EP1516153B1 - Projectile or warhead - Google Patents
Projectile or warhead Download PDFInfo
- Publication number
- EP1516153B1 EP1516153B1 EP03730148A EP03730148A EP1516153B1 EP 1516153 B1 EP1516153 B1 EP 1516153B1 EP 03730148 A EP03730148 A EP 03730148A EP 03730148 A EP03730148 A EP 03730148A EP 1516153 B1 EP1516153 B1 EP 1516153B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- projectile
- warhead according
- warhead
- active
- alp
- 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.)
- Expired - Lifetime
Links
- 239000012634 fragment Substances 0.000 claims abstract description 39
- 238000013467 fragmentation Methods 0.000 claims abstract description 35
- 238000006062 fragmentation reaction Methods 0.000 claims abstract description 35
- 239000002360 explosive Substances 0.000 claims abstract description 30
- 230000035939 shock Effects 0.000 claims description 26
- 230000001133 acceleration Effects 0.000 claims description 18
- 229910001385 heavy metal Inorganic materials 0.000 claims description 16
- 239000000463 material Substances 0.000 claims description 14
- 230000035515 penetration Effects 0.000 claims description 11
- 230000005540 biological transmission Effects 0.000 claims description 9
- 239000007787 solid Substances 0.000 claims description 6
- 230000001960 triggered effect Effects 0.000 claims description 6
- 229910052751 metal Inorganic materials 0.000 claims description 5
- 239000002184 metal Substances 0.000 claims description 5
- 229910000831 Steel Inorganic materials 0.000 claims description 4
- 239000010959 steel Substances 0.000 claims description 4
- 239000011159 matrix material Substances 0.000 claims description 3
- 239000007788 liquid Substances 0.000 claims description 2
- 238000010304 firing Methods 0.000 claims 2
- 230000011218 segmentation Effects 0.000 claims 1
- 230000008054 signal transmission Effects 0.000 claims 1
- 230000009471 action Effects 0.000 abstract description 8
- 206010041662 Splinter Diseases 0.000 description 72
- 230000000694 effects Effects 0.000 description 32
- 239000013543 active substance Substances 0.000 description 10
- 238000009826 distribution Methods 0.000 description 9
- 230000008901 benefit Effects 0.000 description 8
- 238000005474 detonation Methods 0.000 description 6
- 238000010276 construction Methods 0.000 description 5
- 238000000926 separation method Methods 0.000 description 5
- 238000011144 upstream manufacturing Methods 0.000 description 5
- 230000015572 biosynthetic process Effects 0.000 description 3
- 230000008859 change Effects 0.000 description 3
- 239000002131 composite material Substances 0.000 description 3
- 238000005520 cutting process Methods 0.000 description 3
- 238000000354 decomposition reaction Methods 0.000 description 3
- 230000000149 penetrating effect Effects 0.000 description 3
- 238000001228 spectrum Methods 0.000 description 3
- 238000010521 absorption reaction Methods 0.000 description 2
- 230000015556 catabolic process Effects 0.000 description 2
- 239000003795 chemical substances by application Substances 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 230000007123 defense Effects 0.000 description 2
- 230000003111 delayed effect Effects 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 238000005192 partition Methods 0.000 description 2
- 238000007493 shaping process Methods 0.000 description 2
- 239000011343 solid material Substances 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 241000251729 Elasmobranchii Species 0.000 description 1
- 102100040287 GTP cyclohydrolase 1 feedback regulatory protein Human genes 0.000 description 1
- 101710185324 GTP cyclohydrolase 1 feedback regulatory protein Proteins 0.000 description 1
- 229910000760 Hardened steel Inorganic materials 0.000 description 1
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 1
- AYCPARAPKDAOEN-LJQANCHMSA-N N-[(1S)-2-(dimethylamino)-1-phenylethyl]-6,6-dimethyl-3-[(2-methyl-4-thieno[3,2-d]pyrimidinyl)amino]-1,4-dihydropyrrolo[3,4-c]pyrazole-5-carboxamide Chemical compound C1([C@H](NC(=O)N2C(C=3NN=C(NC=4C=5SC=CC=5N=C(C)N=4)C=3C2)(C)C)CN(C)C)=CC=CC=C1 AYCPARAPKDAOEN-LJQANCHMSA-N 0.000 description 1
- 241000237983 Trochidae Species 0.000 description 1
- 238000004026 adhesive bonding Methods 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
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005422 blasting Methods 0.000 description 1
- 230000009172 bursting Effects 0.000 description 1
- 230000002301 combined effect Effects 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000007373 indentation Methods 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 229910000765 intermetallic Inorganic materials 0.000 description 1
- 229910052749 magnesium Inorganic materials 0.000 description 1
- 239000011777 magnesium Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 230000010534 mechanism of action Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 230000001902 propagating effect Effects 0.000 description 1
- 239000003380 propellant Substances 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000001007 puffing effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000002441 reversible effect Effects 0.000 description 1
- 238000005476 soldering Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 229910052715 tantalum Inorganic materials 0.000 description 1
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- 208000008918 voyeurism Diseases 0.000 description 1
- 238000004073 vulcanization Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 238000003466 welding Methods 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
- 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
- F42B12/201—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 target class
- F42B12/204—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 target class for attacking structures, e.g. specific buildings or fortifications, ships or vehicles
-
- 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
- F42B12/34—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect expanding before or on impact, i.e. of dumdum or mushroom type
-
- 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
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/367—Projectiles fragmenting upon impact without the use of explosives, the fragments creating a wounding or lethal effect
Definitions
- the invention relates to a multi-purpose projectile, a warhead or a missile with ALP module.
- the overall end ballistic effect of penetration depth and area occupation is combined by end ballistic active elements such as KE penetrators, shaped charges or projectile-forming charges and by the various splinters (ALP splitter and / or splitter head), disk, ring or P-charge or shaped charge splitter Blast effects provided.
- the object of the present invention is to provide an improved projectile or an improved warhead which uses an active active body according to the ALP principle in a particularly effective manner.
- the hybrid, polyvalent projectile or the hybrid, polyvalent warhead according to the invention comprises an active agent donating agent projectile part (first projectile part), wherein the active agents preferably in the tip or near-field of the projectile or Warhead are positioned; an ALP projectile part (second projectile part), which is preferably arranged behind the active agent projectile part, with an end-ballistically effective casing and an inert pressure transfer medium provided inside the casing; and a pyrotechnic device provided between the active agent projectile part and the ALP projectile part both for triggering the active agents in the active agent projectile part and for building up a pressure field via the inert pressure transfer medium of the ALP projectile part.
- first projectile part active agent donating agent projectile part
- ALP projectile part second projectile part
- a pyrotechnic device provided between the active agent projectile part and the ALP projectile part both for triggering the active agents in the active agent projectile part and for building up a pressure field via the inert pressure transfer medium of the
- a particularly simple linkage between the ALP principle and projectiles with splinters or functional support-emitting heads or projectile segments is effected by the detonative or pyrotechnic device simultaneously serving as two elements of action as a pressure-generating / accelerating element.
- MZ projectiles multi-purpose projectiles
- the invention relates to an active penetrator, an active projectile, an active missile or an active laterally effective multi-purpose projectile (MZ, hybrid projectile) in combination with axial and radial splitter modules or separate accelerator explosives component accelerators.
- MZ multi-purpose projectile
- the overall end ballistic effect of fragmentation, disk action, penetration depth and axial and radial surface coverage / surface loading is initiated by means of a device (device) which can be triggered in an optimum position of the active body for triggering the effectiveness (or the effect effects).
- the arc of primarily pyrotechnic based disintegrating penetrators extends to partially inert projectiles (eg PELE module and integrated KE active part or KE). Module alone) with a pure splitter head for special Zielbeetzschlagept.
- PELE DE 197 00 349 C1
- ALP EP-A-1 316 774
- FIGS. 1A to 1C show examples according to the invention. These are penetrators with active lateral effective parts in combination with a splinter, P-charge, disc or HL head.
- FIG. 1A is a shorter (eg swirl-stabilized) version of a projectile 1 with a local, splitter accelerating and at the same time in the subsequent module pressure-generating element 7A for splitter assignment 11, and
- FIG. 1B shows a longer (eg aerodynamically stabilized) construction 2 with the splitter accelerating element 7B for the splinter occupancy 12 and a central, further pressure-generating element (detonating cord) 9.
- Figure 1C shows a likewise aerodynamically stabilized, three-part version 3 with HL head 13, wherein the explosive of the HL part simultaneously supplies the pressure for the subsequent ALP module.
- the shell 4 of the ALP module enveloping the pressure-transmitting medium 6 on account of its material property, mass and speed, forms the central radial splitter-forming unit. This is followed by a feature component.
- the medium 6 transmits the pressure generated by means of a controllable, pyrotechnic device 7A, 7B, 7C on the enveloping body 4 and thus causes a decomposition into fragments / sub-projectiles with a lateral movement components. All examples are provided here with an external ballistic hood 5.
- the triggering device 8 may consist of a simple touch detector, a timer, a programmable module, a receiving part and a fuse components.
- the device 8 can with the locally concentrated pressure-generating unit 7A, 7B, 7C by means of a cylinder-like (ignition cord-like) pyrotechnic module 9 (see FIG. FIGS. 1B and 1C ) or by means of a line 10, which may also have pyrotechnic properties, be connected (see. Figure 1A ).
- the tip represents a parameter that is essential for the efficiency of a projectile EP-A-1 316 774 has already been pointed out (see there FIG. 15 ) that the tip can be designed as a splitter module.
- this aspect is dealt with in more detail.
- tip as a construction space
- explosive tip and tip as an upstream penetrator.
- the tip may be partially hollow or filled. It is also conceivable that performance-supporting elements are integrated into the top.
- FIG. 2 Figure 43B in EP-A-1 316 774
- FIG. 3A ( Figure 43C in EP-A-1 316 774 ) shows an ALP module 23 upstream tip 19 with a pyrotechnic element 17 in a sleeve 20th
- FIG. 3B ( Figure 43D in EP-A-1 316 774 ) shows another tip design, such as a tip element 21 upstream of the ALP module 24, in which the pyrotechnic module 17 is also located in a sleeve and at the same time projects into the tip filled with a medium 22.
- the active components introduced in the front part of the bullet or directly in the region of the tip can be effective separately (eg in conjunction with KE modules) or triggered or controlled independently.
- they are combined directly with technical embodiments in the context of the present invention with the aim of an optimal overall function.
- components which provide high axial power at a correspondingly high propagation (advance) speed such as shaped charges, flat-cone charges and also disc-shaped explosive-accelerated projectiles (cf. FIGS. 6 . 10 . 28 . 35-38 ).
- Such structures are of particular interest, for example, when systems such as active and reactive components are to be triggered on the target side before the impact of the projectile.
- Such systems are particularly suitable for controlling deeper target structures, components, walls and bunker walls, since the leading active component leads to a pre-destruction of the structure.
- the subsequent Penetratormodule not eaten prematurely or can penetrate or break without breaking and thus achieve very high performance.
- Bullets of this type are, for example, in combination with the ALP principle in an excellent way to combat oncoming threats such as warheads or combat or reconnaissance drones that can not be fought with direct hits. Even conventional fragmentation bullets are practically ineffective due to the encounter situation with drones and their very limited splinter distribution.
- the operation of the present invention in combination with a corresponding trip unit promises a previously unachievable efficiency.
- the distances to the target of interest a distinction can be made between the immediate vicinity (less than 1 m), the near zone (1 m to 3 m), the near zone (3 m to 10 m), the central distance zone (10 m to 30 m ) and the more distant area (over 30 m).
- the range over 30 m may still be interesting, since charges already exist which act over a distance of well over 100 calibres.
- FIGS. 4 to 10 show a number of illustrative examples and technical design proposals, of course, even more basic arrangements are possible.
- the arrows, which symbolize the resultant of the propagation direction of the active agents or splinters, indicate the mass or the speed of the active components in terms of length and thickness.
- FIG. 4 is shown as a cross-sectional drawing an ALP tip module 25 with four mainly laterally acting splinter charges 26. These are accelerated by a central explosive body 27. This results in four splitter fields with preferred propagation directions 30A to 30D. Due to the shape of the body 27 and the surface configuration 29 of the fragment body 26, the fields can be varied, that is, for example, have more scattering effect or be aligned more concentrated. By tapering the body 27 towards the tip, the axial component of the splitter speed can also be increased. Further simple possibilities of change are the shape, the mass and the material of the splinters 26 or the accelerated active surfaces. The splitter panels 26 may also fill the entire space 28 to the housing 31. It is also conceivable to produce the splitter body 26 from a pressed material or from a block of material which is either accelerated as a disk (plate) or disassembled during the detonation of 27. Also multi-layered and combined combinations are possible.
- FIG. 5 shows again in cross-section as another example of the design of a projectile or warhead a module 32 with six laterally acting area splitter distributions from a central pyrotechnic module 34 in conjunction with corresponding metallic inserts 35 of copper, tantalum, tungsten or other heavy as possible ductile materials and build up splinter surfaces in six directions 36A to 36G.
- the number of charges is freely selectable and depends primarily on the dimensions of such a module 32.
- the housing wall 33 may also give splinters with appropriate design.
- FIG. 6 shows as longitudinal and cross-section two further variants of a tip design according to the invention.
- an ALP tip module 37 with four charges acting obliquely forwards / outwards (speed-resulting 38) (eg P charges 39, formed from the central explosive element 40 and the metallic insert 41).
- P charges 39 formed from the central explosive element 40 and the metallic insert 41.
- P charges 39 formed from the central explosive element 40 and the metallic insert 41.
- P charges 39 formed from the central explosive element 40 and the metallic insert 41
- This technical variant 44 is in the lower part of FIG. 6 shown.
- FIG. 7 shows two further examples of an ALP tip module 45 with a predominantly axially acting fragment head, here in the upper half, formed from three splinter cones 47 (propagation direction 53) behind an outer ballistic hood 48.
