EP1893935B1 - Projectile or warhead - Google Patents
Projectile or warhead Download PDFInfo
- Publication number
- EP1893935B1 EP1893935B1 EP05763381A EP05763381A EP1893935B1 EP 1893935 B1 EP1893935 B1 EP 1893935B1 EP 05763381 A EP05763381 A EP 05763381A EP 05763381 A EP05763381 A EP 05763381A EP 1893935 B1 EP1893935 B1 EP 1893935B1
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- EP
- European Patent Office
- Prior art keywords
- explosive
- layer
- projectile
- damming
- shell
- 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.)
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- 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
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- 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
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- 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
- F42B12/208—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 a plurality of charges within a single high explosive warhead
Definitions
- the present invention relates to a fragment or sub-projectile projectile or warhead.
- Explosive projectiles are used to achieve end-ballistic effects with areal easy targets, regardless of the impact velocity of a projectile or warhead by means of explosive-accelerated splinters with a high initial velocity.
- Such explosive projectiles are characterized in that their volume is taken up for the most part by explosives.
- projectiles or explosives-filled warheads contain a relatively large mass of explosives, which is not effective to a considerable extent or partially for physical reasons can not be effective at all.
- the constructive scope is so limited in the previously known ammunition and focuses on the design of the fragmentation shell and the pyrotechnic components.
- the claim that it is not necessary to dispose a high explosive mass over the entire cross-section of the missile in order to achieve a high penetration rate refers to the explosive bending of the inside hollow warhead jacket. Because the interior of the missile is undoubtedly formed by the drive, the control devices and a Wirkladung.
- the inner jacket 12c has no function associated with the splitter jacket. Instead, it represents the housing of the engine with the control elements. This is also expressed by the fact that an insulating layer 19 of heat-insulating material is arranged between this jacket 12c and the explosive coating.
- the EP 0 718 590 A1 which forms a basis for the preamble of claim 1, describes the active part of a rocket or a warhead, which accelerates preformed elements to increase the lateral effectiveness by means of a circular cross-sectional explosive occupancy.
- the main objective of the described construction is to convert the high detonation velocity of the explosive layer into a relatively low velocity of propagation of the accelerated elements or active parts.
- the explosive ring 43 accelerating the active parts is initiated via a ring of pellets (ignition elements 82).
- the explosive jacket 43 is basically in its construction and in its function with the in the DE 35 22 008 identical arrangement described. Due to the property of the explosive or of the explosive mixture, in particular the propagation velocity in connection with the dimensioning of the surrounding sub-projectiles (56) is influenced.
- projectiles which contain a pyrotechnic charge to increase the end-ballistic effect.
- U.S. Patent 3,302,570 It describes a type of bullet designed primarily for the purpose of breaking armored steel protection structures while minimizing the required projectile energy. This goal is achieved by a massive penetrator with a relatively small diameter and relatively large length of heavy metal as the core of the projectile structure.
- the effect in or behind the target should be increased by the use of explosives or fire.
- the effect of two incendiary devices and the bullet-specific disruption processes are named as factors in addition to the actual target strike.
- a high density combustible material encloses a penetrator with a thickened head.
- the material of high density surrounding the penetrator gives the penetrator additional mass and thus projectile energy and also penetrates through the hole punched by the penetrator head. Due to the larger diameter of the head stripping of the combustible material should be prevented.
- the combustible material is ignited and splinters are generated or burned spent in the target.
- the central penetrator and the combustible material surrounding it are surrounded by the actual projectile body, which is required to stabilize the projectile in the pipe and in flight.
- the present invention is based on the consideration that in conventional blasting projectiles, a significant proportion of the pyrotechnic components can not make any appreciable contribution to splinter acceleration. As a result of the detonation of the explosive, it is dissociated, and the splinter shell is essentially accelerated by the resulting reaction gases. The lateral acceleration of the splinter shell causes a direct increase in volume and thus relaxation, so that the pressure components of the explosive inner body can only deliver a correspondingly reduced acceleration component.
- the aim of the present invention is an end ballistic high efficiency of fragment-forming projectiles and warheads regardless of the impact velocity when using the lowest possible explosive mass. This is achieved by combining an explosive casing with a damming inner body in conjunction with an accelerated to high speed outer shell.
- an explosive casing with a damming inner body in conjunction with an accelerated to high speed outer shell.
- the achievable with relatively low explosives occupancy splinter or sub-floor speeds are between a few 100 m / s to near 2,000 m / s and are thus close to those of pure blasting.
- the explosive compression of the inner damming body results in a wide field of additional possibilities of action.
- the inner body it is possible to use the inner body to increase the performance of the entire system.
- examples include the use of special materials, multilayer arrangements, the introduction of sub-floors and the integration of an additional central pyrotechnic component for disassembly and / or acceleration of the inner body.
- a direction-controlled effect of the splitter can be achieved by the design of the inner damming, in conventional explosive projectiles in this form not possible.
- Special effects can also be achieved by integrating reactive damming components in the penetrator or warhead interior.
- the overall performance of the splinters of accelerating ammunition proposed here is far above those of known explosive projectiles or special munitions.
- the present invention relies on the effect of internal containment coupled with significantly lower explosive mass to achieve comparable slab or sub-bunker speeds as compared to conventional explosive projectiles.
- An estimate of the achievable splitter speed is made below.
- the velocity of the envelope is determined by three largely independent effects: the mass distribution between the shell to be accelerated and the inner support, the energy of the explosive layer (energy per unit volume and thickness), and the considered area element size (influenced by the forming element) splitter sizes).
- This circumstance is illustrated by the theoretical estimate of the fragmentation speed, which can be done, for example, using the Gurney equation known from the relevant literature.
- the mass distribution of the two accelerated sheets ie the damming ratio
- play a decisive role but also the sandwich size.
- the theoretical speed is 5 mm steel coverage, large explosive thickness (> 20 mm) and high internal containment above 2,000 m / s.
- the initial splitter speed in the order of 1,000 m / s and the speed of the inwardly accelerated hollow cylinder due the relatively low attenuation still at about 500 m / s.
- D / 3 can be assumed to be a good approximation to the characteristic Gurney speed.
- the splitter speed is thus proportional to the detonation velocity of the explosive used.
- D / 3 values between 2,600 m / s and 3,000 m / s (mean 2,800 m / s) can be assumed. This formulation is helpful, since it is usually the detonation velocity that is known rather than the Gurney velocity.
- the optimal implementation of the explosive energy in fragmentation speed so that correspondingly high speeds at relatively low explosive thicknesses possible.
- the influence of the inner damming can be taken into account by a factor, which should be called the Damming Factor (VF). It is dependent on the sizes M / C, M inner-insulation / M- shell , Rho- core , sigma- core and the Hygoniot-properties of the inner medium. The following estimates can be assumed: Thick sheaths and thick explosive layers as well as thin sheaths and thick explosive layers result in a factor of 1.1 to 1.2. This corresponds to a speed increase of 10% to 20%.
- VF Damming Factor
- Fig. 1A shows the basic structure of a spin-stabilized explosive layer chip projectile 1 A with a splinter shell / a splinter shell / a fragmentary projectile casing 2, an underlying explosive layer / explosives occupancy / explosives surface / pyrotechnic layer 3 and a damming inner body 4.
- Indicated are integrated ignition elements with control or Ignition electronics for the explosive layer.
- the triggering and triggering of the explosive layer must be adapted to the respective state of the art. The effectiveness of the arrangement remains largely unaffected.
- Fig. 1B shown schematically.
- the basic structure of the explosive layer chip projectile 1 B with splinter shell 2, explosive layer 3 and damming inner body 4 and ignition elements or other projectile or warhead devices is shown.
- the positioning of the ignition elements is not relevant to the function of the fragment-forming projectile; they can be located in the floor of the floor, in the damming inner body 4, in the bullet point or as modules in several places (cf., eg Fig. 24 and 45 ).
- Fig. 2 to 23 and Figs. 42 to 45 and 47 to 51 show examples of the cross-sectional configuration of projectiles or warheads according to the present invention.
- the damming, dynamically correspondingly incompressible inner body 4 is designed as a solid, homogeneous cylindrical component.
- materials for the damming component are basically all materials into consideration, which cause a desired dynamic damming.
- Their dynamic properties, and in particular the consequent degree of clogging, are determinative of the achievable splinter speed or the required explosive thickness for achieving a desired acceleration of the casing.
- the effect of the insulation on the achievable splitter speed is equivalent to the influence of the explosive thickness
- Fig. 3 the cross section through an explosive layer chipboard with damming inner body 5 is shown.
- it has an annular cross-section which surrounds a cavity 6.
- Thickness and material of the ring 5 are to be chosen so that sufficient insulation of the explosive layer takes place.
- the explosive zone can be composed of one layer as well as of two or more identical or different layers.
- incompressibility of the damming medium is not a mandatory requirement. Rather, the degree of compressibility affects the achievable speed of the splitter to be accelerated.
- Fig. 4 is a cross-section with multi-layer damming internal structure is shown, wherein in the hollow cylinder designed as a damming inner shell / inner body 5, a second inner body / central body 7 is.
- components 5 and 7 may have different mechanical or physical properties.
- an inner body is first compressed and only then causes sufficient or increased damming.
- Verdämmungs takes place by the design or the structure of the inner body a temporally changing Verdämmungs Escape corresponding to the technical requirements. This property can be referred to as Verdämmungssprung.
- a whole range of materials with corresponding Hygoniot curves is suitable. According to these considerations, particularly interesting effects can be achieved with materials which have specific Hygoniot properties. These include, for example, glass or glassy substances or liquid or pasty components.
- FIG. 15 shows an example in which the explosive layer 3A has a circular shape on the outside and an arbitrary shape on the inside (octagonal in this example).
- the damming inner body 8 shows a corresponding contour.
- the explosive layer (the explosive shell) 3A can exert a differentiated effect on the splitter shell by virtue of its shape. This can support fragmentation and influence the fragment shape and splinter speed.
- Fig. 6 shows an example with damming inner body of the explosive layer 3B, which here has an octagonal outer cross section and a circular inner cross section.
- the splinter shell 2A has an octagonal inner contour corresponding to the shape of the explosive.
- the fragmentation process of the shell can be influenced by means of different shell thicknesses, densities and explosive layer thicknesses as well as by means of pyrotechnic properties.
- Fig. 7 shows an example with a basically arbitrary, square in this example cross-section of the damming inner body 9.
- the explosive body / the explosive part is separated under the splitter shell 2 by the inner body.
- a simultaneous or non-simultaneous ignition of the explosive segments 10 is possible.
- the damming inner body 9 can of course also be dimensioned so that the explosive shell is closed for a ring ignition.
- the inner body 9 can be held in position by means of webs, for example.
- an inner body 11 having (in this example) a triangular cross-section is combined with inert, pressure-transmitting balance segments 12 that fill the space between the outer surfaces of FIG. 11 and the annular (cylindrical) explosive shell 3.
- These inert segments 12, for which the same conditions apply to the materials as for the damming inner bodies, can be formed as fragment-forming bodies. Besides, they can contain additional active parts. Of course, these segments can also be assigned other functions. Thus, for example, they can be manufactured as sub-penetrators, for example made of heavy metal, hard metal or hardened steel, for achieving end-ballistic performances.
- FIG. 9 Another construction for a projectile according to the invention is in Fig. 9 shown. Shown are two variants of cross sections with dynamically effective inner layers / ring surfaces. This dynamic efficiency derives from the specific properties of the layer relative to the passage of shock waves. The interfaces between the dynamic layer and the adjacent materials are crucial. The physical properties result from the acoustic impedance. This determines the reflectance of the shock waves in the interface between two media by the ratio m-1 / m + 1 with m as the quotient of the products density and longitudinal speed of sound of the two media.
- FIG. 9 shows a projectile cross-section with two damming, hollow inner bodies 5, 5A and a dynamically acting layer 13 between the explosive layer 3 and the confinement 5.
- an additional body 7A for example, a central penetrator.
- the lower part of the illustration shows a dynamically effective layer 13A between the damming first body 5 and a second damming layer 5A as an inner part in FIG. 5.
- FIG. B buffering (shock-absorbing or the Stosswellen pressgang influencing or the shock-enhancing) properties for temporal influence on the impact or insulation effect and thus the splitter speed, splintering and / or splinter distribution.
- Fig. 10 is a cross section with damming inner body 4 and a dynamically acting layer 13 B between the explosive layer 3 and splinter shell 3 shown. Due to the properties and structure of the dynamic layer 13B, the acceleration effect of the explosive layer 3 on the splinter shell 2 can be influenced.
- FIG Fig. 11 A similar construction is shown in the lower partial cross section in FIG Fig. 11
- the dynamically active layer 13C is positioned in the outer splintering region of the split splitter outer shell 14.
- the fragment development of the overlying fragmentation shell 2 is to be influenced.
- the upper partial cross section an example with outer shell / shell jacket 14A and underlying fragmentation shell 2 is shown.
- the design of the outer projectile casing 14A can not only be derived from internal ballistic requirements, but this can also develop a dynamic effect in the sense described.
- Fig. 12 shows an example with outer shell 14A and a splitter body or a matrix 16A.
- preformed projectiles 16 or other, ballistically active elements such as fragment-forming body 15 may be embedded.
- the acceleration / activation in turn takes place through the explosive jacket 3.
- an ignition element 18 is embedded here, which can support or cause an additional decomposition of the damming component.
- a dynamic compression effect can also be achieved by the formation of a pressure field. In this way, for example, a decomposition of 17 can be initiated after arrival or only within the destination.
- FIG. 13 Further examples are shown with integrated ignition elements.
- the cross-sectional configuration here includes a (in the representation square) damming inner body 9 and explosive segments 10A.
- the explosive layer or the explosive segment 10A contains an ignition element 18A, which can be designed as a planar, linear or punctiform device.
- a corresponding ignition element 18B is introduced into the inner body 9.
- Fig. 14 shows an example of the cross-sectional configuration with basically arbitrarily shaped, in this example square explosive surface 3C. Between 3C and the chip layer 2 are pressure transmitting segments 12A.
- the damming inner body 9 has a corresponding to the explosive layer 3C square cross section.
- the segments 1 2A in turn, in addition to their pressure-transmitting function to meet a number of other specific requirements, such as having a damping or the splitter speed of 2 influencing effect. Also in this case, as with Fig. 5 to 7 , different splitter speeds or splinter shapes for the fragmenting splinter shell are set, here due to the different thickness of the active segments 12A.
- Fig. 15 illustrates an example with two-layer explosive coating 19, 20 and correspondingly two Däfflemmungs Anlagenen 4A, 21 represents.
- the ignition of the explosives assignments can be made simultaneously or at different times.
- Such a structure results in a particularly wide range of effects.
- the outer layer in front of a target, the inner component in the target passage or only in the target interior are ignited.
- the inner damming layer 4A may be made to have end ballistic performance, that is, it may be a penetrator. In this way, a broadly staggered, the combat order optimally adapted power delivery can be achieved.
- a multi-part damming inner body 23 which is here composed of four circular segments 24, which may consist of similar or different materials. Between the segments 24, layers 25 may be located. These may be designed as dynamically effective layers in the sense of the above description, ie consist of rubber / elastomeric materials or of materials with plastic or damping properties.
- the individual components 23 may be loosely mounted or fixed, eg connected by gluing, screwing or vulcanization.
