EP0341270A1 - Multiple connector for propellant charge modules - Google Patents
Multiple connector for propellant charge modulesInfo
- Publication number
- EP0341270A1 EP0341270A1 EP19880907265 EP88907265A EP0341270A1 EP 0341270 A1 EP0341270 A1 EP 0341270A1 EP 19880907265 EP19880907265 EP 19880907265 EP 88907265 A EP88907265 A EP 88907265A EP 0341270 A1 EP0341270 A1 EP 0341270A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- propellant charge
- plug
- ring
- charge modules
- modules
- 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.)
- Ceased
Links
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
- F42B5/38—Separately-loaded propellant charges, e.g. cartridge bags
Definitions
- the invention relates to a plug connection for at least two propellant charge modules according to the preamble of patent claim 1.
- propellant charge modules which are lined up several times in succession for a charging process of a gun to increase the longitudinal stiffness and partial cartridges designed as propellant charge containers and having different lengths
- Sorting process requires a considerable amount of time for the push-on process.
- a propellant charge module is known from WO 86/01584, the module structure of which allows any interchangeability and enables simple manual and also automatic chargeability of the individual modules.
- the modules are axially and rotationally symmetrical of the same size, so that they can be used advantageously for all charge levels.
- no way is shown to manually feed several propellant guns for hand-loaded weapons, in particular weapons without an automatic loader, to the charge chamber of the barrel weapon.
- the object of the invention is to provide propellant charge modules with a plug-in connection in order to shorten the manual charging time, which ensures an arbitrary plug-in direction of the modules one behind the other and an arbitrary charge direction of assembled propellant charge modules.
- the plug-in ring according to the invention advantageously enables simple and quick assembly of rotationally and axially symmetrical propellant charge modules for a common manual charging process.
- the plug ring is designed as a single element, so that the propellant charge modules can be connected in any axial direction through the plug ring.
- the fact that each propellant charge module both. is constricted in the side of the coat, can be used by anyone
- Propellant charge module a plug-in ring on both sides and thus a stable series of modules can be achieved according to the desired range.
- any combination of identical propellant charge modules means that there are no longer any propellant charges.
- the propellant charge modules which can be used in different gradations, can be plugged together in a variety of ways, for example as exercise and combat charges. so that there are no problems with aging of the propellant charge modules.
- the equality of the components additionally ensures simple training of the operating personnel and also enables simple stowability.
- FIG. 1 illustrates two rotationally and axially symmetrical propellant charge containers 4 for propellant charge modules 2, the internal structure and ignition mechanism of which for the propellant charge 3 can be gathered from WO 86/01584 as known.
- Each jacket of the container 4 contains a constricted area 5 on both sides for attaching a separate plug ring 6.
- half of the plug ring 6 overlaps the area 5 of a jacket diameter constriction of a propellant charge module 2.
- the outer diameter of the plug ring 6 corresponds to the outer diameter of the propellant charge container 4, so that caliber equality is achieved.
- the plug ring 6 is combustible and can be produced in a particularly advantageous manner in the manufacture of the container 4 by separating the plug ring from the combustible jacket of the container 4 ' which can be connected together from two parts.
- the fastening means can, on the one hand, consist of a pressure sensitive adhesive which can be applied, for example sprayed, onto a smooth inside of the plug ring 6 .
- Fastening means on the other hand, can also consist of a corrugation 8 (FIG. 2) arranged on the inner surface 7, the corrugation 8 can consist, for example, of longitudinal corrugations, which in a particularly advantageous manner without additional work already during the pressing process of a known pressing method can be produced. 2 shows that the longitudinal grooves are not only arranged on the support ring 6, but also on the inner surface 10 of the container 4, the outer diameter of the container 4 being constricted in the region 5 by a further working step on the inner diameter of the plug ring 6 has been.
- Knobs 9 arranged on the inner surface 7 and directed radially inwards, as shown in FIG. 3, can also serve as fastening means for the plug ring 6. These knobs 9 do not require any special effort for production, because they can also be produced directly by another known pressing method.
- the corrugation 8 and the knobs 9 are advantageously arranged at a distance of up to 20 mm from one another and can have a height of up to 1.5 mm, for example with a caliber of 155 mm a stable clamping connection even at a distance of 10 mm and. a height of 0.4 mm is reached. Such a clamp connection can be released and closed as often as required.