- the acceleration charge 49 for the fragment cones 47 is simultaneously according to the invention an element to which, for example, another explosive cylinder / detonating cord for the active disassembly of the projectile casing 50 via the here preferably solid (eg metallic) pressure transmission medium 51 connects.
- the charge 49 may also be separate from subsequent charges such as charge 9 (see lower half of the figure).
- the splinter distribution can also be influenced by the type of external damming.
- the ring surrounding the acceleration component 49 may be designed as a fragment charge 54 (propagation direction 55) (lower half of the figure). It may then be useful to provide a separation 52 between the fragment head and the Restpenetrator.
- FIG. 8 Figure 2 shows two further examples of an ALP tip module 56 (top) and 57 (bottom) with a splitter head. This is again covered by an outer ballistic hood 58. This may be hollow (top) or additional splinters or other active agents 59 included (below). By means of a corresponding shaping of the surface 64 of the acceleration unit 62, the propagation direction 61 of the splinters of the splitter body 60 can be predetermined. Behind 62 may be a damming and simultaneously pressure-transmitting medium 63, in which other, arbitrarily shaped splitter can be embedded evenly or unevenly distributed.
- MZ projectiles which are predominantly large caliber ammunition in the caliber range 60 mm to over 155 mm
- weaker armored point targets e.g. Fixed-wing aircraft and helicopters such as unarmoured or less armored ground targets of larger surface area or lighter targets in larger combat distances.
- FIG. 9 shows two examples of an ALP tip module 65 with an axially effective components of high breakdown power (direction of action 66) with simultaneously lateral components. Shown is a shaped charge module with the explosive part 67 and a pointed cone (trumpet-shaped, degressive or progressive) insert 68. Around the explosive charge 67 may also be a splitter ring 54 as a damming (lower half of the picture).
- the pressure-transmitting medium 70 is to be selected here so that it acts dynamically damming / supporting for the hollow charge. However, in terms of strength and density, a plastic may already be sufficient. This of course also applies to the other examples shown so far and the following examples.
- FIG. 10 Various possibilities in the design of the insert 68 are in FIG. 10 shown. These range from pure HL inserts 68 to the formation of fast shaped charge jets at top speeds up to over 8,000 m / s (slender velocity arrow 66) over projectile flat-cone or spherical shell liners 71 which still measure at 2,000 m / s to 3,000 m / s approaching the target or striking a target projectile P-charge 73 (thicker, relatively short velocity arrow 69). Furthermore, the axially accelerated active part can also consist of a plate, disc or annular support 74, which can reach speeds of a few 100 m / s to 2,000 m / s.
- Such disc concepts can achieve punch performance, which are to be compared with those of P-charge mines.
- Such disk heads may also be constructed of two or more disks, which may consist of different materials and different thickness. For better dynamic separation, it may also be useful to introduce a pyrotechnic or a pressure-transmitting medium between the individual discs.
- the efficiency of the cannon is the deciding factor in case of tube-dropped ammunition.
- FIG. 11 the muzzle velocity for the caliber 120 mm achievable with predetermined masses to be accelerated (total or pipe masses) is plotted (continuous line).
- masses between 16 kg and 22 kg must be accelerated.
- a subcaliber ratio of 2: 1 corresponding to a flight level diameter of 60 mm
- 4: 3 corresponding to a flight level diameter of 90 mm as from the outside ballistic view highest sub-caliber ratio
- FIG. 11 is also that in consideration of the already emerging after publications inside ballistic performance increases (eg by means of DNDA (Di-nitro-di-AZA) - propellant powder) resulting performance field registered. Thereafter, an increase in the muzzle velocity of about 100 m / s to 120 m / s can be assumed - cf. dashed function course. The resulting displacement of the design range both in terms of a desired increase in speed (direction A) and in terms of a larger Verschuss- or penetrator mass (direction B) is located. Thus, the above estimated bullet (mass 16 kg) can be fired at about 1,300 m / s.
- DNDA Di-nitro-di-AZA
- a corresponding estimation for another caliber can be based either on a storkbill-like enlargement or reduction or, for example, on a constant length.
- the masses change approximately with the third power of the dimensions, in the latter case with the square of the diameter change. For example, assuming a transition from 120 mm to eg 155 mm, this results in a factor of 2.16 for stork-billed transmission, and a factor of 1.67 for a projectile length that is kept constant.
- FIGS. 12 to 18 and 26 to 38 Further examples of bullets / warheads according to the present invention are shown.
- FIG. 12 So is in FIG. 12 an ALP with fragment head shown as swirl-stabilized version.
- the ALP module has a jacket with inner cone 76.
- FIG. 13 shows a bullet accordingly FIG. 12 but still with an additional inner core 78.
- This can be made of heavy metal, carbide or hardened steel.
- the cap / hood 77 protects the hard core against unacceptable shock loads, eg when hitting massive or high-strength targets.
- the trigger or control unit 8 is protected by a strong shell 75 here. This also serves to ensure the pressure in the pressure-generating medium 6 for the disassembly of the shell 76th
- Shells with cores corresponding FIG. 13 are particularly suitable for lower impact speeds (below 800 m / s to 1,000 m / s).
- the hardness of a penetrator still plays the dominant role for the fürdring elaborate.
- the density of a penetrator becomes increasingly important.
- heavy metal cores are advantageously introduced.
- projectiles according to the invention with embedded hard cores even at relatively low speeds (400 m / s to 600 m / s) in particular then compared to penetrators, which are designed for high impact speeds, still considerable penetration rates expected when the core penetrates not destroyed.
- the specific surface loading of the core is the decisive factor for the penetration capacity, ie, to a first approximation, the length of the core.
- FIG. 14 shows as a further, fundamental example of a modular projectile 79 with a hard metal or heavy metal core 80 in the tip area. This can either be arranged within an outer ballistic hood 5 or replace it (even partially). Downstream of this is the fragment-dispensing part with a pyrotechnic unit 82 conically formed here.
- the splinters 81 are preferably ejected in the direction 84, with the conical rear side 83 of the core 80 causing an additional radial component.
- FIG. 15 An example of a pronounced splinter bullet is in FIG. 15 shown. It is a projectile 85 (or a projectile head) with two-stage fragment part (formed from the pyrotechnic units 86 and 87 and the splitter assignments 88 and 89) and downstream ALP module. The resultant of the accelerated Slivers are represented by the arrows 90 (for 88), 91 (for 89) and 92 (for 4).
- This example may also be combined with a directional splitter acceleration 93 as shown in FIG FIG. 16 is shown.
- the splitter occupancy 95 is divided here by means of the partitions 94 into four splitter segments 95, so that they can also be controlled separately (the corresponding resulting splitter arrow 96 is also shown).
- FIGS. 17 and 18 show examples of multipurpose projectiles 97 and 99 with cores and ALP and PELE modules, respectively. So is in FIG. 17 a splitter head of explosive 62 and splitter 61 positioned in front of a hard or heavy metal core 98 which displaces a crater in front of the following PELE module. The ignition of 62 is again via the element 8 and the control or connecting line 10. This line 10 can either run in the wall 4 or lie directly in the pressure-transmitting medium 6 (see. FIG. 18 ).
- FIG. 18 shows a multi-purpose storey with one opposite FIG. 17 reverse order of the modules downstream of the splitter head.
- the fragmentation head / ALP part forms the fragment-producing components, which follow a hard or heavy metal core 100 to achieve a high penetration performance.
- the shape of the splitter-accelerating elements with effects primarily in the weft direction must be adapted according to the desired fragmentation distribution.
- the acceleration of the splitter in the axial direction will be flat (disk / annular) pyrotechnic elements 105, which may be provided, for example, with a flat inner cone 107 for splinter-focusing (cf. Figures 1A . 12 . 13 and 15 ) or with a flat or stronger outer cone 1 13 (see. FIG. 7 ) or a lighter convex curvature (cf. FIGS. 8 . 17 . 18 . 19 . 30-34 ) or more convex shape (cf. Figures 1B and 8th ) may be provided for radial splitter distribution.
- FIGS. 19 to 25 For example, some embodiments of such applications are compiled.
- FIG. 19 serves the representation of the closer considered area. Damming takes place either via an outer ring 109 (cf. FIG. 20 ) or via the projectile casing 110 (cf. FIG. 21 ). Lies the igniter 108 more within the charge 105 (left side of FIG FIG. 20 ), as a rule, the self-attenuation is sufficient.
- FIG. 20 This directional effect can be enhanced by constructive measures.
- FIG. 21 illustrated arrangement 111 with rear inert body 112 for shock wave steering.
- FIG. 21 shows Figure 22A , There, via a front (viewed in the direction of the shot) inert body with inner cone 115, the shock waves emitted after the ignition of the explosive 105 by means of the ignition charge 108 are deflected. It is also an annular ignition 108A conceivable.
- an outer cone 115B for shock wave steering is possible; see. Figure 22B ,
- shock wave steering is basically known in the case of hollow or P charges for steering or better distribution of the shock waves in the charges accelerating the deposits. There, however, he should primarily cause a better shock wave symmetry and thus a more accurate beam formation.
- This effect is to be assisted by a corresponding splitter distribution of the splitter surface 106 and / or design of the surface of the pyrotechnic element 105 (for example concave, convex, conical).
- FIGS. 23 to 25 Further examples of a fragmentation shock wave steering are shown.
- a shock wave steering body 117 This can be made of a metallic compound or of plastic or from the explosive effect supporting substances.
- assembly 118 a plurality of igniters 108 are introduced, which are separated by a wall 119. By a different ignition, a desired direction can be specified here.
- the inserted front conical inert body 115 supports this effect.
- an assembly 120 is shown in which the individual igniter / accelerator elements 121 (or the explosive agent ring) in correspondingly shaped pockets between the inner and outer inert bodies 122 and 123 for shock wave steering are located.
- FIG. 26 shows FIG. 26 another basic design for a projectile / warhead 124. It is in principle an ALP, which is carried out in the rear part in the known manner, while the front part consists of a splitter chamber 127, in which the splitter 128 embedded in a matrix material are. The charge 126 ignited via the trigger / controller 8 accelerates both projectile modules.
- the splinters 128 in the rear part of the chamber 127 in the case of a thin, ie dividing wall, also become self-confused by the front one Material more radially accelerated (resulting arrow for speed and mass 131), in the front part mainly axial (arrow for speed and mass 132).
- a more massive wall or lower axial acceleration on the part 126 a purely axial ejection of the splitter 128 from the pocket / container 127 can be achieved. It is also a fragment filled tip 125 (lower half) with corresponding resulting arrow 125A conceivable.
- the overall energy balance can not be surpassed.
- the ram which forms during beam formation, on which the rapidly axially propagating beam is supported is pressed into the ALP module, thus increasing its lateral efficiency.
- FIG. 27 shows a projectile according to the invention with P-charge head and core with Zerlegerladung (detonating cord) 135.
- This central charge 135 can be designed so that it can not overcome the externally applied pressure in homogeneous targets despite ignition, so that the core can penetrate quasi-homogeneous through the target.
- the pressure applied by 135 is sufficient to disassemble the core, making it into several fragments can disassemble and thus gives its performance in the target with a corresponding lateral effect (see also FIG. 29 ).
- FIG. 28 shows a HL warhead 136 with a beam focusing device 137.
- a trumpet-shaped insert 138 was chosen to achieve high jet speeds. Accordingly slim here is the channel 137 is formed. It is also conceivable to manufacture the channel-forming body 137 from a fragment-forming medium.
- FIG. 29 a radially segmented module 140 (formed here of four segments 142) may be provided with a bursting charge 141. The resulting arrows 143 are drawn.
- FIG. 30 shows a projectile 144 with fragment head, ALP module with a long / slender central penetrator (high slenderness degree) 145 for the highest possible penetration power.
- the tip of the penetrator 145 is protected by a cap / hood, a cylinder or similar device 146 against shock loads of the pyrotechnic unit and also by the impact and penetration into a target (vg. FIG. 13 ).
- FIG. 31 shows a projectile 147 according to the invention with a fragment-forming head and a composite, here very large designed core 148.
- This consists for example of a hard metal tip 149 and a rear core member 150 made of heavy metal.
- the connection between 149 and 150 takes place by means of an intermediate layer 151. It stands for a compound of gluing, vulcanization, friction welding or soldering. Of course, however, any other positive or non-positive connection is possible.
- Such composite cores also have the advantage that they can be processed in heavy metal or steel part.
- the interface between 149 and 150 may also be tapered to prevent the heavy metal cylinder 150 from being dynamically puffed up on the back surface of the hard core 149 as the tip 149 retards.
- FIG. 32 a modular bullet 152 having a further core structure with a carbide tip 149 and a sleeve-based rear core part 154.
- the sleeve 153 may be made of another hard metal, heavy metal, steel or other solid material.
- the inner core shaft 154 may be connected to the tip 149, integrally formed therewith, or simply inserted. It is also a conical shape of the rear core part conceivable, for example, to reduce friction when penetrating deeper targets.
- the central core consists of a segmented arrangement 156.
- the projectile / the missile 155 again consists of a fragment head with subsequent ALP module.
- the pressure transmission medium 6 consists of a solid material such as magnesium, aluminum or GFRP
- the segmented penetrator 156 can be introduced into it by means of a corresponding bore.
- the medium 6 consists of a liquid which is not sufficiently stable or mechanically (for the transmission of the launch acceleration), the penetrator 156 could be provided with its own sleeve 153.
- the central penetrator 156 is composed of two frontal cores 157 (preferably carbide or heavy metal) of low slenderness (low L / D ratio) separated by a buffer 160.
- This buffer 160 may also be made of the same material as the pressure transfer medium 6.
- the back core part is here formed of two slenderer cores 158 of higher aspect ratio (high L / D ratio). Between the cores 158, an impact-reducing layer 159 may be located. This layer 159 may also separate two cores 158 of different materials.