- the bullet structure in this example is provided with a central pyrotechnic body 22, which provides an additional decomposition / lateral component (especially for the individual components 24).
- the segments 24 may in turn be fragment-forming, contain body or have their own end ballistic performance in the sense of central penetrators.
- FIG. 17 Two further examples with multi-part damming inner bodies / central penetrators 26 are shown. These consist, for example, of four cylindrical penetrators 27. In the upper part of the image, in the center of the cylindrical penetrators 27, there is a central pyrotechnic body 22A, which gives the inner body 26 designed as a combination of penetrators a lateral velocity component. In the lower part of the image, instead of 22A, there is an inert central body 28 (or an inner space) between the components 27A.
- the explosive layer 3D surrounding the inner body 26 has a different thickness due to the shape of 26 and 27, respectively. This results in a different local acceleration of the sheath fragments.
- the explosives can be interrupted by the elements introduced (above) or through them (below).
- Fig. 18 shows an example with projectile casing / sheath 14A, lying below 14A fragmentation jacket 29 with geometrically shaped inner surface, a correspondingly shaped explosive layer 33 and the inner insulation 4.
- elements 31 A By reaching into the splinter shell 29 form elements 31 A, a local weakening of the fragmentation sheath 29 is achieved allowing fragmentation in a determinable manner (eg, stripe-like, latticed to form particular fragments).
- a corresponding principle lies in Fig. 19 the cross-sectional configuration with geometrically modified inner surface of the fragmentation shell 32 and the correspondingly shaped explosive layer 31 based.
- Fig. 20 is in the upper part of the image, the inner surface of the explosive layer 34 geometrically designed, the explosive layer here forms a closed shell.
- the explosive component 35 is composed of explosive longitudinal strips or explosive surface elements 36.
- the correspondingly shaped inner body 4C acts as a separation between the individual explosive components.
- the principle of the segmented explosive shell is also in Fig. 21 realized.
- the example shows the cross-sectional design with internal insulation 4 and in the Explosive layer 36A introduced separating elements or geometric structures basically any configuration. In the present example, they represent longitudinal strips 37.
- Fig. 22 shows an example with a hollow hollow inner ring 21 and a designed as a container central (also possibly supporting the damming) inner body 38 with the wall 38A.
- the filling 39 of the container may be for example a solid, a pasty or liquid substance or an inhomogeneous conglomerate of elements.
- FIG. 23 Also in Fig. 23 are shown cross-sectional configurations with container.
- the projectile is provided with a damming, with a liquid, a pasty or compacted powder mass 39 filled central container 38.
- an annular inner container 38B is connected to the wall 38C and the filling 39A by means of webs 38D with a central inner damming body 4B.
- the webs 38D may be designed as independent active parts (inert or pyrotechnically effective).
- Fig. 24 a longitudinal section with splinter shell 2, stepped / variable-thickness explosive layer 3 and a multi-part damming inner body 41. Plotted are positions for the installation of control or ignition elements for the explosive layer.
- the damming inner body 41 is here formed in two parts. In this way, different splitter speeds and / or different splitter distributions can be achieved in the longitudinal direction. In the head or in the floor area of the projectile control or ignition elements 40 may be installed, which of course also applies to the other presented bullet structures according to the invention.
- Fig. 25 is a longitudinal section through a projectile with variable explosive thickness and cylindrical fragmentation shell shown in two variants.
- the upper part of the diagram shows an arrangement with a longitudinally variable explosive layer 42 and a correspondingly shaped damming, while the lower partial image shows a variant with a thickness-changing fragmentation jacket 43 and a variable explosive layer 42A.
- the explosive layer / inner body have a diameter jump.
- the projectile shown in the upper part of the image has a variable thickness of the explosive layer 44 with a continuous damming inner body 45 with a diameter jump or a different diameter change.
- the lower part of the picture shows a projectile with a divided damming body or an inserted penetrator or penetrator ring 41 A with different diameters.
- the inner bodies can fulfill different functions.
- Fig. 27 shows an example of variable thickness of the explosive jacket 44A and cylindrical inner body 4.
- the splinter shell 45 and the explosive layer 44A have a diameter jump or a continuous change in diameter.
- the upper variant is provided with multipart, here separated explosive layers 47 and adapted fragmentation sheath 45.
- the damming, stepped inner body 46 accordingly shows a variable diameter.
- the projectile shown in the lower part has a continuous explosive layer 48 with a change in diameter.
- Arrangements in accordance with the present invention make it possible to achieve highly effective combinations or designs of splinter casings and explosive layers in a technically particularly simple manner.
- Fig. 24 be in Fig. 29 to 31 Examples shown.
- Fig. 29 a geometric design of the splinter shell for achieving desired effects or preferred splitter directions.
- directional control and rotation of the fragmentation body / splitter rings 50 are effected.
- the longitudinal sawtooth-shaped explosive layer 49 is provided here continuously with a cylindrical damming inner body 4.
- This in Fig. 30 shown example with separate explosive layers 49A causes a direction control of the splitter body 50A.
- the damming inner body 4 is geometrically adjusted.
- Fig. 31 shows a splitter assignment 51 for different splitter directions and splitter speeds with appropriately matched explosive layer 49B.
- FIGS. 32 to 34 as well as 37 to 41 further embodiments of the arrangement according to the invention are shown by the combination with designated projectile components.
- Fig. 35 and 36 Examples of integration / combination of arrangements with penetrators are shown.
- Fig. 32 shows two longitudinal sections with internal sprengstoffbelegtem splitter body 2 and a space 52 between the outer shell 14 B and splitter body and an empty or partially filled outer ballistic hood 53 (upper panel) and a solid / filled tip (lower panel).
- This representation represents, for example, subcaliber projectiles, projectiles with sabot or full caliber bullets with inner active part of smaller diameter.
- Fig. 33 shows two longitudinal sections with complete (continuous) explosives occupancy 3 and 54.
- the upper part of the image shows the projectile body and the internally dammed tip portion 55, the lower part of an explosive-filled tip 56th
- Fig. 34 a longitudinal section is shown with an explosive body 57 inserted into the damming inner region 4 of basically any shape.
- an explosive component can locally cause particularly high lateral splitter velocities or even desired effects in the body 4 itself Compressions or mechanical loads to disassembly or accelerations effect.
- Fig. 35 shows two longitudinal sections with a embedded in the damming inner region 4 hard or heavy metal core 58 (upper panel) and a slender cylinder with a top 59 (lower panel).
- hard or heavy metal core 58 upper panel
- any variant of an end ballistic effective body can be introduced.
- the combination of breakdown power and fragmentation shown here covers a particularly broad range of effects.
- FIG. 2 shows two examples with a core 58A embedded in the damming interior, with a focusing inwardly tapered rear portion 60 of the core.
- an acceleration and / or a decomposition of the core 58A can be effected (upper partial image).
- the lower part of the figure shows a core with stepped tip 58B and conical rear part 62 with centering, the core accelerating explosive deposit 61 A.
- the effective directions of the configurations of the rear area with core and splinter shell are symbolized by the arrows 60A and 62A.
- FIG. 37 two longitudinal sections with inner body 64 and corresponding Sprengstoffbelegung 63 in conjunction with a top module 72 for directed increased fragmentation effect in the axial direction (upper panel) and with splitter directivity by shaping of damming inner body 64, explosive surface 66 and fragmentation shell 65 (lower panel) are shown.
- the corresponding arrows 72A, 65A which symbolize the directions of action are also shown (cf. Fig. 40 ).
- Fig. 38 shows a longitudinal section corresponding to the lower part of Fig. 37 with fragmentation jacket 67 and additional splinter components in a splitter pocket or fragmentation ring 68 with the embedded active parts 68A (knitting arrows 68B).
- Fig. 39 shows two longitudinal sections with (here) two-stage damming inner body 70A with directional fragmentation effect by a special design of the damming inner body 70 or 70A and continuous explosive occupation 69 (top) as well as non-continuous explosive charge / separate explosive rings 69A (below).
- Fig. 40 shows an example with additional, primarily axially accelerated splitter body 73 (symbolized by the action arrows 73A) in the front region of the projectile, accelerated by an explosive surface 71 of the splitter shell 3, which is also dammed up by the inner body 4.
- Fig. 41 shows two longitudinal sections with partial explosive occupancy in the form of a damming body with pronucleus / step core 74 (top).
- a pronucleus 74A can also be introduced separately (below).
- this pronuclear 74A may consist of a highly ballistic end hard material such as hard or heavy metal, or even a brittle material that disintegrates under dynamic load from the impact, such as highly brittle tungsten carbide or pre-fragmented bodies. It primarily serves to penetrate massive target plates. Due to the step-like training the attack on a tilted plate is improved or only possible.
- FIG. 12 is a cross-sectional configuration with explosive-accelerated projectiles or warheads according to the invention with individual (here four) segments 75.
- the individual segments 75 correspond in their function to those of the examples already shown with a circular cross-section. Due to the segmentation and the separation 76, which may be both a structure / supporting inner wall and a shock wave barrier, the individual segments can be controlled separately.
- This example therefore stands for penetrators or warheads with partial occupancy in the longitudinal / axial direction, in which the possibility of a subfield occupancy in the room is given by splinters.
- Fig. 43 shows an example with variable thickness of the splitter shell 77 and explosive segments 78 with (here four) lenticular (but basically free to be designed) cross-sectional shape.
- the inner contour of the explosive segments 78 is formed by the corresponding inner damming body 9A. It goes without saying that the fragment and the explosive layer correspondingly Fig. 42 can run separately or continuously. By means of such arrangements very differentiated splitter distributions are to be achieved, which in Fig. 43 for a segment are symbolized by the arrow field 78A.
- Fig. 44 shows an example of the cross-sectional configuration with designed as a convex strip explosive surface 80 and adapted inner damming body 9B.
- Fig. 45 shows a corresponding example with (here eight) segments 81 with the explosive occupancy 80 A, which are separated by the surfaces 75 A. While in Fig. 44 the fragment-forming arrangement is located in a shell 14, lie in Fig. 45 free the splintering (or homogeneous) stripes 79A.
- this example still has a central ring 82, which supports the damming of the segments 81.
- the cylinder 82 may be hollow or contain a central penetrator.
- Fig. 46 shows a longitudinal section through a basic projectile structure 83 with multi-part damming inner body, which may be constructed from radial, axial or combined elements. In this way, the damming effect may be combined with mechanical pre-fragmentation, or different bodies with different mechanical and physical properties may be combined.
- Fig. 47 shows the cross-sectional shapes of a projectile Fig. 46 with splitter shell and damming inner body 84, here constructed of cylinders 86 (continuous or stacked) of the same or different diameter or materials in a pressure transmitting matrix 85.
- the central region 87 may be formed by a penetrator or also filled with individual bodies. Also an additional pyrotechnic component accordingly Fig. 12 can be introduced.
- the cylinders 86 may have a higher degree of slimming (length / diameter ratio) or may be formed from a stack of short cylinders.
- Fig. 48 shows another example of the cross-sectional design of a projectile Fig. 46 segmented, single or multi-layer internal damming body 88 and a central penetrator 82A.
- Fig. 49 is a longitudinal section through an explosive layer-splitter projectile 89 shown, which is constructed as a multi-part / multi-stage active body. This can be formed, for example, from different, separated by a layer 91 or related stages with different functions or introduced construction spaces 90.
- FIGS. 50 and 51 Here are some examples shown. So owns in Fig. 50 the splitter body 92 has a square cross section corresponding to an explosive layer 3F Fig. 14 is accelerated. In 51 For example, the splinter shell has an octagonal cross section 92A as an example of the arbitrary shape. The acceleration takes place here via an annular explosive layer 3.
- the shatter-forming active components or sheaths containing fragments or sub-projectiles are accelerated by means of an explosive layer which is thin relative to the projectile or warhead diameter.
- the explosive mass needed to accelerate splinters is minimized. Compared with conventional explosive projectiles, the explosive mass can be reduced by 50% to 80%, depending on the caliber and technical design, at comparable splinter or sub-floor speeds.
- the least strength of the explosive layer is determined by ensuring ignition or spark ignition.
- ignition aids such as detonating cords very thin planar explosive layers can be ignited.
- the choice of explosive is free, so that very small thicknesses up to an order of 2 mm can be realized.
- the explosive layer may be in the form of a hollow cylinder and have a constant or variable wall thickness and / or cross-sectional shape.
- the explosive layer can be prefabricated and incorporated as a film or as an arbitrarily shaped body, be cast in or introduced in any manner, such as e.g. pressed or sucked in by vacuum. It can consist of one or more superimposed layers.
- a projectile or warhead may contain a continuous layer of explosive or may be composed of multiple explosive layers in both the axial and radial directions.
- the explosive layer may be homogeneous or contain admixtures or embedded bodies.
- Ignition of the explosive layer or zones or explosive fragments may be accomplished in any conceivable manner in accordance with the prior art blasting projectiles or warheads.
- the velocities and the direction of the fragmentation or sub-projectiles can be varied within very wide limits.
- the damming inner body can be one or more parts. It may consist of metallic or non-metallic materials or of their combination. There is thus an almost unlimited variety of materials with different mechanical, physical or chemical properties to choose from.
- a homogeneous metallic inner body on one side e.g. consist of a metal of low density such as magnesium, on the other side of a heavy or hard metal body (homogeneous or segmented) high density with a correspondingly high end ballistic performance.
- Hygoniot properties can be determined their behavior or it can be selectively selected materials with specific dynamic properties in conjunction with the pyrotechnic components used and the technical design of the projectile or warhead.
- Homogeneous inert inner damming bodies may consist of or contain such metallic or non-metallic matter which is reactive under high pressure at locally high temperature.
- the damming inner body can be made of brittle or embrittled under dynamic load material. Likewise, he can pre-fragmented or mechanically or thermally pretreated yours.
- the damming inner body can also be designed as a hollow cylinder or contain a cavity in any cross-sectional area. This inner cavity may in turn be empty or filled with a more or less damming substance. This results in a further possibility for influencing the damming and thus the speed or the acceleration of the shell of fragment-forming or sub-projectile projectiles or warheads.
- the damming inner body can represent or contain a container.
- the inner cavity or container may be e.g. be filled with a solid, powdery, pasty or liquid substance. Furthermore, it may contain a reactive substance, e.g. contain a flammable liquid.
- the shell of the projectile or the warhead is homogeneous.
- their pretreatment in support of fragmentation it is possible to use all methods and techniques which correspond to the state of the art in conventional fragmentation projectiles.
- the accelerated shell may also consist wholly or partly of preformed splinters or sub-floors.
- a layer may itself represent the projectile casing or be incorporated as a layer between the explosive and the outer shell.
- This structure can be introduced between the explosive layer and the outer shell and a pre-fragmented or very brittle or embrittled under dynamic load layer.
- the explosive layer and the damming inner body there may be a layer dynamically supporting the damming. Their mode of action is determined by the acoustic impedance of the materials involved.
- a medium having a dynamic damping action can be introduced as a layer which reduces the acceleration impact.
- the explosive layer may be composed of contiguous surfaces or of surfaces separated in the radial or axial direction.
- the explosive layer can have an arbitrarily shaped surface (contour), so that spatially different splinter formations and also splitter speeds can be achieved.
- the explosive layer can form an angle to the projectile axis.
- splinters or sub-projectiles can be accelerated direction-controlled.
- Such arrangements may be provided at certain positions of the projectile (e.g., in the tip region) or extend over the entire surface.