Abstract
Bei bekannten Kartuschen ist für einen manuellen Ladevorgang die axiale Richtung der Teilkartuschen durch eine Steckverbindung vorgeschrieben, so daß eine beliebige Aufsteckrichtung der Kartuschen hintereinander und eine beliebige Laderichtung zusammengesteckter Kartuschen nicht gewährleistet ist. Diese Steckverbindung läßt sich zur Verkürzung der manuellen Ladezeit dann nicht auf rotations- und axialsymmetrisch gleiche Treibladungsmodule übertragen, wenn diese Treibladungsmodule in beliebiger Folge, Anzahl, Aufsteck- und Laderichtung für einen manuellen Ladervorgang zusam mengesteckt werden sollen. Abhilfe schafft hier eine Steckverbindung (1) für wenigstens zwei rotations- und axialsymmet risch gleiche Treibladungsmodule (2), die beidseitig an jedem ihrer Behälter (4) einen eingeschnürten Mantelbereich (5) aufweisen und zwei benachbarte Behälter (4) auf ihren einander zugekehrten Mantelbereichen (5) durch einen separaten Steckring (6) verbunden sind. Der Steckring verleiht insbesondere durch eine zusätzliche Klemm- oder Klebeverbindung eine hohe Stabilität der entsprechend der Schußweite in unterschiedlichen Abstufungen beliebig zusammensteckbaren Treibladungsmodule. In known cartridges, the axial direction of the partial cartridges is for a manual loading process by a Plug connection prescribed, so that any plug-in direction of the cartridges in a row and any one Loading direction of assembled cartridges is not guaranteed. This connector can be used Shortening the then do not transfer the manual charging time to rotationally and axially symmetrically identical propellant charge modules if these Propellant charge modules in any order, number, plug-in and charging direction for a manual loading process together should be plugged in. A plug-in connection (1) for at least two rotational and axially symmetric The same propellant charge modules (2), constricted on both sides of each of their containers (4) Coat area (5) and two adjacent containers (4) on their mutually facing jacket areas (5) by one separate Plug ring (6) are connected. The plug ring lends in particular through an additional clamping or Adhesive connection a high degree of stability according to the range in any increments pluggable Propellant charge modules.
In the case of known cartouches, the direction of axial insertion of sub-cartouches is determined during manual loading by a multiple connector which does not allow the cartouches to be inserted one behind the other in any desired direction or the assembled cartouches to be loaded in any desired direction. This multiple connector can therefore not be used, to reduce the manual loading time, with identical rotationally symmetrical and axially symmetrical propellant charge modules, if these modules are to be assembled in any desired sequence, number, direction of insertion and direction of loading during manual loading. This problem is resolved by a multiple connector (1) for at least two identical rotationally symmetrical and axially symmetrical propellant charge modules (2), which have a constricted case region (5) on other side of the container (4), two adjacent containers (4) being connected on the side of the region of the casing (5) in mutual contact by a separate connector ring (6). The connector ring, in particular by virtue of an additional connection by clamping or adhesion, guarantees a high stability of the propellant charge modules which can be intercon nected as desired in various graduations corresponding to their range. In the case of known cartouches, the direction of axial insertion of sub-cartouches is determined during manual loading by a multiple connector which does not allow the cartouches to be inserted one behind the other in any desired direction or the assembled cartouches to be loaded in any desired direction. This multiple connector can therefore not be used, to reduce the manual loading time, with identical rotationally symmetrical and axially symmetrical propellant charge modules, if these modules are to be assembled in any desired sequence, number, direction of insertion and direction of loading during manual loading. This problem is resolved by a multiple connector (1) for at least two identical rotationally symmetrical and axially symmetrical propellant charge modules (2), which have a constricted case region (5) on other side of the container (4), two adjacent containers (4) being connected on the side of the region of the casing (5) in mutual contact by a separate connector ring (6). The connector ring, in particular by virtue of an additional connection by clamping or adhesion, guarantees a high stability of the propellant charge modules which can be intercon nected as desired in various graduations corresponding to their range.
Description
. Steckverbindung für Treibladungsmodule. . Plug connection for propellant charge modules.