- FIG. 34 shows a projectile / warhead 161 whose front splitter component is formed from a chip-dispensing tip and a stack of splitter disks 163 and the respective pyrotechnic elements 164. This is followed either by a solid shaft or an ALP module (cf. FIG. 35 ). This example also includes a long central penetrator 162, which is either solid or in a sleeve 165. The discs can of course be arranged without pyrotechnic intermediate layers, but then the desired separation is not ensured.
- the splintering tip is replaced by a massive tip 167.
- This can, for example, penetrate heavier preliminary targets, in order to allow passage of the residual penetrator in this way, so that subsequently the fragments 163 accelerated by the pyrotechnic elements 164 can open radially.
- a conical tip such discs can still receive a mechanically caused lateral component by the thorns.
- FIGS. 36 to 38 Other, non-conventional tip or penetrator designs are in the FIGS. 36 to 38 shown. So shows FIG. 36 a projectile / warhead 168 with a along the entire length extending central penetrator 169, which is surrounded in the front of rings or ring segments 171. These can be conically designed to support the lateral components (see the resulting arrow 173) in the manner of cup springs. These are accelerated by the planar pyrotechnic elements 172. The remainder of the projectile is designed as an ALP module, which is pressure-loaded here by its own pyrotechnic element 170. The central penetrator 169 is provided with its own tip 174. This can also be stepped.
- FIG. 37 shows a variant 175 of FIG. 36 ,
- the central penetrator 177 has a hexagonal cross-section. It is surrounded by six planar elements 176 (per layer / plane). These are held together by the outer ring / shell 178.
- This sheath 178 may also be formed as a shatter-forming coat.
- further geometrical configurations according to the technical requirements or desired effects are possible.
- the exit velocity is usually low, for caliber 155 mm, for example. at about 800 m / s.
- the tip shapes to be used are determined by the external ballistics. At low speeds, it may make sense to deviate from conventional tip shapes or to dispense with external ballistic hoods. Even tread tips are conceivable that are to be dimensioned solely from end ballistic specifications, for example, to better attack oblique / inclined target surfaces.
- the discs 180 have a different cone angle and a different thickness with appropriately adapted pyrotechnic elements 181.
- the hood on the flight or target approach also mechanically removed (eg unfolded), dropped, blasted or during the flight eroded.
- Such a hybrid, polyvalent active system of the invention is in addition to the acceleration by means of cannons in a special way for the purpose of using missiles, missile defense systems, controlled / guided bombs or missiles to cruise missiles. Due to the almost unlimited scope for interpretation in connection with almost all known mechanisms of action, such systems have to combat heavily armored ballistic targets via large and / or deep target structures such as lighter targets, airplanes, ships and structures as well as strategic objects.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Radar Systems Or Details Thereof (AREA)
- Superconductor Devices And Manufacturing Methods Thereof (AREA)
- Vibration Dampers (AREA)
Abstract
Description
Die Erfindung betrifft ein Mehrzweckgeschoss, einen Gefechtskopf oder einen Flugkörper mit ALP-Modul. Die endballistische Gesamtwirkung aus Eindringtiefe und Flächenbelegung wird durch endballistische Wirkelemente wie KE-Penetratoren, Hohlladungen oder projektilbildende Ladungen und durch die diversen Splitter (ALP-Splitter und/oder Splitterkopf), Scheiben-, Ring- oder P-Ladungs- oder Hohlladungssplitter in Verbindung mit Blasteffekten erbracht.The invention relates to a multi-purpose projectile, a warhead or a missile with ALP module. The overall end ballistic effect of penetration depth and area occupation is combined by end ballistic active elements such as KE penetrators, shaped charges or projectile-forming charges and by the various splinters (ALP splitter and / or splitter head), disk, ring or P-charge or shaped charge splitter Blast effects provided.
Bei splitterbildenden oder Splitter abgebenden endballistischen Wirkungsträgem unterscheidet man üblicherweise zwischen Sprenggeschossen mit Zündeinrichtung, sog. Mehrzweckgeschossen/Hybridgeschossen (Spreng-/Splitterwirkung kombiniert mit HL-Wirkung), Gefechtsköpfen (meist mit HL- und/oder Splitter/Sprengwirkung) oder Flugkörpern und neuerdings Wirkungsträger nach dem Prinzip der Penetratoren mit erhöhter Lateralwirkung (PELE) und dem Prinzip der aktiven lateralwirksamen Penetratoren (ALP). Das PELE-Prinzip ist z.B. in der
Weiter offenbart die
Der vorliegenden Erfindung liegt die Aufgabe zugrunde, ein verbessertes Geschoss oder einen verbesserten Gefechtskopf bereitzustellen, das bzw. der einen aktiven Wirkkörper nach dem ALP-Prinzip in besonders effektiver Weise einsetzt.The object of the present invention is to provide an improved projectile or an improved warhead which uses an active active body according to the ALP principle in a particularly effective manner.
Diese Aufgabe wird durch ein Geschoss oder einen Gefechtskopf mit den Merkmalen des Anspruchs 1 gelöst. Vorteilhafte Ausgestaltungen und Weiterbildungen der Erfindung sind in den abhängigen Ansprüchen angegeben.This object is achieved by a projectile or a warhead with the features of
Das hybride, polyvalente Geschoss bzw. der hybride, polyvalente Gefechtskopf gemäß der Erfindung weist ein Wirkmittel abgebendes Wirkmittel-Geschossteil (erstes Geschossteil), wobei die Wirkmittel vorzugsweise in der Spitze oder im spitzennahen Bereich des Geschosses oder Gefechtskopfes positioniert sind; ein vorzugsweise hinter dem Wirkmittel-Geschossteil angeordnetes ALP-Geschossteil (zweites Geschossteil) mit einer endballistisch wirksamen Hülle und einem innerhalb der Hülle vorgesehenen inerten Druckübertragungsmedium; und eine zwischen dem Wirkmittel-Geschossteil und dem ALP-Geschossteil vorgesehenen pyrotechnische Einrichtung sowohl zum Auslösen der Wirkmittel in dem Wirkmittel-Geschossteil als auch zum Aufbauen eines Druckfeldes über das inerte Druckübertragungsmedium des ALP-Geschossteils auf. Dabei sind mehrere, hintereinander oder lateral angeordnete erste Geschossteile vorgesehen.The hybrid, polyvalent projectile or the hybrid, polyvalent warhead according to the invention comprises an active agent donating agent projectile part (first projectile part), wherein the active agents preferably in the tip or near-field of the projectile or Warhead are positioned; an ALP projectile part (second projectile part), which is preferably arranged behind the active agent projectile part, with an end-ballistically effective casing and an inert pressure transfer medium provided inside the casing; and a pyrotechnic device provided between the active agent projectile part and the ALP projectile part both for triggering the active agents in the active agent projectile part and for building up a pressure field via the inert pressure transfer medium of the ALP projectile part. In this case, several, successively or laterally arranged first floor parts are provided.
Mit der vorliegenden Erfindung erfolgt eine besonders einfache Verknüpfung zwischen dem ALP-Prinzip und Geschossen mit Splitter oder Wirkungsträger abgebenden Köpfen oder Geschosssegmenten, indem die detonative bzw. pyrotechnische Einrichtung gleichzeitig beiden Wirkungsträgem als druckerzeugendes/beschleunigendes Element dient. In Kombination mit den im Zusammenhang mit ALP beschriebenen Möglichkeiten zum Aufbau mehrteiliger/multifunktionaler Geschosse ergibt sich damit eine Bandbreite von sog. Mehrzweckgeschossen (MZ-Geschossen), die bisher mit keinem System erreicht wurde und die auch in ihrer Kombinationsvielfalt und Gesamtwirkungsbreite nicht mehr zu übertreffen sein dürfte.With the present invention, a particularly simple linkage between the ALP principle and projectiles with splinters or functional support-emitting heads or projectile segments is effected by the detonative or pyrotechnic device simultaneously serving as two elements of action as a pressure-generating / accelerating element. In combination with the possibilities described in connection with ALP for the construction of multi-part / multi-functional projectiles, this results in a range of so-called multi-purpose projectiles (MZ projectiles), which was previously not achieved with any system and which can not be outdone even in their combination diversity and overall effectiveness should be.
Bei Wirkkörpern nach dem ALP-Prinzip ist zur Zerlegung zwar grundsätzlich keine Eigengeschwindigkeit mehr Voraussetzung, jedoch ist bei einer geringen Auftreff- bzw. Interaktionsgeschwindigkeit (etwa bei sehr großen Kampfentfernungen oder grundsätzlich langsam fliegenden Bedrohungen) die endballistische Wirkung begrenzt. Diese Einsatzlücke wird entsprechend der vorliegenden Erfindung durch eine zusätzliche Einrichtung geschlossen, welche z.B. als pyrotechnische Einheit (P-Ladung, Hohlladung) die erforderliche Wirkung erbringt. Weiterhin können auch scheibenartige (tellerförmige/ringförmige) Körper oder entsprechende Splitterformen in die gewünschten Richtungen (insbesondere in axialer Richtung) beschleunigt werden. Da dieser Wirkmechanismus bei Geschossen noch nicht bekannt ist, wird er hier als "Scheiben- oder Ringladung" bezeichnet. In der Regel werden die entstehenden Druckfelder zur Auslösung weiterer Effekte (ALP) herangezogen. Es ist jedoch grundsätzlich auch denkbar, die Splitter oder sonstige Wirkmittel abgebenden Module autonom einstufig oder in mehrstufiger Bauweise wirken zu lassen.In principle, no intrinsic velocity is required for decomposition according to the ALP principle, but the end-ballistic effect is limited at a low impact or interaction speed (for example in the case of very large combat distances or generally slowly flying threats). This insert gap is closed according to the present invention by an additional device, which e.g. as pyrotechnic unit (P-charge, shaped charge) provides the required effect. Furthermore, disk-like (dish-shaped / annular) bodies or corresponding splitter molds can also be accelerated in the desired directions (in particular in the axial direction). Since this mechanism of action is not yet known on projectiles, it is referred to here as "disk or ring charge". As a rule, the resulting pressure fields are used to trigger further effects (ALP). However, it is basically also conceivable to have the splitter or other active agent-emitting modules act autonomously in one stage or in a multi-stage design.
Das Prinzip eines mehrteiligen Geschosses bzw. einer kombinierten Wirkung (HybridGeschoss) ist bereits in einer Vielzahl von Lösungen verwirklicht, wobei Tandem-Hohlladungsgeschosse und Tandem-P-Ladungs-Gefechtsköpfe die bekanntesten Vertreter sind. Es ist aber bereits hier darauf hinzuweisen, dass sich derartige zusätzliche Wirkkomponenten in Verbindung mit einem Penetrator entsprechend der vorliegenden Erfindung besonders wirkungsvoll kombinieren lassen. Dabei ist es ein besonderer Vorzug der hier präsentierten Lösungen, dass z.B. in erster Linie nicht nur vergleichbare Detektions- und Auslöseeinrichtungen wie bei bekannten Geschossen oder Gefechtsköpfen zu verwenden sind, sondern auch aufgrund der neuartigen Wirkprinzipien oder Wirkungskombinationen Lösungen mit geringeren technischen Ansprüchen an derartige Einrichtungen möglich sind. Weiterhin ergibt sich im vorliegenden Falle eine ungleich größere Kombinationsvielfalt unterschiedlicher Wirkungen. Auf diesen Sachverhalt wird in Zusammenhang mit den Ausführungsbeispielen zu Mehrzweckgeschossen im Zusammenhang mit dieser Erfindung noch näher eingegangen.The principle of a multi-part bullet or a combined effect (hybrid bullet) is already implemented in a variety of solutions, with tandem shaped charge projectiles and tandem P charge warheads are the most prominent representatives. It should be noted, however, that such additional active components in conjunction with a penetrator according to the present Combine invention particularly effectively. It is a particular advantage of the solutions presented here that, for example, primarily not only comparable detection and triggering devices are to be used as in known projectiles or warheads, but also possible due to the novel action or effect combinations solutions with lower technical standards for such facilities are. Furthermore, in the present case results in a much larger variety of combinations of different effects. This fact will be discussed in more detail in connection with the embodiments of multi-purpose projectiles in connection with this invention.
In gravierender Erweiterung des ALP-Einsatzfeldes betrifft die Erfindung einen aktiven Penetrator, ein aktives Geschoss, einen aktiven Flugkörper oder ein aktives lateral wirksames Mehrzweckgeschoss (MZ-, Hybridgeschoss) in Kombination mit axialen und radialen Splittermodulen oder getrennten Wirkungsträgern mit beschleunigender Sprengstoffkomponente. Die endballistische Gesamtwirkung aus Splitter-, Scheibenwirkung, Eindringtiefe sowie axialer und radialer Flächenbelegung/Flächenbelastung wird mittels einer in optimaler Position des Wirkkörpers auslösbaren Vorrichtung (Einrichtung) zur Auslösung der Wirksamkeit (bzw. der Wirkeffekte) eingeleitet. So spannt sich der Bogen von vornehmlich auf pyrotechnischer Basis zerlegenden Penetratoren (z.B. durch die Kombination Splitterkopf/ALP-Teil mit oder ohne Sprengstoff-Splitter-Modul) bis hin zu teilweise inerten Geschossen (z.B. PELE-Modul und integriertem KE-Wirkteil oder KE-Modul allein) mit einem reinen Splitterkopf für spezielle Zielbeaufschlagungen.In grave extension of the ALP application field, the invention relates to an active penetrator, an active projectile, an active missile or an active laterally effective multi-purpose projectile (MZ, hybrid projectile) in combination with axial and radial splitter modules or separate accelerator explosives component accelerators. The overall end ballistic effect of fragmentation, disk action, penetration depth and axial and radial surface coverage / surface loading is initiated by means of a device (device) which can be triggered in an optimum position of the active body for triggering the effectiveness (or the effect effects). Thus, the arc of primarily pyrotechnic based disintegrating penetrators (eg by combining fragment head / ALP part with or without explosive splitter module) extends to partially inert projectiles (eg PELE module and integrated KE active part or KE). Module alone) with a pure splitter head for special Zielbeaufschlagungen.