- the explosive layer will usually have the shape of a hollow cylinder. This can be open at the ends or closed on one or both sides by means of a front or rear explosive layer.
- Explosive disks can be introduced over the entire penetrator length.
- inner bodies can be accelerated in the axial direction.
- Parts of the tip can be accelerated via a frontal explosive coating.
- the tip of the projectile or warhead may be wholly or partially filled with explosives.
- the tip or tip region may also consist of or contain an end ballistic inert body to effect end-ballistic effects via this component.
- the active bodies may be cannon-fired projectiles, combat components of a missile or missile, parts of a bomb or the active part of a torpedo.
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Abstract
Description
Die vorliegende Erfindung betrifft ein/einen Splitter oder Subgeschosse bildendes/bildenden Geschoss oder Gefechtskopf.The present invention relates to a fragment or sub-projectile projectile or warhead.
Sprenggeschosse werden eingesetzt, um unabhängig von der Auftreffgeschwindigkeit eines Geschosses oder Gefechtskopfes mittels sprengstoffbeschleunigter Splitter mit großer Anfangsgeschwindigkeit endballistische Wirkungen bei flächenhaften leichten Zielen zu erreichen. Derartige Sprenggeschosse sind dadurch gekennzeichnet, dass ihr Volumen zum größten Teil von Sprengstoff eingenommen wird. Durch ihren Aufbau beinhalten Sprenggeschosse oder sprengstoffgefüllte Gefechtsköpfe eine verhältnismäßig große Sprengstoffmasse, die zu einem erheblichen Teil nicht effektiv ist bzw. teilweise aus physikalischen Gründen überhaupt nicht zur Wirkung kommen kann. Der konstruktive Spielraum ist damit bei den bisher bekannten Munitionen stark begrenzt und konzentriert sich auf die Ausgestaltung der Splitterhülle und die pyrotechnischen Komponenten.Explosive projectiles are used to achieve end-ballistic effects with areal easy targets, regardless of the impact velocity of a projectile or warhead by means of explosive-accelerated splinters with a high initial velocity. Such explosive projectiles are characterized in that their volume is taken up for the most part by explosives. By their design, projectiles or explosives-filled warheads contain a relatively large mass of explosives, which is not effective to a considerable extent or partially for physical reasons can not be effective at all. The constructive scope is so limited in the previously known ammunition and focuses on the design of the fragmentation shell and the pyrotechnic components.
Bei Splitterbildenden Geschossen ist die Verteilung ausreichend schnell beschleunigter Splitter auf eine möglichst große Zielfläche bzw. das Belegen eines möglichst großen Raums (Tiefe) die entscheidende Größe. Dieses Ziel ist bei reinen Sprenggeschossen jedoch nur eingeschränkt zu erreichen, da bei einer Detonation die Steuerungsmöglichkeiten hinsichtlich Splitterbildung und Splitterverteilung begrenzt sind. In Verbindung mit einer ausreichenden Auftreffgeschwindigkeit des Geschosses und dem Einsatz relativ geringer Sprengstoffmengen wurden die oben genannten Forderungen bisher nur mit so genannten ALP-Geschossen (Aktive Lateralwirksame Penetratoren) erreicht. Bei diesen lateral zerlegenden, aktiven Geschossen auf der Basis des PELE-Prinzips (Penetratoren mit erhöhter Lateralwirkung) sind die erreichbaren Lateralgeschwindigkeiten je nach Art und Masse des eingesetzten pyrotechnischen Mittels und des konstruktiven Aufbaus jedoch begrenzt. Dies entspricht durchaus der Zielsetzung derartiger Penetratoren oder Gefechtsköpfe, da die eigentliche endballistische Leistung durch die Geschossgeschwindigkeit erbracht wird. Das Funktionsprinzip eines Geschosses nach dem ALP-Prinzip ist die aktive Zerlegung eines Penetrators vor Erreichen des Ziels in Fragmente oder Subgeschosse. Die Geschwindigkeit dieser Komponenten ergibt sich aus der eingesetzten geringen Sprengstoffmenge, deren Energie über ein inertes Übertragungsmedium entsprechend der Stoßwellentheorie und der eingesetzten Werkstoffe an die äußere Wirkkomponente übertragen wird. Die Geschwindigkeiten dieser Wirkkomponenten liegen zwischen wenigen m/s und etwa 200 m/s. Die Wirksamkeit bzw. die Durchschlagsleistung der Wirkteile ist damit bei ALP-Geschossen wie bei herkömmlichen Wuchtgeschossen primär von der Auftreffgeschwindigkeit abhängig.In shatter-forming projectiles, the distribution of sufficiently fast accelerated fragments to the largest possible target area or the occupying of the largest possible space (depth) is the decisive factor. However, this goal can only be achieved to a limited extent in the case of pure blasting projectiles, since with a detonation the control possibilities with respect to fragment formation and fragmentation distribution are limited. In conjunction with a sufficient impact velocity of the projectile and the use of relatively small quantities of explosives, the abovementioned requirements have hitherto only been achieved with so-called ALP projectiles (Active Lateral Effective Penetrators). In these laterally dispersive, active projectiles based on the PELE principle (penetrators with increased lateral action), however, the achievable lateral velocities are limited, depending on the type and mass of the pyrotechnic composition used and the structural design. This quite corresponds to the objective of such penetrators or warheads, since the actual end ballistic performance is provided by the projectile velocity. The functional principle of a projectile according to the ALP principle is the active decomposition of a penetrator before reaching the target in fragments or sub-projectiles. The speed of these components results from the small amount of explosive used, the energy is transmitted via an inert transmission medium according to the shockwave theory and the materials used to the outer active component. The speeds of these active components are between a few m / s and about 200 m / s. The effectiveness or the breakdown power of the active parts is thus dependent primarily on the impact velocity on ALP projectiles as in conventional balancing projectiles.
Bisher bei Sprenggeschossen bekannte Anordnungen beschränken sich auf den Ladungsaufbau und die Ausgestaltung des Splittermantels. Ein repräsentatives Beispiel für den Ladungsaufbau beschreibt das
Bei Gefechtsköpfen und Flugkörpern ist es das erklärte Ziel, durch besondere Aufbauten eine möglichst schonende Beschleunigung von Subgeschossen oder außen angebrachten Behältern durch Sprengstoffhinterlegungen zu erreichen. Als Stand des Wissens können die beiden Schriften
Die
Weiterhin sind Geschosse bekannt, die eine pyrotechnische Ladung zur Steigerung der endballistischen Wirkung enthalten. Als repräsentatives Beispiel dient das
Ein brennbares Material von hoher Dichte umschließt einen Penetrator mit einem verdickten Kopf. Das den Penetrator umgebende Material hoher Dichte verleiht dem Penetrator zusätzliche Masse und damit Geschossenergie und dringt ebenfalls durch das vom Penetratorkopf geschlagene Loch. Durch den größeren Durchmesser des Kopfes soll ein Abstreifen des brennbaren Materials verhindert werden. Durch das Zerschellen des Penetrators beim Durchgang durch härtere Ziele wird das brennbare Material gezündet und Splitter werden generiert bzw. Brandmittel in das Ziel verbracht. Im hinteren Teil des Geschosses sind der zentrale Penetrator und das ihn umgebende brennbare Material vom eigentlichen Geschosskörper umgeben, der erforderlich ist, das Projektil im Rohr und im Flug zu stabilisieren. Mittels einer Schneidkante am gehärteten vorderen Rand des Geschosskörpers soll das Loch des von dem zentralen Hauptpenetrator bereits durchschlagenen Zielmaterials vergrößert und durch Mitnahme von Zielmaterial größerer Schaden im Inneren verursacht werden. Um den Raum zwischen dem Zentralpenetrator (13) und dem Geschosskörper (17) zu füllen, wird eine weitere Schicht eines brennbaren Materials (16) geringer Dichte eingebracht. Die zusätzliche Schicht soll den Zentralpenetrator in seiner Position halten. Beim Zerschellen des Geschosses beim Eintritt in härtere Ziele werden die Brandsätze gezündet. Der erfinderische Ansatz ist also ein anderer als bei der vorliegenden Erfindung. In der
Zur vorliegenden Erfindung: Dieser liegt die Überlegung zu Grunde, dass bei herkömmlichen Sprenggeschossen ein erheblicher Teil der pyrotechnischen Komponenten keinen nennenswerten Beitrag zur Splitterbeschleunigung leisten kann. Durch die Detonation des Sprengstoffs wird dieser dissoziiert, und die Splitterhülle wird im Wesentlichen durch die entstehenden Reaktionsgase beschleunigt. Die laterale Beschleunigung der Splitterhülle bewirkt eine unmittelbare Volumenvergrößerung und damit Entspannung, sodass die Druckanteile des Sprengstoff-Innenkörpers nur noch einen entsprechend reduzierten Beschleunigungsanteil liefern können.The present invention is based on the consideration that in conventional blasting projectiles, a significant proportion of the pyrotechnic components can not make any appreciable contribution to splinter acceleration. As a result of the detonation of the explosive, it is dissociated, and the splinter shell is essentially accelerated by the resulting reaction gases. The lateral acceleration of the splinter shell causes a direct increase in volume and thus relaxation, so that the pressure components of the explosive inner body can only deliver a correspondingly reduced acceleration component.
Ziel der vorliegenden Erfindung ist eine endballistisch hohe Wirksamkeit von splitterbildenden Geschossen und Gefechtsköpfen unabhängig von der Auftreffgeschwindigkeit beim Einsatz einer möglichst geringen Sprengstoffmasse. Erreicht wird dies durch die Kombination einer Sprengstoffummantelung mit einem verdämmenden Innenkörper in Verbindung mit einer auf hohe Geschwindigkeit beschleunigten Außenhülle. Durch diese Anordnung wird nicht nur eine bestmögliche Umsetzung der Sprengstoffenergie erreicht, sondern es eröffnet sich auch ein großer konstruktiver Spielraum für die Auslegung derartiger Munitionen oder Gefechtsköpfe. Die mit relativ geringen Sprengstoffbelegungen erreichbaren Splitter- bzw. Subgeschossgeschwindigkeiten liegen zwischen wenigen 100 m/s bis nahe 2.000 m/s und liegen damit nahe bei denen reiner Sprenggeschossen. Durch das Sprengverdichten des inneren verdämmenden Körpers ergibt sich ein weites Feld zusätzlicher Wirkmöglichkeiten. Insbesondere besteht die Möglichkeit, den inneren Körper zur Leistungssteigerung des gesamten Systems heranzuziehen. Beispiele hierfür sind der Einsatz spezieller Materialien, mehrschichtige Anordnungen, das Einbringen von Subgeschossen und die Integration einer zusätzlichen zentralen pyrotechnischen Komponente zur Zerlegung und/oder Beschleunigung des Innenkörpers. Weiterhin ist durch die Ausgestaltung der inneren Verdämmung eine richtungsgesteuerte Wirkung der Splitter zu erreichen, die bei herkömmlichen Sprenggeschossen in dieser Form nicht möglich ist. Besondere Effekte lassen sich auch durch die Integration reaktionsfähiger verdämmender Komponenten im Penetrator- oder Gefechtskopfinneren erzielen. In Verbindung mit konstruktiven Vorteilen und der Möglichkeit des Einsatzes weiterer Wirkkomponenten liegt die Gesamtleistung der hier vorgeschlagenen Splitter beschleunigenden Munition weit über derjenigen bekannter Sprenggeschosse oder Spezialmunitionen.The aim of the present invention is an end ballistic high efficiency of fragment-forming projectiles and warheads regardless of the impact velocity when using the lowest possible explosive mass. This is achieved by combining an explosive casing with a damming inner body in conjunction with an accelerated to high speed outer shell. By this arrangement, not only the best possible implementation of the explosive energy is achieved, but it also opens up a large constructive scope for the design of such ammunition or warheads. The achievable with relatively low explosives occupancy splinter or sub-floor speeds are between a few 100 m / s to near 2,000 m / s and are thus close to those of pure blasting. The explosive compression of the inner damming body results in a wide field of additional possibilities of action. In particular, it is possible to use the inner body to increase the performance of the entire system. Examples include the use of special materials, multilayer arrangements, the introduction of sub-floors and the integration of an additional central pyrotechnic component for disassembly and / or acceleration of the inner body. Furthermore, a direction-controlled effect of the splitter can be achieved by the design of the inner damming, in conventional explosive projectiles in this form not possible. Special effects can also be achieved by integrating reactive damming components in the penetrator or warhead interior. In conjunction with constructive advantages and the possibility of using further active components, the overall performance of the splinters of accelerating ammunition proposed here is far above those of known explosive projectiles or special munitions.
Die vorliegende Erfindung stützt sich im Wesentlichen auf die Wirkung einer inneren Verdämmung in Verbindung mit einer erheblich geringeren Sprengstoffmasse zum Erzielen vergleichbarer Splitter- bzw. Subgeschossgeschwindigkeiten im Vergleich zu herkömmlichen Sprenggeschossen. Im Folgenden wird eine Abschätzung der erreichbaren Splittergeschwindigkeit vorgenommen.Essentially, the present invention relies on the effect of internal containment coupled with significantly lower explosive mass to achieve comparable slab or sub-bunker speeds as compared to conventional explosive projectiles. An estimate of the achievable splitter speed is made below.
Grundsätzlich wird die Geschwindigkeit der Hülle durch drei voneinander weitgehend unabhängige Effekte bestimmt: von der Massenverteilung zwischen der zu beschleunigenden Hülle und der inneren Abstützung, von der Energie der Sprengstoffschicht (Energie pro Volumeneinheit und Dicke) und von der betrachteten Flächenelementgröße (beeinflusst durch die sich bildenden Splittergrößen). Dieser Umstand wird durch die theoretische Abschätzung der Splittergeschwindigkeit veranschaulicht, die z.B. über der aus der einschlägigen Literatur bekannten Gurney-Gleichung erfolgen kann. Es bieten sich zwei Betrachtungsweisen für die hier vorliegenden Anordnung an: die eine geht von einer zylindrischen Form aus, die andere basiert auf einer Abwicklung des zylindrischen Aufbaus, um ein ebenes Flächenelement zu erhalten. Dieses würde dann in erster Näherung einer reaktiven Schutzanordnung entsprechen. Dort spielt nicht nur die Massenverteilung der beiden beschleunigten Bleche (also das Verdämmungsverhältnis) eine entscheidende Rolle, sondern auch die Sandwichgröße. Bei einer 10 mm dicken Sprengstoffschicht und einer 5 mm dicken Stahlhülle sowie einer starken einseitigen Verdämmung ergeben sich z.B. nach Gurney bei sehr großen Flächen Geschwindigkeiten von 1.500 m/s. Bei einem 10 mm dicken hinteren Blech errechnen sich noch 750 m/s. Bei einem schmalen Sandwich (Streifen) werden noch etwa 60% dieser Werte erreicht.Basically, the velocity of the envelope is determined by three largely independent effects: the mass distribution between the shell to be accelerated and the inner support, the energy of the explosive layer (energy per unit volume and thickness), and the considered area element size (influenced by the forming element) splitter sizes). This circumstance is illustrated by the theoretical estimate of the fragmentation speed, which can be done, for example, using the Gurney equation known from the relevant literature. There are two approaches to the present arrangement: one assumes a cylindrical shape, the other is based on a development of the cylindrical structure in order to obtain a planar surface element. This would then correspond in a first approximation to a reactive protection arrangement. Not only does the mass distribution of the two accelerated sheets (ie the damming ratio) play a decisive role, but also the sandwich size. With a 10 mm thick explosive layer and a 5 mm thick steel casing as well as a strong one-sided damming, for example, according to Gurney, velocities of 1,500 m / s result for very large areas. With a 10 mm thick rear sheet still 750 m / s are calculated. With a narrow sandwich (strip) about 60% of these values are still reached.
