EP2179247B1 - Cartouche - Google Patents
Cartouche Download PDFInfo
- Publication number
- EP2179247B1 EP2179247B1 EP08785061.6A EP08785061A EP2179247B1 EP 2179247 B1 EP2179247 B1 EP 2179247B1 EP 08785061 A EP08785061 A EP 08785061A EP 2179247 B1 EP2179247 B1 EP 2179247B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- casing
- cartridge
- propellant charge
- container
- sack
- 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 44
- 239000000843 powder Substances 0.000 claims description 15
- 239000004033 plastic Substances 0.000 claims description 4
- 229920000742 Cotton Polymers 0.000 claims description 3
- 230000001419 dependent effect Effects 0.000 claims description 3
- 239000004744 fabric Substances 0.000 claims description 2
- 239000000203 mixture Substances 0.000 claims 10
- 230000007704 transition Effects 0.000 description 3
- VEXZGXHMUGYJMC-UHFFFAOYSA-N Hydrochloric acid Chemical compound Cl VEXZGXHMUGYJMC-UHFFFAOYSA-N 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 229920006328 Styrofoam Polymers 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000002991 molded plastic Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 239000008261 styrofoam 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
- F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
- F42B33/02—Filling cartridges, missiles, or fuzes; Inserting propellant or explosive charges
- F42B33/0207—Processes for loading or filling propulsive or explosive charges in containers
-
- 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
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/16—Cartridges, i.e. cases with charge and missile characterised by composition or physical dimensions or form of propellant charge, with or without projectile, or powder
-
- 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
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/18—Caseless ammunition; Cartridges having combustible cases
- F42B5/181—Caseless ammunition; Cartridges having combustible cases consisting of a combustible casing wall and a metal base; Connectors therefor
Definitions
- the invention relates to a cartridge with a propellant charge powder at least partially filled propellant charge tube and a front side of the propellant charge shell subsequent bullet.
- the propellant charge sleeve usually consists of a sleeve cover, a sleeve casing and a sleeve bottom made of metal, wherein the existing of a combustible material sleeve casing is connected on the one hand via the sleeve cover with the projectile part and on the other hand via a spring plate and a locking ring with the sleeve bottom.
- Propellant cases of the aforementioned type can be used both in combat cartridges and training cartridges.
- the invention has for its object to avoid the above drawback.
- the invention is based essentially on the idea of centering the propellant charge powder provide in the laboratory space both radially and in the axial direction of the cartridge. But it should be used less as a laboratory aid on filling pieces or Laborierusionn, but rather on a kind of powder bag or bag, which receives the propellant charge and centered. Patches have the disadvantage that, if they are made of styrofoam, they develop hydrochloric acid in the combustion in the pipe or, if they are made of cotton, can get stuck after firing in the tail. The use of Laborierusionn has the disadvantage that the discs must be fixed by means of adhesive.
- Bagloads for holding propellant charges as such are known in particular in modular propellant charges. However, their task and structure, etc. stored differently than suggested here.
- the Treiblessnessladungen be supplied to a weapon system separated from a projectile, such as the DE 198 21 050 A1 removable.
- the arrangement of these bag loads in a gun barrel shows the DE 198 52 360 C2 .
- a method and apparatus for handling combinable propellant charges are disclosed in U.S. Patent No. 5,376,854 DE 697 21 037 T2 disclosed.
- the US 5 090323 which serves as a starting point for the preamble of claim 1, relates to an encapsulating bag for a propellant charge. This is designed in two parts and attached far ahead, below a sealing strip on the projectile.
- a bag-shaped (elongated) container which is completely filled with the appropriate amount of propellant powder is arranged in such a way that the container, and thus also the propellant charge powder, extends in the direction of the central longitudinal axis of the cartridge Longitudinal axis is the symmetry axis of the bag-shaped container at the same time.
- the bottom-side end portion of the bag-shaped container is also secured by means of a spring plate on the sleeve bottom of the propellant charge shell and the projectile end of the bag-shaped container on a preferably made of injection-molded plastic Laborier Anlagen extending perpendicular to the longitudinal axis of the cartridge and / or force with its outer circumference and / or is positively connected to the sleeve casing and / or the sleeve cover of the propellant charge sleeve.