Die Erfindung betrifft eine Steckverbindung für wenigstens zwei Treibladungsmodule nach dem Oberbegriff des Patentan¬ spruches 1.The invention relates to a plug connection for at least two propellant charge modules according to the preamble of patent claim 1.
5 Aus dem DE-GBM 70 00 615 sind Treibladungsmodule bekannt, die für einen Ladungsvorgang eines Geschützes zur Erhöh¬ ung der Längssteifigkeit mehrfach hintereinander aneinan¬ dergereiht sind und als Treibladungsbehälter ausgebildete und unterschiedliche Längen aufweisende Teilkartuschen5 DE-GBM 70 00 615 propellant charge modules are known, which are lined up several times in succession for a charging process of a gun to increase the longitudinal stiffness and partial cartridges designed as propellant charge containers and having different lengths
10 aufweisen, welche einseitig mit einer Wandverlängerung zum Aufstecken auf eine benachbarte Teilkartusche versehen sind Diese Teilkartuschen müssen jedoch, insbesondere aufgrund einer in der Form abweichenden Anfangskartüsche, in einer vorgeschriebenen Reihenfolge und Richtung sortiert auf-10, which are provided on one side with a wall extension for plugging onto an adjacent partial cartridge. However, these partial cartridges must be sorted in a prescribed order and direction, in particular due to a different starting cartridge.
15 einandergesteckt werden;. Durch einen derartigen. Sortie - vorgang entsteht jedoch für den Aufsteckvorgang ein erheb¬ licher Zeitbedarf.15 inserted one into the other ;. By such. Sorting process, however, requires a considerable amount of time for the push-on process.
Für den Fall, daß bereits zusammengesteckte Teilkartuschen '20 im Kampfraum des Geschützes bevorratet sind, muß deswei¬ teren bei jedem Ladevorgang auf eine richtige Laderichtung • und eine richtige Wahl der Kartuschen geachtet werden. Müssen bei einer verkürzten Schußweite die komplett zusam¬ mengesteckten Teilkartuschen in ihrer Stückzahl reduziert 25 werden, so ist für die Unterbringung einer nicht benutzten verbleibenden Teilkartusche ein zusätzlicher Platzbedarf erforderlich.
Aus der WO 86/01584 ist ein Treibladungsmodul bekannt, dessen Modulaufbau eine beliebige Austauschbarkeit-ge¬ stattet und eine einfache manuelle und auch automatische Ladbarkeit der einzelnen Module ermöglicht. Die Module sind axial- und rotationssymmetrisch gleich groß, so daß sie für alle Ladungsstufungen vorteilhaft eingesetzt werden könn Es wird jedoch kein Weg aufgezeigt, für handladbare Waffen, insbesondere Waffen ohne automatischen Lader, mehrere Treibladuπgsrao.dule gemeinsam manuell dem Laduπgsraum der Rohrwaffe zuzuführen.In the event that already mated part cartridges are stored in the '20 fighting compartment of the gun must deswei¬ more advanced with each loading process on a correct loading direction • and a correct choice of cartridges are respected. If, in the case of a shortened firing range, the number of pieces of the completely assembled partial cartridges has to be reduced, then additional space is required to accommodate an unused remaining partial cartridge. A propellant charge module is known from WO 86/01584, the module structure of which allows any interchangeability and enables simple manual and also automatic chargeability of the individual modules. The modules are axially and rotationally symmetrical of the same size, so that they can be used advantageously for all charge levels. However, no way is shown to manually feed several propellant guns for hand-loaded weapons, in particular weapons without an automatic loader, to the charge chamber of the barrel weapon.
Aufgabe der Erfindung ist es, Treibladungsmodule zur Ver¬ kürzung der manuellen Ladezeit mit einer Steckverbindung zu versehen, die eine beliebige AufSteckrichtung der Modu- le hintereinander und eine beliebige Laderichtuπg zusammen¬ gesteckter Treibladungsmodule gewährleistet.The object of the invention is to provide propellant charge modules with a plug-in connection in order to shorten the manual charging time, which ensures an arbitrary plug-in direction of the modules one behind the other and an arbitrary charge direction of assembled propellant charge modules.
