EP0437992A1 - Sprengladung zum Bilden mehrerer Bolzen und/oder Stacheln - Google Patents
Sprengladung zum Bilden mehrerer Bolzen und/oder Stacheln Download PDFInfo
- Publication number
- EP0437992A1 EP0437992A1 EP90403485A EP90403485A EP0437992A1 EP 0437992 A1 EP0437992 A1 EP 0437992A1 EP 90403485 A EP90403485 A EP 90403485A EP 90403485 A EP90403485 A EP 90403485A EP 0437992 A1 EP0437992 A1 EP 0437992A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- coatings
- explosive charge
- charge
- covers
- charge 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.)
- Granted
Links
- 239000002360 explosive Substances 0.000 title claims abstract description 35
- 230000007423 decrease Effects 0.000 claims abstract description 7
- 238000000576 coating method Methods 0.000 claims description 89
- 239000011248 coating agent Substances 0.000 claims description 34
- 239000000463 material Substances 0.000 claims description 23
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 18
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims description 12
- 229910052715 tantalum Inorganic materials 0.000 claims description 10
- 229910052742 iron Inorganic materials 0.000 claims description 9
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 8
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 7
- 229910052802 copper Inorganic materials 0.000 claims description 6
- 239000010949 copper Substances 0.000 claims description 6
- 230000003247 decreasing effect Effects 0.000 claims description 5
- 229910052751 metal Inorganic materials 0.000 claims description 5
- 239000002184 metal Substances 0.000 claims description 5
- 229910052770 Uranium Inorganic materials 0.000 claims description 4
- 229910052759 nickel Inorganic materials 0.000 claims description 4
- JFALSRSLKYAFGM-UHFFFAOYSA-N uranium(0) Chemical compound [U] JFALSRSLKYAFGM-UHFFFAOYSA-N 0.000 claims description 4
- 229910045601 alloy Inorganic materials 0.000 claims description 2
- 239000000956 alloy Substances 0.000 claims description 2
- 229910001092 metal group alloy Inorganic materials 0.000 claims description 2
- 150000002739 metals Chemical class 0.000 claims description 2
- 230000037452 priming Effects 0.000 claims description 2
- 230000035939 shock Effects 0.000 abstract description 16
- 239000004429 Calibre Substances 0.000 abstract description 2
- 230000001747 exhibiting effect Effects 0.000 abstract 1
- 239000002245 particle Substances 0.000 description 11
- 239000000470 constituent Substances 0.000 description 5
- 230000016571 aggressive behavior Effects 0.000 description 4
- 238000010586 diagram Methods 0.000 description 4
- 238000005474 detonation Methods 0.000 description 3
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000000945 filler Substances 0.000 description 2
- 239000011368 organic material Substances 0.000 description 2
- 230000004224 protection Effects 0.000 description 2
- 240000008042 Zea mays Species 0.000 description 1
- 230000003416 augmentation Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000001186 cumulative effect Effects 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 235000012830 plain croissants Nutrition 0.000 description 1
- 230000006798 recombination Effects 0.000 description 1
- 238000005215 recombination Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
- 230000003068 static effect Effects 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
- F42B1/00—Explosive charges characterised by form or shape but not dependent on shape of container
- F42B1/02—Shaped or hollow charges
- F42B1/032—Shaped or hollow charges characterised by the material of the liner
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B1/00—Explosive charges characterised by form or shape but not dependent on shape of container
- F42B1/02—Shaped or hollow charges
- F42B1/028—Shaped or hollow charges characterised by the form of the liner
Definitions
- the technical sector of the present invention is that of explosive charges generating jets or cores, intended for piercing the armor of armored vehicles.
- US-A-4,702,171 describes a two-layer coating, one of which generates a jet and the other a core. These coatings are attached contiguously over a portion of their surface and their impedance to shocks decreases from the outside to the inside. In addition, the charge described does not generate two jets or cores, but a continuous assembly as shown in Figure 2 of this patent.
- US-A-4,498,367 describes a charge with two coatings generating a single high energy jet.
- the internal coating, on the explosive side has greater ductility than that of the external coating and these two coatings are positioned contiguously.
- the shock impedance decreases from the outside to the inside (explosive charge side).
- the proposed invention relates to an architectural evolution of the charges generating nuclei and / or jets moving away from the three axes of force mentioned above; it significantly increases the potential for aggression of these charges on current or future armor.