- the bag is thereby stretched and forms a kind of inner sleeve.
- the laboratory aid is hat-shaped and has a hemispherical bulge extending in the direction of the projectile part, which adjoins the bag-shaped container axially and has a flat edge region surrounding the bulge, which is provided with the sleeve shell and / or or the sleeve cover is non-positively and / or positively connected.
- At least two opposing slot-shaped recesses are provided in the transition region between the hemispherical bulge and the flat edge region, passed through which two front, axially separate flag-shaped areas of the bag-shaped container and front side connected to the spherical bulge are.
- the two flag-shaped end portions of the bag-shaped container can be knotted together or glued to the hemispherical bulge.
- the Laborier Anlagen itself can be integrated in the Trieibladungshülse and snaps into the sleeve cover. It serves as a positive connection between the sleeve and the sleeve cover. Both are held by a plug or the like.
- the bag can be filled from above as well as from below.
- the sleeve cover preferably made of plastic, has at least one guide band with predetermined breaking points and undercuts behind which the laboratory aid can snap.
- a centering according to the object of the invention by a further sleeve can be created with a smaller diameter than the bullet sleeve.
- the second narrower sleeve is intended for the propellant charge.
- the constant diameter improves the internal ballistics.
- Fig.1 1 denotes a practice cartridge according to the invention which comprises a propellant charge sleeve 2 and a cage projectile 3 fastened to the front of the propellant charge sleeve 2.
- the latter essentially consists of a subcaliber penetrator 4 with a conical structure (not shown) and a cage 6 (guide cage).
- the propellant charge tube 2 is composed of a sleeve cover 7, a combustible material consisting of relatively thin sleeve jacket 8 and a steel sleeve base 9 consisting for example of steel.
- the sleeve jacket 8 is fixed by means of a spring plate 10 and a retaining ring (not shown) in a conventional manner to a central projection 11 of the sleeve bottom 9.
- This projection 11 is also connected to a known propellant charge igniter 12, which extends axially into the interior of the propellant charge shell 2.
- the propellant charge powder 13 contained in the propellant charge casing 2 is arranged in a bag-shaped container 14 made of a cotton fabric which extends in the direction of the longitudinal axis 100 of the practice cartridge 1 and whose bottom end region 15 is likewise fastened to the casing bottom 9 by means of the spring plate 10 is so that it also contains the propellant charge 12.
- the projectile-side end portion 16 of the bag-shaped container 14 is attached to a Laborierford 17 made of plastic.
- This has in the center a hemispherical bulge 18, which has a diameter which corresponds to the diameter of the bag-shaped container 14, and a flat edge region 19 comprising this bulge 18.
- the edge region 19 is frontally connected in the transition region between the sleeve jacket 8 and sleeve cover 7 form-fitting manner with the propellant charge sleeve 2 and causes an axial and radial centering of the sack-shaped container 14 and the propellant charge powder 13 therein.
- Figure 3 It has at its bottom end portion 15 an opening 22 by means of which the container 14 is pushed onto the projection 11 of the sleeve bottom 9 and then secured to the spring plate 10.
- the projectile-side end region 16 of the sack-shaped container 14 is separated axially, so that two separate flag-shaped regions 23, 24 result.
- These flag-shaped regions 23, 24 are each passed through a slot-shaped recess 25 of the laboratory 17, which are arranged between the hemispherical bulge 18 and the flat edge portion 19 and each having an approximately sickle-shaped shape ( Figure 4 ).
- the two flag-shaped portions 23, 24 are knotted together (in Fig.1 indicated as a pointed area 26). But it can also be provided that the flag-shaped regions 23, 24 are glued to the front of the laboratory 17.
- the resulting space in the bag-shaped container 14 for the propellant charge powder 13 is essentially dependent on the diameter of the spring plate used 10, the size of the slot-shaped recesses 25 in the Laborierefficiency 17, the fixed axial position of the Laborierefficiency 17 within the propellant charge shell 2 and the shape of the Laborierefficiency 17 and therefore, according to the amount of propellant to be labored, can be varied within wide limits.
- Fig. 5 shows the sleeve cover 7 (also sleeve cap) in a perspective view.