Mit der vorliegenden Erfindung wird das Leistungsspektrum der in der
Wie bereits in der
Weitere Merkmale, Einzelheiten und Vorzüge der vorliegenden Erfindung ergeben sich aus den Patentansprüchen in Verbindung mit der Beschreibung sowie anhand der einzelnen Figuren und den entsprechenden Erläuterungen. Hierbei zeigen:
- Fig. 1A
- ein drallstabilisiertes Geschoss mit einer Kombination aus Splitterkopf und ALP-Modul gemäß der Erfindung;
- Fig. 1B
- ein aerodynamisch stabilisiertes Geschoss mit einer Kombination aus Splitterkopf und ALP-Modul gemäß der Erfindung;
- Fig. 1C
- ein dreiteiliges aerodynamisch stabilisiertes Geschoss mit einer Kombination aus HL-Kopf, ALP- und KE-Modul gemäß der Erfindung;
- Fig. 2
- eine Spitze mit integriertem Wirkungsträger (vgl.
EP-A-1 316 774 - Fig. 3A und 3B
- Beispiele für Spitzen mit Splitterwirkung (vgl.
EP-A-1 316 774 - Fig. 4
- ein ALP-Splitterkopf-Geschoss mit (hier vier) lateral wirkenden Splitterladungen;
- Fig. 5
- ein ALP-Splitterkopf-Geschoss mit (hier sechs) Flächen aufbauende Ladungen;
- Fig. 6
- ein ALP-Spitzenmodul mit (hier vier) schräg nach vorne/außen wirkenden Ladungen (z.B. P-Ladungen, Scheiben- oder Splitterladungen);
- Fig. 7
- ein ALP-Splitterkopf-Geschoss, ausgeführt als Splitterkopf mit drei Splitterkegeln;
- Fig. 8
- ein ALP-Splitterkopf-Geschoss, ausgeführt als konvexer Splitterkopf unterschiedlicher Belegungsdicke;
- Fig. 9
- ein ALP-Splitterkopf-Geschoss mit integriertem HL-/P-Ladungs-Modul;
- Fig. 10
- Einlageformen für HL- oder P-Ladungen bzw. Scheiben-Ladungen;
- Fig. 11
- ein Diagramm zur Erläuterung der Abhängigkeit der Mündungsgeschwindigkeit von der zu beschleunigenden Masse für
das Kaliber 120 mm; - Fig. 12
- ein ALP-Geschoss mit Splitterkopf;
- Fig. 13
- ein ALP-Geschoss mit Splitterkopf und Innenkern;
- Fig. 14
- ein modulares Geschoss (oder Geschosskopf) mit Kern im Spitzenbereich, Splitterteil, ALP- und KE-Modul;
- Fig. 15
- ein Geschoss (oder Geschosskopf) mit mehrstufigem Splitterteil;
- Fig. 16
- ein Beispiel für richtungsgesteuerte Splitter- bzw. Scheibenbeschleunigung;
- Fig. 17
- ein modulares Geschoss mit Splitterkopf, Kern und PELE-Modul;
- Fig. 18
- ein Geschoss mit Splitterkopf, PELE-Modul und Kern;
- Fig. 19
- einen Geschosskopf mit Splittermodul;
- Fig. 20
- eine richtungsgesteuerte Splitterladung mit seitlicher Verdämmung;
- Fig. 21
- eine richtungsgesteuerte Splitterladung mit einem untenliegenden Inertkörper;
- Fig. 22A
- eine Splitterladung mit einem oberen Inertkörper und Ringzündung;
- Fig. 22B
- eine Splitterladung mit einem äußeren oberen Inertkörper;
- Fig. 23
- eine Splitterladung mit Detonationswellenlenkung;
- Fig. 24
- eine richtungsgesteuerte Splitterladung mit Inertkörper und Mehrfach-Zündladung;
- Fig. 25
- eine Splitterladung mit Kammern zur Detonationswellenlenkung;
- Fig. 26
- ein modulares Geschoss (oder Gefechtskopf) mit Splittertasche und ALP-Modul;
- Fig. 27
- ein Geschoss mit P-Ladungskopf und Kern mit Zerlegerladung;
- Fig. 28
- einen HL-Gefechtskopf mit Strahlfokussierung;
- Fig. 29
- einen radial segmentierten Penetrator mit zentraler Zerlegeeinrichtung;
- Fig. 30
- ein Geschoss mit Splitterkopf und einem zentralen Penetrator hohen Schlankheitsgrades mit Schockdämpfung;
- Fig. 31
- ein modulares Geschoss mit Splitterkopf und zweiteiligem Kern;
- Fig. 32
- ein modulares Geschoss mit Splitterkopf und mehrteiligem Kern;
- Fig. 33
- ein modulares Geschoss mit segmentiertem zentralen Penetrator;
- Fig. 34
- ein modulares Geschoss mit Splitterkopf/Splitterringen und einem zentralen langen Penetrator;
- Fig. 35
- ein modulares Geschoss mit massiver Spitze, Splitterringen und zentralem Kern sowie ALP-Modul;
- Fig. 36
- ein modulares Geschoss mit einem langen zentralen Penetrator, konischen Splitterscheiben und ALP-Modul;
- Fig. 37
- einen Geschossquerschnitt mit einem sechseckigen zentralen Penetrator, flächigen Splitterelementen und Außenhülle; und
- Fig. 38
- ein modulares Geschoss ohne Spitze / außenballistische Haube mit Splitterringen, einem langen zentralen Penetrator und ALP-Modul.
- Fig. 1A
- a spin stabilized bullet with a combination of fragmentation head and ALP module according to the invention;
- Fig. 1B
- an aerodynamically stabilized projectile with a combination of fragmentation head and ALP module according to the invention;
- Fig. 1C
- a three-part aerodynamically stabilized projectile with a combination of HL head, ALP and KE module according to the invention;
- Fig. 2
- a tip with integrated functional support (cf.
EP-A-1 316 774 - FIGS. 3A and 3B
- Examples of spikes with splinter effect (cf.
EP-A-1 316 774 - Fig. 4
- an ALP fragmentation projectile with (here four) laterally acting fragmentation charges;
- Fig. 5
- an ALP fragmentation projectile with (here six) surfaces constituting charges;
- Fig. 6
- an ALP tip module with (here four) obliquely forward / outward acting charges (eg P-charges, disc or splinter charges);
- Fig. 7
- an ALP fragmentation projectile, designed as a splitter head with three splinter cones;
- Fig. 8
- an ALP fragmentation projectile, designed as a convex fragmentation head of varying thickness;
- Fig. 9
- an ALP fragmentation projectile with integrated HL / P charge module;
- Fig. 10
- Insert molds for HL or P charges or disk charges;
- Fig. 11
- a diagram illustrating the dependence of the muzzle velocity of the mass to be accelerated for the
caliber 120 mm; - Fig. 12
- an ALP projectile with fragment head;
- Fig. 13
- an ALP projectile with fragment head and inner core;
- Fig. 14
- a modular projectile (or bullet head) with a core in the tip area, fragment part, ALP and KE module;
- Fig. 15
- a projectile (or projectile head) with a multi-stage fragment part;
- Fig. 16
- an example of directional splinter acceleration;
- Fig. 17
- a modular projectile with fragment head, core and PELE module;
- Fig. 18
- a projectile with fragment head, PELE module and core;
- Fig. 19
- a bullet head with splinter module;
- Fig. 20
- a directional splinter load with lateral containment;
- Fig. 21
- a directionally controlled fragmentation charge with an underlying inert body;
- Fig. 22A
- a fragmentation charge with an upper inert body and ring ignition;
- Fig. 22B
- a fragmentation charge with an outer upper inert body;
- Fig. 23
- a fragmentation charge with detonation wave steering;
- Fig. 24
- a direction-controlled fragmentation charge with inert body and multiple ignition charge;
- Fig. 25
- a fragmentation charge with detonation wave deflection chambers;
- Fig. 26
- a modular projectile (or warhead) with splitter pocket and ALP module;
- Fig. 27
- a projectile with P-charge head and core with burster charge;
- Fig. 28
- a HL warhead with beam focusing;
- Fig. 29
- a radially segmented penetrator with central decomposition device;
- Fig. 30
- a projectile with a fragment head and a central penetrator of high slenderness with shock absorption;
- Fig. 31
- a modular projectile with fragment head and two-piece core;
- Fig. 32
- a modular projectile with fragment head and multipart core;
- Fig. 33
- a modular projectile with segmented central penetrator;
- Fig. 34
- a modular projectile with fragmentation head / splinter rings and a central long penetrator;
- Fig. 35
- a modular bullet with solid tip, splinter rings and central core and ALP module;
- Fig. 36
- a modular projectile with a long central penetrator, conical slivers and ALP module;
- Fig. 37
- a projectile cross-section with a hexagonal central penetrator, flat splinter elements and outer shell; and
- Fig. 38
- a modular bullet without tip / outer ballistic hood with splinter rings, a long central penetrator and ALP module.
Die
In
Die Auslöseeinrichtung 8 kann aus einem einfachen Berührungsmelder, einem Zeitglied, einem programmierbaren Modul, einem Empfangsteil und einer Sicherungskomponenten bestehen. Die Einrichtung 8 kann mit der örtlich konzentrierten druckerzeugenden Einheit 7A, 7B, 7C mittels eines zylinderähnlichen (zündschnurähnlichen) pyrotechnischen Moduls 9 (vgl.
Grundsätzlich stellt die Spitze einen für die Leistungsfähigkeit eines Geschosses wesentlichen Parameter dar. In der
Die
Die im vorderen Geschossteil oder direkt im Bereich der Spitze eingebrachten Wirkkomponenten können (z.B. in Verbindung mit KE-Modulen) getrennt wirksam sein oder eigenständig ausgelöst bzw. angesteuert werden. Vorzugsweise werden sie direkt mit technischen Ausführungen im Rahmen der vorliegenden Erfindung mit dem Ziel einer optimalen Gesamtfunktion kombiniert. Hierbei können auch Komponenten integriert werden, die eine hohe axiale Leistung bei einer entsprechend hohen Ausbreitungs-(Vorauseil-)Geschwindigkeit erbringen wie Hohlladungen, Flachkegelladungen und auch scheiben/tellerförmige sprengstoffbeschleunigte Projektile (vgl.
Geschosse dieser Art eignen sich z.B. in Kombination mit dem ALP-Prinzip in hervorragender Weise zur Bekämpfung anfliegender Bedrohungen wie Gefechtsköpfe oder Kampf- bzw. Aufklärungsdrohnen, die mit Direkttreffern nicht zu bekämpfen sind. Auch herkömmliche Splittergeschosse sind praktisch auf Grund der Begegnungssituation mit Drohnen und ihrer sehr begrenzten Splitterverteilung wenig wirksam. Die Wirkungsweise der vorliegenden Erfindung in Kombination mit einer entsprechenden Auslöseeinheit verspricht hier eine bisher nicht erreichbare Effizienz.Bullets of this type are, for example, in combination with the ALP principle in an excellent way to combat oncoming threats such as warheads or Combat or reconnaissance drones that can not be fought with direct hits. Even conventional fragmentation bullets are practically ineffective due to the encounter situation with drones and their very limited splinter distribution. The operation of the present invention in combination with a corresponding trip unit promises a previously unachievable efficiency.
Bezüglich der interessierenden Abstände zum Ziel kann unterschieden werden zwischen dem unmittelbaren Nahbereich (kleiner 1 m), dem nahen Bereich (1 m bis 3 m), dem näheren Bereich (3 m bis 10 m), dem mittleren Entfernungsbereich (10 m bis 30 m) und dem zielferneren Bereich (über 30 m). Bei P-Ladungen und auch bei entsprechend geformten Scheiben-Ladungen kann noch der Bereich über 30 m interessant sein, da bereits Ladungen existieren, die über eine Entfernung von weit über 100 Kalibern wirken. Auch hier wird offensichtlich, dass mit Geschossaufbauten entsprechend der Erfindung eine nahezu beliebige Palette zur Verfügung steht, um gewünschte Wirkungen entsprechend des bekannten oder zu erwartenden Zielszenarios in einer bisher nicht erreichbaren Bandbreite zu erzielen.With regard to the distances to the target of interest, a distinction can be made between the immediate vicinity (less than 1 m), the near zone (1 m to 3 m), the near zone (3 m to 10 m), the central distance zone (10 m to 30 m ) and the more distant area (over 30 m). In the case of P charges and also with correspondingly shaped disk charges, the range over 30 m may still be interesting, since charges already exist which act over a distance of well over 100 calibres. Again, it will be apparent that with bullet assemblies in accordance with the invention, an almost arbitrary range is available to achieve desired effects corresponding to the known or expected target scenario in a previously unachievable range.
