WO2009103408A1 - Obus explosif - Google Patents
Obus explosif Download PDFInfo
- Publication number
- WO2009103408A1 WO2009103408A1 PCT/EP2009/000674 EP2009000674W WO2009103408A1 WO 2009103408 A1 WO2009103408 A1 WO 2009103408A1 EP 2009000674 W EP2009000674 W EP 2009000674W WO 2009103408 A1 WO2009103408 A1 WO 2009103408A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- explosive
- projectile
- liquid
- compensation element
- interior
- Prior art date
Links
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
- F42B12/20—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
Definitions
- the invention relates to an explosive projectile with a projectile casing, which encloses an interior, which is filled for the most part with an explosive, to which a volume compensation element filling the remaining interior is connected.
- An encapsulated, easy to handle made disintegrant describes the DE 23 45 070 B2, an explosive DE 38 43 443 A1.
- Various explosive projectiles are known inter alia from DE 602 02 419 T2, DE 601 08 817 T2, DE 20 2004 019 504 111, DE 295 19 568 U1, DE 39 13 543 C1 and DE 196 26 660 C2.
- the explosive is usually filled in liquid form into the interior of the projectile casing and then cured. This can lead to cavities during the casting as well as during curing of the explosive and possibly also to cracks in the explosive.
- Such voids and cracks represent a not insignificant security risk, because due to the high acceleration at the launch of the explosive projectile blowholes and cracks change their shape very quickly and the air in the voids and cracks can heat up so much due to the resulting compression that it comes to an ignition of the corresponding explosive.
- a method for producing a large-caliber explosive projectile is also known from EP 1 338 860 A2, in which a plastic-bound explosive charge is located in the interior of the projectile casing, which is introduced into a deployable plastic casing introduced into the projectile.
- the invention has for its object to provide an explosive projectile in which the risk of accidental ignition of the explosive at launch is less than in explosive ordnance with hardened liquid explosive.
- the invention is essentially based on the idea of using a liquid explosive as explosive, which does not harden after being introduced into the interior of the projectile casing, but remains liquid.
- the space not filled by the explosive in the projectile casing is filled by a volume compensation element, which compensates both the volume changes of the liquid explosive with temperature changes, as well as the liquid explosive seals and reliably prevents leakage of the explosive from the projectile casing.
- the explosive projectile according to the invention has, inter alia, the advantage that it can be produced in a simple manner, since a hardening of the explosive after its introduction into the projectile casing is eliminated.
- the volume compensation element consists of a container made of an elastic material (for example, a suitable plastic film) filled with a compressible gas or a compressible liquid, the container being gas-tightly connected (eg glued) to the inner wall of the projectile casing such that no gas is present , in particular no air, between the compensation element and the liquid explosive can pass.
- an elastic material for example, a suitable plastic film
- the container of the volume compensation element must be made of a material that is compatible with both the explosive and with the other materials used in the projectile (if they come into contact with the container), so that the corresponding material properties over a longer period in the given Temperature range to be maintained. So it is not uncommon that the buyer of corresponding explosive projectiles requires a useful life of such bullets of, for example, 25 years.
- the material of the container must be chosen such that no escape of the gas in it or the liquid contained in it can take place during the guaranteed service life.
- the volume compensation element is preformed and adjusted to the planned position in the store log. During insertion, in a vacuum or negative pressure, into the projectile, the volume compensation element is preferably folded or compressed. By preforming the volume compensation element and the gas contained, the body relaxes after insertion and fits into the orgive.
- the adhesive should first be applied in the area of the ogive, where the volume compensation element will sit, to get a uniform adhesive layer. The application can preferably be carried out by spraying.
- the blasting projectile 1 comprises a projectile casing 2 made of steel, which has an opening 3 on the front side into which an impact fuse (not shown) can be screwed.
- the explosive 6 is liquid explosive.
- volume compensation element 7 which is prestressed, for example, by means of a pressure plate arranged on the igniter side (not shown).
- this volume compensation element 7 consists of a container 8 made of elastic material (for example, a plastic film), in which a compressible gas 9 is located.
- the volume compensation element 7 Upon heating of the liquid explosive 6, the volume compensation element 7 is compressed by the expansion of the explosive 6. On cooling of the liquid explosive 6, however, the volume compensation element 7 expands to compensate for the shrinkage of the explosive 6 in this case.