Weitere Berechnungsbeispiele: Ohne Randeinflüsse (also eine ausreichend ausgedehnte Elementgröße vorausgesetzt) beträgt die theoretische Geschwindigkeit bei 5 mm Stahlbelegung, großer Sprengstoffdicke (> 20 mm) und hoher innerer Verdämmung über 2.000 m/s. Bei einer Hüllendicke von 5 mm und einer 5 mm dicken Sprengstoffschicht sowie einer inneren Verdämmung durch einen Aluminium-Hohlzylinder mit einer Dicke von 20 mm liegt die Splitter-Anfangsgeschwindigkeit in der Größenordnung von 1.000 m/s und die Geschwindigkeit des nach innen beschleunigten Hohlzylinders auf Grund der relativ geringen Verdämmung noch bei etwa 500 m/s. Bei der Kombination einer 8 mm dicken Stahlhülle mit einer 20 mm dicken Sprengstoffschicht sowie einer unterschiedlichen inneren Verdämmung schwanken die Werte zwischen 800 m/s (hohe Verdämmung) und 200 m/s (geringe Verdämmung). Diese Berechnungsbeispiele zeigen auch, dass es mit Anordnungen entsprechend der vorliegenden Erfindung möglich ist, einen großen Bereich von Splitter- bzw. Subgeschossgeschwindigkeiten abzudecken.Further calculation examples: Without boundary effects (ie assuming a sufficiently extended element size), the theoretical speed is 5 mm steel coverage, large explosive thickness (> 20 mm) and high internal containment above 2,000 m / s. With a shell thickness of 5 mm and a 5 mm thick explosive layer and an inner damming by a hollow aluminum cylinder with a thickness of 20 mm, the initial splitter speed in the order of 1,000 m / s and the speed of the inwardly accelerated hollow cylinder due the relatively low attenuation still at about 500 m / s. When combining an 8 mm thick steel shell with a 20 mm thick layer of explosive and a different internal insulation, the values vary between 800 m / s (high damming) and 200 m / s (low damming). These calculation examples also show that with arrangements according to the present invention it is possible to cover a wide range of splitter and sub-floor speeds, respectively.
Bei der Abschätzung der Splittergeschwindigkeit zylindrischer Aufbauten bietet sich eine für Sprengmunition herkömmlicher Bauart geltende Gurney-Gleichung an:
Folgende Berechnungsbeispiele sollen die Verhältnisse bei dieser Betrachtungsweise veranschaulichen: Bei einem Außendurchmesser von 100 mm und einer Wandstärke der Hülle von 10 mm (Innendurchmesser 80 mm) sowie einer Dicke der Sprengstoffschicht von 5 mm ergeben sich als Splitter- /Hüllengeschwindigkeit 25% der Gurney-Geschwindigkeit. Bei einem Innendurchmesser von 40 mm (also bei 20 mm Sprengstoffschicht-Dicke) ergeben sich 45% der Gurney-Geschwindigkeit, also etwa 1.260 m/s. Bei einem Innendurchmesser von 60 mm und einer 10 mm dicken Sprengstoffschicht errechnen sich 35% der Gurney-Geschwindigkeit (ca. 1.000 m/s). Bei mit Sprengstoff gefüllter Hülle ergeben sich 50% der Gurney-Geschwindigkeit, also ca. 1.400 m/s. Bei idealer einseitiger (innerer) Verdämmung und einer sehr dicken Sprengstoffschicht (> 30 mm) wird bei großen Flächen (bzw. Durchmessern) die Gurney-Geschwindigkeit annähernd erreicht.The following calculation examples are intended to illustrate the conditions in this approach: With an outer diameter of 100 mm and a wall thickness of the shell of 10 mm (
Über die innere Verdämmung, die ein zentrales Merkmal der Erfindung darstellt, erfolgt die optimale Umsetzung der Sprengstoffenergie in Splittergeschwindigkeit, sodass entsprechend hohe Geschwindigkeiten bei relativ geringen Sprengstoffdicken möglich werden. Der Einfluss der inneren Verdämmung kann über einen Faktor berücksichtigt werden, der als Verdämmungsfaktor (VF) bezeichnet werden soll. Er ist von den Größen M/C, MinnereVerdämmung/MHülle, rhoKern, sigmaKern und den Hygoniot-Eigenschaften des inneren Mediums abhängig. Es kann von folgenden Schätzwerten ausgegangen werden: Bei dicken Hüllen und dicker Sprengstoffschicht sowie bei dünnen Hüllen und dicker Sprengstoffschicht ergibt sich ein Verdämmungsfaktor von 1,1 bis 1,2. Dies entspricht einer Geschwindigkeitssteigerung von 10% bis 20%. Bei einer dicken Hülle, kombiniert mit dünner Sprengstoffschicht sowie einer dünnen Hülle mit dicker Sprengstoffschicht ergibt sich ein Verdämmungsfaktor von 1,2 bis 1,3 (20% bis 30% Geschwindigkeitssteigerung). Damit lassen sich nicht nur über hohe Verdämmungen und entsprechende Sprengstoffe sehr hohe Splittergeschwindigkeiten bis etwa 2.000 m/s und starke Hüllenfragmentierungen erreichen, sondern auf der anderen Seite über gering verdämmende Innenkörper und trägere Sprengstoffe relativ geringe Splitter- oder Subgeschossgeschwindigkeiten bei entsprechend sanfter Beschleunigung erzielen.About the inner damming, which is a key feature of the invention, the optimal implementation of the explosive energy in fragmentation speed, so that correspondingly high speeds at relatively low explosive thicknesses possible. The influence of the inner damming can be taken into account by a factor, which should be called the Damming Factor (VF). It is dependent on the sizes M / C, M inner-insulation / M- shell , Rho- core , sigma- core and the Hygoniot-properties of the inner medium. The following estimates can be assumed: Thick sheaths and thick explosive layers as well as thin sheaths and thick explosive layers result in a factor of 1.1 to 1.2. This corresponds to a speed increase of 10% to 20%. A thick shell, combined with a thin explosive layer and a thin shell with a thick layer of explosives, results in a damming factor of 1.2 to 1.3 (20% to 30% increase in speed). This not only very high splintering speeds and corresponding explosives can be achieved very high splitter speeds up to about 2,000 m / s and strong shell fragmentation, but on the other hand on low damming inner body and inert explosives achieve relatively low splinter or sub-floor speeds with correspondingly gentle acceleration.
- Fig. 1 AFig. 1 A
- Grundsätzlicher Aufbau eines drallstabilisierten Sprengstoffschicht-Splittergeschosses mit Splittermantel, Sprengstoffschicht und verdämmendem Innenkörper sowie und Steuer- bzw. Zündelementen.Fundamental structure of a spin-stabilized explosive layer fragmentation projectile with splinter shell, explosive layer and damming inner body as well as control and ignition elements.
- Fig. 1 BFig. 1 B
- Grundsätzlicher Aufbau eines aerodynamisch stabilisierten Sprengstoffschicht-Splittergeschosses mit Splittermantel, Sprengstoffschicht und verdämmendem Innenkörper sowie und Steuer- bzw. Zündelementen.Basic structure of an aerodynamically stabilized explosive layer-splitter projectile with splinter shell, explosive layer and damming inner body as well as control and ignition elements.
- Fig. 2Fig. 2
- Beispiel für die Querschnittsgestaltung eines Sprengstoffschicht-Splittergeschosses mit Splitterhülle, Sprengstoffschicht und verdämmendem Innenkörper.Example of the cross-sectional design of an explosive layer fragmentation projectile with splinter shell, explosive layer and damming inner body.
- Fig. 3Fig. 3
- Querschnitt durch ein Sprengstoffschicht-Splittergeschoss mit verdämmendem Innenring bzw. verdämmendem hohlen Innenkörper.Cross-section through an explosive layer chippings bullet with damming inner ring or damming hollow inner body.
- Fig. 4Fig. 4
- Querschnitt durch ein Sprengstoffschicht-Splittergeschoss mit mehrschichtigem verdämmendem Innenaufbau.Cross section through an explosive layer chipboard with multi-layer damming internal structure.
- Fig. 5Fig. 5
- Beispiel für die Querschnittsgestaltung mit kreisförmigem Außenquerschnitt und beliebigem (hier achteckigem) Innenquerschnitt der Sprengstoffschicht.Example of the cross-sectional configuration with a circular outer cross section and any (here octagonal) inner cross section of the explosive layer.
- Fig. 6Fig. 6
- Beispiel für die Querschnittsgestaltung mit verdämmendem Innenkörper und kreisförmigem Innenquerschnitt und beliebigem (hier achteckigem) Außenquerschnitt der Sprengstoffschicht.Example of the cross section design with damming inner body and circular inner cross section and any (here octagonal) outer cross section of the explosive layer.
- Fig. 7Fig. 7
- Beispiel für die Querschnittsgestaltung mit beliebigem (hier quadratischem) Querschnitt des verdämmendem Innenkörpers und segmentiertem Detonationsquerschnitt / Sprengstoff-Flächensegmente (hier: durch den Innenkörper getrennt mit gleichzeitiger oder nicht gleichzeitiger Zündung).Example of the cross-sectional configuration with arbitrary (here square) cross section of the damming inner body and segmented detonation cross section / explosive surface segments (here: separated by the inner body with simultaneous or non-simultaneous ignition).
- Fig. 8Fig. 8
- Beispiel für die Querschnittsgestaltung mit einem Innenkörper beliebigen (hier dreieckigen) Querschnitts und inerten, Druckübertragenden Ausgleichssegmenten zwischen Innenkörper und Sprengstoffschicht.Example of the cross-sectional configuration with an inner body of any (here triangular) cross-section and inert, pressure-transmitting compensation segments between inner body and explosive layer.
- Fig. 9Fig. 9
- Querschnitt mit mehreren (hier zwei) verdämmenden hohlen Innenkörpern und einer dynamisch wirkendem Schicht zwischen Sprengstoffschicht und Innenverdämmung (oben) und/oder zwischen den unterschiedlichen Innenverdämmungen (unten).Cross-section with several (here two) damming hollow inner bodies and a dynamically acting layer between the explosive layer and inner damming (top) and / or between the different inner dammings (bottom).
- Fig. 10Fig. 10
- Querschnitt mit verdämmendem Innenkörper und einer dynamisch wirkenden Schicht zwischen Sprengstoffschicht und Splitterhülle.Cross-section with damming inner body and a dynamically acting layer between explosive layer and splinter shell.
- Fig. 11Fig. 11
- Beispiel für die Querschnittsgestaltung mit Außenhülle / Geschossmantel und darunter liegendem Splittermantel (oben) und einer zusätzlichen, dynamisch wirkenden Schicht zwischen Sprengstoffschicht und Splitterhülle (unten).Example of the outer sheath / bullet jacket cross-section design and underlying fragmentation shroud (top) and an additional, dynamically acting layer between explosive layer and fragment sheath (bottom).
- Fig. 12Fig. 12
- Beispiel für die Querschnittsgestaltung mit Außenhülle und Splitterkörper / vorgeformte Geschosse / thermische oder mechanische Splitterbildende Maßnahmen enthaltende Zwischenschicht.Example of the cross-sectional design with outer shell and fragment body / preformed projectiles / intermediate layer containing thermal or mechanical fragmentation measures.
- Fig. 13Fig. 13
- Beispiel für die Querschnittsgestaltung mit (hier quadratischem) verdämmendem Innenkörper und Sprengstoffsegmenten mit flächenhafter / linienförmiger / punktförmiger Zündeinrichtung in der Sprengstoffschicht (oben) oder mit in den Innenkörper eingebrachten Zündelementen.Example of the cross-sectional configuration with (here square) damming inner body and explosive segments with planar / linear / punctiform ignition device in the explosive layer (top) or with introduced into the inner body ignition elements.
- Fig. 14Fig. 14
- Beispiel für die Querschnittsgestaltung mit beliebig (hier quadratisch) geformter Sprengstofffläche und Druckübertragenden Segmenten zwischen Sprengstoffschicht und Splittermantel bzw. Geschosshülle.Example of the cross-sectional design with arbitrarily (in this case square) shaped explosive surface and pressure-transmitting segments between explosive layer and fragment shell or projectile casing.
- Fig. 15Fig. 15
- Beispiel für die Querschnittsgestaltung mit zweischichtiger Sprengstoffbelegung und zwei Verdämmungsschichten.Example of the cross-sectional design with two-layer explosive coating and two layers of insulation.
- Fig. 16Fig. 16
- Beispiel für ein Geschoss oder einen Gefechtskopf mit mehrteiligem Innenkörper (hier aus vier Kreissegmenten gleichen oder ungleichen Materials bestehend) mit zentralem pyrotechnischem Körper.Example of a projectile or a warhead with a multipart inner body (here consisting of four circle segments of the same or dissimilar material) with a central pyrotechnic body.
- Fig. 17Fig. 17
- Beispiel für ein Geschoss oder einen Gefechtskopf mit mehrteiligem Innenkörper (hier vier zylindrische Penetratoren) mit zentralem pyrotechnischem Körper (oben) oder inertem zentralem Körper bzw. leerem Innenvolumen.Example of a bullet or a warhead with multipart inner body (here four cylindrical penetrators) with central pyrotechnic body (top) or inert central body or empty interior volume.
- Fig. 18Fig. 18
- Beispiel für die Querschnittsgestaltung mit Geschosshülle / geometrisch gestalteter Innenfläche des Splittermantels / entsprechend geformter Sprengstoffschicht und Innenverdämmung.Example of the cross-sectional design with projectile casing / geometrically shaped inner surface of the fragmentation shell / correspondingly shaped explosive layer and inner insulation.
- Fig. 19Fig. 19
- Beispiel für die Querschnittsgestaltung mit geometrisch gestalteter Innenfläche des Splittermantels und entsprechend geformter Sprengstoffschicht.Example of the cross-sectional design with geometrically shaped inner surface of the splinter shell and correspondingly shaped explosive layer.
- Fig. 20Fig. 20
- Beispiel für die Querschnittsgestaltung mit geometrisch geformter Innenfläche der Sprengstoffschicht (oben) oder Sprengstoff-Längsstreifen oder Sprengstoff-Flächenelementen (unten).Example of cross-section design with geometrically shaped inner surface of the explosive layer (top) or explosive longitudinal stripes or explosive surface elements (bottom).
- Fig. 21Fig. 21
- Beispiel für die Querschnittsgestaltung mit Innenverdämmung und in die Sprengstoffschicht eingebrachten trennenden Elementen oder geometrischen Strukturen (hier Längsstreifen).Example of the cross-sectional design with internal insulation and in the explosive layer introduced separating elements or geometric structures (here longitudinal strips).
- Fig. 22Fig. 22
- Beispiel für die Querschnittsgestaltung mit einem verdämmendem hohlen Innenring und einem als Behälter ausgeführten zentralen / verdämmenden Innenkörper.Example of the cross-sectional design with a hollow cylindrical inner ring and a central / damming inner body designed as a container.
