EP2937662B1 - Mine-clearing system - Google Patents
Mine-clearing system Download PDFInfo
- Publication number
- EP2937662B1 EP2937662B1 EP15163825.1A EP15163825A EP2937662B1 EP 2937662 B1 EP2937662 B1 EP 2937662B1 EP 15163825 A EP15163825 A EP 15163825A EP 2937662 B1 EP2937662 B1 EP 2937662B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- launcher
- explosive
- charge
- reel
- fuse
- 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.)
- Not-in-force
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/12—Means for clearing land minefields; Systems specially adapted for detection of landmines
- F41H11/14—Explosive line charges, e.g. snakes
Definitions
- the present invention relates to an explosive charge for destruction of mines and barbed wire barriers in the minefield.
- mine-clearing systems for example POMINS II by Israel Military Industries Ltd. (Ramat Hasharon, Israel) comprising a launcher with a rocket engine, an explosive part of a line charge and two lines with attached spherical concentrated charges.
- the fuse is mounted to one side of the flexible explosive part and a braking rod is mounted to its other side.
- Figs. 1-4 present an example embodiment of the mine-clearing system.
- the mine-clearing system comprises a launcher 1 with a bottom 2. To the middle part of the bottom 2 there is mounted a container 3 with an igniting head 4 and a powder ballast 5, as well as three brackets 6.
- the launcher 1 is connected pivotally, via supports 6, with a mount 7.
- the mount 7 has road wheels 8.
- handling grips 9 and grips 10 supporting the launcher.
- a reel 13, with helically wound part of the explosive charge 14 attached to the reel 13 and comprising a fuse 15, is leaned against the piston 12.
- the explosive part of the charge 14 comprises detonating wires 16 on which there are placed concentrated explosive charges 17 with hollows 18.
- the concentrated explosive charges 17 are separated by flexible tubes 19.
- the reel 13 ends with a flange 20 and a conic cover 21.
- the fuse 15 has electric delayed action initiator 22, which is placed in a booster 23 pressed down to a partition 24 by means of a spring 25.
- the electric delayed action initiator 22 is connected in series with the initiating head 4 from which there are output electrical wires 26.
- a flexible rod 27 is attached to the partition 24 with one end, wherein the second end is attached to the piston 12.
- the partition 24 is protected from moving out by means of plates 28.
- the principle of operation of the mine-clearing system is as follows: the system is placed on the ground in the operating configuration and connected with electric wires 26 of the outer power source. Supplying an electrical pulse to the igniting head 4 causes burning of the powder ballast 5 and production of exhaust gases, which by acting on the piston 12 cause its ejection together with the reel 13 with helically wound part of the explosive charge 14. At the same time, the powder train of the electric delayed action initiator 22 is set on fire. The piston 12 is stopped during the flight by the braking spring 11. This causes unreeling of the explosive part of the charge 14 from the reel 13, pulling out the partition 24 and pressing down of the booster 23 to the detonating wires 16 by the spring 25. When the explosive part of the charge 14 falls to the ground, it detonates automatically due to the action of electric delayed action initiator 22.
- the advantage of the invention is that the explosive part of the charge affects the ground with high efficiency, thanks to the hollows of the concentrated explosive charges mounted on detonating wires.
- the advantage is also that there is no significant noise produced during the pyrotechnic ejection of the reel with the explosive part of the charge and its unreeling, unlike in case of operation of the rocket engine, which would expose the breached area of the minefield.
- the advantage is also a simple charge construction.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Portable Nailing Machines And Staplers (AREA)
Description
- The present invention relates to an explosive charge for destruction of mines and barbed wire barriers in the minefield.
- There are known mine-clearing systems, for example POMINS II by Israel Military Industries Ltd. (Ramat Hasharon, Israel) comprising a launcher with a rocket engine, an explosive part of a line charge and two lines with attached spherical concentrated charges. The fuse is mounted to one side of the flexible explosive part and a braking rod is mounted to its other side.
- There is a need to provide an effective mine neutralization system that has a quiet operation, as well as a simple construction.
- There is presented herein a mine-clearing system according to the appended claims.