Gelöst wird diese Aufgabe durch die im Patentanspruch 1 angegebenen gekennzeichneten Merkmale. Vorteilhafte Ausge- staltungeπ und Weiterbildungen der Erfindung gehen aus den Unteransprüchen hervor.This object is achieved by the marked features specified in claim 1. Advantageous embodiments and further developments of the invention emerge from the subclaims.
Durc den erfindungsgemäßen Steckring wird in vorteilhafter Weise eine einfache und schnelle Montage rotations- und axialsymmetrischer Treibladungsmodule für einen gemeinsamen manuellen Ladevorgang ermöglicht. Der Steckring ist als Einzelelement ausgebildet, so daß die Treibladungsmodule in beliebiger axialer Richtung durch den Steckring verbunde werden können. Dadurch, daß jedes Treibladungsmodul beid- . seitig im Mantelbereich eingeschnürt ist, kann bei jedemThe plug-in ring according to the invention advantageously enables simple and quick assembly of rotationally and axially symmetrical propellant charge modules for a common manual charging process. The plug ring is designed as a single element, so that the propellant charge modules can be connected in any axial direction through the plug ring. The fact that each propellant charge module both. is constricted in the side of the coat, can be used by anyone
Treibladungsmodul auf beiden Seiten ein Steckring aufgestec werden und somit eine stabile Aneinanderreihung der Module entsprechend der gewünschten Schußweite erzielt werden.Propellant charge module a plug-in ring on both sides and thus a stable series of modules can be achieved according to the desired range.
In weiter vorteilhafter Weise fallen durch die beliebige Zusammenstellung gleicher Treibladungsmodule keine Rest- treibladuπgen mehr an. Die in unterschiedlichen Abstufungen eiπsetzbaren Treibladuπgsmodule sind vielfältig - beispiels weise als Übuπgs- und Gefechtsladungen - zusammensteckbar,.
so daß keine Probleme hinsichtlich einer Überalterung der Treibladungsmodule entstehen. Die Gleichheit der Bauteile gewährleistet zusätzlich eine einfache Ausbil¬ dung des Bedienungspersonales und ermöglicht darüber hinaus eine einfache Verstaubarkeit.In a further advantageous manner, any combination of identical propellant charge modules means that there are no longer any propellant charges. The propellant charge modules, which can be used in different gradations, can be plugged together in a variety of ways, for example as exercise and combat charges. so that there are no problems with aging of the propellant charge modules. The equality of the components additionally ensures simple training of the operating personnel and also enables simple stowability.
Die Erfindung wird anhand der Zeichnung näher erläutert. Es zeigtThe invention is explained in more detail with reference to the drawing. It shows
Fig 1: zwei durch einen Steckring aneinandergereihte Treibladungsmodule,1: two propellant charge modules lined up by a plug-in ring,
Fig. 2: ' ausschnittsweise den auf einem Behälter des Treibladungsmoduls aufgesteckten Steckring gemäß einem in der Fig. 1 mit II-II angege¬ benen Schnittverlauf,2: 'a section of the plug-in ring which is plugged onto a container of the propellant charge module in accordance with a sectional profile indicated by II-II in FIG. 1,
Fig. 3: eine ausschnittsweise dargestellte Innenseite des Steckringes gemäß einer in der Fig. 1 mit III angegebenen Pfeilrichtung.3: a section of the inside of the plug-in ring according to an arrow direction indicated by III in FIG. 1.
Die Fig. 1 verdeutlicht zwei rotations- und axialsym¬ metrische Treibladungsbehälter 4 für Treibladuπgsmodule 2, deren Iπnenaufbau und Zündmechanismus für die Treibladun 3 aus der WO 86/01584 als bekannt zu entnehmen ist.1 illustrates two rotationally and axially symmetrical propellant charge containers 4 for propellant charge modules 2, the internal structure and ignition mechanism of which for the propellant charge 3 can be gathered from WO 86/01584 as known.
Jeder Mantel des Behälters 4 enthält beidseitig einen eingeschnürten Bereich 5 zum Aufstecken eines separaten Steckringes 6. Zur Herstellung dieser Steckverbindung überlappt eine Hälfte des Steckringes 6 jeweils den Be- reich 5 einer Manteldurchmessereinschnurung eines Treib¬ ladungsmoduls 2. Der Außendurchmesser des Steckringes 6 entspricht dem Außendurchmesser des Treibladungsbehäl¬ ters 4, so daß Kalibergleichheit erzielt wird.