- the invention therefore relates to an explosive charge generating cores and / or jets, comprising n coating, n being a number between 2 and 5, and an explosive charge initiated by a priming device, characterized in that the coatings are placed contiguously, the relative distance between the two coatings being between approximately 0.1 mm and 0.11 gauge and in that the materials have an equal or decreasing impact impedance from the inside, on the explosive charge side, outward, free surface side.
- the coatings can be in the form of caps with surfaces of revolution generated by a conical curve and whose convexity is directed towards the explosive charge.
- conical curve is meant a sphere, an elispsoid, a paraboloid, etc.
- the distance may decrease from the edges to the center of the coverings.
- the average thickness of the coatings expressed in load rating can be between 0.01 / n and 0.15 / n, n being the number of coatings.
- Each coating consists of a unique metal or alloy.
- the coatings can be produced from metals or metal alloys selected from the group consisting for example of uranium, tantalum, nickel, copper and iron.
- the filler can comprise two coatings, the internal and external coatings being constituted respectively by tantalum and iron.
- the two coatings can be spaced a constant distance of 0.1 mm.
- the internal and external coatings can each have a thickness of the order of 2.5% of the size of the load.
- the load can comprise three coatings constituted respectively from the inside to the outside by tantalum, copper and iron.
- An advantage of the present invention lies in the fact that in the aggression of inert targets, such a charge makes it possible to combine (at least at short and medium action distance, around 100 calibers) the effects of several nuclei and to obtain a perforation of greater depth, than with a conventional load.
- Another advantage lies in the fact that during the aggression of targets over-protected by inert or reactive elements, the effects of a tandem charge are obtained: the first nucleus destroys the first over-protection, which allows the nuclei following to attack the remaining part of the target.
- Another advantage lies in the integration in an ammunition to thus present a mass and a compact size, compared to those of a conventional tandem load.
- Tandem charges of interest mainly only in the attack of multi-stage protections (two stages for a charge with two cores), if one of the stages is difficult to destroy with a nucleus, it is then attacked with a jet.
- a double generation charge of cores has been represented, consisting of a safety and ignition device 1 to initiate a ignition relay 2 which amplifies in power and stabilizes in form and speed the detonating signal coming from of device 1.
- This relay 2 can possibly integrate a wave shaping device, such as a screen.
- Relay 2 is followed by an explosive charge 3 which is put into detonic mode by the signal which relay 2 delivers and which has the role of propelling the bi-layer coating 4 and 5.
- This two-layer coating generates two cores corresponding to the two elementary coatings 4 and 5 constituting it.
- the entire structure described is integrated inside a metal casing 6 of conventional type.
- the two coatings 4 and 5 are spaced from each other, for example, by an air gap 7 whose thickness is between approximately 0.1 mm and 0.11 caliber of the load.
- the coating 4 is constituted by tantalum and the coating 5 by iron.
- the distance separating the two coatings can be constant or even be greater at the periphery than at the centers of the coatings.
- the free volume existing between the two coatings can be occupied for example by an organic material. This material can be an adhesive.
- FIG 2 there is shown a load comprising three coatings 8, 9, and 10, spaced from each other by successive air knives 11 and 12, the other elements of the structure being identical.
- the two coatings 8 and 9 are separated from each other by the air gap 11 whose thickness is constant and between 0.1 mm and 0.11 caliber of the load.
- the coating 8 is constituted by tantalum and the coating 9 by copper.
- the two coverings 9 and 10 are separated from each other by the air gap 12 whose thickness decreases from the periphery towards the center of these coatings from a value b, to a value a, such as 0.1 mm ⁇ a ⁇ b ⁇ 0.11 caliber.
- the coating 10 consists of iron.
- the volumes existing between the coatings 8 and 9 on the one hand and 9 and 10 on the other hand can be occupied for example by an organic material. This material can be an adhesive.
- FIG. 3 illustrates the operation of a load with two coatings.
- the two cores 13 and 14 formed respectively from the coatings 5 and 4. They are separated after a time of the order of 500 ⁇ s from a distance of 60 mm.
- the detonation wave induces in the first elementary coating 4 a shock which, in a diagram "pressure P, particle velocity u", is determined by the intersection of the dynamic adiabatic of the detonation products of l explosive of loading 3 and of the Hugoniot curve of the material of the elementary coating 8 (point of coordinates P1, u1).
