| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 141 | JPS509176A - | JP3219674 | 1974-03-20 | JPS509176A | 1975-01-30 | |
| An open chamber gas powered tool and gas generating charge for the tool. The charge has a hollow open-ended plastic jacket of uniform noncircular cross-section from end to end containing a propellant, such as nitrocellulose, which may be electrically ignited through an open end of the jacket by a spark, hot wire or the like or ignited by detonation of a dab of priming compound contained within a recess in one end of the jacket. The tool has an open chamber breech mechanism including a cylinder containing a firing chamber opening through the cylinder circumference for transporting charges to firing position wherein the chamber is closed by the breech frame, a trigger actuated firing means for firing the charges in firing position, and operating means powered by the gas generated by each fired charge for performing a work function. | ||||||
| 142 | Treibladungskörper | EP11007293.1 | 2011-09-08 | EP2428762A2 | 2012-03-14 | Pfersmann, Axel, Dr. |
Die Erfindung betrifft einen Treibladungskörper (1) zum Einbringen in eine Treibladungskammer (10) einer Schusswaffe zum Verschießen hülsenloser Munition, wobei der Treibladungskörper (1) einen ein Treibladungsmittel enthaltenden Grundkörper (1a) aufweist, der einen gegenüber dem Innendurchmesser (D) der Treibladungskammer (10) geringeren Durchmesser (d) aufweist. In einem oder mehreren Teilbereichen auf dem Umfang des Grundkörpers (1a) sind radiale Vorsprünge (2) angeordnet, welche den Radius (r) des Grundkörpers (1a) in diesen Teilbereichen an den Innenradius (R) der Treibladungskammer (10) angleichen.
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| 143 | MUNITION HANDLING APPARATUS | EP09785706.4 | 2009-09-30 | EP2342525A1 | 2011-07-13 | CHETCUTI, Raphael, Joseph, Francis |
| There is disclosed a munition handling apparatus (10) where the conventional ram is replaced with a high pressure fluid actuaction. For this the apparatus is provided with a container (60) that incorporates a piston (105) which slides along the container to urge the munition out as the fluid pressure is applied. | ||||||
| 144 | Munition handling apparatus | EP08253205.2 | 2008-10-01 | EP2172732A1 | 2010-04-07 | The designation of the inventor has not yet been filed |
There is disclosed a munition handling apparatus where the conventional ram is replaced with a high pressure fluid actuaction. For this the apparatus is provided with a container (101) that incorporates a piston (105) which slides along the container to urge the munition out as the fluid pressure is applied.
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| 145 | CHARGE MOUNT | EP08762630.5 | 2008-07-02 | EP2162696A1 | 2010-03-17 | TAYLOR, John; CHETCUTI, Raphael, Joseph Francis; MARSHALL, Charles, Thomas; MACKENZIE, Colin, Carson |
| The following invention relates to a mount (10) for holding a charge (18) in a breech (16). The mount (10) attaches, or is integral to, a charge (18) and is provided with a dilation means (14) which rests within a breech (16) of a gun to prevent the charge (18) from sliding back out of the breech (16) when the gun is held at a high angle. The dilation means (14) is fabricated from a material which, when the gun is fired, combusts to leave negligible debris in the breech (16). | ||||||
| 146 | Propellant charge for recoilless gun | EP07117803.2 | 2007-10-03 | EP2045568A1 | 2009-04-08 | Gustafsson, Pär; Irdell, Henrik |
The present invention relates to a propellant charge for a recoilless gun, in particular a propellant charge for a round of a reloadable support weapon. Said propellant charge (4, 22) is cylindrically shaped and adapted for loading into a charge chamber (16) formed between an inner casing (2) and an outer casing (14) of said round.
