EP1123482B1 - Munition mit einer hülse, deren wand aus einem verbrennbaren oder verzehrbaren wickelkörper besteht - Google Patents
Munition mit einer hülse, deren wand aus einem verbrennbaren oder verzehrbaren wickelkörper besteht Download PDFInfo
- Publication number
- EP1123482B1 EP1123482B1 EP99955854A EP99955854A EP1123482B1 EP 1123482 B1 EP1123482 B1 EP 1123482B1 EP 99955854 A EP99955854 A EP 99955854A EP 99955854 A EP99955854 A EP 99955854A EP 1123482 B1 EP1123482 B1 EP 1123482B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- wound package
- filaments
- ammunition
- projectile
- threads
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000004804 winding Methods 0.000 claims abstract description 87
- 230000006978 adaptation Effects 0.000 claims description 34
- 238000007789 sealing Methods 0.000 claims description 10
- 230000008719 thickening Effects 0.000 claims description 10
- 239000002360 explosive Substances 0.000 claims description 8
- 239000011230 binding agent Substances 0.000 claims description 6
- 239000000126 substance Substances 0.000 claims description 3
- 230000008021 deposition Effects 0.000 claims 1
- 239000003380 propellant Substances 0.000 description 15
- 239000011148 porous material Substances 0.000 description 7
- 239000007789 gas Substances 0.000 description 5
- 239000002184 metal Substances 0.000 description 5
- 238000002485 combustion reaction Methods 0.000 description 4
- 230000003628 erosive effect Effects 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 239000011295 pitch Substances 0.000 description 4
- 238000005516 engineering process Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 239000000203 mixture Substances 0.000 description 3
- 230000000087 stabilizing effect Effects 0.000 description 3
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 2
- 241000209035 Ilex Species 0.000 description 2
- 239000000020 Nitrocellulose Substances 0.000 description 2
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 238000000151 deposition Methods 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000004744 fabric Substances 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 229920001220 nitrocellulos Polymers 0.000 description 2
- 239000004033 plastic Substances 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 238000012549 training Methods 0.000 description 2
- 239000004604 Blowing Agent Substances 0.000 description 1
- 230000001154 acute effect Effects 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 238000009954 braiding Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 239000002737 fuel gas Substances 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 238000005470 impregnation Methods 0.000 description 1
- 239000003999 initiator Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 239000002557 mineral fiber Substances 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 238000012805 post-processing Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000009987 spinning Methods 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 239000004753 textile Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/18—Caseless ammunition; Cartridges having combustible cases
- F42B5/181—Caseless ammunition; Cartridges having combustible cases consisting of a combustible casing wall and a metal base; Connectors therefor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/18—Caseless ammunition; Cartridges having combustible cases
Definitions
- the invention relates to ammunition according to the preamble of the first Claim.
- a rocket body is known from US Pat. No. 3,745,927, the wall of which is made of Nitrocellulose threads are wound. An adaptation of the structure of the wall different loads over the length of the winding body is not described.
- a jacket in FR-A 2 488 390 a jacket is described as a winding body, which in Mainly suitable for projectiles, grenades and bombs. It consists of two Layers that have been wound from mineral fibers, with the fibers in the outer Position at an angle of 90 ° and the fibers in the position below an angle of 0 ° to the axis of rotation of the body.
- propellant charges which consist of a winding body Nitrocellulose threads are made. When used for projectiles is the bullet sleeve made of metal.
- the invention presented in DE-PS 305 157 relates to the connection of a Gun bullet with a metal cartridge case by means of a ring slightly melting metal.
- US Patent 5,048,421 relates to the closure of a cartridge from a flammable material with a bottom made of metal, which is threaded on the end the cartridge can be screwed on.
- the object of the present invention is to provide ammunition with a combustible or to introduce edible bobbins, the threads in the Windings optimally to the different possible loads and that desired burning behavior are stored in a coordinated manner.
- the winding body according to the invention is in one piece. On his sleeve mouth, the Adaptation area for the floor, the floor is inserted and attached to his on the other end he carries a stub with the primer. Due to the one-piece training advantageously eliminates the separate manufacture of the sleeve halves and a process step for assembling the sleeve halves.
- the filaments are deposited over the length of the winding body uneven.
- the winding density that is the number, how many times that of the thread or the threads are deposited over the length of the bobbin is on the actual and possible loads as well as the desired Burning behavior coordinated. For example, the higher the pressure load on one Sleeve in one area, the higher the number of thread deposits in this Area selected.
