EP2686636B1 - Munition insensible - Google Patents
Munition insensible Download PDFInfo
- Publication number
- EP2686636B1 EP2686636B1 EP12705063.1A EP12705063A EP2686636B1 EP 2686636 B1 EP2686636 B1 EP 2686636B1 EP 12705063 A EP12705063 A EP 12705063A EP 2686636 B1 EP2686636 B1 EP 2686636B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- propellant charge
- ring
- annular gap
- cartridge ammunition
- ammunition according
- 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
- 239000003380 propellant Substances 0.000 claims description 25
- 239000000463 material Substances 0.000 claims description 10
- 238000002844 melting Methods 0.000 claims description 6
- 230000008018 melting Effects 0.000 claims description 6
- 238000010304 firing Methods 0.000 claims description 4
- 238000007789 sealing Methods 0.000 claims description 4
- 239000007787 solid Substances 0.000 claims description 4
- 229910001152 Bi alloy Inorganic materials 0.000 claims description 2
- 229910001297 Zn alloy Inorganic materials 0.000 claims description 2
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 claims description 2
- 239000004429 Calibre Substances 0.000 claims 1
- 239000000843 powder Substances 0.000 description 3
- 230000009172 bursting Effects 0.000 description 2
- CQHDPRBPWAYYKI-UHFFFAOYSA-N [Cd].[Cd].[Cd].[Cd].[Cd].[Cd].[Cd].[Cd].[Cd].[Cd].[Cd].[Cd].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi] Chemical class [Cd].[Cd].[Cd].[Cd].[Cd].[Cd].[Cd].[Cd].[Cd].[Cd].[Cd].[Cd].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Sn].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Pb].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi].[Bi] CQHDPRBPWAYYKI-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000013270 controlled release Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 239000012528 membrane Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 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
- F42B39/00—Packaging or storage of ammunition or explosive charges; Safety features thereof; Cartridge belts or bags
- F42B39/20—Packages or ammunition having valves for pressure-equalising; Packages or ammunition having plugs for pressure release, e.g. meltable ; Blow-out panels; Venting arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/26—Cartridge cases
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B30/00—Projectiles or missiles, not otherwise provided for, characterised by the ammunition class or type, e.g. by the launching apparatus or weapon used
- F42B30/04—Rifle grenades
Definitions
- the invention is concerned with a cartridge ammunition, especially in the middle caliber (for example, 40 mm) and as a training ammunition, as well as a simpler constructed so-called Berstêt.
- a cartridge ammunition with a bursting device known as a connection between bullet and drive This bursting device comprises a membrane with at least one predetermined breaking point, which opens at a predetermined pressure in the high-pressure chamber of the drive.
- insensitive ammunition i. an ammunition with an insensitive drive
- demands of increasing security must be increasingly taken into account. For example, it should not explode or disassemble if, for example, it is exposed to fire or other higher temperatures.
- the invention has the object to show a further possibility for the compliance with the safety criteria even at higher temperatures.
- the invention is based on the idea to provide the cartridge with a kind of releasable closure, which opens before the actual ignition temperature of the primer, so that the resulting inside the cartridge internal pressure can escape early to the outside. This explosion pressure is relieved through a hole in which the closure is integrated, in the propellant charge floor.
- the closure is preferably formed by a metal sealing plug, which also receives the primer cap.
- An annular gap is provided between the sealing plug and the sleeve of the insensitive drive. This is sealed by a fuse or a ring of fusible material to the propellant charge. Alternatively, this fusible material may also be incorporated in the annular gap. Combinations of both variants are also possible. If the ammunition is subject to a predetermined temperature and the fuse comes into effect, moves the plug with the primer without resistance to the outside. This creates a large opening (through the release of the hole) in the sleeve bottom, which prevents the propellant charge powder is exploded and it can come to a maximum slow combustion.
- the fuse or the ring of melting, solid and pressure-tight material preferably a Ostalloy- ring can be introduced by pressing and riveting in the sleeve bottom.
- the Ostalloy fuse can in turn consist of a bismuth / zinc alloy. There are no longer any holes in the propellant charge case.
- the ring in turn, can be stamped from rolled strip of material without the need for reworking.
- Fig. 1 an ammunition 1 is shown, which has a projectile 2 and a propellant charge sleeve 3, which is fixed to the projectile 2 and its floor 10, for example via a screw 4.