Die
In
Bei der Art der Splitterbelegung und bei der vorgegebenen Splitterrichtung 53 besteht ein relativ großer Gestaltungsspielraum. So können hier unterschiedlich in Material und Form gefertigte Komponenten zum Einsatz kommen. Eine Mischung aus schweren (großen) und leichten (kleinen) Splittern kann ebenfalls vorteilhaft sein. Ebenso kann der die Beschleunigungskomponente 49 umgebende Ring als Splitterladung 54 (Ausbreitungsrichtung 55) ausgebildet sein (untere Bildhälfte). Es kann dann sinnvoll sein, zwischen dem Splitterkopf und dem Restpenetrator eine Trennung 52 vorzusehen.In the type of splinter assignment and the given
Wie bereits erwähnt, kann eine Einrichtung entsprechend der vorliegenden Erfindung in Verbindung mit weiteren Wirkungsträgem auf eine bisher nicht zu erreichende Weise kombiniert werden. Dabei kann ein entsprechend ausgelegter ALP bereits ein effizientes Mehrzweckgeschoss (MZ-Geschoss) sein. MZ-Geschosse (hierbei handelt es sich überwiegend um großkalibrige Munition im Kaliberbereich 60 mm bis über 155 mm) haben primär die Aufgabe, solche Ziele zu bekämpfen, bei denen der Einsatz von auf eine hohe Durchschlagsleistung ausgelegten Geschossen nicht sinnvoll oder allein ausreichend ist. Dies gilt ebenso für schwächer gepanzerte Punktziele wie z.B. Starrflügler und Hubschrauber wie für ungepanzerte oder schwächer gepanzerte Bodenziele größerer Flächenausdehnung oder leichtere Ziele in größeren Kampfentfernungen. Diese Aufgaben werden in der Regel mittels splitterabgebenden Einrichtungen, oft in Kombination mit einem Hohlladungs- oder P-Ladungs-Modul, erreicht.As already mentioned, a device according to the present invention can be combined in conjunction with other effective elements in a manner not previously achieved. An appropriately designed ALP can already be an efficient multipurpose projectile (MZ projectile). MZ projectiles (which are predominantly large caliber ammunition in the
Es ist ein grundsätzlicher Vorteil von Anordnungen der gezeigten Art, dass praktisch die gesamte Splitter/Subgeschoss-Masse mit konstruktiv vorgebbaren Geschwindigkeitskomponenten vornehmlich in Richtung des zu bekämpfenden Ziels abgegeben wird. Dies ist insbesondere unter dem Aspekt von Interesse, dass z.B. bei herkömmlichen Mehrzweckgeschossen ein erheblicher Teil der Splitter nach hinten ausgestoßen wird und damit wirkungslos bleibt. Hier ist jedoch anzumerken, dass bereits Anordnungen bekannt sind, bei denen im Kopfbereich von Sprenggeschossen Splitter, auch solche mit geometrischer Gestaltung oder Belegung angeordnet sind. Es ist ein Vorzug der vorliegenden Erfindung, dass alle bisher bekannten Ausführungen integriert werden und mit den erfindungsspezifischen Komponenten verknüpft werden können.It is a fundamental advantage of arrangements of the type shown that virtually the entire splitter / sub-mass is discharged with structurally predeterminable velocity components primarily in the direction of the target to be counteracted. This is particularly in the aspect of interest that e.g. In conventional multi-purpose projectiles, a significant portion of the splinters is ejected to the rear and thus remains ineffective. Here, however, it should be noted that arrangements are already known in which splinters, including those with geometric design or occupancy are arranged in the head of explosive projectiles. It is an advantage of the present invention that all previously known designs can be integrated and linked to the invention-specific components.
Diverse Möglichkeiten bei der Ausgestaltung der Einlage 68 sind in
Hier ist anzumerken, dass Anordnungen bereits bekannt sind, bei denen sich eine HL-Komponente (Vorhohlladung) vor einer Hauptladung eines HL-Geschosses, insbesondere zur Auslösung reaktiver Ziele, befindet (Tandem-Ladungen). Es ist jedoch wiederum ein besonderer Vorteil der vorliegenden Erfindung, dass alle bisher bekannten Vorhohlladungen integriert und mit erfindungsspezifischen Komponenten verknüpft werden können. Im Gegensatz zu Tandem-Hohlladungen ist hier die im Strahlengang der Hauptladung positionierte Vorladung nicht leistungsmindernd, sondern kommt der Gesamtleistung eines Geschosses entsprechend der Erfindung in vollem Umfang zugute. Diese Überlegungen gelten auch für vorgeschaltete P-Ladungen.It should be noted that arrangements are already known in which an HL component (Vorhohlladung) before a main charge of a HL projectile, in particular for triggering reactive targets, is located (tandem charges). However, it is again a particular advantage of the present invention that all previously known Vorhohlladungen can be integrated and linked with invention-specific components. In contrast to tandem shaped charges, the precharge positioned in the beam path of the main charge does not reduce the performance, but benefits the entire output of a projectile in accordance with the invention in its entirety. These considerations also apply to upstream P charges.
Bisher nicht bekannt ist die Kombination von teller-, scheiben- oder ringförmigen pyrotechnisch beschleunigten Elementen in Verbindung mit einem sich dem Ziel nähernden oder auf ein Ziel auftreffenden Projektil. Aufgrund ihres großen Wirkungsdurchmessers in Verbindung mit ihrem Vorauseilen sind derartige Komponenten besonders geeignet, reaktive Ziele wirkungsvoll zu bekämpfen.So far unknown is the combination of plate, disc or annular pyrotechnic accelerated elements in connection with a projectile approaching the target or impinging on a target. Due to their large diameter of action in conjunction with their advance, such components are particularly suited to effectively combat reactive targets.
Unabhängig von den einzelnen Munitionskonzepten ist bei rohrverschossener Munition die Leistungsfähigkeit der Kanone die entscheidende Größe. In
Mit den obigen Werten ist auch eine noch durchaus beachtliche endballistische Wirksamkeit eines Geschosses entsprechend der vorliegenden Erfindung sowohl als KE- bzw. PELE-Geschoss als auch als ALP zu erwarten. Eine angenommene mittlere Masse für den Penetrator von 16 kg könnte sich dann bei einer Mündungsgeschwindigkeit von 1200 m/s beispielsweise folgendermaßen aufteilen: Masse des Splitter/Subgeschoss-Mantels 8 kg, Masse eines zentralen Penetrators (zentralen bzw. axialen Elementes) 3 kg, Masse der druckerzeugenden Elemente 0,2 kg, Masse der druckübertragenden/zusätzlich wirksamen Medien bzw. Wirkteile 2 kg, Masse für splitterabgebende Spitze oder HL- bzw. P-Ladungs-Spitze, Leitwerk und sonstige Elemente 2,8 kg.With the above values, a still quite remarkable end-ballistic effectiveness of a projectile according to the present invention is to be expected both as a KE or PELE projectile and as an ALP. An assumed mean mass for the penetrator of 16 kg could then be divided at a muzzle velocity of 1200 m / s, for example as follows: mass of the splitter /
In
Damit ist ein Geschoss entsprechend der in Zusammenhang mit
Bei der Abschätzung der endballistischen Leistung ist zu beachten, dass derartige Penetratoren aufgrund ihres sehr großen und insbesondere sich dynamisch vergrößernden Durchmessers beim Durchdringen insbesondere von Schottenzielen oder reaktiven Panzerungen Durchschlagsleistungen erreichen können, die mit denen von Hochleistungspenetratoren zu vergleichen sind oder diese noch übertreffen. In Verbindung mit konstruktiven Maßnahmen (vgl. Bemerkungen on Zusammenhang mit den
Bei einer entsprechenden Abschätzung für ein anderes Kaliber kann entweder von einer storchschnabelähnlichen Vergrößerung oder Verkleinerung ausgegangen werden oder z.B. von einer konstant gehaltenen Länge. Im ersten Fall ändern sich die Massen etwa mit der dritten Potenz der Abmessungen, im letzten Fall mit dem Quadrat der Durchmesseränderung. Bei einem angenommenen Übergang von 120 mm auf z.B. 155 mm ergibt sich damit bei storchschnabelmäßiger Übertragung der Faktor 2,16, bei konstant gehaltener Geschosslänge der Faktor 1,67.A corresponding estimation for another caliber can be based either on a storkbill-like enlargement or reduction or, for example, on a constant length. In the first case, the masses change approximately with the third power of the dimensions, in the latter case with the square of the diameter change. For example, assuming a transition from 120 mm to eg 155 mm, this results in a factor of 2.16 for stork-billed transmission, and a factor of 1.67 for a projectile length that is kept constant.
In den
So ist in
Geschosse mit Hartkernen entsprechend
Ein Beispiel für ein ausgesprochenes Splittergeschoss wird in
Die
Die Form der splitterbeschleunigenden Elemente mit Effekten vornehmlich in Schussrichtung ist entsprechend der gewünschten Splitterverteilung anzupassen. Grundsätzlich wird es sich bei der Beschleunigung der Splitter in axialer Richtung um flache (scheiben/ringförmige) pyrotechnische Elemente 105 handeln, die z.B. mit einem flachen Innenkonus 107 zur Splitterfokussierung (vgl.
Zusätzlich zu diesen geometrischen Maßnahmen kann noch eine Richtungssteuerung der Splitter vorgesehen werden. Diese ist insbesondere in Verbindung mit einem intelligenten Geschoss/Gefechtskopf interessant. In den
Um eine bestimmte Ausbreitungsrichtung (Splitterlenkung) der Splitterbelegung 106 zu erreichen, können z.B. am Umfang eines pyrotechnischen Beschleunigungselementes 105 mehrere Zünder bzw. Zündladungen 108 verteilt werden, die getrennt anzusteuern sind -
In konsequenter Ausgestaltung dieses Lösungsweges ist auch eine "Splitterkopf-Stoßwellenlenkung" denkbar. Der Begriff der Stosswellenlenkung ist bei Hohl- oder P-Ladungen zur Lenkung bzw. besseren Verteilung der Stosswellen in den die Einlagen beschleunigenden Ladungen her grundsätzlich bekannt. Dort soll er jedoch in erster Linie eine bessere Stosswellensymmetrie und damit eine exaktere Strahlbildung bewirken. Im Gegensatz dazu wird im Rahmen dieser Erfindung vorgeschlagen, den Effekt einer Stosswellenlenkung mittels in die Stosswellen-Ausbreitungsfelder eingebrachten Körpern eine asymmetrische Verteilung der Stosswellen und damit der Stosswellenenergie zu erreichen, um z.B. einer Splitterbelegung eine ungleichmäßige Verteilung oder eine besondere Richtung zu geben (Splitterkopf-Stoßwellenlenkung). Zu unterstützen ist dieser Effekt durch eine entsprechende Splitterverteilung der Splitterfläche 106 und/oder Ausgestaltung der Oberfläche des pyrotechnischen Elementes 105 (z.B. konkav, konvex, konisch).In a consistent embodiment of this approach, a "splitter head shock wave steering" is conceivable. The term shock wave steering is basically known in the case of hollow or P charges for steering or better distribution of the shock waves in the charges accelerating the deposits. There, however, he should primarily cause a better shock wave symmetry and thus a more accurate beam formation. In contrast, it is proposed in the context of this invention to achieve the effect of shock wave guidance by means of bodies introduced into the shock wave propagation fields, an asymmetrical distribution of the shock waves and thus of the shock wave energy, e.g. a splitter assignment to give an uneven distribution or a special direction (splitter head shock wave steering). This effect is to be assisted by a corresponding splitter distribution of the
In den
In den
Handelt es sich um ein Geschoss entsprechend der vorliegenden Erfindung mit einem HL- oder P-Ladungs-Kopf (vgl.
In Ergänzung zu den Ausführungen von
In Ergänzung zu
In
Bei dem in
Weitere, nicht konventionelle Spitzen- bzw. Penetrator-Gestaltungen sind in den
Insbesondere bei Flugkörpern oder bei sehr großen Kalibern liegt die Abgangsgeschwindigkeit in der Regel niedrig, für das Kaliber 155 mm z.B. bei etwa 800 m/s. Damit ist bei sehr großen Kampfentfernungen (20 km) mit relativ geringen Auftreffgeschwindigkeiten (400 m/s bis 500 m/s) zu rechnen. Die zu verwendenden Spitzenformen werden von der Außenballistik bestimmt. Bei geringen Geschwindigkeiten kann es durchaus sinnvoll sein, von konventionellen Spitzenformen abzuweichen oder auf außenballistische Hauben zu verzichten. Auch Stufenspitzen sind denkbar, die allein aus endballistischen Vorgaben zu dimensionieren sind, beispielsweise zum besseren Angreifen schräger/geneigter Zielflächen.In particular, for missiles or very large calibers, the exit velocity is usually low, for
Bei der in
Es ist selbstverständlich, dass komplexere Ausgestaltungen der splittergebenden Systeme in erster Linie vom Kaliber der Munition (und dort in erster Näherung mit der 3. Potenz des Kalibers) abhängen. Während die grundlegende Idee der vorliegenden Erfindung je nach technischem Aufwand bereits auch bei kleineren Kalibern bzw. Geschossdurchmessern durchaus sinnvoll sein kann, bleiben aufwendigere Lösungen mittleren und vor allem größeren Kalibern (ab 60 mm) oder großen Kalibern (ab 90 mm) vorbehalten.It is self-evident that more complex designs of the splintering systems depend primarily on the caliber of the ammunition (and there in the first approximation with the third power of the caliber). While the basic idea of the present invention, even with smaller calibers or projectile diameters, may well be useful depending on the technical complexity, more complex solutions are reserved for medium and, above all, larger calibers (from 60 mm) or large calibers (from 90 mm).
In der
Ein derart hybrides, polyvalentes Wirksystem der Erfindung eignet sich neben der Beschleunigung mittels Kanonen auch in besonderer Weise zum Verbringen mittels Raketen, Flugkörper-Abwehrsystemen, gesteuerten/gelenkten Bomben oder Flugkörpern bis hin zu Marschflugkörpern. Durch den nahezu unbegrenzten Auslegungsspielraum in Verbindung mit nahezu allen bekannten Wirkmechanismen sind mit derartigen Systemen von stark gepanzerten ballistischen Zielen über großflächige und/oder tiefe Zielstrukturen wie leichtere Ziele, Flugzeuge, Schiffe sowie Bauwerke bis hin zu strategischen Objekten zu bekämpfen.Such a hybrid, polyvalent active system of the invention is in addition to the acceleration by means of cannons in a special way for the purpose of using missiles, missile defense systems, controlled / guided bombs or missiles to cruise missiles. Due to the almost unlimited scope for interpretation in connection with almost all known mechanisms of action, such systems have to combat heavily armored ballistic targets via large and / or deep target structures such as lighter targets, airplanes, ships and structures as well as strategic objects.