- Fig. 23Fig. 23
- Beispiel für die Querschnittsgestaltung mit einem verdämmendem zentralen Behälter (oben) bzw. einem zentralen Innenkörper und einem mit Stegen versehenen Raum zwischen Sprengstoffschicht und Innenkörper.Example of the cross-sectional configuration with a damming central container (top) or a central inner body and a provided with webs space between the explosive layer and inner body.
- Fig. 24Fig. 24
-
Beispiel für einen Längsschnitt mit Splittermantel, Sprengstoffschicht, verdämmendem (hier zweiteiligem) Innenkörper sowie Steuer- bzw.
Zündelemente für die Sprengstoffschicht.Example of a longitudinal section with splinter shell, explosive layer, damming (here two-part) inner body and control or
Ignition elements for the explosive layer. - Fig. 25Fig. 25
- Beispiel für einen Längsschnitt mit veränderlicher Sprengstoffdicke und zylindrischem Splittermantel (oben) und mit veränderlicher Splittermantel- und Sprengstoffdicke (unten).Example of a longitudinal section with variable explosive thickness and cylindrical fragment shell (top) and with variable fragment shell and explosive thickness (bottom).
- Fig. 26Fig. 26
- Beispiel für einen Längsschnitt mit Sprengstoffschicht / Innenkörper-Durchmessersprung (oben) oder geteiltem verdämmenden Körper / eingesetztem Penetratorkörper oder Penetratorring (unten).Example of a longitudinal section with explosive layer / inner diameter jump (above) or split damming body / inserted penetrator body or penetrator ring (below).
- Fig. 27Fig. 27
- Beispiel für einen Längsschnitt mit Durchmessersprung von Splitterhülle und Sprengstoffschicht.Example of a longitudinal section with diameter jump of splinter shell and explosive layer.
- Fig. 28Fig. 28
- Beispiel für einen Längsschnitt mit mehrteiligen (hier getrennten) Sprengstoffschichten und (hier) unterschiedlichem Splitterhüllendurchmesser (oben) oder durchgehender Sprengstoffschicht mit Durchmessersprung (unten).Example of a longitudinal section with multi-part (here separated) explosive layers and (here) different splinter shell diameter (top) or continuous explosive layer with a diameter jump (bottom).
- Fig. 29Fig. 29
- Beispiel für die geometrische Gestaltung des Splittermantels zum Erzielen gewünschter Effekte oder bevorzugter Splitterrichtungen. Hier: Richtungssteuerung und Drehung der Splitterkörper / Splitterringe und durchgehender Sprengstoffschicht mit zylindrischem verdämmendem Innenkörper.Example of the geometric design of the splinter shell to achieve desired effects or preferred splitter directions. Here: Direction control and rotation of the fragment body / splinter rings and continuous explosive layer with cylindrical damming inner body.
- Fig. 30Fig. 30
- Beispiel für die geometrische Gestaltung des Splittermantels zum Erzielen gewünschter Effekte oder bevorzugter Splitterrichtungen. Hier: Richtungssteuerung der Splitterkörper und getrennte Sprengstoffschichten und geometrisch angepasster verdämmender Innenkörper.Example of the geometric design of the splinter shell to achieve desired effects or preferred splitter directions. Here: Direction control of the fragment bodies and separate explosive layers and geometrically adapted damming inner body.
- Fig. 31Fig. 31
- Beispiel für die geometrische Gestaltung des Splittermantels zum Erzielen gewünschter Effekte oder bevorzugter Splitterrichtungen. Hier: Sprengstoffbelegung für unterschiedliche Splitterrichtungen und Splittergeschwindigkeiten.Example of the geometric design of the splinter shell to achieve desired effects or preferred splitter directions. Here: explosive charge for different splinter directions and splitter speeds.
- Fig. 32Fig. 32
- Beispiel für einen Längsschnitt durch ein Sprengstoffschicht-Splittergeschoss oder Gefechtskopf mit innen liegendem sprengstoffbelegtem Splitterkörper und einem Zwischenraum zwischen Außenhülle und Splitterkörper sowie einer leeren oder teilweise gefüllten außenballistischen Haube (oben) oder einer massiven/gefüllten Spitze (unten).Example of a longitudinal section through an explosive layer chipboard or warhead with internal explosive occupied fragment body and a space between the outer shell and Sliver body and an empty or partially filled outer ballistic hood (top) or a solid / filled top (bottom).
- Fig. 33Fig. 33
- Beispiel für einen Längsschnitt mit vollständiger Sprengstoffbelegung (Geschosskörper und Spitzenbereich - oben) und sprengstoffgefüllter Spitze (unten).Example of a longitudinal section with complete explosive coverage (projectile body and tip area - top) and explosive-filled tip (bottom).
- Fig. 34Fig. 34
- Beispiel für einen Längsschnitt mit einem in den verdämmenden Innenbereich eingesetzten Sprengstoffkörper.Example of a longitudinal section with an explosives body inserted into the damming interior.
- Fig. 35Fig. 35
- Beispiel für einen Längsschnitt mit einem in den verdämmenden Innenbereich eingebetteten Kern (oben) oder schlanken Zylinder mit Spitze (unten).Example of a longitudinal section with a core embedded in the damming inner area (top) or a slender cylinder with a top (bottom).
- Fig. 36Fig. 36
- Beispiel für einen Längsschnitt mit einem in den verdämmenden Innenbereich eingebetteten spitzen Kern mit fokussierender / den Heckbereich des Kerns zerlegender Sprengstoffhinterlegung (oben) oder einem Kern mit Stufenspitze und zentrierender (den Kern beschleunigender) Sprengstoffhinterlegung (unten).Example of a longitudinal section with a pointed core embedded in the damming inner area with focusing / decaying explosive deposit (top) or core with step tip and centering (core accelerating) explosive deposit (bottom).
- Fig. 37Fig. 37
- Beispiel für einen Längsschnitt mit geometrisch gestaltetem Innenkörper und entsprechender Sprengstoffbelegung zur gerichteten Splitterwirkung (oben) oder mit Splitter-Richtwirkung durch Formgebung von verdämmendem Innenkörper, Sprengstofffläche und Splitterhülle (unten).Example of a longitudinal section with geometrically designed inner body and corresponding explosive assignment for directional splintering effect (top) or with splitter directivity by shaping of damming inner body, explosive surface and splinter casing (bottom).
- Fig. 38Fig. 38
-
Beispiel für einen Längsschnitt entsprechend
Fig. 37 mit zusätzlichen Splitterkomponenten.Example of a longitudinal section accordinglyFig. 37 with additional splitter components. - Fig. 39Fig. 39
- Beispiel für einen Längsschnitt mit (hier) zweistufiger gerichteter Splitterwirkung und durchgehender Sprengstoffbelegung (oben) und nicht durchgehender Sprengstoffbelegung (unten).Example of a longitudinal section with (here) two-stage directional fragmentation effect and continuous explosive charge (top) and non-continuous explosive charge (bottom).
- Fig. 40Fig. 40
- Beispiel für einen Längsschnitt mit zusätzlichem, primär axial beschleunigtem Splitterkegel im vorderen Bereich des Geschosses, beschleunigt durch eine Sprengstofffläche.Example of a longitudinal section with additional, primarily axially accelerated splinter cone in the front area of the projectile, accelerated by an explosive surface.
- Fig. 41Fig. 41
- Zwei Beispiele für einen Längsschnitt mit Vorkern/Stufenkern als verdämmendem Medium.Two examples of a longitudinal section with pronuclear / step core as damming medium.
- Fig. 42Fig. 42
- Beispiel für die Querschnittsgestaltung mit sprengstoffbeschleunigten einzelnen Segmenten.Example of the cross-sectional design with explosive-accelerated individual segments.
- Fig. 43Fig. 43
- Beispiel für die Querschnittsgestaltung mit veränderlicher Dicke des Splittermantels und (hier vier) Sprengstoffsegmenten mit linsenförmigem (grundsätzlich frei zu gestaltenden) Querschnitt.Example of the cross-sectional configuration with variable thickness of the splinter shell and (here four) explosive segments with lenticular (in principle free to design) cross-section.
- Fig. 44Fig. 44
- Beispiel für die Querschnittsgestaltung mit einer geformten Sprengstofffläche und angepasstem verdämmenden Innenkörper.Example of the cross-sectional design with a shaped explosive surface and adapted inner damming body.
- Fig. 45Fig. 45
- Beispiel für die Querschnittsgestaltung mit (hier acht) Segmenten und frei gestalteter Sprengstofffläche.Example of the cross-sectional design with (here eight) segments and freely designed explosive surface.
- Fig. 46Fig. 46
- Beispiele für einen Längsschnitt mit mehrteiligem verdämmendem Innenkörper (z.B. radial und axial geteilt).Examples of a longitudinal section with multi-part damming inner body (e.g., radially and axially divided).
- Fig. 47Fig. 47
-
Beispiel für die Querschnittsgestaltung eines Geschosses oder Gefechtskopfes nach
Fig. 42 mit verdämmendem Innenkörper, hier aufgebaut aus Zylindern in einer Druckübertragenden Matrix.Example of the cross-sectional design of a projectile or warhead according toFig. 42 with damming inner body, here constructed of cylinders in a pressure-transmitting matrix. - Fig. 48Fig. 48
-
Beispiel für die Querschnittsgestaltung eines Geschosses oder Gefechtskopfes nach
Fig. 43 mit segmentiertem, ein- oder mehrschichtigem verdämmendem Innenkörper sowie zentralem Penetrator.Example of the cross-sectional design of a projectile or warhead according toFig. 43 with segmented, single or multilayer damming inner body and central penetrator. - Fig. 49Fig. 49
- Beispiel für einen Längsschnitt, ausgeführt als mehrteiliger Wirkkörper (unterschiedliche Stufen mit unterschiedlichen Funktionen) und unterschiedlicher Ausgestaltung bzw. Belegung.Example of a longitudinal section, executed as a multi-part active body (different levels with different functions) and different configuration or occupancy.
- Fig. 50Fig. 50
- Beispiel für die beliebige Querschnittsgestaltung eines Sprengstoffschicht-Splittergeschosses oder Gefechtskopfes.Example of the arbitrary cross-sectional configuration of an explosive layer chip projectile or warhead.
- Fig. 5151
- Weiteres Beispiel für die beliebige Querschnittsgestaltung.Another example of the arbitrary cross-sectional design.
Das erfindungsgemäße Funktionsprinzip erlaubt gleichermaßen die Anwendung auf aerodynamisch stabilisierte Geschosse, wie in
In
So zeigt
Weitere wirkungsrelevante Eigenschaften sind die geometrischen Abmessungen der Splitterhülle bzw. deren Masse und auch deren mechanische dynamische Eigenschaften. Es ist jedoch ein besonderer Vorzug der Erfindung, dass keinerlei besonderen Ansprüche an die einzelnen Komponenten zu stellen sind. So sind nahezu sämtliche Eigenschaften durch eine entsprechende Materialwahl ohne hohen technischen Aufwand zu erreichen.Further impact-relevant properties are the geometric dimensions of the fragmentation shell or its mass and also their mechanical dynamic properties. However, it is a particular advantage of the invention that no special demands are placed on the individual components. So almost all properties can be achieved by a suitable choice of material without high technical complexity.
In
In
Für die Eigenschaften und die technische bzw. materialspezifische Ausgestaltung der Splitterhülle bzw. des Geschoss- oder Gefechtskopfmantels kommen grundsätzlich alle Ausführungsformen und technologischen Möglichkeiten in Betracht, die im Zusammenhang mit herkömmlichen Splittergeschossen bekannt sind.For the properties and the technical or material-specific design of the fragmentation shell or the projectile or warhead mantle basically all embodiments and technological possibilities come into consideration, which are known in connection with conventional fragmentation projectiles.
In
Ein weiterer Aufbau für ein Geschoss gemäß der Erfindung ist in
Der obere Bildteil von
In
Einen ähnlichen Aufbau zeigt der untere Teilquerschnitt in
In
In
In
In
Das Prinzip der segmentierten Sprengstoffhülle ist auch in
Auch in
Nach diesen Beispielen für die Querschnittsgestaltung von Anordnungen entsprechend der vorliegenden Erfindung folgt in
So zeigt
In
In
Bei den Beispielen in
Durch Anordnungen entsprechend der vorliegenden Erfindung sind auf technisch besonders einfache Weise höchst wirkungsvolle Kombinationen bzw. Ausgestaltungen von Splitterhüllen und Sprengstoffschichten zu erreichen. Ausgehend von einem Geschoss entsprechend
So zeigt
In
In
In
In
In
Bei den bisher dargestellten Beispielen wurden zylindrische Splitterhüllen dargestellt. Dies ist selbstverständlich keine zwingende Voraussetzung für Anordnungen entsprechend der Erfindung. Durch schichtartige beschleunigende Elemente können vielmehr beliebige Formen auch bei äußeren Komponenten ohne jede Einschränkung der Wirksamkeit realisiert werden. Dadurch sind der gestalterischen Möglichkeit keine Grenzen gesetzt. Ebenso selbstverständlich ist es auch, dass Anordnungen entsprechend der Erfindung nicht auf einzelne Körper beschränkt sind. Gerade durch die gestalterische Freiheit können entsprechende splitterbildende Einrichtungen in Gruppen angeordnet sein.In the examples presented so far cylindrical fragmentation sheaths were shown. This is of course no mandatory requirement for arrangements according to the invention. By layer-like accelerating elements rather any shapes can be realized even with external components without any limitation of the effectiveness. As a result, there are no limits to the design possibilities. It is equally obvious that arrangements according to the invention are not limited to individual bodies. Precisely by the creative freedom, corresponding fragment-forming devices can be arranged in groups.
In
Selbstverständlich sind die als Beispiele aufgeführten Anordnungen auch sowohl in einem Geschoss als auch in einem Gefechtskopf kombinierbar, soweit dies sinnvoll ist.Of course, the arrangements listed as examples can also be combined both in a projectile and in a warhead, if this makes sense.
Im Folgenden sind die wesentlichen Merkmale und die Vorteile der Erfindung zusammengefasst:The main features and advantages of the invention are summarized below:
Die splitterbildenden Wirkkomponenten bzw. die Splitter oder Subgeschosse enthaltenden Hüllen werden über eine im Verhältnis zum Geschoss- oder Gefechtskopfdurchmesser dünnen Sprengstoffschicht beschleunigt.The shatter-forming active components or sheaths containing fragments or sub-projectiles are accelerated by means of an explosive layer which is thin relative to the projectile or warhead diameter.
Die für die Beschleunigung von Splittern benötigte Sprengstoffmasse wird minimiert. Gegenüber herkömmlichen Sprenggeschossen kann bei vergleichbaren Splitter- bzw. Subgeschossgeschwindigkeiten die Sprengstoffmasse je nach Kaliber und technischer Ausgestaltung um 50% bis 80% vermindert werden.The explosive mass needed to accelerate splinters is minimized. Compared with conventional explosive projectiles, the explosive mass can be reduced by 50% to 80%, depending on the caliber and technical design, at comparable splinter or sub-floor speeds.
Die eingesparte Sprengstoffmasse steht als zusätzliche Wirkmasse zur Verfügung. Dadurch wird der Spielraum bei der Auslegung von Splitter oder Subgeschosse beschleunigenden Geschossen oder Gefechtsköpfen erheblich erweitert.The saved explosive mass is available as additional active mass. As a result, the scope in the interpretation of splinters or sub-projectiles accelerating projectiles or warheads is considerably expanded.