- the winding density is essentially influenced by the crossing angle.
- the Crossing angle is when the threads are deposited on the circumference in a crossing manner of the winding body the angle between two ends to be stacked in the depositing direction Threads in a so-called double layer.
- a double layer consists of one layer Threads that have been deposited towards one end of the bobbin are and the overlying layer of threads that are in the opposite Direction, towards the other end of the winding body are. Since the threads on the circumference of the winding body in a helical shape
- the direction of the longitudinal axis of the ammunition determines the slope of the Put down the crossing angle. With a slight slope, the crossing angle is also small, also large on a steep incline.
- the strength and Resilience of a winding body and its burning behavior are additional influenced by the winding technique. For example, a thread alone or several threads running parallel to each other at a small distance from each other Be wound.
- the crossing angle of the threads is Winding body in the adaptation area for the floor and in the adaptation area for the Stub sleeve smaller than in the intermediate area of the winding body.
- the crossing angle in Adaption area of the floor may be smaller than in the adaption area of the End socket.
- the shell of a tank ammunition has a mass of several kilograms. So that the projectile is held securely in the sleeve, the Wall of the sleeve have a corresponding load capacity. This is through a denser thread deposit than in the rest of the package, that is achieved by one smaller distance between the threads placed side by side, by a smaller Crossing angle. The stub sleeve loads the winding body less than that Bullet.
- the crossing angles can be, for example, at ammunition with a caliber of 120 mm should be distributed over the winding body as follows: In Adaption area of the floor approximately between 15 ° and 30 °, in the adaption area the stub sleeve approximately between 30 ° and 50 ° and in the central area of the Winding body up to 90 °. However, the invention is based on these gradations and on the limit values mentioned.
- the crossing angles are on that Caliber and the purpose of the ammunition and thus essentially on the Match diameter and length of the sleeve.
- the crossing angle can be in a winding body consisting of several double layers exists, the crossing angles in the respective double layers from each other differ.
- the outermost layers can withstand a higher pressure load than the inner layers. This causes a radial deformation of the sleeve when the propellant charge burns up higher resistance opposed, so the effect of the propellant charge in axial Direction towards the floor is supported.
- a particularly high strength of a layer of the winding body is then achieved if the threads are intertwined at least within a double layer.
- the walls of a sleeve built up from cross layers of the threads individual thread layers, also in a double layer, separately one above the other.
- the threads can be intertwined, the Crossing angle can also deviate from 90 °, as is common in fabrics.
- the braiding pattern can affect the load on the sleeve as well as the burning behavior of the winding body can be matched.
- the walls of the sleeves, their winding bodies have a structure of intertwined threads have a special high strength and are therefore particularly suitable for large projectiles, for example for tank ammunition.
- the spaces between the threads and the thread layers be at least partially filled with an explosive.
- the unfilled ones Spaces between the threads and the individual thread layers form pores and can help support the combustion or consumption of the bobbin be used.
- the oxygen in the remaining pores supports the trapped air the combustion.
- the pores also offer one Area of attack for the propellant gases, which means the erosion or Consumption accelerates. Burning in this context means that the Components of the winding body actively participate in the combustion process.
- Suitable materials for the threads and Compositions of the blowing and binding agents are from DE 38 25 581 C1 known.
- the winding technique it is possible to control the filing of the threads so that especially in the adaptation areas for the projectile or the stub sleeve be shaped so that a simple assembly of the ammunition is possible.
- the adaptation area for the projectile for example, a flange-shaped thickening can be formed.
- the adaptation can be configured by means of an adapter, one Storey receiving adapter, which can be integrated into the winding body, the means that, for example, already in the manufacture of the winding body on the Wickeldom is stuck and overwrapped.
- Winding body may be required in the adaptation areas, for example grinding or spinning.
- the stub sleeve can be glued to the winding body or according to one of the known Joining techniques can be mechanically connected to it.
- the stub is like this built that the end portion of their cylindrical wall for attaching the Coil is provided.
- the stub sleeve is with this part in the Pushed in the winding body.
- the remaining part of the stub sleeve is like this designed that it contains a sealing ring with which a gas leakage, that is, a The propellant gas escapes against the direction of conveyance of the projectile on the floor over the sleeve, is prevented.
- one or more sealing rings can be provided.
- FIG. 1 shows a winding body 1 in a simplified, schematic representation. It is part of the shell of a large-caliber ammunition that is not fully shown here, for example caliber 120 mm.