- Alternative compounds are crimp, Aufsteck- and locking connections, etc., such as from the DE 10 1004 017 464 B4 or the US 3,645,208 A known.
- a high pressure chamber 5 forming insert (drive chamber) 6 is involved, at the same time a (pyrotechnic) propellant charge 7, here in the form of powder, receives.
- the propellant charge powder 7 has für Bachmandassmandassmandassmandassmandassmandassmandassmandassmandassmandassunassunaspenta solid, which are guided by the insert and open from the high pressure chamber 5 in the low pressure chamber 8.
- the propellant charge tube 3 is preferably made of aluminum and takes a Anzündhütchen 11 in a bore (opening) 12 on the sleeve bottom 13.
- the primer cap 11 itself is integrated in a stopper 14 acting as a stopper, which is inserted into the bore (opening) 12. Plug 14 and primer 11 are sealed, for example, with a Ringfugenlack.
- the bore 12 in turn should preferably be arranged centrally in the s
- annular gap 17 is now provided between the plug 14 and the propellant charge sleeve 3, which extends through the sleeve bottom to the outside ( Fig.2 ).
- the annular gap 17 can be uniform or, as in Fig. 3 shown, extending 17 'executed and allows, if necessary, a controlled release of the plug 14.
- a fusible circlip 16 is further introduced into the propellant charge case 3. This can be riveted at an edge 18 on the plug 14.
- the retaining ring 16 can be pressed against the sleeve 3 and compacted.
- the melting temperature of the material is below the ignition temperature of the ignition and propellant charges. Subjecting the ammunition 1 in their transport, storage, etc. too high a temperature, the melting material of the retaining ring 16 begins to liquefy and passes through the annular gap 17 to the outside. The plug 14 is exposed by this measure and loses the mechanical support to the propellant charge shell 3. Thus, the plug 14, the bore 12 is free, so that a larger opening in the sleeve bottom 13 is formed.
- the stopper 14 When firing the ammunition from a gun barrel (not shown in detail), the stopper 14, the primer cap 11 and the propellant charge shell 3 against a weapon lock (not shown) from, so that it is ensured that the plug 14 when shooting is not out of the bore 12th can be pushed out.
- the circlip 16 takes on the firing of the ammunition 1 in normal use on this fuse or ring 16 acting gas pressure (from about 3000 bar) and seals the annular gap 17 from the propellant charge 7 down, so that the ring 16 in its dual function here acts as a sealing ring.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Portable Nailing Machines And Staplers (AREA)
- Safety Valves (AREA)
- Air Bags (AREA)
Claims (9)
- Munition à douille, notamment de calibre moyen, comportant un projectile (2) et une douille de charge propulsive (3) qui est reliée au projectile (2), dans lequel il est prévu dans une chambre (6) de la douille de charge propulsive (3) une charge propulsive (7) qui est reliée fonctionnellement à une amorce (11) d'un dispositif de mise à feu qui est placé dans un obturateur (14) pouvant être logé dans un alésage (12) du culot (13) de la douille de charge propulsive (3), caractérisée en ce qu'une fente annulaire (17, 17') qui traverse le culot (13) vers l'extérieur est intégrée entre l'obturateur (14) et la douille de charge propulsive (3), et la fente annulaire (17, 17') est étanchéifiée par une bague (16) vis-à-vis de la charge propulsive (7), dans lequel la bague (16) se compose d'un matériau fusible, solide et résistant à la pression dont le point de fusion est au moins inférieur au point de fusion de la température d'allumage du dispositif de mise à feu et de la charge propulsive (7).
- Munition à douille selon la revendication 1, caractérisée en ce que la fente annulaire (17) peut être réalisée dans une dimension constante ou de manière évasée (17').
- Munition à douille selon la revendication 1 ou 2, caractérisée en ce que l'alésage (12) peut être disposé de manière centrale ou décentrée dans le culot (13) .
- Munition à douille selon l'une quelconque des revendications 1 à 3, caractérisée en ce que la bague (16) fonctionne en tant qu'élément de sécurité et d'étanchéité.
- Munition à douille selon l'une quelconque des revendications 1 à 4, caractérisée en ce que la bague (16) se compose d'un alliage de bismuth/zinc.