- the elastic container 8 is glued to the inner wall 10 of the projectile casing 2 (the adhesive layer is provided with the reference numeral 11 in the figure), so that the volume compensation element 7 is arranged fixed in position in the projectile casing 2 and no air passes past the head igniter between the latter Volume compensation element 7 and the liquid explosive 6 can get.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Portable Nailing Machines And Staplers (AREA)
- Toys (AREA)
Abstract
L'invention concerne un obus explosif comportant une enveloppe (2) qui entoure un espace intérieur (5) rempli en grande partie de matière explosive (6) dans le prolongement de laquelle se trouve un élément de compensation de volume (7) qui remplit l'espace restant. Afin que le risque d'explosion involontaire de la matière explosive (6) lors du tir soit faible, la matière explosive (6) utilisée est liquide, cette matière explosive ne durcissant pas mais restant liquide lorsqu'elle se trouve dans l'espace intérieur (5) de l'enveloppe (2) de l'obus.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP09713160A EP2245418A1 (fr) | 2008-02-22 | 2009-02-03 | Obus explosif |
CA2715693A CA2715693A1 (fr) | 2008-02-22 | 2009-02-03 | Obus explosif |
ZA2010/05624A ZA201005624B (en) | 2008-02-22 | 2010-08-05 | Explosive projectile |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102008010706A DE102008010706A1 (de) | 2008-02-22 | 2008-02-22 | Sprenggeschoss |
DE102008010706.9 | 2008-02-22 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2009103408A1 true WO2009103408A1 (fr) | 2009-08-27 |
Family
ID=40678923
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2009/000674 WO2009103408A1 (fr) | 2008-02-22 | 2009-02-03 | Obus explosif |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP2245418A1 (fr) |
CA (1) | CA2715693A1 (fr) |
DE (1) | DE102008010706A1 (fr) |
WO (1) | WO2009103408A1 (fr) |
ZA (1) | ZA201005624B (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102016008391B4 (de) | 2016-07-09 | 2018-05-24 | Diehl Defence Gmbh & Co. Kg | Geschoss |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2373883A (en) | 1942-10-30 | 1945-04-17 | Clyde B Ferrel | Shell structure |
US4011818A (en) * | 1976-04-01 | 1977-03-15 | The United States Of America As Represented By The Secretary Of The Navy | Warhead explosive liner |
EP1338860A2 (fr) * | 2002-02-21 | 2003-08-27 | Rheinmetall W & M GmbH | Procédé de fabrication d'un projectile explosif de grand calibre et projectile produit avec une telle méthode |
DE102004045361B3 (de) | 2004-09-18 | 2006-05-11 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Verfahren und Vorrichtung zur Herstellung einer Hohlladung |
DE102005050973A1 (de) * | 2005-10-25 | 2007-04-26 | Rheinmetall Waffe Munition Gmbh | Sprenggeschoss |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2251482B (en) | 1987-06-09 | 1993-09-22 | Royal Ordnance Plc | Explosive devices |
DE3913543C1 (en) | 1989-04-25 | 1990-10-31 | Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De | One-piece projectile housing - has recess which allows mfr. from rear |
DE29519568U1 (de) | 1995-12-09 | 1997-04-03 | Diehl GmbH & Co, 90478 Nürnberg | Sprenggeschoß |
DE19626660C2 (de) | 1996-07-03 | 2002-06-27 | Diehl Stiftung & Co | Sprenggeschoß |
FR2812385B1 (fr) | 2000-07-28 | 2003-02-21 | Giat Ind Sa | Munition explosive a corps fragmentable |
FR2830931B1 (fr) | 2001-10-12 | 2004-04-02 | Giat Ind Sa | Munition explosive |
DE202004019504U1 (de) | 2004-12-17 | 2006-04-20 | Diehl Bgt Defence Gmbh & Co. Kg | Sprenggeschoss |
-
2008
- 2008-02-22 DE DE102008010706A patent/DE102008010706A1/de not_active Withdrawn
-
2009
- 2009-02-03 WO PCT/EP2009/000674 patent/WO2009103408A1/fr active Application Filing
- 2009-02-03 EP EP09713160A patent/EP2245418A1/fr not_active Withdrawn
- 2009-02-03 CA CA2715693A patent/CA2715693A1/fr not_active Abandoned
-
2010
- 2010-08-05 ZA ZA2010/05624A patent/ZA201005624B/en unknown
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2373883A (en) | 1942-10-30 | 1945-04-17 | Clyde B Ferrel | Shell structure |
US4011818A (en) * | 1976-04-01 | 1977-03-15 | The United States Of America As Represented By The Secretary Of The Navy | Warhead explosive liner |
EP1338860A2 (fr) * | 2002-02-21 | 2003-08-27 | Rheinmetall W & M GmbH | Procédé de fabrication d'un projectile explosif de grand calibre et projectile produit avec une telle méthode |
DE102004045361B3 (de) | 2004-09-18 | 2006-05-11 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Verfahren und Vorrichtung zur Herstellung einer Hohlladung |
DE102005050973A1 (de) * | 2005-10-25 | 2007-04-26 | Rheinmetall Waffe Munition Gmbh | Sprenggeschoss |
Also Published As
Publication number | Publication date |
---|---|
EP2245418A1 (fr) | 2010-11-03 |
DE102008010706A1 (de) | 2009-08-27 |
ZA201005624B (en) | 2011-06-29 |
CA2715693A1 (fr) | 2009-08-27 |
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