- the sleeve cover 7 has sharp-edged predetermined breaking points 7.1 and a circumferential neck 7.2, on which the cage 6 engages.
- the invention is not limited to the embodiment described above.
- the Laborierindustrial also have only a disc-shaped shape or, for example, have a parabolic shaped bulge.
- the attachment of the Laborier infrastructure in the area between sleeve casing and sleeve cover can be done by different, familiar to the expert form and / or frictional connection.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Manufacturing & Machinery (AREA)
- Containers And Packaging Bodies Having A Special Means To Remove Contents (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Closures For Containers (AREA)
Claims (10)
- Cartouche (1) comprenant une douille à charge propulsive (2) au moins partiellement remplie d'une poudre de charge propulsive (13) et une partie projectile (3) dans le prolongement de la douille à charge propulsive (2) du côté avant,* la douille à charge propulsive (2) comprenant un couvercle de douille (7), une enveloppe de douille (8) et un fond de douille (9),* l'enveloppe de douille (8) étant reliée d'un côté par le biais du couvercle de douille (7) à la partie projectile (3) et de l'autre côté par le biais d'une tôle flexible (10) au fond de douille (9),* la poudre de charge propulsive (13) étant disposée dans un récipient en forme de sac (14) qui s'étend dans la direction de l'axe longitudinal (100) de la cartouche (1),
caractérisée en ce que* une zone d'extrémité (16) côté projectile du récipient en forme de sac (14) est fixée à une aide à la préparation (17) constituée de préférence de matière plastique injectable, laquelle s'étend perpendiculairement à l'axe longitudinal (100) de la cartouche (1) et est reliée avec son pourtour extérieur par force et/ou complémentarité de formes avec l'enveloppe de douille (8) et/ou le couvercle de douille (7) de la douille à charge propulsive (2), le récipient en forme de sac (14) étant ainsi allongé et formant ainsi une douille intérieure. - Cartouche (1) selon la revendication 1, caractérisée en ce que la zone d'extrémité côté fond (15) du récipient en forme de sac est fixée au fond de douille (9) au moyen de la tôle flexible (10) et la zone d'extrémité côté projectile (16) du récipient en forme de sac est reliée à l'aide à la préparation (17) disposée transversalement à l'axe longitudinal (100) de la cartouche (1), dont la zone de bordure (19) de configuration plate est reliée du côté frontal par force et/ou complémentarité de formes avec l'enveloppe de douille (8) et/ou le couvercle de douille (7).
- Cartouche (1) selon la revendication 1 ou 2, caractérisée en ce que l'aide à la préparation (17) est réalisée en forme de chapeau et présente une grosseur (18) en forme de demi-sphère qui s'étend en direction de la partie projectile (3) ainsi qu'une zone de bordure (19) de configuration plate qui entoure la grosseur (18), le diamètre intérieur de la grosseur (18) correspondant au diamètre intérieur du récipient en forme de sac (14).
- Cartouche (1) selon la revendication 3, caractérisée en ce que l'aide à la préparation (17) présente dans la zone de transition entre la grosseur (18) et la zone de bordure (19) plate au moins deux évidements (25) opposés en forme de fente à travers lesquels deux zones avant en forme de fanion (23, 24) espacées l'une de l'autre dans le sens axial de la zone d'extrémité côté projectile (16) du récipient en forme de sac (14) sont passées et sont reliées par force du côté avant avec la grosseur (18).
- Cartouche (1) selon la revendication 3, caractérisée en ce que les deux zones (23, 24) en forme de fanion du récipient en forme de sac (14) sont nouées l'une à l'autre.
- Cartouche (1) selon la revendication 3, caractérisée en ce que les zones (23, 24) en forme de fanion sont collées à la grosseur (18) de l'aide à la préparation (17).
- Cartouche (1) selon l'une des revendications 1 à 6, caractérisée en ce que l'aide à la préparation (17) est constituée d'une matière plastique injectable.
- Cartouche (1) selon l'une des revendications 1 à 7, caractérisée en ce que la fixation côté frontal de l'aide à la préparation (17) s'effectue dans la zone de transition entre l'enveloppe de douille (8) et le couvercle de douille (7).