- Munition à douille selon l'une quelconque des revendications 1 à 5, caractérisée en ce que le matériau fusible, solide et résistant à la pression présent dans la fente annulaire (17, 17') peut être intégré.
- Munition à douille selon l'une quelconque des revendications 1 à 6, caractérisée en ce que la bague (16) est rivetée sur une arête supérieure (18) au niveau de l'obturateur (14).
- Munition à douille selon l'une quelconque des revendications 1 à 7, caractérisée en ce que la bague (16) est comprimée contre la douille de charge propulsive (3) en étanchéifiant la fente annulaire (17) vis-à-vis de la charge propulsive.
- Munition à douille selon l'une quelconque des revendications 1 à 8 caractérisée en ce que la fente annulaire (17) permet une séparation en continu de l'obturateur.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102011014402A DE102011014402A1 (de) | 2011-03-18 | 2011-03-18 | Insensitive Munition |
PCT/EP2012/000677 WO2012126554A1 (fr) | 2011-03-18 | 2012-02-16 | Munition insensible |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2686636A1 EP2686636A1 (fr) | 2014-01-22 |
EP2686636B1 true EP2686636B1 (fr) | 2017-06-28 |
Family
ID=45722583
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP12705063.1A Active EP2686636B1 (fr) | 2011-03-18 | 2012-02-16 | Munition insensible |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP2686636B1 (fr) |
DE (1) | DE102011014402A1 (fr) |
WO (1) | WO2012126554A1 (fr) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102014001576A1 (de) * | 2014-02-06 | 2015-08-06 | Diehl Bgt Defence Gmbh & Co. Kg | Treibladungshülse für eine Patronenmunition |
DE102014005997B3 (de) * | 2014-04-28 | 2015-03-26 | Rheinmetall Waffe Munition Gmbh | Patrone und Verfahren zu ihrer Herstellung |
DE102014013316B4 (de) | 2014-09-08 | 2016-04-07 | Diehl Bgt Defence Gmbh & Co. Kg | Behältnis zur Aufbewahrung eines Explosivstoffs |
US20180135953A1 (en) * | 2016-11-15 | 2018-05-17 | Nostromo Holdings, Llc | Ammunition cartridge with a base plug vent |
DE102017110871A1 (de) * | 2017-05-18 | 2018-11-22 | Rheinmetall Waffe Munition Gmbh | Antriebssystem für Patronenmunition |
DE102017114950B4 (de) | 2017-07-05 | 2022-05-05 | Technische Universität Dresden | Elektrisch betreibbare Schlauchpumpe |
US11668550B2 (en) | 2019-10-04 | 2023-06-06 | Bae Systems Land & Armaments L.P. | Scalable insensitive munitions primer |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3645208A (en) | 1970-02-17 | 1972-02-29 | Us Army | Fuzeless target practice cartridge |
US6523477B1 (en) * | 1999-03-30 | 2003-02-25 | Lockheed Martin Corporation | Enhanced performance insensitive penetrator warhead |
US6752085B2 (en) * | 2002-05-06 | 2004-06-22 | Lockheed Martin Corporation | Method and apparatus for releasably attaching a closure plate to a casing |
DE102004017464B4 (de) | 2004-04-08 | 2006-05-18 | Nico-Pyrotechnik Hanns-Jürgen Diederichs GmbH & Co. KG | Patronierte Übungsmunition |
DE102004020838B3 (de) | 2004-04-08 | 2005-06-23 | Nico-Pyrotechnik Hanns-Jürgen Diederichs GmbH & Co. KG | Patronenmunition, insbesondere mit mittlerem Kaliber |
DE102009048365B3 (de) | 2009-10-06 | 2010-10-07 | Rheinmetall Waffe Munition Gmbh | Patronierte Munition mit einer Berstvorrichtung als Verbindung zwischen Geschoss und Antrieb |
-
2011
- 2011-03-18 DE DE102011014402A patent/DE102011014402A1/de not_active Withdrawn
-
2012
- 2012-02-16 WO PCT/EP2012/000677 patent/WO2012126554A1/fr active Application Filing
- 2012-02-16 EP EP12705063.1A patent/EP2686636B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
DE102011014402A1 (de) | 2012-09-20 |
EP2686636A1 (fr) | 2014-01-22 |
WO2012126554A1 (fr) | 2012-09-27 |
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