Der Steckring 6 ist verbrennbar und kann in besonders vor¬ teilhafter Weise bei der Herstellung des Behälters 4 durch Abtrennen des Steckringes vom verbrennbaren Mantel des aus zwei Teilen zusammenverbindbaren Behälters 4 'hergestellt werden.Each jacket of the container 4 contains a constricted area 5 on both sides for attaching a separate plug ring 6. To produce this plug connection, half of the plug ring 6 overlaps the area 5 of a jacket diameter constriction of a propellant charge module 2. The outer diameter of the plug ring 6 corresponds to the outer diameter of the propellant charge container 4, so that caliber equality is achieved. The plug ring 6 is combustible and can be produced in a particularly advantageous manner in the manufacture of the container 4 by separating the plug ring from the combustible jacket of the container 4 ' which can be connected together from two parts.
Durch ein zwischen der Innenfläche 7 des Steckringes 6 und dem eingeschnürten Mantelbereich 5 des Treibladungsmo¬ duls 2 angeordnetes Befestiguπgsmifrtel wird eine stabile Verbindung zwischen jeweils zwei benachbarten Treibladuπgs- modulen 2 erreicht und eine der Schußentfernung entsprechen de Aneinanderreihung mit hoher Längssteifigkeit für einen schnellen manuellen Ladevorgang erzielt.By means of a fastening means arranged between the inner surface 7 of the plug-in ring 6 and the constricted jacket area 5 of the propellant charge module 2, a stable connection is achieved between two adjacent propellant charge modules 2 and a line-up corresponding to the shot distance is achieved with a high longitudinal stiffness for a quick manual loading process .
Das Befestigυngsmittel kann einerseits aus einem Haftkle¬ ber bestehen, der auf einer glatten Innenseite des Steck¬ ringes 6 aufgetragen, beispielsweise aufgesprüht, werden kann.Das .Befestigungsmittel kann andererseits auch aus ein an der Innenfläche 7 angeordneten Riffelung 8 (Fig. 2) be- stehen, wobei die Riffelung 8 beispielsweise aus Längsril¬ len bestehen kann, die in besonders vorteilhafter Weise ohne zusätzlichen Arbeitsaufwand bereits beim Preßvorgang eines an sich bekannten Preßverfahrens hergestellt werden können. Die Fig. 2 verdeutlicht, daß die Längsrillen nicht nur auf dem Stützring 6, sondern auch auf der Innenfläche 10 des Behälters 4 angeordnet sind, wobei der Außendurch¬ messer des Behälters 4 im Bereich 5 durch einen weiteren Arbeitsschritt auf den Innendurchmesser des Steckringes 6 eingeschnürt worden ist.The fastening means can, on the one hand, consist of a pressure sensitive adhesive which can be applied, for example sprayed, onto a smooth inside of the plug ring 6 . Fastening means, on the other hand, can also consist of a corrugation 8 (FIG. 2) arranged on the inner surface 7, the corrugation 8 can consist, for example, of longitudinal corrugations, which in a particularly advantageous manner without additional work already during the pressing process of a known pressing method can be produced. 2 shows that the longitudinal grooves are not only arranged on the support ring 6, but also on the inner surface 10 of the container 4, the outer diameter of the container 4 being constricted in the region 5 by a further working step on the inner diameter of the plug ring 6 has been.
Als Befestigungsmittel des Steckringes 6 können auch auf der Innenfläche 7 angeordnete und radial nach innen ge¬ richtete Noppen 9 dienen, wie sie in der Fig. 3 dargestell sind. Auch diese Noppen 9 benötigen zur Herstellung keinen besonderen Aufwand, weil sie ebenfalls direkt durch ein weiteres bekanntes Preßverfahren erzeugbar sind.
Die Riffelung 8 und die Noppen 9 sind vorteilhaft in einem Abstand bis zu 20 mm voneinander angeordnet und können eine Höhe bis zu 1,5 mm aufweisen, wobei bei¬ spielsweise bei einem Kaliber von 155 mm eine stabile Klemmverbindung bereits bei einem Abstand von 10 mm und. einer Höhe von 0,4 mm erreicht wird..Eine derartige Klemmverbindung kann beliebig oft gelöst und geschlossen werden.