- 11
- drallstabilisiertes Geschoss mit Kombination Splitterkopf/ALP-Modulspin-stabilized projectile with combination splitter head / ALP module
- 22
- aerodynamisch stabilisiertes Geschoss mit Kombination Splitterkopf/ALP-ModulAerodynamically stabilized projectile with combination splitter head / ALP module
- 33
- dreiteiliges aerodynamisch stabilisiertes Geschoss mit Kombination HL-Kopf und ALP-Modul sowie KE-Modulthree-piece aerodynamically stabilized projectile with combination HL head and ALP module and KE module
- 44
- Splitter/Subgeschosse erzeugendes GehäuseSplitter / sub-floor generating housing
- 55
- Spitze / außenballistische HaubeLace / outside ballistic hood
- 66
- druckübertragendes Medium im ALP-Modulpressure-transmitting medium in the ALP module
- 7A7A
- druckerzeugendes Element / Detonator/Sprengstoff für Splitter- und ALP-Modulpressure generating element / detonator / explosive for splitter and ALP module
- 7B7B
- druckerzeugendes Element / Detonator/Sprengstoff für Splitter- und ALP-Modulpressure generating element / detonator / explosive for splitter and ALP module
- 7C7C
- druckerzeugendes Element als HL-Modulpressure-generating element as HL module
- 88th
- Auslösevorrichtung (programmiertes Teil, Sicherungs- und Auslöseteil)Trip device (programmed part, fuse and trip part)
- 99
- zylindrisches druckerzeugendes Element/Sprengschnurcylindrical pressure generating element / detonating cord
- 1010
- Übertragungsleitungtransmission line
- 1111
- Splitterbelegung von 7ASplitter assignment of 7A
- 1212
- Splitterbelegung von 7BSplitter assignment of 7B
- 1313
- HL-KopfHL-head
- 1414
- Spitze mit aktivem ZerlegemodulTip with active cutting module
- 1515
- SplittermantelFragmentation casing
- 1616
- DruckübertragungsmediumPressure transmission medium
- 1717
- pyrotechnisches Elementpyrotechnic element
- 1818
- Spitzenhülletop shell
- 1919
- massives aktives Spitzenmodulmassive active tip module
- 2020
- Hülse für druckerzeugendes ElementSleeve for pressure-generating element
- 2121
- mit Wirkmittel gefülltes Spitzenmodulfilled with active agent tip module
- 2222
- Füllung der Spitze 21Filling the top 21
- 2323
- ALP-ModulALP module
- 2424
- ALP-ModulALP module
- 2525
- ALP-Spitzenmodul mit 4 lateral wirkenden/fokussierten SplitterladungenALP tip module with 4 lateral acting / focused splinter charges
- 2626
- Splitterladungfragmentation charge
- 2727
- Sprengstoff-Zentralkörper von 25Explosive Central Body of 25
- 2828
- Raum zwischen 29 und 31Space between 29 and 31
- 2929
- Oberflächenform von 26Surface shape of 26
- 3030
- Ausbreitungsrichtungen der Splitterladungen 26Propagation directions of the fragmentation charges 26
- 3131
- Gehäusecasing
- 3232
-
ALP-Spitzenmodul mit sechs lateral wirkenden Schneidladungen 33ALP tip module with six laterally acting
cutting charges 33 - 3333
- Gehäusewand von 32Housing wall of 32
- 3434
- Sprengstoff-Zentralkörper von 32Explosive center body of 32
- 3535
- metallische Einlagemetallic insert
- 3636
- Ausbreitungsrichtungen der Schneidladungen bzw. Splitterfelder von 35Propagation directions of the cutting charges or splitter fields of 35
- 3737
- ALP-Spitzenmodul mit schräg nach vom / außen wirkenden P-LadungenALP tip module with oblique to / from the outside acting P-charges
- 3838
-
Resultierende der Ausbreitungsrichtung der umgeformten P-Ladungs-Einlage 41Resultant of the propagation direction of the reformed P-
charge insert 41 - 3939
- P-LadungP-charge
- 4040
- zentrale Sprengladungcentral explosive charge
- 4141
- metallische Einlage von 40metallic insert of 40
- 4242
- Resultierende der Ausbreitungsrichtung des SplitterfeldesResultant of the propagation direction of the splinter field
- 43A43A
-
Splittertasche mit Splitterladung 26Splinter bag with
splinter load 26 - 43B43B
- Splitterladungfragmentation charge
- 4444
- ALP-Spitzenmodul mit schräg nach vom / außen wirkenden Splitterladungen 43BALP tip module with slanted forward / outward splinter charges 43B
- 4545
- Beispiel für ALP-Spitzenmodul mit vornehmlich axial wirkendem SplitterkegelExample of ALP tip module with primarily axial splinter cone
- 4646
- Beispiel für ALP-Spitzenmodul mit vornehmlich radial wirkenden SplitternExample of ALP tip module with primarily radially acting splinters
- 4747
- Splitterbelegungensplitter assignments
- 4848
- außenballistische Haubeoutside ballistic hood
- 4949
- Beschleunigungsladung für 47 bzw. 54Acceleration charge for 47 or 54
- 5050
- Splitterhülle nach ALP- PrinzipSplinter shell according to ALP principle
- 5151
- DruckübertragungsmediumPressure transmission medium
- 5252
- Trenn- / Dämpfungs- / VerzögerungselementSeparation / damping / delay element
- 5353
- Ausbreitungsrichtungen von 47Propagation directions of 47
- 5454
- radial wirkende Splitterladungradially acting splinter charge
- 5555
- Ausbreitungsrichtungen von 54Propagation directions of 54
- 5656
- Beispiel für ALP-Spitzenmodul mit SplitterkopfExample of ALP tip module with splitter head
- 5757
- Beispiel für ALP-Spitzenmodul mit SplitterkopfExample of ALP tip module with splitter head
- 5858
- außenballistische Haube von 56, 57outside ballistic hood of 56, 57
- 5959
- Wirkmittel-Füllung von 58Active agent filling of 58
- 6060
- Ausbreitungsrichtungen der Splitter von 61Propagation directions of the splinters of 61
- 6161
- Splitterladungfragmentation charge
- 6262
- pyrotechnische Ladungpyrotechnic charge
- 6363
- verdämmendes Medium (auch mit eingebetteten Splittern)Damming medium (also with embedded splinters)
- 6464
- Oberflächenform von 62Surface shape of 62
- 6565
- ALP-Spitzenmodule mit vorgeschalteter/integrierter HL- oder P-LadungALP tip modules with upstream / integrated HL or P charge
- 6666
-
Ausbreitungsrichtung des vom Kegel 65 gebildeten Projektils/StrahlsPropagation direction of the projectile / beam formed by the
cone 65 - 6767
- Sprengstoffexplosive
- 6868
- Kegel / EinlageCone / insert
- 6969
-
Ausbreitungsrichtung 71 der Wirkelemente 74
Propagation direction 71 of theactive elements 74 - 7070
- druckübertragendes Mediumpressure transmitting medium
- 7171
- P-Ladungs-EinlageP-charge insert
- 7373
- P-Ladungs-ProjektilP-charge projectile
- 7474
- scheiben- oder tellerförmiges Element/Auflagedisk-shaped or plate-shaped element / support
- 7575
- Hülle / Mantel für 8Sheath / Coat for 8
- 7676
- konischer Splittermantelconical splinter coat
- 7777
- Schutzkappe für 78Protective cap for 78
- 7878
- Kerncore
- 7979
- Beispiel für modulares Geschoss mit Splitterteil und HartkernspitzeExample of modular projectile with fragment part and hard core tip
- 8080
- Hartkern oder Schwermetall-KernHard core or heavy metal core
- 8181
- Splittersplinter
- 8282
- pyrotechnische Einheit für Splitterbeschleunigungpyrotechnic unit for splinter acceleration
- 8383
-
Rückseite des Kerns 80Back of the
core 80 - 8484
-
bevorzugte Splitterausbreitungsrichtung der Belegung 81preferred splitter propagation direction of
occupancy 81 - 8585
- Beispiel für Geschoss oder Geschosskopf mit mehrstufigem SplitterteilExample of projectile or projectile head with multistage fragment part
- 8686
- erste pyrotechnische Einheit von 85first pyrotechnic unit of 85
- 8787
- zweite pyrotechnische Einheit von 85second pyrotechnic unit of 85
- 8888
- Splitterbelegung von 86Splinter assignment of 86
- 8989
- Splitterbelegung von 87Splinter assignment of 87
- 9090
-
resultierende Splitterausbreitung der Belegung 88resulting splitter propagation of
occupancy 88 - 9191
-
resultierende Splitterausbreitung der Belegung 89resulting splitter propagation of
occupancy 89 - 9292
-
resultierende Splitterausbreitung des ALP-Mantels 4resulting splitter propagation of the
ALP jacket 4 - 9393
- Beispiel für richtungsgesteuerte SplitterbeschleunigungExample of directional splinter acceleration
- 9494
- TrennflächenPartitions
- 9595
- Splitterkammer bzw. partielle SplitterbelegungSplinter chamber or partial splinter assignment
- 9696
-
resultierende Ausbreitung der Splitter 95resulting spread of
splinters 95 - 9797
- modulares Geschoss mit Splitterkopf, Kern und PELE-Modulmodular projectile with fragment head, core and PELE module
- 9898
- Hart- oder Schwermetall-KernHard or heavy metal core
- 9999
- Geschossbeispiel mit Splitterkopf, ALP-Modul und KernBullet example with fragment head, ALP module and core
- 100100
- Kern/KE-ModulCore / KE module
- 104104
-
richtungsgesteuerte Splitterladung mit seitlicher starker Verdämmung 109Direction-controlled fragmentation load with lateral
strong damming 109 - 105105
- pyrotechnisches Mediumpyrotechnic medium
- 106106
- Splitterbelegungsplitter occupancy
- 107107
- Innenkonus von 105Inner cone of 105
- 108108
- Zündladungsquib
- 108A108A
- ringförmige Zündladungannular ignition charge
- 109109
- äußere Verdämmungouter damming
- 110110
- Wand/GeschosshülleWall / floor envelope
- 111111
-
richtungsgesteuerte Splitterladung mit hinterem Inertkörper 112direction-controlled splinter charge with rear
inert body 112 - 112112
- Inertkörper für StosswellenlenkungInert body for shock wave steering
- 113113
- Außenkonus von 105Outer cone of 105
- 114114
-
richtungsgesteuerte Splitterladung mit vorderem Inertkörper 115Direction-controlled splinter charge with front
inert body 115 - 115A115A
- vorderer Inertkörper mit Innenkegel zur Stosswellenlenkungfront inert body with inner cone for shock wave steering
- 115B115B
- vorderer Außenkonus zur Stosswellenlenkungfront outer cone for shock wave guidance
- 116116
- richtungsgesteuerte Splitterladung mit DetonationswellenlenkungDirection-controlled splinter charge with detonation wave steering
- 117117
- Innenkörper zur StoßwellenlenkungInner body for shock wave steering
- 118118
- richtungsgesteuerte Splitterladung mit Inertkörper und MehrfachzündladungDirection-controlled splinter charge with inert body and multiple ignition charge
- 119119
- Trennung der Zündladungen 108Separation of the ignition charges 108
- 120120
- richtungsgesteuerte Splitterladung mit Kammern und DetonationswellenlenkungDirection-controlled fragmentation charge with chambers and detonation shaft steering
- 121121
- Beschleunigungsladung / ZünderAcceleration charge / detonator
- 122122
- Inertkörper zur inneren StoßwellenlenkungInert body for internal shock wave steering
- 123123
- Inertkörper zur äußeren StoßwellenlenkungInert body for external shock wave steering
- 124124
- Geschoss mit Splitter- und ALP-ModulProjectile with splinter and ALP module
- 125125
- splittergefüllte Spitzesplinter filled tip
- 125A125A
- resultierender Pfeil für Masse und Geschwindigkeit von 125resulting arrow for mass and speed of 125
- 126126
- pyrotechnische Einheitpyrotechnic unit
- 127127
- Splitterkammersplitter chamber
- 128128
- Splittersplinter
- 129129
- Matrixmaterial zwischen 128Matrix material between 128
- 130A130A
- resultierende Splitterausbreitungsrichtungen von 4resulting splitter propagation directions of 4
- 130B130B
- resultierende Splitterausbreitungsrichtungen von 4resulting splitter propagation directions of 4
- 131131
- vornehmlich radiale Splitterausbreitungsrichtung von 128primarily radial splinter propagation direction of 128
- 132132
- vornehmlich axiale Splitterausbreitungsrichtung von 128primarily axial splinter propagation direction of 128
- 133133
- Geschoss mit P-Ladungskopf und Kern mit ZerlegerladungProjectile with P-charge head and core with burster charge
- 134134
- Kern mit BohrungCore with hole
- 135135
- Zerlegerladung für 134Burster charge for 134
- 136136
- Geschoss/Gefechtskopf mit StrahlfokussierungProjectile / warhead with beam focusing
- 137137
- Vorrichtung zur StrahlfokussierungDevice for beam focusing
- 138138
- trompetenförmige Einlagetrumpet-shaped insert
- 139139
- Kanal für HL-StrahlChannel for HL-beam
- 140140
- viergeteilter Penetratorfour-part penetrator
- 141141
- zentrales pyrotechnisches Elementcentral pyrotechnic element
- 142142
-
Segment des KE-Penetrators 140Segment of
KE penetrator 140 - 143143
- resultierender Pfeil für 142resulting arrow for 142
- 144144
- Geschoss mit Splitterkopf und ALP-Modul mit zentralem PenetratorProjectile with fragment head and ALP module with central penetrator
- 145145
- zentraler Penetrator hohen Schlankheitsgradescentral penetrator of high slenderness
- 146146
- Schockdämpfung für 145Shock absorption for 145
- 147147
-
Geschoss mit Splitterkopf und mehrteiligem/zusammengesetztem Kern 148Projectile with fragment head and multipart /
compound core 148 - 148148
- zusammengesetzter Kerncomposite core
- 149149
- Hartmetall-Kernspitze/vorderer KernteilCarbide core point / front core part
- 150150
- Schwermetall - Kernschaft / hinterer KernteilHeavy metal - core shaft / rear core part
- 151151
- Verbindung zwischen 149 und 150Connection between 149 and 150
- 152152
- Geschoss mit Splitterkopf und hülsengeschütztem KernBullet with fragment head and sleeve-protected core
- 153153
- Kernhülsecore sleeve
- 154154
- Kernschaftcore shaft
- 155155
- Geschoss mit Splitterkopf und mehrteiligem/segmentiertem KernProjectile with fragment head and multipart / segmented core
- 156156
- mehrteiliger/segmentierter Kernmulti-part / segmented core
- 157157
- Einzelkern mit geringem L/D-VerhältnisSingle core with low L / D ratio
- 158158
- Einzelkem mit mittlerem L/D-VerhältnisSingle core with medium L / D ratio
- 159159
- Zwischenscheibewasher
- 160160
- Zwischenpufferintermediate buffer
- 161161
-
Geschoss mit Splitterkopf, zentralem Penetrator 162 und Splitterscheiben 163Bullet with fragment head,
central penetrator 162 andsplinter disks 163 - 162162
- zentraler Penetratorcentral penetrator
- 163163
- Splitterscheibesplitter plate
- 164164
- pyrotechnische Scheibenpyrotechnic discs
- 165165
- Hülseshell
- 166166
- Geschoss mit zentralem Penetrator, massiver Spitze, Splitterscheiben und ALP-ModulBullet with central penetrator, solid tip, splitter discs and ALP module
- 167167
- massive Spitzemassive top
- 168168
- Geschoss mit durchgehendem zentralen Penetrator, ALP-Modul und kegeligen SplitterscheibenBullet with continuous central penetrator, ALP module and conical splitter discs
- 169169
- durchgehender zentraler Penetratorcontinuous central penetrator
- 170170
- beschleunigendes Element des ALP-Modulsaccelerating element of the ALP module
- 171171
- konische Splitterscheiben/Ringsegmenteconical splitter disks / ring segments
- 172172
- beschleunigte pyrotechnische Scheiben für 171accelerated pyrotechnic disks for 171
- 173173
- resultierender Pfeilresulting arrow
- 174174
- Spitze von 169Top of 169
- 175175
-
Geschossquerschnitt mit sechseckigem Penetrator, Scheibensegmenten / Flächensegmenten und Hülle 178Bullet cross section with hexagonal penetrator, disk segments / surface segments and
shell 178 - 176176
- Scheibensegment/FlächensegmentDisk segment / surface segment
- 177177
- zentraler sechseckiger Penetratorcentral hexagonal penetrator
- 178178
- Außenring/HülleOuter ring / shell
- 179179
- Geschoss ohne außenballistische Haube mit Splitterscheiben und ALP-ModulProjectile without outer ballistic hood with splinter disks and ALP module
- 180180
- konische Scheibenconical disks
- 181181
- pyrotechnische Elementepyrotechnic elements
Claims (42)
- A hybrid polyvalent projectile or hybrid polyvalent warhead, comprising: a first projectile portion for delivering active means (11), said active means being disposed in the nose (5) or in a region near the nose of the projectile or warhead, and a second projectile portion, wherein
a pyrotechnic means (7) both for triggering said active means in said first projectile portion and also for building up a pressure field is provided between said first projectile portion and said second projectile portion; and
said second projectile portion comprises a terminal-ballistically operative casing (4),
characterized in that
said second projectile portion further comprises an inert pressure transmission medium (6) provided within said casing, for merely transmitting the pressure filed built up by said pyrotechnic means (7) tto said casing (4); and
a plurality of successively or laterally arranged first projectile portions is provided. - The projectile or warhead according to claim 1, wherein said first projectile portion and/or said second projectile portion are in the form of modules.