- the winding body 1 is rotationally symmetrical to the axis 2 of the ammunition. In the present exemplary embodiment, it is composed of double layers crossing threads 3 built.
- the winding body 1 has a cylindrical part 4 and a conical part 5.
- the cylindrical part 4 essentially envelops the Propellant charge, the conical part 5 takes up the floor.
- the view of the winding body 1 shows that the crossing angle 6 over its length are different sizes.
- the threads 3 are with different pitches been wrapped. If the threads 3 are wound with a slight pitch, cross each other with an acute crossing angle 6a or 6b.
- This Winding structure is particularly in the end regions 7 and 8 of the winding body 1 preferred, in the adaptation area 7 for the stub sleeve, not shown here for example with crossing angles 6b of approximately 40 ° and in the adaptation area 8 for the projectile not shown here, for example with crossing angles 6a of about 20 °. In these areas, the winding body 1 is attached by the Stub sleeve or the projectile exposed to greater loads.
- the increased The number of threads 3 and their orientation during storage increases the compressive strength the wall of the sleeve, the winding body 1, in these areas.
- the crossing angles 6c are larger, here by 75 ° because the pitch of the deposited threads is also greater.
- the gaps 28 between the threads 3 become larger. They can remain as pores or at least partially filled with explosive.
- With growing Crossing angle takes the tensile strength of the winding body in the direction of axis 2 the ammunition.
- By specifying the crossing angle that is, by the The predefined pitch of the threads when depositing can be an optimal structure of the winding body can be achieved, which is due to the loads and the erosion in the individual areas.
- a thickening 20 of the winding body 1 is provided, for example in Form of a flange used to fasten the projectile in the sleeve becomes.
- FIG. 2 shows a section of a winding body 1 in which the threads 3 are intertwined within a double layer 25.
- the crossing angle 6 is 90 ° in the present exemplary embodiment, as in a fabric.
- the Spaces 28 of the braid 9 can remain as pores or at least partially filled with explosives. With the degree of integration the threads 3 rise together due to the increased friction of the threads among themselves both the radial and the axial strength. Even the density of the Braid 9 affects the strength.
- Winding bodies with this structure are For example, can be used advantageously for ammunition with thin-walled sleeves and large caliber ammunition. Instead of individual threads 3, several can be narrow adjacent threads are intertwined. For example With 120 mm caliber ammunition, nine threads can be which form a ribbon about 25 mm wide, with a slope of 100 mm one revolution of the winding body to be deposited to the winding pattern shown produce.
- FIG. 3 shows a section through an artillery ammunition 10 with a training projectile 11.
- the complete sleeve 12 consists of the winding body 1 and the stub sleeve 13 with the initiator 14.
- the stub sleeve 13 is made of metal, a solid Plastic or other combustible material.
- the stub sleeve 13 is in the adaptation area 7 of the winding body 1 with its adaptation area 7a inserted and glued there with the winding body 1.
- the connection of The winding body and stub sleeve is shown enlarged again as a detail.
- This sealing ring can be made of plastic. It has a sealing lip 18 which is directed radially outwards and in the firing direction and to serve as a gas seal.
- the interior 19 of the sleeve is part of the practice floor 11 and how not shown here, filled with the propellant charge.
- a thickening of Sleeve mouth provided in the form of a flange 20.
- Practice floor 11 is Can be dismantled into at least two parts, into a lower part 21 with the stabilizing wings 22 and a head 23. The head 23 can be screwed to the lower part 21 or in connectable in another form.
- the lower part 21 is inserted so far into the sleeve 12 inserted until that the conical edge 24 in the adaptation area 8 on the winding body 1 is present. Then the head 23 is screwed on until it lies firmly against the flange 20. As a result, the practice floor 11 with its conical edge 24 in Adaptation area 8 fixed in the sleeve 12 by means of a clamp fit.
- FIG. 4 shows a detail of the conical part 5 of the winding body 1 the adaptation area 8 for the floor, partly in section.
- a top view of a double layer 25 of the winding body 1 can be seen below axis 2 .
- the Crossing angle of the crossing threads 2 take in the direction of Adaptation area 8 of the projectile from the larger crossing angle 6c to smaller crossing angle 6a.
- the flange 10 shows an almost parallel winding of the Threads 2.
- Above the axis 2, the winding body 1 is cut. The For the sake of clarity, only two double layers 25 are shown here. Every layer of Thread 2 is over the other.