Knobs 9 arranged on the inner surface 7 and directed radially inwards, as shown in FIG. 3, can also serve as fastening means for the plug ring 6. These knobs 9 do not require any special effort for production, because they can also be produced directly by another known pressing method. The corrugation 8 and the knobs 9 are advantageously arranged at a distance of up to 20 mm from one another and can have a height of up to 1.5 mm, for example with a caliber of 155 mm a stable clamping connection even at a distance of 10 mm and. a height of 0.4 mm is reached. Such a clamp connection can be released and closed as often as required.
Claims
1. Steckverbindung (1) für wenigstens zwei Treibladungs¬ module (2) , wobei die Treibladungsmodule (2) jeweils einen Treibladungspulver (3) aufnehmenden verbreπnbaren Behälter (4) aufweisen und die Steckverbindung (1)1. Plug connection (1) for at least two Treibladungs¬ modules (2), the propellant charge modules (2) each having a propellant charge powder (3) receiving expandable container (4) and the plug connection (1)
5 kalibergleich einen benachbarten Behälter (4) in einem eingeschnürten Mantelbereich (5) verbindet, d a ¬ d u r c g e k e n n z e i c h n e t , daß der eingeschnürte Mantelbereich (5) beidseitig symmetrisch an jedem Behälter (4) angeordnet ist, und daß zwei 10 benachbarte Behälter (4) im Mantelbereich (5) ihrer einander zugekehrten Manteleinschnürung durch einen separaten Steckring (6) verbunden sind.5 caliber-like an adjacent container (4) in a constricted jacket area (5), since ¬ durc noted that the constricted jacket area (5) is symmetrically arranged on both sides of each container (4), and that two 10 adjacent containers (4) in the jacket area (5) their mutually facing jacket constriction are connected by a separate plug ring (6).
2. Steckverbindung nach Anspruch 1, d a d u r c h2. Connector according to claim 1, d a d u r c h
15 g e k e n n z e i c h n e t , daß zwischen dem einge¬ schnürten Mantelbereich (5) der benachbarten Behälter (4) und der Innenfläche (7) des Steckringes (6) Befesti¬ gungsmittel angeordnet sind.15, that fastening means are arranged between the constricted jacket region (5) of the adjacent containers (4) and the inner surface (7) of the plug-in ring (6).
20 3. Steckverbindung nach Anspruch 1 und 2, d a d u r c h g e k e n n z e i c h n e t , daß das Befestigungsmit¬ tel aus einem Haftkleber besteht. 20 3. Connector according to claim 1 and 2, characterized in that the Befestigungsmit¬ tel consists of a pressure sensitive adhesive.
4. Steckverbindung nach Anspruch 1 und 2, d a d u r c h g e k e n n z e i c h n e t , daß die Befestigungsmittel an der Steckringinnenfläche (7) angeordnet sind.4. Plug connection according to claim 1 and 2, that the fastening means are arranged on the inner surface of the plug ring (7).
5. Steckverbindung nach einem der Ansprüche 1, 2 und 4, d a d u r c h g e k e n n z e i c h n e t , daß die Befestigungsmittel aus einer Riffe.lung (8)' der Steckringinnenfläche (7) besteht.5. Plug connection according to one of claims 1, 2 and 4, characterized in that the fastening means consists of a Riffe.lung (8) 'of the inner ring surface (7).
Steckverbindung nach einem der Ansprüche 1, 2 und 4, d a d u r c h g e k e n n z e i c h π e t , daß die Befestigungsmittel aus von der Steckringinnenfläche (7) nach innen stehenden Noppen (9) bestehen. Plug connection according to one of claims 1, 2 and 4, so that the fastening means consist of knobs (9) protruding inwards from the inner surface of the plug ring (7).
