction
- αα
- Kegelwinkel von 7'Cone angle of 7 '
- ββ
- konkaver Kegelwinkelconcave cone angle
Claims (15)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
HUE16405018 HUE044204T2 (en) | 2016-10-20 | 2016-10-20 | Multi-purpose projectile |
EP19154258.8A EP3514479B1 (en) | 2016-10-20 | 2016-10-20 | Multi-purpose projectile |
SI201630240T SI3312546T1 (en) | 2016-10-20 | 2016-10-20 | Multi-purpose projectile |
EP16405018.9A EP3312546B1 (en) | 2016-10-20 | 2016-10-20 | Multi-purpose projectile |
HRP20190745TT HRP20190745T1 (en) | 2016-10-20 | 2019-04-19 | Multi-purpose projectile |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP16405018.9A EP3312546B1 (en) | 2016-10-20 | 2016-10-20 | Multi-purpose projectile |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
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EP19154258.8A Division EP3514479B1 (en) | 2016-10-20 | 2016-10-20 | Multi-purpose projectile |
Publications (2)
Publication Number | Publication Date |
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EP3312546A1 true EP3312546A1 (en) | 2018-04-25 |
EP3312546B1 EP3312546B1 (en) | 2019-01-30 |
Family
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EP19154258.8A Active EP3514479B1 (en) | 2016-10-20 | 2016-10-20 | Multi-purpose projectile |
EP16405018.9A Active EP3312546B1 (en) | 2016-10-20 | 2016-10-20 | Multi-purpose projectile |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
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EP19154258.8A Active EP3514479B1 (en) | 2016-10-20 | 2016-10-20 | Multi-purpose projectile |
Country Status (4)
Country | Link |
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EP (2) | EP3514479B1 (en) |
HR (1) | HRP20190745T1 (en) |
HU (1) | HUE044204T2 (en) |
SI (1) | SI3312546T1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3845853A1 (en) * | 2019-12-30 | 2021-07-07 | RUAG Ammotec AG | Projectile and ammunition |
EP4163584A1 (en) * | 2021-10-05 | 2023-04-12 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Method for finishing a base component and component with such a post-processed base component |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102017106526A1 (en) * | 2017-03-27 | 2018-10-11 | Rheinmetall Waffe Munition Gmbh | Bullet, especially in the middle caliber range |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE308457C (en) * | 1918-04-25 | 1920-01-08 | Becker Ludwig | FIRE BULLET WITH STEEL CORE |
US3208385A (en) | 1962-12-24 | 1965-09-28 | Diehl | Incendiary shell |
DE2323798A1 (en) | 1973-05-11 | 1974-11-21 | Diehl Fa | FIRE BULLET |
DE2727970A1 (en) | 1976-07-01 | 1978-01-05 | Raufoss Ammunisjonsfabrikker | PROJECTILE |
EP0068528A1 (en) | 1981-05-25 | 1983-01-05 | Schweizerische Eidgenossenschaft vertreten durch die Eidg. Munitionsfabrik Thun der Gruppe für Rüstungsdienste | Cold formable, plastics-bound high power explosive and process for preparing it |
US4444112A (en) | 1981-03-27 | 1984-04-24 | A/S Raufoss Ammunisjonsfabrikker | Multi-capability projectile and method of making same |
BE905373A (en) * | 1986-09-04 | 1987-03-04 | Herstal Sa | Anti-tank shell with casing and axial bore - contg. explosive and incendiary charges and a plug |
EP0531697A2 (en) | 1991-08-01 | 1993-03-17 | Raufoss A/S | A multipurpose projectile and a method of making it |
-
2016
- 2016-10-20 SI SI201630240T patent/SI3312546T1/en unknown
- 2016-10-20 EP EP19154258.8A patent/EP3514479B1/en active Active
- 2016-10-20 HU HUE16405018 patent/HUE044204T2/en unknown
- 2016-10-20 EP EP16405018.9A patent/EP3312546B1/en active Active
-
2019
- 2019-04-19 HR HRP20190745TT patent/HRP20190745T1/en unknown
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE308457C (en) * | 1918-04-25 | 1920-01-08 | Becker Ludwig | FIRE BULLET WITH STEEL CORE |
US3208385A (en) | 1962-12-24 | 1965-09-28 | Diehl | Incendiary shell |
DE2323798A1 (en) | 1973-05-11 | 1974-11-21 | Diehl Fa | FIRE BULLET |
DE2727970A1 (en) | 1976-07-01 | 1978-01-05 | Raufoss Ammunisjonsfabrikker | PROJECTILE |
US4444112A (en) | 1981-03-27 | 1984-04-24 | A/S Raufoss Ammunisjonsfabrikker | Multi-capability projectile and method of making same |
EP0068528A1 (en) | 1981-05-25 | 1983-01-05 | Schweizerische Eidgenossenschaft vertreten durch die Eidg. Munitionsfabrik Thun der Gruppe für Rüstungsdienste | Cold formable, plastics-bound high power explosive and process for preparing it |
BE905373A (en) * | 1986-09-04 | 1987-03-04 | Herstal Sa | Anti-tank shell with casing and axial bore - contg. explosive and incendiary charges and a plug |
EP0531697A2 (en) | 1991-08-01 | 1993-03-17 | Raufoss A/S | A multipurpose projectile and a method of making it |
Non-Patent Citations (1)
Title |
---|
TREIBSTOFFE & TREIBLADUNG SYSTEME, 2016, Retrieved from the Internet <URL:www.ict.fraunhofer.de/de/komp/em/treib.html> |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3845853A1 (en) * | 2019-12-30 | 2021-07-07 | RUAG Ammotec AG | Projectile and ammunition |
EP4163584A1 (en) * | 2021-10-05 | 2023-04-12 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Method for finishing a base component and component with such a post-processed base component |
Also Published As
Publication number | Publication date |
---|---|
EP3514479B1 (en) | 2024-02-28 |
SI3312546T1 (en) | 2019-08-30 |
EP3514479C0 (en) | 2024-02-28 |
HUE044204T2 (en) | 2019-10-28 |
HRP20190745T1 (en) | 2019-06-14 |
EP3312546B1 (en) | 2019-01-30 |
EP3514479A1 (en) | 2019-07-24 |
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