- the shock moves towards the interface of the elementary coatings 4 and 5 by compressing the medium it crosses and bringing it to the pressure P1 and to the particle speed u1.
- the shock is transmitted to the second elementary coating 5 by compressing it; its constituent material, since it has a shock impedance lower than that of the material of the first elementary coating 4, is crossed by the shock at the pressure P′2 less than P1 and at the particle speed u′2 greater than u1.
- the pressure P′2 and the particle speed u′2 are slightly altered values by passing the shock through the volume at constant thickness 7 of the pressure P2 and the particle speed u2 (P2 and u2 are graphically given in the diagram " pressure, particle velocity "by the intersection of the symmetrical curve with respect to the line parallel to the pressure axis passing through the point (P1, u1) of the Hugoniot curve of the first elementary coating 4 and of the curve d 'Hugoniot of the second elementary covering 5).
- the equilibrium state is reached in elementary coatings generally after several tens of microseconds; the time to reach the equilibrium state corresponds to the time necessary for the cancellation of the pressure in the materials due to the recombinations of the compression and expansion waves which circulate there.
- the first elementary coating 4 moves and deforms according to its own characteristics (geometric, metallurgical %) and the energy communicated to it during the initial impact and also by the detonation products generated by the explosive.
- the second elementary coating 5 moves and deforms as a function of its own characteristics and of the energy communicated to it by the first elementary coating 4.
- the shock wave is transmitted to the elementary coatings 8, 9 and 10 by compressing them.
- the material constituting the third coating since it has a lower shock impedance than that of the material of the second elementary 9, is crossed by a shock at the pressure P′3 lower than P′2 and at the particle speed u′3 greater than u′2.
- the pressure P′3 and the particle speed u′3 are the values slightly altered by passing the shock through the air gap 12 of variable thickness of the pressure P3 and the particle speed u3 (P3 and u3 are graphically given in a "pressure, particle velocity" diagram by the intersection of the symmetrical curve with respect to the line parallel to the pressure axis passing through the point (P2, u2) of the Hugoniot curve of the second elementary covering 9 and of the Hugoniot curve of the third elementary covering 10).
- the third elementary covering 10 moves and deforms as a function of its own characteristics and of the energy communicated to it by the second elementary covering 9.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8916214A FR2655719B1 (fr) | 1989-12-07 | 1989-12-07 | Charge explosive engendrant plusieurs noyaux et/ou jets. |
FR8916214 | 1989-12-07 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0437992A1 true EP0437992A1 (de) | 1991-07-24 |
EP0437992B1 EP0437992B1 (de) | 1993-09-15 |
Family
ID=9388270
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19900403485 Expired - Lifetime EP0437992B1 (de) | 1989-12-07 | 1990-12-07 | Sprengladung zum Bilden mehrerer Bolzen und/oder Stacheln |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0437992B1 (de) |
DE (1) | DE69003374T2 (de) |
ES (1) | ES2046746T3 (de) |
FR (1) | FR2655719B1 (de) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5279228A (en) * | 1992-04-23 | 1994-01-18 | Defense Technology International, Inc. | Shaped charge perforator |
GB2303687A (en) * | 1995-07-27 | 1997-02-26 | Western Atlas Int Inc | Shaped charges |
US5633475A (en) * | 1996-03-08 | 1997-05-27 | Western Atlas International, Inc. | Circulation shaped charge |
US6035785A (en) * | 1997-02-06 | 2000-03-14 | Giat Industries | Explosively-formed charge with attachment means between the liner and the casing |
US6250229B1 (en) * | 1996-04-02 | 2001-06-26 | Giat Industries | Performance explosive-formed projectile |
WO2006054081A1 (en) * | 2004-11-16 | 2006-05-26 | Qinetiq Limited | Improvements in and relating to oil well perforators |