Die geringste Stärke der Sprengstoffschicht wird durch die Sicherstellung der Zündung bzw. einer Durchzündung bestimmt. Durch eingebrachte Zündhilfen wie etwa Sprengschnüre können sehr dünne flächenhafte Sprengstoffschichten gezündet werden. Ebenso ist die Wahl des Sprengstoffs frei, sodass sehr geringe Dicken bis zu einer Größenordnung von 2 mm realisiert werden können.The least strength of the explosive layer is determined by ensuring ignition or spark ignition. By introduced ignition aids such as detonating cords very thin planar explosive layers can be ignited. Likewise, the choice of explosive is free, so that very small thicknesses up to an order of 2 mm can be realized.
Über größere Sprengstoff-Schichtstärken können je nach innerer Verdämmung entsprechend dicke Hüllen zerlegt bzw. auf hohe Geschwindigkeiten beschleunigt werden. Die theoretische Maximalgeschwindigkeit der Splitter wird bei Sprengstoffschichten in der Größenordnung von 20 mm bei hoher Innenverdämmung annähernd erreicht.Larger explosive layer thicknesses can be used to disassemble or accelerate to high speeds, depending on the internal insulation. The theoretical maximum speed of the splinters is approximately reached with explosive layers in the order of 20 mm with high internal insulation.
Die Sprengstoffschicht kann in Form eines Hohlzylinders ausgebildet sein und eine gleich bleibende oder veränderliche Wandstärke und / oder Querschnittsform besitzen.The explosive layer may be in the form of a hollow cylinder and have a constant or variable wall thickness and / or cross-sectional shape.
Die Sprengstoffschicht kann als Folie oder als beliebig geformter Körper vorgefertigt und eingebracht sein, eingegossen werden oder auf beliebige Weise eingebracht werden wie z.B. eingepresst oder über Unterdruck eingesogen werden. Sie kann aus einer oder aus mehreren übereinander liegenden Schichten bestehen.The explosive layer can be prefabricated and incorporated as a film or as an arbitrarily shaped body, be cast in or introduced in any manner, such as e.g. pressed or sucked in by vacuum. It can consist of one or more superimposed layers.
Ein Geschoss oder Gefechtskopf kann eine durchgehende Sprengstoffschicht enthalten oder aus mehreren Sprengstoffschichten sowohl in axialer als auch in radialer Richtung aufgebaut sein.A projectile or warhead may contain a continuous layer of explosive or may be composed of multiple explosive layers in both the axial and radial directions.
Die Sprengstoffschicht kann homogen sein oder Beimengungen bzw. eingebettete Körper enthalten.The explosive layer may be homogeneous or contain admixtures or embedded bodies.
Die Zündung der Sprengstoffschicht oder der Sprengstoffzonen bzw. der Sprengstofffragmente kann auf jede denkbare Art und Weise entsprechend dem Stand der Technik bei Sprenggeschossen oder Gefechtsköpfen erfolgen.Ignition of the explosive layer or zones or explosive fragments may be accomplished in any conceivable manner in accordance with the prior art blasting projectiles or warheads.
Über die Art der Zündung und die Ausgestaltung der Sprengstoffschicht und der Innenkörper können die Geschwindigkeiten und die Richtung der Splitter- bzw. Subgeschosse in sehr weiten Grenzen variiert werden.About the type of ignition and the design of the explosive layer and the inner body, the velocities and the direction of the fragmentation or sub-projectiles can be varied within very wide limits.
Der verdämmende innere Körper kann ein- oder mehrteilig sein. Er kann aus metallischen oder nichtmetallischen Materialien bestehen oder aus deren Kombination. Damit steht eine nahezu unbegrenzte Vielfalt von Materialien unterschiedlicher mechanischer, physikalischer oder chemischer Eigenschaften zur Auswahl. So kann ein homogener metallischer Innenkörper auf der einen Seite z.B. aus einem Metall geringer Dichte wie etwa Magnesium bestehen, auf der anderen Seite aus einem Schwer- oder Hartmetallkörper (homogen oder segmentiert) großer Dichte mit entsprechend hohem endballistischem Leistungsvermögen.The damming inner body can be one or more parts. It may consist of metallic or non-metallic materials or of their combination. There is thus an almost unlimited variety of materials with different mechanical, physical or chemical properties to choose from. Thus, a homogeneous metallic inner body on one side, e.g. consist of a metal of low density such as magnesium, on the other side of a heavy or hard metal body (homogeneous or segmented) high density with a correspondingly high end ballistic performance.
Über die Eigenschaften des Innenkörpers oder der Innenkörper unter Hochdruckbelastung (Hygoniot-Eigenschaften) kann deren Verhalten bestimmt werden bzw. es können in Verbindung mit den eingesetzten pyrotechnischen Komponenten und der technischen Ausgestaltung des Geschosses oder Gefechtskopfes gezielt Materialien mit bestimmten dynamischen Eigenschaften ausgewählt werden.On the properties of the inner body or the inner body under high pressure load (Hygoniot properties) can be determined their behavior or it can be selectively selected materials with specific dynamic properties in conjunction with the pyrotechnic components used and the technical design of the projectile or warhead.
Homogene verdämmende inerte Innenkörper können aus einem unter hohem Druck bei örtlich auftretender hoher Temperatur reaktionsfähigen metallischen oder nichtmetallischen Stoff bestehen oder solche Stoffe enthalten.Homogeneous inert inner damming bodies may consist of or contain such metallic or non-metallic matter which is reactive under high pressure at locally high temperature.
Durch die Kombinationsmöglichkeiten bei verdämmenden Innenkörpern ergibt sich, dass (z.B. durch den Einsatz unterschiedlicher Materialien wie etwa durch Einbetten von Subgeschossen in einen Matrixwerkstoff) der Auslegungsbandbreite praktisch keine Grenzen gesetzt sind.Due to the combination possibilities with damming inner bodies, it follows that (eg through the use of different materials, such as by embedding of sub-floors in a matrix material) the design bandwidth are practically no limits.
Der verdämmende Innenkörper kann aus sprödem oder unter dynamischer Belastung versprödendem Material sein. Ebenso kann er vorfragmentiert oder mechanisch oder thermisch vorbehandelt dein.The damming inner body can be made of brittle or embrittled under dynamic load material. Likewise, he can pre-fragmented or mechanically or thermally pretreated yours.
Der verdämmende Innenkörper kann auch als Hohlzylinder ausgeführt sein oder bei beliebiger Querschnittsfläche einen Hohlraum enthalten. Dieser innere Hohlraum kann wiederum leer oder mit einem ebenfalls mehr oder weniger verdämmenden Stoff gefüllt sein. Damit ergibt sich eine weitere Möglichkeit für die Einflussnahme auf die Verdämmung und damit auf die Geschwindigkeit bzw. die Beschleunigung der Hülle von splitterbildenden oder Subgeschosse ausstoßenden Geschossen oder Gefechtsköpfen.The damming inner body can also be designed as a hollow cylinder or contain a cavity in any cross-sectional area. This inner cavity may in turn be empty or filled with a more or less damming substance. This results in a further possibility for influencing the damming and thus the speed or the acceleration of the shell of fragment-forming or sub-projectile projectiles or warheads.
In einer besonderen Ausgestaltung kann der verdämmende Innenkörper einen Behälter darstellen oder einen solchen enthalten. Der innere Hohlraum bzw. der eingebrachte Behälter kann z.B. mit einem festen, pulverförmigen, pastösen oder flüssigen Stoff gefüllt sein. Weiterhin kann er einen reaktionsfähigen Stoff wie z.B. eine brennbare Flüssigkeit enthalten.In a particular embodiment, the damming inner body can represent or contain a container. The inner cavity or container may be e.g. be filled with a solid, powdery, pasty or liquid substance. Furthermore, it may contain a reactive substance, e.g. contain a flammable liquid.
Im einfachsten Fall ist die Hülle des Geschosses oder des Gefechtskopfes homogen. Hinsichtlich ihrer Vorbehandlung zur Unterstützung der Splitterbildung können alle Verfahren und Techniken eingesetzt werden, die dem technischen Stand bei herkömmlichen Splittergeschossen entsprechen.In the simplest case, the shell of the projectile or the warhead is homogeneous. With regard to their pretreatment in support of fragmentation, it is possible to use all methods and techniques which correspond to the state of the art in conventional fragmentation projectiles.
Die beschleunigte Hülle kann auch ganz oder teilweise aus vorgeformten Splittern oder Subgeschossen bestehen. Eine derartige Schicht kann selbst die Geschosshülle darstellen oder als Schicht zwischen dem Sprengstoff und der Außenhülle eingebracht sein. Über diesen Aufbau kann zwischen Sprengstoffschicht und Außenhülle auch eine vorfragmentierte oder sehr spröde bzw. eine unter dynamischer Belastung versprödende Schicht eingebracht sein.The accelerated shell may also consist wholly or partly of preformed splinters or sub-floors. Such a layer may itself represent the projectile casing or be incorporated as a layer between the explosive and the outer shell. About this structure can be introduced between the explosive layer and the outer shell and a pre-fragmented or very brittle or embrittled under dynamic load layer.
Bei einer großkalibrigen Munition oder bei Gefechtsköpfen ist es auch denkbar, dass sich zwischen der Sprengstoffschicht und der Außenhaut eine mit einem pastösen oder liquiden Stoff gefüllte Zwischenschicht befindet, die auch feste Stoffe oder einzelne Körper enthalten kann.In a large caliber ammunition or warheads, it is also conceivable that between the explosive layer and the outer skin is filled with a pasty or liquid substance intermediate layer, which may also contain solids or individual body.
Zwischen der Sprengstoffschicht und dem verdämmenden Innenkörper kann sich eine die Verdämmung dynamisch unterstützende Schicht befinden. Deren Wirkungsweise wird durch die akustische Impedanz der beteiligten Materialien bestimmt.Between the explosive layer and the damming inner body there may be a layer dynamically supporting the damming. Their mode of action is determined by the acoustic impedance of the materials involved.
Ebenso kann zwischen der Sprengstoffschicht und der Splitterhülle ein dynamisch dämpfend wirkendes Medium als eine den Beschleunigungsstoß mindernde Schicht eingebracht sein.Likewise, between the explosive layer and the fragmentation shell, a medium having a dynamic damping action can be introduced as a layer which reduces the acceleration impact.
Die Sprengstoffschicht kann aus zusammenhängenden Flächen oder aus in radialer oder axialer Richtung getrennten Flächen aufgebaut sein.The explosive layer may be composed of contiguous surfaces or of surfaces separated in the radial or axial direction.
Die Sprengstoffschicht kann eine beliebig geformte Oberfläche (Kontur) besitzen, sodass örtlich unterschiedliche Splitterbildungen und auch Splittergeschwindigkeiten erreicht werden können.The explosive layer can have an arbitrarily shaped surface (contour), so that spatially different splinter formations and also splitter speeds can be achieved.
Über die Form der inneren Verdämmung kann die Sprengstoffschicht einen Winkel zur Geschossachse bilden. Damit können Splitter oder Subgeschosse richtungsgesteuert beschleunigt werden. Derartige Anordnungen können sowohl an bestimmten Positionen des Geschosses vorgesehen sein (z.B. im Spitzenbereich) oder sich über die gesamte Oberfläche erstrecken.Through the shape of the inner damming, the explosive layer can form an angle to the projectile axis. Thus, splinters or sub-projectiles can be accelerated direction-controlled. Such arrangements may be provided at certain positions of the projectile (e.g., in the tip region) or extend over the entire surface.
Die Sprengstoffschicht wird in der Regel die Form eines Hohlzylinders haben. Dieser kann an den Enden offen oder ein- bzw. beidseitig mittels einer stirn- oder heckseitigen Sprengstoffschicht geschlossen sein.The explosive layer will usually have the shape of a hollow cylinder. This can be open at the ends or closed on one or both sides by means of a front or rear explosive layer.
Über die gesamte Penetratorlänge können Sprengstoffscheiben (Sprengstoffbrücken) eingebracht sein. Damit können z.B. innere Körper in axialer Richtung beschleunigt werden.Explosive disks (explosive bridges) can be introduced over the entire penetrator length. Thus, for example, inner bodies can be accelerated in the axial direction.
Über eine stirnseitige Sprengstoffbelegung können Teile der Spitze beschleunigt werden. Darüber hinaus kann die Spitze des Geschosses oder Gefechtskopfes ganz oder teilweise mit Sprengstoff gefüllt sein.Parts of the tip can be accelerated via a frontal explosive coating. In addition, the tip of the projectile or warhead may be wholly or partially filled with explosives.
Die Spitze oder der Spitzenbereich kann auch aus einem endballistisch wirksamen inerten Körper bestehen oder einen solchen enthalten, um über diese Komponente endballistische Effekte zu bewirken.The tip or tip region may also consist of or contain an end ballistic inert body to effect end-ballistic effects via this component.
Weitere Ausgestaltungen von Anordnungen entsprechend der vorliegenden Erfindung ergeben sich durch das Einbringen einer zusätzlichen pyrotechnischen Komponente innerhalb des verdämmenden Innenkörpers. Diese kann entweder durch die Detonation der Sprengstoffschicht gezündet werden oder direkt angesteuert sein.
Bei derartigen Anordnungen können z.B. in Ergänzung zu Splittern bzw. Subgeschossen aus dem Hüllenbereich radial beschleunigte Elemente aus dem Innenbereich erzeugt werden.Further embodiments of arrangements according to the present invention result from the introduction of an additional pyrotechnic component within the damming inner body. This can either be ignited by the detonation of the explosive layer or be controlled directly.
In such arrangements, for example, in addition to splinters or sub-floors from the shell area radially accelerated elements can be generated from the interior.
Funktion und Effizienz von Anordnungen entsprechend der Erfindung sind unabhängig von der Art der Stabilisierung. So können die Wirkkörper kanonenverschossene Projektile, Gefechtsteile eines Flugkörpers bzw. einer Rakete, Teile einer Bombe oder der Wirkteil eines Torpedos sein.Function and efficiency of arrangements according to the invention are independent of the type of stabilization. Thus, the active bodies may be cannon-fired projectiles, combat components of a missile or missile, parts of a bomb or the active part of a torpedo.