- Threads with a binder or the filling of the gaps 28 between the threads with explosive are not shown Threads with a binder or the filling of the gaps 28 between the threads with explosive.
- the flange 20 is as a thickening on the end of the conical part 5 thanks to additional layers of thread lying one above the other, running almost parallel 26 have been formed.
- a Post-processing especially in the adaptation areas 7 and 8, for example by overturning or sanding the surfaces to keep them clean and level To create adhesive or contact surfaces.
- FIG. 30 Another example of an artillery ammunition 30 is shown in FIG.
- Features corresponding to the previous embodiment are shown with the same reference numerals. Agreement regarding the previous embodiment exists with regard to the design of the Winding body 1.
- the present Embodiment is a warhead.
- the stub sleeve 31 is in the present embodiment by means of a Clamp connection connected to the winding body 1.
- a clamping ring is located in a first groove 33 in the adaptation area 7a of the stub sleeve 31 34 used the clamping connection between the winding body 1 and stub sleeve 31 manufactures.
- a sealing ring 36 for example a rubber O-ring, around the Protect propellant charge from moisture.
- the stub sleeve 31 is comparable to the previous one Embodiment, a groove 37 in which a sealing ring 17 with sealing lip 18th is used, which is to serve as a gas seal.
- a groove 37 in which a sealing ring 17 with sealing lip 18th is used which is to serve as a gas seal.
- the stub sleeve bottom 38 is the Initial igniter 14 used.
- the installation of the warhead 32 in the winding body 1 takes place, in contrast to previous embodiment, by means of a projectile adapter 39.
- This projectile adapter 39 is already in the manufacture of Winding body 1 integrated into the winding body.
- the Projectile adapter pushed onto the mandrel on which the winding body is produced, and covered with the thread layers.
- the assembly of the Warhead 32 takes place in such a way that first the upper part 40 of the warhead 32 is inserted without the stabilizing wing 41 in the winding body 1.
- the bullet adapter 39 for example Glue or, as in the present embodiment, by a screw respectively.
- Glue for example Glue
- a thread 42 is provided for this is in the floor adapter 39 and on the Warhead top 32 a thread 42 is provided.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Building Environments (AREA)
- Storage Of Web-Like Or Filamentary Materials (AREA)
- Filamentary Materials, Packages, And Safety Devices Therefor (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Closures For Containers (AREA)
Description
- Figur 1
- die Ansicht eines erfindungsgemäßen Wickelkörpers mit sich änderndem Kreuzungswinkel der Fäden über die Länge des Wickelkörpers, insbesondere in den Adaptionsbereichen für das Geschoß und die Stummelhülse,
- Figur 2
- die Ansicht einer Doppellage eines Wickelkörpers, in der die Fäden miteinander verflochten sind,
- Figur 3
- einen Schnitt durch eine Granate mit einer flanschförmigen Verdickung am Hülsenmund zur Befestigung eines Geschosses, sowie eine Klebeverbindung zwischen dem Wickelkörper der Hülse und der Stummelhülse, die einen Dichtring trägt,
- Figur 4
- als Detail den Aufbau der Verdickung des Hülsenmunds in der Ansicht und im Schnitt und
- Figur 5
- einen Schnitt durch eine Granate mit einem Adapter zur Befestigung eines Geschosses sowie eine kraftschlüssige Verbindung zwischen dem Wickelkörper der Hülse und der Stummelhülse.
Claims (12)
- Munition mit einer Hülse, deren Wand aus einem verbrennbaren oder verzehrbaren Wickelkörper mit mindestens einer Doppellage sich kreuzender Fäden besteht, wobei die Fäden mit einem Bindemittel getränkt oder überzogen sind und wobei eine die Zündladung enthaltende Stummelhülse mit dem Wickelkörper verbunden ist, dadurch gekennzeichnet, dass der Wickelkörper (1) einteilig ist, dass durch eine sich ändernde Ablage der Fäden (3) über die Länge des Wickelkörpers (1) die Wickeldichte des Wickelkörpers (1) in Abstimmung auf die Belastung der Hülse (12) unterschiedlich ist und dass die Größe des Kreuzungswinkels in den Bereichen mit höherer Belastung kleiner ist als in den Bereichen mit geringerer Belastung.
- Munition nach Anspruch 1, dadurch gekennzeichnet, daß die Wickeldichte des Wickelkörpers (1) durch die Größe des Kreuzungswinkels (6) der Fäden bestimmt ist.