- The projectile or warhead according to claim 2, wherein said first projectile portion and/or said second projectile portion are in the form of exchangeable modules.
- The projectile or warhead according to any one of claims 1 to 3, wherein said first projectile portion contains as the active means (11) an explosive (blast, fragmentation, HC or P) charge or a combination thereof.
- The projectile or warhead according to any one of claims 1 to 4,wherein a directional control means (108, 112, 115, 117) of said active means (106) is integrated therein.
- The projectile or warhead according to claim 5, wherein the directional control (112, 115, 117) of said active means (106) is effected by way of a shock wave guidance.
- The projectile or warhead according to claim 5, wherein the directional control (108) of said active means (106) is carried out by means of an asymmetrical firing of the acceleration charge.
- The projectile or warhead according to claim 5, wherein the directional control of said active means is carried out by means of a structural segmentation.
- The projectile or warhead according to any one of claims 1 to 8, wherein spherically, cuboidally or cylindrically shaped active means (11) of equal or different sizes of the same or different materials are accelerated out of said first projectile portion.
- The projectile or warhead according to any one of claims 1 to 9, wherein plate-shaped, ring-shaped, disk-shaped or areally elements (74) of any contour are accelerated out of said first projectile portion in axial direction or predominantly axial direction.
- The projectile or warhead according to any one of claims 4 to 10, wherein said active means are predominantly axially ejected from a container or a fragment pocket (127).
- The projectile or warhead according to claim 10, wherein said active means (128) are embedded in a matrix or supported against each other upon acceleration.
- The projectile or warhead according to any one of claims 4 to 12, wherein one or more disk-shaped active means (171) which consist of equal or different materials or contain reacting / pressure-producing intermediate layers are predominantly axially accelerated.
- The projectile or warhead according to any one of claims 1 to 13, wherein said pyrotechnic means (7) comprises a plurality of pressure-producing elements (86, 87).
- The projectile or warhead according to claim 14, whereinsaid pressure-producing elements (86, 87) of said pyrotechnic means (7) are provided with a position or time-controlled safety and/or firing system or connected thereto.
- The projectile or warhead according to claim 14 or 15, wherein said pressure-producing elements (86, 87) of said pyrotechnic means (7) are controlled or actuated separately or are connected together by means of a signal transmission line, by means of fuse cord means or by way of a radio signal.
- The projectile or warhead according to any one of claims 1 to 16, wherein the triggering of said pyrotechnic means (7) is provided in form of a triggering device (8) working in a time-programmed fashion, by means of contact, mechanically, optically, electronically, by radio and/or by radar.
- The projectile or warhead according to claim 17, wherein said triggering devicve (8) is triggerable by a time-controlled signal upon launch or during the flight phase or by a signal upon impact, upon penetration or in the interior of a target structure.
- The projectile or warhead according to claim 17, wherein said triggering device (8) is controlled by a target guidance system and/or a target recognition system.
- The projectile or warhead according to any one of claims 1 to 19, wherein said active means (11) are triggered simultaneously or in time-displaced relationship.
- The projectile or warhead according to any one of claims 1 to 20, wherein said second projectile portion is combined with a PELE projectile portion.
- The projectile or warhead according to any one of claims 1 to 21, wherein said second projectile portion includes at least one central penetrator (145, 162, 169).
- The projectile or warhead according to claim 22, wherein a part of said penetrator represents a pure fragmentation component.
- The projectile or warhead according to claim 22 or 23, wherein said central penetrator is in the form of a separating, radially segmented element.
- The projectile or warhead according to any one of claims 1 to 24, wherein said terminal-ballistically operative casing (4) of said second projectile portion consists of a homogeneous material, preformed fragments, sub-projectiles or independently operative penetrators.
- The projectile or warhead according to any one of claims 1 to 25, wherein different configurations are provided over the periphery and/or over the length.
- The projectile or warhead according to any one of claims 1 to 26, wherein further operative components (sub-projectiles, fragment pockets, liquid or solid active means) are additionally included.
- The projectile or warhead according to any one of claims 1 to 27, further comprising a cylindrical penetrator (150), a core or a core tip (149) made from steel, hard metal and heavy metal.
- The projectile of warhead according to claim 28, wherein said core / said core tip (149) has a shock-reducing cap / hood.
- The projectile or warhead according to claim 28 or 29, wherein said penetrator, said core or said core tip consists of a combination of different materials.
- The projectile or warhead according to any one of claims 28 to 30, further comprising a stepped tip, an ogival or conical tip or an external-ballistic hood.
- The projectile or warhead according to claim 31, wherein an axially leading active component is focussed by the nose.
- The projectile or warhead according to any one of claims 1 to 32, which is spin stabilised or aerodynamically stabilised.
- The projectile or warhead according to any one of claims 1 to 33, which is combined with an explosive projectile.
- The projectile or warhead according to any one of claims 1 to 34, which is combined with a weight projectile made from steel, heavy metal or hard metal.
- The projectile or warhead according to claim 28 or 35, wherein said weight projectile or said module being inertly operating, homogenous or axially or radially segmented includes a self-destructing means.
- The projectile or warhead according to any one of claims 1 to 36, which is combined with a guided or final phase-controlled system.
- The projectile or warhead according to any one of claims 1 to 37, which includes a safety self-destructing means.
- The projectile or warhead according to any one of claims 1 to 38, which is integrated into a missile or a rocket.
- The projectile or warhead according to any one of claims 1 to 39, wherein active components according to any one of preceding claims are ejected from a system such as a penetrator, projectile, container, warhead or rocket.
- The projectile or warhead according to any one of claims 1 to 38, which can be accelerated or ejected by means of a rocket drive / a booster.
- The projectile or warhead according to any one of claims 1 to 38, which is integrated into an underwater warhead or a high-velocity torpedo.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP03730148A EP1516153B1 (en) | 2002-06-26 | 2003-06-03 | Projectile or warhead |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP02014007 | 2002-06-26 | ||
EP02014007 | 2002-06-26 | ||
EP03730148A EP1516153B1 (en) | 2002-06-26 | 2003-06-03 | Projectile or warhead |
PCT/EP2003/005792 WO2004003460A1 (en) | 2002-06-26 | 2003-06-03 | Projectile or warhead |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1516153A1 EP1516153A1 (en) | 2005-03-23 |
EP1516153B1 true EP1516153B1 (en) | 2011-12-21 |
Family
ID=29797136
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP03730148A Expired - Lifetime EP1516153B1 (en) | 2002-06-26 | 2003-06-03 | Projectile or warhead |
Country Status (8)
Country | Link |
---|---|
US (2) | US20040069176A1 (en) |
EP (1) | EP1516153B1 (en) |
AT (1) | ATE538359T1 (en) |
AU (1) | AU2003240740A1 (en) |
ES (1) | ES2379546T3 (en) |
NO (1) | NO332833B1 (en) |
PT (1) | PT1516153E (en) |
WO (1) | WO2004003460A1 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2522178C1 (en) * | 2013-03-13 | 2014-07-10 | Открытое акционерное общество "Научно-производственное объединение "СПЛАВ" | Jet projectile warhead |
DE102012012409B4 (en) * | 2012-06-25 | 2015-05-13 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Penetrator with a shaped charge |
DE102020120850A1 (en) | 2020-08-07 | 2022-02-10 | Rheinmetall Waffe Munition Gmbh | Process for the production of a thermally stable empennage and corresponding empennage |
Families Citing this family (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8414718B2 (en) * | 2004-01-14 | 2013-04-09 | Lockheed Martin Corporation | Energetic material composition |
US20090320711A1 (en) * | 2004-11-29 | 2009-12-31 | Lloyd Richard M | Munition |
US7503259B2 (en) * | 2005-02-15 | 2009-03-17 | Lockheed Martin Corporation | Anti-submarine warfare cluster munitions and cluster depth charges |
WO2008097241A2 (en) * | 2006-05-30 | 2008-08-14 | Lockheed Martin Corporation | Selectable effect warhead |
US8250985B2 (en) * | 2006-06-06 | 2012-08-28 | Lockheed Martin Corporation | Structural metallic binders for reactive fragmentation weapons |
FR2912211B1 (en) * | 2007-02-05 | 2009-10-23 | Nexter Munitions Sa | PROJECTILE INCORPORATING A FLAT GENERATOR |
US7506587B1 (en) | 2007-02-20 | 2009-03-24 | The United States Of Americas As Represented By The Secretary Of The Navy | Modular projectile system |
IL195003A (en) * | 2008-10-30 | 2013-12-31 | Rafael Advanced Defense Sys | Artllery projectile with separately controlled booster actuation and fragment dispersion |
GB0903404D0 (en) | 2009-03-02 | 2009-04-08 | Rolls Royce Plc | Surface profile evaluation |
JP5461059B2 (en) * | 2009-05-07 | 2014-04-02 | 株式会社Ihiエアロスペース | Ammunition system |
DE102009050162A1 (en) * | 2009-10-21 | 2011-04-28 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Damping device for mounting parts in penetrators |
CZ306529B6 (en) * | 2010-07-12 | 2017-03-01 | Explosia A.S. | A projectile with a tubular penetrator |
DE102010053896A1 (en) * | 2010-12-09 | 2012-06-14 | Lfk-Lenkflugkörpersysteme Gmbh | Target engagement system |
RU2462683C2 (en) * | 2011-01-11 | 2012-09-27 | Александр Иванович Голодяев | Blaster |
RU2466347C2 (en) * | 2011-01-11 | 2012-11-10 | Александр Иванович Голодяев | Explosive device - shell |
RU2463283C2 (en) * | 2011-03-16 | 2012-10-10 | Александр Иванович Голодяев | Device made from metal hydride for ammunition |
RU2454624C2 (en) * | 2011-04-07 | 2012-06-27 | Александр Иванович Голодяев | Warhead of shell (rocket) |
RU2486436C1 (en) * | 2012-02-21 | 2013-06-27 | Николай Евгеньевич Староверов | Staroverov's shot - 7 (versions) |
RU2486432C1 (en) * | 2012-02-21 | 2013-06-27 | Николай Евгеньевич Староверов | Staroverov's shot - 4 (versions) |
RU2486434C1 (en) * | 2012-02-21 | 2013-06-27 | Николай Евгеньевич Староверов | Staroverov's shot - 5 (versions) |
RU2498202C1 (en) * | 2012-03-22 | 2013-11-10 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Московский государственный технический университет имени Н.Э. Баумана" (МГТУ им. Н.Э. Баумана) | Fragmentation-beam barrel projectile "tverityanka-2" with ejected throwing unit |
US8943971B1 (en) | 2012-08-03 | 2015-02-03 | The United States Of America As Represented By The Secretary Of The Navy | Compounded high explosive composites for impact mitigation |
RU2516938C1 (en) * | 2012-10-10 | 2014-05-20 | Шепеленко Виталий Борисович | Jet round with optical target sensor |
RU2520191C1 (en) * | 2012-12-28 | 2014-06-20 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Московский государственный технический университет имени Н.Э. Баумана" (МГТУ им. Н.Э. Баумана) | Light shell of close-range weapon (mining, infantry) |
US9212876B1 (en) * | 2013-08-30 | 2015-12-15 | The United States Of America As Represented By The Secretary Of The Army | Large caliber frangible projectile |
DE102014019202A1 (en) | 2014-12-19 | 2016-06-23 | Diehl Bgt Defence Gmbh & Co. Kg | bullet |
EP3414513B1 (en) * | 2016-01-15 | 2021-09-29 | Saab Bofors Dynamics Switzerland Ltd. | Warhead |
DE102017105565A1 (en) * | 2017-03-15 | 2018-09-20 | Rheinmetall Waffe Munition Gmbh | Ammunition and logistics concept for in particular artillery projectiles |
DE102017106526A1 (en) * | 2017-03-27 | 2018-10-11 | Rheinmetall Waffe Munition Gmbh | Bullet, especially in the middle caliber range |
US10502537B1 (en) * | 2017-10-20 | 2019-12-10 | The United States Of America As Represented By The Secretary Of The Army | Enhanced terminal performance medium caliber multipurpose traced self-destruct projectile |
RU2692116C1 (en) * | 2018-09-06 | 2019-06-21 | Российская Федерация, от имени которой выступает Государственная корпорация по атомной энергии "Росатом" (Госкорпорация "Росатом") | Method of determining throwing object speed |
DE102019201176A1 (en) * | 2019-01-30 | 2020-07-30 | Atlas Elektronik Gmbh | Ordnance with a deflagration primer and method for operating such an ordnance |