- Cartouche (1) selon l'une des revendications 1 à 8, caractérisée en ce que le récipient en forme de sac (14) est constitué d'un tissu en coton.
- Cartouche (1) selon l'une des revendications 1 à 9, caractérisée en ce que l'espace produit dans le récipient en forme de sac (14) pour la poudre de charge propulsive (13) dépend sensiblement du diamètre de la tôle flexible (10) utilisée, de la taille des évidements (25) en forme de fente dans le disque de préparation (17), de la position axiale définie du disque de préparation (17) à l'intérieur de la douille à charge propulsive (2) ainsi que de la forme du disque de préparation (17), de sorte que celui-ci peut varier dans de larges limites conformément à la quantité de poudre de charge propulsive (13) à préparer.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102007039532.0A DE102007039532B4 (de) | 2007-08-21 | 2007-08-21 | Patrone |
PCT/EP2008/006108 WO2009024245A1 (fr) | 2007-08-21 | 2008-07-25 | Cartouche |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2179247A1 EP2179247A1 (fr) | 2010-04-28 |
EP2179247B1 true EP2179247B1 (fr) | 2015-09-02 |
Family
ID=40090016
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP08785061.6A Active EP2179247B1 (fr) | 2007-08-21 | 2008-07-25 | Cartouche |
Country Status (6)
Country | Link |
---|---|
US (1) | US8516964B2 (fr) |
EP (1) | EP2179247B1 (fr) |
KR (1) | KR101346893B1 (fr) |
DE (1) | DE102007039532B4 (fr) |
SG (1) | SG188171A1 (fr) |
WO (1) | WO2009024245A1 (fr) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20110179965A1 (en) * | 2009-11-02 | 2011-07-28 | Mark Mason | Ammunition assembly |
WO2012039796A2 (fr) * | 2010-06-11 | 2012-03-29 | Bae Systems Land & Armaments L.P. | Ensemble cartouche comprenant un système de retenue intégré |
US8763535B2 (en) | 2011-01-14 | 2014-07-01 | Pcp Tactical, Llc | Narrowing high strength polymer-based cartridge casing for blank and subsonic ammunition |
US8807008B2 (en) | 2011-01-14 | 2014-08-19 | Pcp Tactical, Llc | Polymer-based machine gun belt links and cartridge casings and manufacturing method |
US8869702B2 (en) | 2011-01-14 | 2014-10-28 | Pcp Tactical, Llc | Variable inside shoulder polymer cartridge |
US10197366B2 (en) * | 2011-01-14 | 2019-02-05 | Pcp Tactical, Llc | Polymer-based cartridge casing for blank and subsonic ammunition |
EP2663831B1 (fr) * | 2011-01-14 | 2015-03-04 | PCP Tactical, LLC | Douille à base de polymère haute résistance pour une munition à blanc et subsonique |
EP2770293B1 (fr) | 2011-01-14 | 2018-02-28 | PCP Tactical, LLC | Boîtier de cartouche à base de polymères à haute résistance et procédé de fabrication |
USD715888S1 (en) | 2012-01-13 | 2014-10-21 | Pcp Tactical, Llc | Radiused insert |
DE102012008019A1 (de) | 2012-04-24 | 2013-10-24 | Rheinmetall Waffe Munition Gmbh | Übungspatrone |
KR101665803B1 (ko) | 2014-12-23 | 2016-10-13 | 주식회사 포스코 | 풀림방지 볼트용 선재, 풀림방지 볼트 및 그들의 제조방법 |
US10126104B2 (en) | 2015-08-26 | 2018-11-13 | Atlantis Specialist Technologies Proprietary Limited | Cartridge ammunition |
US11448491B2 (en) | 2018-07-30 | 2022-09-20 | Pcp Tactical, Llc | Polymer cartridge with enhanced snapfit metal insert and thickness ratios |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1316786A (en) * | 1918-02-16 | 1919-09-23 | Paul Gerli | Powder-container or the like. |