- Munition nach Anspruch 1 oder 2, dadurch gekennzeichnet, daß die Kreuzungswinkel (6a, 6b) der Fäden (3) des Wickelkörpers (1) im Adaptionsbereich (8) für das Geschoß (11, 32) und im Adaptionsbereich (7) für die Stummelhülse (13, 31) kleiner sind als die Kreuzungswinkel (6c) im übrigen Bereich des Wickelkörpers (1).
- Munition nach einem der Ansprüche1 bis 3, dadurch gekennzeichnet, daß die Kreuzungswinkel (6) der Fäden (3) im Wickelkörper (1) in Richtung auf die Adaptionsbereiche (7,8) kontinuierlich abnehmen.
- Munition nach einem der Ansprüche 1 bis 4, dadurch gekennzeichnet, daß der Wickelkörper (1) aus mehreren Doppellagen (25) besteht und daß sich die Kreuzungswinkel (6) in den jeweiligen Doppellagen (25) voneinander unterscheiden.
- Munition nach einem der Ansprüche 1 bis 5, dadurch gekennzeichnet, daß innerhalb einer Doppellage (25) des Wickelkörpers (1) die Fäden (3) ein Geflecht (9) bilden.
- Munition nach einem der Ansprüche 1 bis 6, dadurch gekennzeichnet, daß dem Bindemittel für die Fäden (3) ein Explosivstoff beigemischt ist.
- Munition nach einem der Ansprüche 1 bis 6, dadurch gekennzeichnet, daß die Zwischenräume (28) zwischen den Fäden (3) mindestens teilweise mit einem Explosivstoff gefüllt sind.
- Munition nach einem der Ansprüche 1 bis 8, dadurch gekennzeichnet, daß der Adaptionsbereich (8) für das Geschoß (11) so geformt ist, daß der Geschoßkörper (11) mit dem Wickelkörper (1) verbindbar ist.
- Munition nach Anspruch 9, dadurch gekennzeichnet, daß zur Befestigung des Geschoßkörpers (11) eine Verdickung (20) des Wickelkörpers (1) aus zusätzlichen Fadenlagen (26) geformt ist, wobei die Fäden (3) überwiegend parallel zueinander auf dem Wickelkörper (1) abgelegt sind.
- Munition nach einem der Ansprüche 1 bis 8, dadurch gekennzeichnet, daß im Adaptionsbereich (8) für das Geschoß (32) ein auf das Geschoß (32) abgestimmter Geschoßaufnahmeadapter (39) in dem Wickelkörper (1) integriert ist.
- Munition nach einem der Ansprüche 1 bis 11, dadurch gekennzeichnet, daß auf der Stummelhülse (13, 31), außerhalb des Bereichs (7a), in dem die Adaption mit dem Wickelkörper (1) erfolgt, zur Verhinderung von Gasleckage mindestens ein Dichtring (17) konzentrisch zur Achse (2) der Munition (10, 29) angeordnet ist.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19849824 | 1998-10-29 | ||
| DE19849824A DE19849824A1 (de) | 1998-10-29 | 1998-10-29 | Munition mit einer Hülse, deren Wand aus einem verbrennbaren oder verzehrbaren Wickelkörper besteht |
| PCT/EP1999/007862 WO2000026604A1 (de) | 1998-10-29 | 1999-10-16 | Munition mit einer hülse, deren wand aus einem verbrennbaren oder verzehrbaren wickelkörper besteht |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP1123482A1 EP1123482A1 (de) | 2001-08-16 |
| EP1123482B1 true EP1123482B1 (de) | 2003-07-23 |
Family
ID=7886016
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP99955854A Expired - Lifetime EP1123482B1 (de) | 1998-10-29 | 1999-10-16 | Munition mit einer hülse, deren wand aus einem verbrennbaren oder verzehrbaren wickelkörper besteht |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US6523476B1 (de) |
| EP (1) | EP1123482B1 (de) |
| AT (1) | ATE245799T1 (de) |
| CA (1) | CA2349542C (de) |
| DE (2) | DE19849824A1 (de) |
| IL (1) | IL142830A (de) |
| WO (1) | WO2000026604A1 (de) |
| ZA (1) | ZA200104079B (de) |
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|---|---|---|---|---|
| US8776690B2 (en) | 2009-08-04 | 2014-07-15 | Nitrochemie Aschau Gmbh | Sleeve for accommodating propellant charge powder |