- 1 A1 A
-
drallstabilisiertes Sprengstoffschicht-Splittergeschoss mit Splittermantel 2, Sprengstoffschicht 3 und Innenkörper 4Spin-stabilized explosive layer chipboard with
splinter shell 2,explosive layer 3 andinner body 4 - 1 B1 B
-
pfeilstabilisiertes Sprengstoffschicht- Splittergeschoss mit Splittermantel 2, Sprengstoffschicht 3 und Innenkörper 4arrow-stabilized explosive layer chip projectile with
splinter shell 2,explosive layer 3 andinner body 4 - 22
- Splitterhülle / Splittermantel / splitterbildende GeschosshülleSplinter shell / splinter shell / fragmental projectile shell
- 2A2A
- Splitterhülle mit grundsätzlich beliebigem (hier achteckigem) InnenquerschnittSplinter shell with basically any (here octagonal) inner cross section
- 33
- Sprengstoffmantel / Sprengstoffbelegung / Sprengstoffschicht / Sprengstofffläche / pyrotechnische SchichtExplosive shell / explosives cover / explosive layer / explosive surface / pyrotechnic layer
- 3A3A
- Sprengstoffmantel mit grundsätzlich beliebigem (hier polygonem) InnenquerschnittExplosive shell with basically any (here polygonal) inner cross-section
- 3B3B
- Sprengstoffschicht mit grundsätzlich beliebigem (hier achteckigem) AußenquerschnittExplosive layer with basically any (here octagonal) outer cross section
- 3C3C
- Sprengstoffschicht mit grundsätzlich beliebigem (hier rechteckigem) QuerschnittExplosive layer with basically any (here rectangular) cross section
- 3D3D
- mit Sprengstoff gefüllter Zwischenraum zwischen 27 und 2filled with explosive space between 27 and 2
- 44
- verdämmender Innenkörper / innere Verdämmungdamming inner body / inner damming
- 4A4A
- Verdämmung für 20Damming for 20
- 4B4B
- zentraler Innenkörpercentral inner body
- 4C4C
- Innenkörper mit OberflächenstrukturInner body with surface structure
- 55
- hohler verdämmender Innenkörper / verdämmender Innenmantel / Innenring / StützringHollow damming inner body / damming inner casing / inner ring / support ring
- 5A5A
- zweite (innere) verdämmende Schichtsecond (inner) damming layer
- 66
- zentraler Hohlraum (beliebigen Querschnitts)central cavity (arbitrary cross section)
- 77
- zweiter (hier zentraler) verdämmender Innenkörpersecond (here central) damming inner body
- 7A7A
- Innenkörper / zentraler PenetratorInner body / central penetrator
- 88th
- verdämmender Innenkörper mit grundsätzlich beliebigem (hier oktagonalem Querschnitt)damming inner body with basically any (here octagonal cross-section)
- 99
- verdämmender Innenkörper mit (grundsätzlich beliebigem) hier quadratischem Querschnittdamming inner body with (basically arbitrary) here square cross-section
- 9A9A
- verdämmender Innenkörperdamming inner body
- 9B9B
- verdämmender Innenkörperdamming inner body
- 9C9C
- verdämmender Innenkörperdamming inner body
- 1010
- Sprengstoffsegment zwischen 9 und 2Explosive segment between 9 and 2
- 10A10A
- Sprengstoffsegment zwischen 9 und 2Explosive segment between 9 and 2
- 1111
- zentraler Körper mit grundsätzlich beliebigem (hier dreieckigem) Querschnittcentral body with basically any (here triangular) cross-section
- 1212
- inertes / druckübertragendes Segment (homogen oder Körper enthaltend) / Splitterbildendes Segment zwischen 11 und 3inert / pressure transmitting segment (homogeneous or body containing) / fragment forming segment between 11 and 3
- 12A12A
- inertes / druckübertragendes Segment (homogen oder Körper enthaltend) / Splitterbildendes Segment zwischen 3C und 2inert / pressure transmitting segment (homogeneous or body containing) / fragment forming segment between 3C and 2
- 1313
- dynamisch wirkende Schicht zwischen 9 und 3dynamic layer between 9 and 3
- 13A13A
- dynamisch wirkende Schicht zwischen 5 und 7dynamic layer between 5 and 7
- 13B13B
- dynamisch wirkende Schicht zwischen 3 und 2dynamic acting layer between 3 and 2
- 13C13C
- dynamisch wirkende Schicht zwischen 2 und 14dynamically acting layer between 2 and 14
- 1414
- äußerer Splitterringouter splinter ring
- 14A14A
- Geschosshülle / Geschossmantel / AußenhautProjectile shell / bullet jacket / outer skin
- 14B14B
- Geschosshülle / GefechtskopfwandBullet casing / warhead wall
- 1515
- Splitter / vorgeformte Elemente enthaltende Ringfläche zwischen 14 und 3Splitter / preformed elements containing ring area between 14 and 3
- 1616
- in 16A eingebettete Körper / vorgeformte Splitter / vorgeformte Geschosse16A embedded bodies / preformed fragments / preformed projectiles
- 16A16A
- Matrix von 1 5Matrix of 1 5
- 1717
- Innenkörper (zentral oder dezentral) mit eingebettetem Zündelement 18Inner body (central or decentralized) with embedded ignition element 18th
- 1818
- in 17 eingebettetes Zündelement (Sprengschnur)embedded in 17 ignition element (detonating cord)
- 18A18A
- Zündelement in 10A, 18Ignition element in FIGS. 10A, 18
- 18B18B
- in 10A eingelegtes Zündelement / Zündleitung beliebiger Form und beliebigen Querschnitts10A inserted ignition element / ignition cable of any shape and any cross-section
- 1919
- äußere Sprengstoffschichtouter explosive layer
- 2020
- innere Sprengstoffschichtinner explosive layer
- 2121
- innerer Wirkmantel / innerer Splitterring (Verdämmung für 19 und Splitterhülle für 20)inner sheath / inner splinter ring (stowage for 19 and splinter sheath for 20)
- 2222
- zentrale Ladung (Sprengschnur) / pyrotechnischer Körpercentral charge (detonating cord) / pyrotechnic body
- 22A22A
- zentraler Sprengstoffkörper zur radialen Beschleunigung oder Zerlegung von 26central explosive body for radial acceleration or disassembly of 26
- 2323
- mehrteiliger (hier in vier Kreissegment-Querschnitte 24 unterteilter) Innenkörpermulti-part (here divided into four circular segment cross-sections 24) inner body
- 2424
- einzelnes Element von 23single element of 23
- 2525
-
Trennung / Trennschicht zwischen den Elementen 24Separation / separation layer between the
elements 24 - 2626
-
mehrteiliger, grundsätzlich beliebig geformter Innenkörper (hier aus vier Zylindern 27 bzw. 27A gebildet)multi-part, in principle arbitrarily shaped inner body (here formed by four
27 and 27A)cylinders - 2727
- Zylinder / Körper mit grundsätzlich beliebigem (hier kreisförmigem) QuerschnittCylinder / body with basically any (here circular) cross-section
- 27A27A
- Körper mit grundsätzlich beliebigem (hier kreisförmigem) QuerschnittBody with basically any (here circular) cross-section
- 2828
- inerter zentraler Körper in 26 / Innenraum / Hohlrauminert central body in 26 / interior / cavity
- 2929
- Splitterhülle mit veränderlicher Wandstärke / mit Einschnitten / mit Innenstruktur 30Variable wall splinter cover / with incisions / with internal structure 30
- 3030
- Einschnitt / InnenstrukturIncision / internal structure
- 3131
- Sprengstoffschicht mit strukturierter AußenkonturExplosive layer with structured outer contour
- 31 A31 a
- Sprengelement / SprengstoffstegBlasting element / explosive bridge
- 3232
- Splitterhülle mit strukturierter / mit Formteilen besetzter InnenseiteSplinter shell with structured / molded inside
- 3333
- Sprenghülle mit EinschnittenExplosive shell with incisions
- 3434
- Sprengstoffschicht mit Durchmesseränderung / Durchmessersprung / Einkerbungen / Einschnitten auf der InnenseiteExplosive layer with diameter change / diameter jump / notches / incisions on the inside
- 3535
- segmentierte / unterbrochene / stegartige (aus Flächenelementen bestehende) SprengstoffschichtSegmented / interrupted / web-like (consisting of surface elements) explosive layer
- 3636
- Sprengstoffstreifen / Sprengstoff-FlächenelementExplosive strip / explosive surface element
- 36A36A
- Sprengstoffstreifen / SprengstoffsegmentExplosives strip / Explosives segment
- 3737
- Trennschicht / Trennelement / Trennstreifen / Trenngitter zwischen 36ASeparating layer / separating element / separating strip / separating grid between 36A
- 3838
- zentraler Behälter / Innenkörpercentral container / inner body
- 38A38A
- Wand von 38Wall of 38
- 38B38B
- Behälter in Form einer ZwischenschichtContainer in the form of an intermediate layer
- 38C38C
- Wand von 38BWall of 38B
- 38D38D
- Steg / Halterung / VerbindungsstrukturBridge / bracket / connection structure
- 3939
- Füllung / Inhalt von 38Filling / content of 38
- 39A39A
- Füllung / Inhalt von 38B / Liquid-RingFill / Content of 38B / Liquid Ring
- 4040
- Steuer- / ZündelementControl / ignition element
- 4141
- mehrteiliger / mehrstufiger verdämmender Körpermulti-part / multi-level damming body
- 41 A41 a
- mehrteiliger verdämmender Körper (gleicher oder ungleicher Durchmesser)multi-part damming body (same or unequal diameter)
- 4242
- Sprengstoffschicht veränderlicher Dicke (hier Innendurchmesser variabel)Explosive layer of variable thickness (here inner diameter variable)
- 42A42A
- wie 42, Außendurchmesser variabellike 42, outer diameter variable
- 4343
- Splitterhülle mit veränderlicher DickeFragmentation sheath with variable thickness
- 4444
- Sprengstoffmantel mit (hier innerem) Durchmessersprung / DurchmesseränderungExplosive jacket with (here inner) diameter jump / diameter change
- 44A44A
- Durchmessersprung / DurchmesseränderungDiameter jump / diameter change
- 4545
- gestufte Splitterhülle / Splitterhülle mit veränderlicher Dickestepped splinter shell / splinter shell with variable thickness
- 4646
- gestufter Innenkörperstepped inner body
- 4747
- geteilter / mehrteiliger Sprengstoffmanteldivided / multipart explosive jacket
- 4848
- Sprengstoffmantel mit Durchmessersprung / DurchmesseränderungExplosive jacket with diameter jump / diameter change
- 4949
- Sprengstoffmantel (hier durchgehend) für eine gerichtete SplitterwirkungExplosive shell (here continuous) for a directed fragmentation effect
- 49A49A
- Sprengstoffmantel aus Einzelabschnitten / angestellten, getrennten RingflächenExplosive jacket of individual sections / employed, separate annular surfaces
- 49B49B
- strukturierter (hier aus Ringflächen mit Kreiselement-Querschnitt bestehender) Sprengstoffmantelstructured (here consisting of annular surfaces with circular cross-section) explosive jacket
- 5050
- Splitterbelegung zum Erzielen einer gerichteten WirkungSplinter assignment to achieve a directional effect
- 50A50A
- segmentierte Splitterbelegung von 49Asegmented splitter assignment of 49A
- 5151
- Splitterhülle aus konvexen RingenFragmentation of convex rings
- 5252
- Hohlraum zwischen 2 und 14B (leer oder mit Innenstruktur)Cavity between 2 and 14B (empty or with internal structure)
- 5353
-
Spitze mit Sprengstoffmantel 54 / außenballistische HaubeTip with
explosive jacket 54 / outside ballistic hood - 5454
- Sprengstoffschicht in 53Explosive layer in 53
- 5555
- verdämmender Innenkörper in 53damming inner body in 53
- 5656
- mit Sprengstoff / einem pyrotechnischen Medium gefüllte Spitzefilled with explosives / a pyrotechnic medium tip
- 5757
- in 4 eingebetteter Sprengstoffkörperin 4 embedded explosives body
- 5858
- in 4 eingebetteter Penetrator (hier Hart-, Schwermetall- oder Stahl-Kern 58)in 4 embedded penetrator (here hard, heavy metal or steel core 58)
- 58A58A
-
Kern mit Heck-Innenkegel 60Core with rear
inner cone 60 - 58B58B
-
Kern mit kegelförmigem Heck 62Core with
conical tail 62 - 5959
- in 4 eingebetteter zentraler Penetrator / Zylinderin 4 embedded central penetrator / cylinder
- 6060
- Heck-Innenkegel in 58ARear inner cone in 58A
- 60A60A
- Pfeile, Wirkrichtung der Sprengstoffzone 61 symbolisierendArrows, symbolizing the effective direction of the explosive zone 61
- 6161
- Sprengstoffzone am Heck von 58A zur Beschleunigung / Zerlegung von 58AExplosive zone at the stern of 58A to accelerate / disassemble 58A
- 61 A61 A
- Sprengstoffzone am Heck von 58B zur Beschleunigung von 58BExplosive zone at the stern of 58B to accelerate 58B
- 6262
- kegelförmiges Heck von 58Bconical tail of 58B
- 62A62A
-
Pfeile, Wirkrichtung der Sprengstoffzone 61 A symbolisierendArrows symbolizing the effective direction of
explosive zone 61A - 6363
- Sprengstoffbelegung zur partiell verstärkten axialen SplitterwirkungExplosive composition for partially reinforced axial fragmentation effect
- 6464
- Innenkörper in 63Inner body in 63
- 64A64A
- Innenkörper in 65Inner body in 65
- 6565
- Splitterhülle mit axialer SplitterwirkungSplinter shell with axial fragmentation effect
- 65A65A
- Pfeil, Wirkrichtung symbolisierendArrow, symbolizing effect direction
- 6666
- Sprengstoffmantelexplosives jacket
- 6767
-
Splittermantel entsprechend 65 mit Splittertasche 68Splinter jacket corresponding to 65 with
splitter pocket 68 - 6868
- Splittertasche / SplitterringSliver pocket / splinter ring
- 68A68A
- in 68 eingebettete Körperin 68 embedded bodies
- 68B68B
- Pfeile, die Wirkrichtung der Splittertaschen 67 symbolisierendArrows, the direction of effect of the splinter pockets 67 symbolizing
- 6969
- Sprengstoffhülle mit variablem Innendurchmesser zur gerichteten SplitterbeschleunigungExplosive shell with variable inside diameter for directional splinter acceleration
- 69A69A
- Sprengstoffhüllenelemente zur gerichteten Splitterbeschleunigung (hier mit sektionsweiser / mehrstufiger Sprengstoffschicht)Explosive sheath elements for directional splinter acceleration (here with section-wise / multi-level explosive layer)
- 7070
- verdämmender Innenkörper mit Außenkontur zur gerichteten Splitterwirkungdamming inner body with outer contour for directional splintering effect
- 70A70A
- verdämmender Innenkörper mit Außenkontur zur gerichteten Splitterwirkungdamming inner body with outer contour for directional splintering effect
- 7171
- axial wirkende Sprengstoffzoneaxially acting explosive zone
- 7272
- Spitzenmodul mit gerichteter SplitterwirkungTip module with directed fragmentation effect
- 7373
- Pfeil, Wirkrichtung symbolisierendArrow, symbolizing effect direction
- 73A73A
- Pfeile, die Wirkrichtung der Splitterbelegung von 73 symbolisierendArrows, symbolizing the effective direction of fragmentation of 73
- 7474
- verdämmender Innenkörper mit partieller Sprengstoffbelegungdamming inner body with partial explosive occupancy
- 74A74A
- mehrteiliger Innenkörper mit Stufenspitzemulti-part inner body with step tip
- 7575
- Segment eines verdämmenden Innenkörpers mit zylinderförmiger KonturSegment of a damming inner body with a cylindrical contour
- 75A75A
- Segment eines verdämmenden Innenkörpers mit zylinderförmiger KonturSegment of a damming inner body with a cylindrical contour
- 7676
- Trennflächeinterface
- 7777
- SplittermantelFragmentation casing
- 7878
- linsenförmiges Sprengstoffsegment / Segment beliebigen Querschnittslenticular explosive segment / segment of any cross section