US2399398A (en) * | 1940-07-05 | 1946-04-30 | Smith William Herbert | Ammunition |
GB950609A (en) * | 1959-08-14 | 1964-02-26 | Military Training Device Co Ak | Improvements in or relating to ammunition cartridges |
DE1287492B (fr) * | 1961-03-22 | 1969-01-16 | ||
US3362328A (en) * | 1966-01-24 | 1968-01-09 | Army Usa | Wear reduction additives |
DE7234535U (de) * | 1972-09-20 | 1976-03-25 | Fa. Diehl, 8500 Nuernberg | Von einer huelse umschlossene treibladung fuer geschosse |
US4098193A (en) * | 1976-09-08 | 1978-07-04 | The United States Of America As Represented By The Secretary Of The Army | Wear and corrosion reducing additive for gun propellants |
DE2641665C2 (de) | 1976-09-16 | 1984-03-01 | Rheinmetall GmbH, 4000 Düsseldorf | Treibladungshülse |
US4887534A (en) | 1988-06-10 | 1989-12-19 | Honeywell Inc. | Ignition system for high intrusion projectile |
US5090323A (en) | 1990-10-31 | 1992-02-25 | 501 Alliant Techsytems Inc. | Two-piece ammunition propellant containment bag |
US5698815A (en) * | 1995-12-15 | 1997-12-16 | Ragner; Gary Dean | Stun bullets |
SE507659C2 (sv) | 1996-12-02 | 1998-06-29 | Bofors Ab | Sätt och anordning för att vid artilleripjäser hantera drivkrutladdningar av olika storlek och laddstyrka |
DE19741842B4 (de) * | 1997-09-23 | 2006-09-07 | Rheinmetall Waffe Munition Gmbh | Patrone |
DE19821050A1 (de) * | 1998-05-11 | 1999-11-18 | Fac Frank Abels Consult & Tech | Vorrichtung zur Verhinderung von Mehrfachladungen bei Waffensystemen, bei welchen Geschoß und Treibladung getrennt zugeführt werden |
DE19852360C2 (de) * | 1998-11-13 | 2001-10-11 | Rheinmetall W & M Gmbh | Vorrichtung zur Ladungsraumbegrenzung einer Waffe |
DE19944375A1 (de) * | 1999-09-16 | 2001-03-22 | Rheinmetall W & M Gmbh | Hülsenboden für großkalibrige Munition |
WO2003036222A1 (fr) * | 2001-10-22 | 2003-05-01 | Armtec Defense Products Co. | Ensemble circulaire a munitions comportant une douille combustible |
DE10248697A1 (de) * | 2002-03-23 | 2003-10-02 | Rheinmetall W & M Gmbh | Patrone |
GB0301690D0 (en) * | 2003-01-24 | 2003-02-26 | Olympic Technologies Ltd | Safety system |
US8146502B2 (en) * | 2006-01-06 | 2012-04-03 | Armtec Defense Products Co. | Combustible cartridge cased ammunition assembly |
US7913625B2 (en) * | 2006-04-07 | 2011-03-29 | Armtec Defense Products Co. | Ammunition assembly with alternate load path |
DE102007039662B4 (de) * | 2007-08-22 | 2014-12-04 | Rheinmetall Waffe Munition Gmbh | Treibladungsanzünder |
-
2007
- 2007-08-21 DE DE102007039532.0A patent/DE102007039532B4/de active Active
-
2008
- 2008-07-25 WO PCT/EP2008/006108 patent/WO2009024245A1/fr active Application Filing
- 2008-07-25 KR KR1020107004998A patent/KR101346893B1/ko active IP Right Grant
- 2008-07-25 SG SG2013012703A patent/SG188171A1/en unknown
- 2008-07-25 US US12/674,641 patent/US8516964B2/en active Active
- 2008-07-25 EP EP08785061.6A patent/EP2179247B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
KR20100063709A (ko) | 2010-06-11 |
DE102007039532A1 (de) | 2009-02-26 |
US8516964B2 (en) | 2013-08-27 |
SG188171A1 (fr) | 2013-03-28 |
WO2009024245A1 (fr) | 2009-02-26 |
DE102007039532B4 (de) | 2021-03-18 |
KR101346893B1 (ko) | 2014-01-02 |
EP2179247A1 (fr) | 2010-04-28 |
US20110290143A1 (en) | 2011-12-01 |
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