| DE102015116985A1 (de) | 2015-10-06 | 2017-04-06 | Rheinmetall Waffe Munition Gmbh | Selbstverzehrendes Geschoss |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE10038751A1 (de) | 2000-05-26 | 2001-11-29 | Dynamit Nobel Ag | Wickelkörper als Hülse für Munition |
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| US9644930B1 (en) * | 2010-11-10 | 2017-05-09 | True Velocity, Inc. | Method of making polymer ammunition having a primer diffuser |
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| FR3113728B1 (fr) * | 2020-09-01 | 2022-12-02 | Nexter Munitions | Douille combustible pour munition |
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| US3348445A (en) * | 1965-02-10 | 1967-10-24 | Isidore G Nadel | Method of making solid propellants in textile form |
| US3304867A (en) * | 1965-02-10 | 1967-02-21 | Isidore G Nadel | Solid propellants in textile form |
| US3745927A (en) * | 1969-05-19 | 1973-07-17 | Celanese Corp | Casing and propellant of nitrocellulose filaments and nitrocellulose fibers |
| US3706279A (en) * | 1971-01-20 | 1972-12-19 | Us Army | Combustible cartridge case |
| NO133382C (de) * | 1973-05-25 | 1976-04-21 | Raufoss Ammunisjonsfabrikker | |
| DE2705278C2 (de) * | 1977-02-09 | 1984-02-23 | Rheinmetall GmbH, 4000 Düsseldorf | Stummelhülse mit Liderung |
| FR2488390B1 (fr) * | 1980-08-07 | 1986-07-04 | Serat | Perfectionnements aux enveloppes de corps de projectile charge en explosif par emploi de structures creuses realisees par enroulement filamentaire |
| DE3534972C1 (de) * | 1985-10-01 | 1992-04-09 | Dynamit Nobel Ag | Huelsenlose Munition |
| US5048421A (en) * | 1990-08-06 | 1991-09-17 | Olin Corporation | Combustible cartridge case base |
| US5323707A (en) * | 1991-08-05 | 1994-06-28 | Hercules Incorporated | Consumable low energy layered propellant casing |
| US5563365A (en) * | 1993-08-09 | 1996-10-08 | The United States Of America As Represented By The Secretary Of The Army | Case base/combustible cartridge case joint |
| DE4342428C2 (de) * | 1993-12-13 | 1999-05-27 | Rheinmetall W & M Gmbh | Geschützmunition mit einer verbrennbaren Treibladungshülse |
-
1998
- 1998-10-29 DE DE19849824A patent/DE19849824A1/de not_active Withdrawn
-
1999
- 1999-10-16 US US09/830,627 patent/US6523476B1/en not_active Expired - Lifetime
- 1999-10-16 AT AT99955854T patent/ATE245799T1/de not_active IP Right Cessation
- 1999-10-16 DE DE59906382T patent/DE59906382D1/de not_active Expired - Lifetime
- 1999-10-16 IL IL14283099A patent/IL142830A/en not_active IP Right Cessation
- 1999-10-16 EP EP99955854A patent/EP1123482B1/de not_active Expired - Lifetime
- 1999-10-16 CA CA002349542A patent/CA2349542C/en not_active Expired - Fee Related
- 1999-10-16 WO PCT/EP1999/007862 patent/WO2000026604A1/de not_active Ceased
-
2001
- 2001-05-18 ZA ZA200104079A patent/ZA200104079B/en unknown
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8776690B2 (en) | 2009-08-04 | 2014-07-15 | Nitrochemie Aschau Gmbh | Sleeve for accommodating propellant charge powder |
| DE102015116985A1 (de) | 2015-10-06 | 2017-04-06 | Rheinmetall Waffe Munition Gmbh | Selbstverzehrendes Geschoss |
| WO2017060109A1 (de) | 2015-10-06 | 2017-04-13 | Rheinmetall Waffe Munition Gmbh | Selbstverzehrendes geschoss |
Also Published As
| Publication number | Publication date |
|---|---|
| US6523476B1 (en) | 2003-02-25 |
| CA2349542A1 (en) | 2000-05-11 |
| IL142830A0 (en) | 2002-03-10 |
| DE59906382D1 (de) | 2003-08-28 |
| ATE245799T1 (de) | 2003-08-15 |
| IL142830A (en) | 2004-09-27 |
| CA2349542C (en) | 2007-09-25 |
| EP1123482A1 (de) | 2001-08-16 |
| DE19849824A1 (de) | 2000-05-04 |
| ZA200104079B (en) | 2002-07-03 |
| WO2000026604A1 (de) | 2000-05-11 |
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