- The mine-clearing system is presented by means of exemplary embodiment on a drawing, in which;
-
Fig. 1 shows the charge when unfolded, in a side view; -
Fig. 2 shows section of explosive part in an isometric view; -
Fig. 3 shows the fuse in longitudinal section in secured position; -
Fig. 4 shows the fuse in longitudinal section in armed position. -
Figs. 1-4 present an example embodiment of the mine-clearing system. - The mine-clearing system comprises a
launcher 1 with abottom 2. To the middle part of thebottom 2 there is mounted acontainer 3 with anigniting head 4 and apowder ballast 5, as well as threebrackets 6. Thelauncher 1 is connected pivotally, viasupports 6, with amount 7. Themount 7 hasroad wheels 8. In the upper part of thelauncher 1 there are mountedhandling grips 9 andgrips 10 supporting the launcher. Inside thelauncher 1, in its lower part, there is abraking spring 11, which is attached to thebottom 2 with one end and to thepiston 12 with the other end. Areel 13, with helically wound part of theexplosive charge 14 attached to thereel 13 and comprising afuse 15, is leaned against thepiston 12. The explosive part of thecharge 14 comprises detonatingwires 16 on which there are placed concentratedexplosive charges 17 withhollows 18. The concentratedexplosive charges 17 are separated byflexible tubes 19. Thereel 13 ends with aflange 20 and aconic cover 21. Thefuse 15 has electricdelayed action initiator 22, which is placed in abooster 23 pressed down to apartition 24 by means of aspring 25. The electricdelayed action initiator 22 is connected in series with the initiatinghead 4 from which there are outputelectrical wires 26. Aflexible rod 27 is attached to thepartition 24 with one end, wherein the second end is attached to thepiston 12. Thepartition 24 is protected from moving out by means ofplates 28. - The principle of operation of the mine-clearing system is as follows: the system is placed on the ground in the operating configuration and connected with
electric wires 26 of the outer power source. Supplying an electrical pulse to the ignitinghead 4 causes burning of thepowder ballast 5 and production of exhaust gases, which by acting on thepiston 12 cause its ejection together with thereel 13 with helically wound part of theexplosive charge 14. At the same time, the powder train of the electricdelayed action initiator 22 is set on fire. Thepiston 12 is stopped during the flight by thebraking spring 11. This causes unreeling of the explosive part of thecharge 14 from thereel 13, pulling out thepartition 24 and pressing down of thebooster 23 to the detonatingwires 16 by thespring 25. When the explosive part of thecharge 14 falls to the ground, it detonates automatically due to the action of electricdelayed action initiator 22. - The advantage of the invention is that the explosive part of the charge affects the ground with high efficiency, thanks to the hollows of the concentrated explosive charges mounted on detonating wires.
- The advantage is also that there is no significant noise produced during the pyrotechnic ejection of the reel with the explosive part of the charge and its unreeling, unlike in case of operation of the rocket engine, which would expose the breached area of the minefield.
- The advantage is also a simple charge construction.
Claims (5)
- A mine-clearing system comprising:- a launcher (1) with a bottom (2);- an explosive part of a charge (14) with a fuse (15) ;characterized in that- the launcher (1) comprises:- a braking spring (11), which is attached at its one end to the bottom (2) at its other end to a piston (12); and- a reel (13) leaned against the piston (12), wherein the reel (13) comprises a helically wound explosive part of the charge (14) ended with the fuse (15) attached to the reel (13);- wherein to the bottom (2) of the launcher (1) there are attached:- a container (3) comprising an igniting head (4) and a powder ballast (5); and- brackets (6), which are connected pivotally with a mount (7) having road wheels (8).
- The system according to claim 1, further comprising handling grips (9) and launcher supporting grips (10), which are placed in the upper part of the launcher (1).
- The system according to any of previous claims, wherein the explosive part of the charge (14) comprises detonating wires (16), on which there are placed concentrated explosive charges (17) with hollows (18), wherein the concentrated explosive charges (17) are separated by means of flexible tubes (19).
- The system according to any of previous claims, wherein the fuse (15) comprises an electric delayed action initiator (22), which is placed in a booster (23) separated from the detonating wires (16) by a partition (24), and a spring (25).
- The system according to claim 4, wherein the partition (24) is connected with the piston (12) by a flexible rod (27).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PL407943A PL224826B1 (en) | 2014-04-18 | 2014-04-18 | Explosive charge for clearing mines |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2937662A1 EP2937662A1 (en) | 2015-10-28 |
EP2937662B1 true EP2937662B1 (en) | 2016-12-28 |
Family
ID=52875607
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP15163825.1A Not-in-force EP2937662B1 (en) | 2014-04-18 | 2015-04-16 | Mine-clearing system |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP2937662B1 (en) |
ES (1) | ES2612543T3 (en) |
PL (1) | PL224826B1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110030875A (en) * | 2019-04-18 | 2019-07-19 | 永卓防务科技有限公司 | A kind of launcher |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1270211A (en) * | 1959-10-30 | 1961-08-25 | Bofors Ab | Improvements to demining lines |
US4683797A (en) * | 1986-09-02 | 1987-08-04 | The United States Of America As Represented By The Secretary Of The Army | Line charge detonation interlock assembly |
AU7050200A (en) * | 1999-05-13 | 2000-12-12 | Brisant Technologies International Llc | Mine clearing device |
DE29922893U1 (en) * | 1999-12-30 | 2000-04-06 | Comet Pyrotech | Device for clearing mines, in particular land mines |
US6415717B1 (en) * | 2001-02-16 | 2002-07-09 | The United States Of America As Represented By The Secretary Of The Navy | Line charge assembly and system for use in shallow-water clearing operations |
-
2014
- 2014-04-18 PL PL407943A patent/PL224826B1/en unknown
-
2015
- 2015-04-16 ES ES15163825.1T patent/ES2612543T3/en active Active
- 2015-04-16 EP EP15163825.1A patent/EP2937662B1/en not_active Not-in-force
Non-Patent Citations (1)
Title |
---|
None * |
Also Published As
Publication number | Publication date |
---|---|
PL407943A1 (en) | 2015-10-26 |
ES2612543T3 (en) | 2017-05-17 |
PL224826B1 (en) | 2017-02-28 |
EP2937662A1 (en) | 2015-10-28 |
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