CN109764771A (en) * | 2019-03-19 | 2019-05-17 | 吉林大学 | The body structure of metal incendiary composition filling |
US11248891B2 (en) * | 2019-06-12 | 2022-02-15 | Insights International Holdings, Llc | Ordnance ballistics deployment system |
DE102019126604A1 (en) | 2019-10-02 | 2021-04-08 | Rheinmetall Waffe Munition Gmbh | Penetrator, use of a penetrator and bullet |
US11644289B2 (en) * | 2021-09-28 | 2023-05-09 | Insights International Holdings, Llc | Ordnance delivery system using a protective housing as an antenna |
Family Cites Families (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1236736A (en) * | 1916-03-17 | 1917-08-14 | Thomas S Miller | Explosive device. |
US3145656A (en) * | 1959-08-14 | 1964-08-25 | Melvin A Cook | Explosive warhead |
US3298308A (en) * | 1960-11-11 | 1967-01-17 | Aerojet General Co | Composite casing for fragmentationtype explosive weapon and method of forming same |
US3703865A (en) * | 1968-02-28 | 1972-11-28 | Us Navy | Electronically controlled aimed blast warhead |
US3980019A (en) * | 1970-04-30 | 1976-09-14 | The United States Of America As Represented By The Secretary Of The Navy | Adaptive ordnance system |
DE2308912C3 (en) * | 1973-02-23 | 1981-01-08 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Electric ignition system for the explosive charge of a warhead or the like |
US3906860A (en) * | 1974-06-04 | 1975-09-23 | Us Army | Dual purpose projectile |
CH655473B (en) * | 1980-09-29 | 1986-04-30 | Eidgenoess Flugzeugwerk Emmen | |
DE3224704A1 (en) * | 1982-07-02 | 1984-01-05 | Rheinmetall GmbH, 4000 Düsseldorf | EXPLOSIVE FLOOR WITH A SINGLE OR MULTILAYERED EXTERNAL COVER |
US4714020A (en) * | 1987-01-30 | 1987-12-22 | Honeywell Inc. | Enabling device for a gas generator of a forced dispersion munitions dispenser |
DE3736842A1 (en) * | 1987-10-30 | 1989-05-11 | Diehl Gmbh & Co | BLASTING BULLET WITH A BULLET BODY |
CH680750A5 (en) * | 1989-12-06 | 1992-10-30 | Eidgenoess Munitionsfab Thun | |
US5014623A (en) * | 1989-10-03 | 1991-05-14 | The United States Of America As Represented By The Secretary Of The Army | Binary munition system |
FR2652892A1 (en) * | 1989-10-11 | 1991-04-12 | Dynamit Nobel Ag | MILITARY HEAD WITH ENHANCED RADIANCE EFFECT. |
US5078069A (en) * | 1990-03-27 | 1992-01-07 | Hughes Aircraft Company | Warhead |
US5229542A (en) * | 1992-03-27 | 1993-07-20 | The United States Of America As Represented By The United States Department Of Energy | Selectable fragmentation warhead |
GB2302395A (en) * | 1995-06-16 | 1997-01-15 | Numerica Limited | Grenade |
DE19648355A1 (en) * | 1996-11-22 | 1999-07-15 | Diehl Stiftung & Co | Artillery shell for shrapnel production |
DE19700349C2 (en) | 1997-01-08 | 2002-02-07 | Futurtec Ag | Missile or warhead to fight armored targets |
EP0950870B1 (en) * | 1998-04-18 | 2003-12-03 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Combination type warhead |
DK1316774T3 (en) | 2001-11-28 | 2006-10-09 | Rheinmetall Waffe Munition | Projectiles with high penetration and lateral effect with integrated disintegration device |
US6983699B1 (en) * | 2003-03-20 | 2006-01-10 | The United States Of America As Represented By The Secretary Of The Army | Explosive fragmentation munition |
-
2003
- 2003-06-03 WO PCT/EP2003/005792 patent/WO2004003460A1/en not_active Application Discontinuation
- 2003-06-03 EP EP03730148A patent/EP1516153B1/en not_active Expired - Lifetime
- 2003-06-03 AU AU2003240740A patent/AU2003240740A1/en not_active Abandoned
- 2003-06-03 ES ES03730148T patent/ES2379546T3/en not_active Expired - Lifetime
- 2003-06-03 AT AT03730148T patent/ATE538359T1/en active
- 2003-06-03 PT PT03730148T patent/PT1516153E/en unknown
- 2003-06-25 US US10/603,370 patent/US20040069176A1/en not_active Abandoned
-
2005
- 2005-01-18 NO NO20050278A patent/NO332833B1/en not_active IP Right Cessation
- 2005-08-05 US US11/198,144 patent/US20070006766A1/en not_active Abandoned
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102012012409B4 (en) * | 2012-06-25 | 2015-05-13 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Penetrator with a shaped charge |
RU2522178C1 (en) * | 2013-03-13 | 2014-07-10 | Открытое акционерное общество "Научно-производственное объединение "СПЛАВ" | Jet projectile warhead |
DE102020120850A1 (en) | 2020-08-07 | 2022-02-10 | Rheinmetall Waffe Munition Gmbh | Process for the production of a thermally stable empennage and corresponding empennage |
DE102020120850B4 (en) | 2020-08-07 | 2022-06-15 | Rheinmetall Waffe Munition Gmbh | Process for the production of a thermally stable empennage and corresponding empennage |
Also Published As
Publication number | Publication date |
---|---|
US20040069176A1 (en) | 2004-04-15 |
US20070006766A1 (en) | 2007-01-11 |
NO332833B1 (en) | 2013-01-21 |
WO2004003460A1 (en) | 2004-01-08 |
NO20050278L (en) | 2005-01-18 |
ATE538359T1 (en) | 2012-01-15 |
ES2379546T3 (en) | 2012-04-27 |
PT1516153E (en) | 2012-03-30 |
EP1516153A1 (en) | 2005-03-23 |
AU2003240740A1 (en) | 2004-01-19 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP1516153B1 (en) | Projectile or warhead | |
EP1316774B1 (en) | High penetration and lateral effect projectiles having an integrated fragment generator | |
EP1000311B1 (en) | Projectile or warhead | |
DE69605539T2 (en) | DOUBLE ACTING EXPLOSION HEAD AND METHOD FOR OPERATING SUCH A HEAD OF HEAVEN | |
US4970960A (en) | Anti-material projectile | |
EP0238818B1 (en) | Sub-calibre projectile using kinetic energy | |
EP1893935B1 (en) | Projectile or warhead | |
DE19524726B4 (en) | warhead | |
EP3171121A1 (en) | Multi-warhead munition with configurable segmented warhead | |
DE60117020T2 (en) | DEVICE AND METHOD FOR SPREADING SUBMUNITION BODIES | |
EP0955517A1 (en) | Ammunition with multiple warheads | |
EP2024706B1 (en) | Projectile, active body or warhead for fighting massive, structured and planar targets | |
DE19917144B4 (en) | Combination action system | |
DE102019007104B3 (en) | Fragmentation warhead for a missile | |
EP1411317B1 (en) | Fragment projectile | |
DE3920016C2 (en) | ||
DE1811331C3 (en) | PaiYLeta cattle storey | |
DE102012021671A1 (en) | Warhead for combating arms-carrying missile in encounter situation, has annular arrangement of radially acting hollow charges, which is arranged on periphery of warhead, where hollow charges are initiated by central ignition device | |
Held | Threats to military transport aircraft: A technical review | |
DD301023A7 (en) | Armor piercing shaped charge explosive device with boost charge |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 20041118 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR |
|
AX | Request for extension of the european patent |
Extension state: AL LT LV MK |
|
DAX | Request for extension of the european patent (deleted) | ||
17Q | First examination report despatched |
Effective date: 20080618 |
|
GRAJ | Information related to disapproval of communication of intention to grant by the applicant or resumption of examination proceedings by the epo deleted |
Free format text: ORIGINAL CODE: EPIDOSDIGR1 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PT RO SE SI SK TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 538359 Country of ref document: AT Kind code of ref document: T Effective date: 20120115 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 50314130 Country of ref document: DE Effective date: 20120308 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: NV Representative=s name: HEPP WENGER RYFFEL AG |
|
REG | Reference to a national code |
Ref country code: SE Ref legal event code: TRGR |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: T3 |
|
REG | Reference to a national code |
Ref country code: PT Ref legal event code: SC4A Free format text: AVAILABILITY OF NATIONAL TRANSLATION Effective date: 20120320 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FG2A Ref document number: 2379546 Country of ref document: ES Kind code of ref document: T3 Effective date: 20120427 |
|
REG | Reference to a national code |
Ref country code: GR Ref legal event code: EP Ref document number: 20120400637 Country of ref document: GR Effective date: 20120417 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20111221 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20111221 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FD4D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20111221 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20111221 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20111221 Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20120321 Ref country code: IE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20111221 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20111221 |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20111221 |
|
26N | No opposition filed |
Effective date: 20120924 |
|
BERE | Be: lapsed |
Owner name: GEKE TECHNOLOGIE G.M.B.H. Effective date: 20120630 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 50314130 Country of ref document: DE Effective date: 20120924 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20120630 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20120630 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20111221 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20120603 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R082 Ref document number: 50314130 Country of ref document: DE Representative=s name: PRUEFER & PARTNER GBR, DE Ref country code: DE Ref legal event code: R082 Ref document number: 50314130 Country of ref document: DE Ref country code: DE Ref legal event code: R082 Ref document number: 50314130 Country of ref document: DE Representative=s name: PRUEFER & PARTNER MBB PATENTANWAELTE RECHTSANW, DE Ref country code: DE Ref legal event code: R082 Ref document number: 50314130 Country of ref document: DE Representative=s name: PAGE, WHITE & FARRER GERMANY LLP, DE |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20030603 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: PT Payment date: 20140602 Year of fee payment: 12 Ref country code: GR Payment date: 20140627 Year of fee payment: 12 Ref country code: AT Payment date: 20140627 Year of fee payment: 12 |
|
REG | Reference to a national code |
Ref country code: PT Ref legal event code: MM4A Free format text: LAPSE DUE TO NON-PAYMENT OF FEES Effective date: 20151203 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 538359 Country of ref document: AT Kind code of ref document: T Effective date: 20150603 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20151203 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20150603 Ref country code: GR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20160112 |
|
REG | Reference to a national code |
Ref country code: GR Ref legal event code: ML Ref document number: 20120400637 Country of ref document: GR Effective date: 20160112 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 14 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 15 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 20170626 Year of fee payment: 15 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: SE Payment date: 20170626 Year of fee payment: 15 Ref country code: NL Payment date: 20170621 Year of fee payment: 15 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: TR Payment date: 20170623 Year of fee payment: 15 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: IT Payment date: 20170628 Year of fee payment: 15 Ref country code: ES Payment date: 20170703 Year of fee payment: 15 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R082 Ref document number: 50314130 Country of ref document: DE Representative=s name: PAGE, WHITE & FARRER GERMANY LLP, DE Ref country code: DE Ref legal event code: R082 Ref document number: 50314130 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 16 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20180621 Year of fee payment: 16 Ref country code: CH Payment date: 20180629 Year of fee payment: 16 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20180621 Year of fee payment: 16 |
|
REG | Reference to a national code |
Ref country code: SE Ref legal event code: EUG |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20180604 |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MM Effective date: 20180701 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20180603 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: NL Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20180701 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20180603 Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20180603 |
|
REG | Reference to a national code |
Ref country code: ES Ref legal event code: FD2A Effective date: 20190916 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20180604 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R119 Ref document number: 50314130 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20200101 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190630 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190630 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20190630 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20180603 |