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19873737704 DE3737704C2 (en) | 1987-11-06 | 1987-11-06 | Plug connection for propellant charge modules |
| DE3737704 | 1987-11-06 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP0341270A1 true EP0341270A1 (en) | 1989-11-15 |
Family
ID=6339936
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP19880907265 Ceased EP0341270A1 (en) | 1987-11-06 | 1988-07-27 | Multiple connector for propellant charge modules |
Country Status (5)
| Country | Link |
|---|---|
| EP (1) | EP0341270A1 (en) |
| JP (2) | JPH02500772A (en) |
| DE (1) | DE3737704C2 (en) |
| DK (1) | DK238689A (en) |
| WO (1) | WO1989004453A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5212342A (en) * | 1991-02-11 | 1993-05-18 | Giat Industries | Container for receiving propellant charges |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE4124657A1 (en) * | 1991-07-25 | 1993-01-28 | Rheinmetall Gmbh | MODULAR DRIVE CHARGE |
| SE512205C2 (en) | 1998-12-18 | 2000-02-14 | Bofors Ab | In the initiation of artillery propellant charges consisting of a plurality of propellant modules arranged one after the other, to achieve an even over-ignition between them and propellant modules and complete charges designed in accordance with the method. |
| SG92814A1 (en) * | 2001-09-20 | 2002-11-19 | Defence Science & Technology A | An artillery propellant charge module |
| DE102005025714A1 (en) * | 2005-06-04 | 2007-01-04 | Nitrochemie Aschau Gmbh | Multi-part ammunition |
| DE102007033832B4 (en) | 2007-07-18 | 2014-06-12 | Rheinmetall Waffe Munition Gmbh | Ammunition with a propellant charge consisting of several partial charges |
Family Cites Families (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| BE545353A (en) * | 1955-03-08 | |||
| NL121817C (en) * | 1958-09-12 | |||
| NL265662A (en) * | 1960-06-07 | |||
| US3176617A (en) * | 1962-06-11 | 1965-04-06 | Beloit Corp | Separate loading of artiliery propellant charges |
| DE1243053B (en) * | 1965-05-08 | 1967-06-22 | Rheinmetall Gmbh | Partial load cartridge |
| FR1514293A (en) * | 1967-01-11 | 1968-02-23 | France Etat | propellant charge elements for artillery ammunition |
| FR1597586A (en) * | 1968-10-25 | 1970-06-29 | ||
| FR1591276A (en) * | 1968-11-05 | 1970-04-27 | ||
| DE7000615U (en) * | 1970-01-09 | 1970-06-11 | Wasagchemie Ag | CONTAINER FOR DRIVING CHARGES. |
| GB2092720B (en) * | 1981-01-29 | 1984-06-13 | Bettix Ltd | Explosive charge container |
| JPS59158897U (en) * | 1983-04-12 | 1984-10-24 | 防衛庁技術研究本部長 | propellant cartridge |
| DE3432291A1 (en) * | 1984-09-01 | 1986-03-13 | Rheinmetall GmbH, 4000 Düsseldorf | DRIVE CHARGE MODULE |
-
1987
- 1987-11-06 DE DE19873737704 patent/DE3737704C2/en not_active Expired - Fee Related
-
1988
- 1988-07-27 EP EP19880907265 patent/EP0341270A1/en not_active Ceased
- 1988-07-27 WO PCT/EP1988/000681 patent/WO1989004453A1/en not_active Application Discontinuation
- 1988-07-27 JP JP50688488A patent/JPH02500772A/en active Pending
-
1989
- 1989-05-16 DK DK238689A patent/DK238689A/en not_active Application Discontinuation
-
1994
- 1994-08-15 JP JP1994010051U patent/JP2585093Y2/en not_active Expired - Lifetime
Non-Patent Citations (1)
| Title |
|---|
| See references of WO8904453A1 * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5212342A (en) * | 1991-02-11 | 1993-05-18 | Giat Industries | Container for receiving propellant charges |
Also Published As
| Publication number | Publication date |
|---|---|
| DE3737704C2 (en) | 1998-03-12 |
| JPH02500772A (en) | 1990-03-15 |
| DE3737704A1 (en) | 1989-05-18 |
| DK238689A (en) | 1989-05-18 |
| WO1989004453A1 (en) | 1989-05-18 |
| JPH0722299U (en) | 1995-04-21 |
| JP2585093Y2 (en) | 1998-11-11 |
| DK238689D0 (en) | 1989-05-16 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
| 17P | Request for examination filed |
Effective date: 19890125 |
|
| AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): DE FR GB IT NL SE |
|
| 17Q | First examination report despatched |
Effective date: 19901126 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION HAS BEEN REFUSED |
|
| 18R | Application refused |
Effective date: 19910808 |