US20130284441A1 (en) * | 2011-06-08 | 2013-10-31 | James E. Brooks | Downhole severing tool |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3628622C1 (de) * | 1986-08-22 | 1996-08-08 | Fraunhofer Ges Forschung | Vorrichtung zur Erzeugung sprenggeformter Projektile |
FR2866701A1 (fr) | 2004-02-20 | 2005-08-26 | Giat Ind Sa | Charge formee generatrice de plusieurs noyaux |
DE102005057254B4 (de) * | 2005-12-01 | 2007-07-26 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Penetrationsgeschoss und Verfahren zur Erzeugung eines solchen Geschosses |
DE102006061445B4 (de) | 2006-12-23 | 2008-09-18 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Penetrationsgeschoss |
DE102020001785A1 (de) | 2020-03-17 | 2021-09-23 | Diehl Defence Gmbh & Co. Kg | Gefechtskopf und Verfahren zur Bekämpfung eines Ziels mit dem Gefechtskopf |
DE102020002460B3 (de) | 2020-04-23 | 2021-09-23 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mit beschränkter Haftung | Gefechtskopf mit mehrschichtiger Lagenfolge |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3224368A (en) * | 1964-09-10 | 1965-12-21 | Honeywell Inc | Dual liner shaped charge |
DE2336750A1 (de) * | 1973-07-19 | 1975-04-10 | Hans Walter Loeckmann | Perforationsgeraet mit hohlladung |
US4498367A (en) * | 1982-09-30 | 1985-02-12 | Southwest Energy Group, Ltd. | Energy transfer through a multi-layer liner for shaped charges |
DE2927555C1 (de) * | 1979-07-07 | 1985-05-09 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Hohlladungsauskleidung und Verfahren zu deren Herstellung |
US4747350A (en) * | 1984-06-18 | 1988-05-31 | Alexander Szecket | Hollow charge |
FR2632394A1 (fr) * | 1986-07-24 | 1989-12-08 | France Etat Armement | Charge explosive generatrice de noyau |
-
1989
- 1989-12-07 FR FR8916214A patent/FR2655719B1/fr not_active Expired - Fee Related
-
1990
- 1990-12-07 ES ES90403485T patent/ES2046746T3/es not_active Expired - Lifetime
- 1990-12-07 DE DE1990603374 patent/DE69003374T2/de not_active Expired - Fee Related
- 1990-12-07 EP EP19900403485 patent/EP0437992B1/de not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3224368A (en) * | 1964-09-10 | 1965-12-21 | Honeywell Inc | Dual liner shaped charge |
DE2336750A1 (de) * | 1973-07-19 | 1975-04-10 | Hans Walter Loeckmann | Perforationsgeraet mit hohlladung |
DE2927555C1 (de) * | 1979-07-07 | 1985-05-09 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Hohlladungsauskleidung und Verfahren zu deren Herstellung |
US4498367A (en) * | 1982-09-30 | 1985-02-12 | Southwest Energy Group, Ltd. | Energy transfer through a multi-layer liner for shaped charges |
US4747350A (en) * | 1984-06-18 | 1988-05-31 | Alexander Szecket | Hollow charge |
FR2632394A1 (fr) * | 1986-07-24 | 1989-12-08 | France Etat Armement | Charge explosive generatrice de noyau |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5279228A (en) * | 1992-04-23 | 1994-01-18 | Defense Technology International, Inc. | Shaped charge perforator |
GB2303687A (en) * | 1995-07-27 | 1997-02-26 | Western Atlas Int Inc | Shaped charges |
US5633475A (en) * | 1996-03-08 | 1997-05-27 | Western Atlas International, Inc. | Circulation shaped charge |
US6250229B1 (en) * | 1996-04-02 | 2001-06-26 | Giat Industries | Performance explosive-formed projectile |
US6035785A (en) * | 1997-02-06 | 2000-03-14 | Giat Industries | Explosively-formed charge with attachment means between the liner and the casing |
WO2006054081A1 (en) * | 2004-11-16 | 2006-05-26 | Qinetiq Limited | Improvements in and relating to oil well perforators |
US7987911B2 (en) | 2004-11-16 | 2011-08-02 | Qinetiq Limited | Oil well perforators |
US9371709B2 (en) | 2010-04-09 | 2016-06-21 | Hunting Titan, Inc. | Downhole severing tool |
US20130284441A1 (en) * | 2011-06-08 | 2013-10-31 | James E. Brooks | Downhole severing tool |
US9140088B2 (en) * | 2011-06-08 | 2015-09-22 | Hunting Titan, Inc. | Downhole severing tool |
Also Published As
Publication number | Publication date |
---|---|
EP0437992B1 (de) | 1993-09-15 |
DE69003374T2 (de) | 1994-02-24 |
FR2655719B1 (fr) | 1994-05-06 |
FR2655719A1 (fr) | 1991-06-14 |
DE69003374D1 (de) | 1993-10-21 |
ES2046746T3 (es) | 1994-02-01 |
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