- 78A78A
- Pfeile, Wirkrichtung symbolisierendArrows, symbolizing effect direction
- 7979
- Splittersegmentsplitter segment
- 79A79A
- Splittersegmentsplitter segment
- 79B79B
-
beschleunigtes Splittersegment 79A
accelerated splitter segment 79A - 79C79C
-
zerlegtes und beschleunigtes Splittersegment 79Adisassembled and accelerated
splitter segment 79A - 8080
- Sprengstoffring aus Segmenten beliebiger GestaltungExplosive ring made of segments of any design
- 80A80A
- Sprengstoffsegment beliebiger GestaltungExplosive segment of any design
- 8181
- Segment eines verdämmenden Innenkörpers mit beliebiger KonturSegment of a damming inner body with any contour
- 8282
- Innenkörper, zentraler PenetratorInner body, central penetrator
- 82A82A
- Innenkörper, zentraler PenetratorInner body, central penetrator
- 8383
- sektionsweise aufgebauter / zusammengesetzter verdämmender InnenkörperSectionally constructed / assembled damming inner body
- 8484
- Ring aus Stäben / Zylindern / Körper beliebigen QuerschnittsRing of rods / cylinders / body of any cross section
- 8585
- Trennschicht zwischen 80Separating layer between 80
- 8686
- Stäbe / Zylinder / Körper beliebigen QuerschnittsRods / cylinders / bodies of any cross section
- 8787
- zentraler Körpercentral body
- 8888
- sektionsweise gestaltete RingeSectionally shaped rings
- 8989
- Geschoss mit unterschiedlichen verdämmenden InnenkörpernProjectile with different damming inner bodies
- 9090
- inerter Abschnittinert section
- 9191
- Abstand / pufferndes inertes Element / TrennschichtDistance / buffering inert element / separation layer
- 9292
- Splitterring / Splittermantel beliebiger (hier quadratischer) FormSplinter ring / splinter coat of any (here square) shape
- 92A92A
- Splitterring / Splittermantel beliebiger (hier achteckiger) FormSplinter ring / splinter coat of any (here octagonal) shape
Claims (29)
- Explosive projectile with a fragment-forming projectile shell (2) and an explosive layer (3) disposed inside the projectile shell (2),
characterised in
that an internal body (4), which tamps the explosive layer, is disposed inside the explosive layer (3), and the explosive layer (3) is of thin formation in relation to the projectile diameter. - Explosive projectile according to Claim 1,
characterised in
that the thickness of the explosive layer (3) is between 2 mm and 20 mm. - Explosive projectile according to Claim 1,
characterised in
that the explosive layer (3) has the shape of a hollow cylinder with a constant or variable wall thickness and/or cross-sectional shape. - Explosive projectile according to Claim 3,
characterised in
that the explosive layer (3) represents a hollow cylinder with ends closed on one or both side(s) or with intermediate layers. - Explosive projectile according to Claim 1,
characterised in
that the explosive layer (3) is homogeneous or contains admixtures or embedded bodies. - Explosive projectile according to Claim 1,
characterised in
that the firing of the individual explosive segments (10) or plurality of explosive layers takes place in a punctual, linear or annular fashion at one or a plurality of location(s). - Explosive projectile according to Claim 1 or 6,
characterised in
that the firing takes place via a time delay, proximity or impact fuse, via a program-controlled signal or by means of radio. - Explosive projectile according to Claim 1,
characterised in
that the internal body (4) is of one-part or multi-part composition. - Explosive projectile according to Claim 1,
characterised in
that the internal body (4) consists of a brittle material or one which embrittles under a dynamic load. - Explosive projectile according to Claim 8,
characterised in
that the internal body (4) is formed as a central penetrator or contains a central penetrator or consists of a plurality of subprojectiles or contains subprojectiles. - Explosive projectile according to Claim 8,
characterised in
that the internal body (4) is prefragmented or mechanically or thermally pretreated. - Explosive projectile according to Claim 10,
characterised in
that the subprojectiles enclose an inert volume. - Explosive projectile according to Claim 1,
characterised in
that the internal body (4) represents or contains a container. - Explosive projectile according to Claim 13,
characterised in
that the internal body (4) is filled with an inert or a reactive medium. - Explosive projectile according to Claim 13,
characterised in
that the internal body (4) contains a pyrotechnic element. - Explosive projectile according to Claim 1,
characterised in
that a layer which dynamically assists the tamping action is located between the explosive layer (3) and the internal body (4). - Explosive projectile according to Claim 1,
characterised in
that the projectile comprises two or more explosive layers in the radial direction. - Explosive projectile according to Claim 1,
characterised in
that the explosive layer (3) is composed of contiguous areas or of areas which are separated (in the radial and/or axial direction). - Explosive projectile according to Claim 1,
characterised in
that the explosive layer (3) forms an angle relative to the projectile axis. - Explosive projectile according to Claim 1,
characterised in
that the projectile shell (2) consists entirely or partly of preformed fragments. - Explosive projectile according to Claim 20,
characterised in
that the fragments are accelerated in a direction-controlled manner. - Explosive projectile according to Claim 1,
characterised in
that fragmentation bodies are introduced between the explosive layer (3) and the projectile shell (2). - Explosive projectile according to Claim 1,
characterised in
that a layer of a brittle material is located between the explosive layer (3) and the projectile shell (2). - Explosive projectile according to Claim 1,
characterised in
that a dynamically damping medium is located between the explosive layer (3) and the projectile shell (2). - Explosive projectile according to Claim 1,
characterised in
that a liquid casing is inserted between the explosive layer (3) and the projectile shell (2). - Explosive projectile according to Claim 1,
characterised in
that a hollow space is located between the explosive layer (3) and the projectile shell (2). - Explosive projectile according to Claim 1,
characterised in
that the projectile is of single- or multi-stage composition in the axial direction. - Explosive projectile according to Claim 1,
characterised in
that a head or a head region of the projectile consists of a terminal-ballistically effective inert part. - Explosive projectile according to Claim 1,
characterised in
that the explosive projectile is composed as a multi-part/multi-stage effective body.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/EP2005/006678 WO2006136185A1 (en) | 2005-06-21 | 2005-06-21 | Projectile or warhead |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1893935A1 EP1893935A1 (en) | 2008-03-05 |
EP1893935B1 true EP1893935B1 (en) | 2008-11-05 |
Family
ID=35134172
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP05763381A Active EP1893935B1 (en) | 2005-06-21 | 2005-06-21 | Projectile or warhead |
Country Status (12)
Country | Link |
---|---|
US (1) | US20100199875A1 (en) |
EP (1) | EP1893935B1 (en) |
KR (1) | KR101255872B1 (en) |
CN (1) | CN101273243A (en) |
AT (1) | ATE413581T1 (en) |
AU (1) | AU2005333448B2 (en) |
CA (1) | CA2611169C (en) |
DE (1) | DE502005005922D1 (en) |
ES (1) | ES2317272T3 (en) |
IL (1) | IL187964A (en) |
NO (1) | NO338274B1 (en) |
WO (1) | WO2006136185A1 (en) |
Families Citing this family (22)
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WO2009145926A1 (en) * | 2008-01-03 | 2009-12-03 | Lockheed Martin Corporation | Thermal enhanced blast warhead |
FR2940683B1 (en) * | 2008-12-31 | 2011-03-18 | Nexter Munitions | MILITARY HEAD PROJECTING BARS. |
FR2953587B1 (en) * | 2009-12-04 | 2016-12-23 | Tda Armements Sas | AMMUNITION COMPRISING A BODY, AN EXPLOSIVE LOADING AND MEANS FOR MOUNTING BETWEEN THE BODY AND EXPLOSIVE LOADING |
DE102010061272B3 (en) * | 2010-12-15 | 2013-04-25 | Krauss-Maffei Wegmann Gmbh & Co. Kg | Projectile casing for an explosive projectile and method for treating a projectile casing |
CN102175102B (en) * | 2011-03-25 | 2013-03-13 | 南京理工大学 | Firework with integral module explosive filling structure in open mode and preparation method thereof |
DE102012001445B3 (en) * | 2012-01-26 | 2013-03-07 | Bundesrepublik Deutschland, vertreten durch das Bundesministerium der Verteidigung, dieses vertreten durch das Bundesamt für Ausrüstung, Informationstechnik und Nutzung der Bundeswehr | Explosive projectile, particularly artillery explosive projectile, has projectile axis, projectile casing, projectile cavity formed with projectile inner wall that has cylinder with cylinder longitudinal axis in section |
US9692408B2 (en) * | 2012-12-21 | 2017-06-27 | Gan Systems Inc. | Devices and systems comprising drivers for power conversion circuits |
FR3002626B1 (en) * | 2013-02-28 | 2015-06-05 | Eurenco France | MODULAR EXPLOSIVE POWER MUNITION |
US10184763B2 (en) * | 2014-02-11 | 2019-01-22 | Raytheon Company | Munition with nose kit connecting to aft casing connector |
AT515209B1 (en) * | 2014-03-14 | 2015-07-15 | Hirtenberger Defence Systems Gmbh & Co Kg | bullet |
US9739583B2 (en) * | 2014-08-07 | 2017-08-22 | Raytheon Company | Fragmentation munition with limited explosive force |
EA025879B1 (en) * | 2014-10-29 | 2017-02-28 | Сергей Николаевич Левин | Explosion detonator cartridge |
DE102014019202A1 (en) | 2014-12-19 | 2016-06-23 | Diehl Bgt Defence Gmbh & Co. Kg | bullet |
WO2016171794A1 (en) * | 2015-03-02 | 2016-10-27 | Nostromo Holdings, Llc | Low collateral damage bi-modal warhead assembly |
JP6766177B2 (en) * | 2016-01-15 | 2020-10-07 | サーブ・ボフォース・ダイナミクス・スウィツァランド・リミテッド | warhead |
US9784541B1 (en) * | 2016-08-15 | 2017-10-10 | The United States Of America As Represented By The Secretary Of The Navy | Increased lethality warhead for high acceleration environments |
DE102017105565A1 (en) * | 2017-03-15 | 2018-09-20 | Rheinmetall Waffe Munition Gmbh | Ammunition and logistics concept for in particular artillery projectiles |
US11027859B2 (en) | 2017-10-16 | 2021-06-08 | The Boeing Company | Variable stiffness flyer plate for penetration device |
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 |
JP7397296B2 (en) * | 2019-10-31 | 2023-12-13 | ダイキン工業株式会社 | warhead |
HUP2000306A1 (en) * | 2020-09-17 | 2022-03-28 | Fueloep Nandor | Bullet |
CN113137897B (en) * | 2021-03-22 | 2022-04-19 | 北京理工大学 | Composite transverse effect enhanced bullet based on active material and inert material |
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US3675577A (en) * | 1964-06-30 | 1972-07-11 | Us Navy | Rod warhead |
US3302570A (en) * | 1965-07-23 | 1967-02-07 | Walter G Finch | Armor piercing, fragmenting and incendiary projectile |
US4106411A (en) * | 1971-01-04 | 1978-08-15 | Martin Marietta Corporation | Incendiary fragmentation warhead |
US4216722A (en) * | 1978-06-05 | 1980-08-12 | Angell Howard N | Exploding bullet |
US5157225A (en) * | 1983-04-19 | 1992-10-20 | The United States Of America As Represented By The Secretary Of The Navy | Controlled fragmentation warhead |
DE3522008A1 (en) | 1985-06-20 | 1987-01-02 | Messerschmitt Boelkow Blohm | Missile |
US4939259A (en) * | 1989-07-24 | 1990-07-03 | Eli Lilly And Company | 2-oxo-pyrido[2,3-g]quinoline derivatives |
FR2678262B1 (en) * | 1991-06-26 | 1993-12-10 | Poudres Explosifs Ste Nale | LITTLE VULNERABLE ELEMENT OF EXPLOSIVE AMMUNITION COMPRISING A BI-COMPOSITION EXPLOSIVE LOADING AND METHOD FOR OBTAINING A SHARD EFFECT. |
USH1048H (en) * | 1991-08-05 | 1992-05-05 | The United States Of America As Represented By The Secretary Of The Navy | Composite fragmenting rod for a warhead case |
DE4139372C1 (en) * | 1991-11-29 | 1995-03-02 | Deutsche Aerospace | Fragmentation warhead |
US5535679A (en) | 1994-12-20 | 1996-07-16 | Loral Vought Systems Corporation | Low velocity radial deployment with predetermined pattern |
US7614348B2 (en) * | 2006-08-29 | 2009-11-10 | Alliant Techsystems Inc. | Weapons and weapon components incorporating reactive materials |
US6598534B2 (en) * | 2001-06-04 | 2003-07-29 | Raytheon Company | Warhead with aligned projectiles |
US7621222B2 (en) * | 2001-08-23 | 2009-11-24 | Raytheon Company | Kinetic energy rod warhead with lower deployment angles |
EP1316774B1 (en) | 2001-11-28 | 2006-05-17 | futurtec AG | High penetration and lateral effect projectiles having an integrated fragment generator |
US6619210B1 (en) * | 2002-03-25 | 2003-09-16 | The United States Of America As Represented By The Secretary Of The Navy | Explosively formed penetrator (EFP) and fragmenting warhead |
US7017496B2 (en) * | 2002-08-29 | 2006-03-28 | Raytheon Company | Kinetic energy rod warhead with imploding charge for isotropic firing of the penetrators |
US7453726B1 (en) | 2007-01-23 | 2008-11-18 | National Semiconductor Corporation | Non-volatile memory cell with improved programming technique and density |
-
2005
- 2005-06-21 EP EP05763381A patent/EP1893935B1/en active Active
- 2005-06-21 CA CA2611169A patent/CA2611169C/en not_active Expired - Fee Related
- 2005-06-21 ES ES05763381T patent/ES2317272T3/en active Active
- 2005-06-21 US US11/993,839 patent/US20100199875A1/en not_active Abandoned
- 2005-06-21 KR KR1020087001189A patent/KR101255872B1/en active IP Right Grant
- 2005-06-21 WO PCT/EP2005/006678 patent/WO2006136185A1/en active Application Filing
- 2005-06-21 AU AU2005333448A patent/AU2005333448B2/en not_active Ceased
- 2005-06-21 CN CNA2005800502153A patent/CN101273243A/en active Pending
- 2005-06-21 DE DE502005005922T patent/DE502005005922D1/en active Active
- 2005-06-21 AT AT05763381T patent/ATE413581T1/en active
-
2007
- 2007-12-06 IL IL187964A patent/IL187964A/en active IP Right Grant
-
2008
- 2008-01-16 NO NO20080336A patent/NO338274B1/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
EP1893935A1 (en) | 2008-03-05 |
NO20080336L (en) | 2008-03-12 |
AU2005333448B2 (en) | 2011-09-15 |
CA2611169C (en) | 2010-02-16 |
CA2611169A1 (en) | 2006-12-28 |
KR101255872B1 (en) | 2013-04-17 |
WO2006136185A1 (en) | 2006-12-28 |
KR20080019293A (en) | 2008-03-03 |
ES2317272T3 (en) | 2009-04-16 |
CN101273243A (en) | 2008-09-24 |
IL187964A0 (en) | 2008-03-20 |
IL187964A (en) | 2012-07-31 |
AU2005333448A1 (en) | 2006-12-28 |
NO338274B1 (en) | 2016-08-08 |
US20100199875A1 (en) | 2010-08-12 |
DE502005005922D1 (en) | 2008-12-18 |
ATE413581T1 (en) | 2008-11-15 |
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