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| 147 | IMPROVEMENTS IN AND RELATING TO DEVICES FOR FILING A PROJECTILE | EP06794931.3 | 2006-10-27 | EP1949018A1 | 2008-07-30 | GILBERT, Robert, Jackson |
| A housing (1; 100, 104, 102) of a cartridge for a device for firing a projectile has separate first and second chambers (10, 12; 106, 114), each of which contains a respective charge (34, 36; 108, 110, 116, 120) of propellant material. Gas produced by the detonation of one of the charges exits the first chamber to propel the projectile, whilst gas from the detonation of the second charge exist rearwardly from the device so as to counteract recoil. A one way valve may also be provided to help to achieve a high pressure difference between the chambers, where the cartridge has a common igniter assembly. | ||||||
| 148 | MEHRTEILIGE MUNITION | EP06753672.2 | 2006-05-17 | EP1888997A1 | 2008-02-20 | LEBACHER, Walter |
| The invention relates to a connecting mechanism for a multiple-part munition (1), for example for artillery charges. It is proposed that a multiple-part munition (1) be connected by means of a simple plug connection to at least two casing elements (2) which can be connected to one another and are arranged axially one behind the other, of a propellent-charge casing (10), with the casing elements (2) having a taper (3) and/or a corresponding opening (4) on their mutually facing end faces or tail faces, and the tapers (3) and/or the inner wall (7) of the openings (4) having projections (8) so that they can be connected to one another with a force fit by pushing them together. | ||||||
| 149 | Waffensystem mit hülsenloser Munition | EP06011440.2 | 2006-06-02 | EP1731867B1 | 2007-11-21 | Könicke, Helmut |
| 150 | PROPELLANT CHARGE MODULE | EP98936776.8 | 1998-08-05 | EP1012527B1 | 2002-10-23 | NILSSON, Neile; LARSSON, Larseric; HAFSTRAND, Anders |
| The present invention relates to a propellant charge module for artillery guns, of the type which is usually referred to by the term "modular charges" (1). A special feature of this type is that, in an otherwise empty pyrophoric relay tube (10) arranged axially in the longitudinal direction of the charge, it has a firing charge which is made up of a plurality of successive powder rings (14), the different ring-shaped parts of this firing charge having distancing members (16) which are directed towards each other and give rise to narrow ignition gaps (18) between them. | ||||||
| 151 | Arrêtoir pour un étui de charge explosive | EP96402312.1 | 1996-10-30 | EP0775887B1 | 2000-03-08 | Barreau, Frédéric; Lacote, Jean-Claude; Hossard, Michel; Deguen, Laurent |
| 152 | Système d'allumage d'une charge propulsive notamment pour munition d'artillerie de campagne et son procédé de fabrication | EP96401512.7 | 1996-07-09 | EP0754927B1 | 1999-12-01 | Brion, Bernard; Julien, Claude |
| 153 | Dispositif permettant de solidariser deux conteneurs et conteneur associé un tel dispositif | EP95401100.3 | 1995-05-11 | EP0684443B1 | 1999-03-24 | Roy, Richard; Paris, Marie-Christine |
| 154 | Dispositif solidarisant deux conteneurs et conteneur associé à un tel dispositif | EP95401372.8 | 1995-06-13 | EP0691520B1 | 1998-07-08 | Eches, Nicolas; Cappy, Yves |
| 155 | Conteneur combustible de charge propulsive pour une munition d'artillerie | EP96401343.7 | 1996-06-20 | EP0757223A1 | 1997-02-05 | Kotas, Bernard; Deguen, Laurent |
Conteneur combustible de charge propulsive pour une munition d'artillerie de campagne, caractérisé en ce que la charge propulsive est une poudre à combustion vive, et en ce que le conteneur :
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| 156 | Conteneur pouvant recevoir une charge propulsive | EP92400169.6 | 1992-01-22 | EP0502753B1 | 1996-05-22 | Brion, Bernard; Eches, Nicolas |
| 157 | Dispositif solidarisant deux conteneurs et conteneur associé à un tel dispositif | EP95401372.8 | 1995-06-13 | EP0691520A1 | 1996-01-10 | Eches, Nicolas; Cappy, Yves |
Le secteur technique de l'invention est celui des dispositifs permettant de rendre solidaires deux conteneurs destinés à contenir un chargement propulsif. Le dispositif selon l'invention permet de solidariser deux conteneurs (1a, 1b) au niveau de leurs faces frontales (2a,2b) et comprend une bague (12) montée de façon coulissante au niveau d'un premier rétreint (8a) aménagé sur un premier conteneur (la) et pouvant coulisser pour venir recouvrir partiellement un deuxième rétreint (8b) aménagé sur un deuxième conteneur (1b), l'extrémité avant de la bague comportant un bec annulaire (18) qui assure un accrochage axial de la bague sur le deuxième conteneur lorsqu'elle vient recouvrir le deuxième rétreint, le bec coopérant avec un redent circulaire (20) porté par un anneau (19) solidaire du deuxième rétreint, le dispositif est caractérisé en ce qu'il comporte des premiers moyens assurant le décrochage de l'extrémité avant de la bague d'avec le deuxième conteneur lorsque les deux conteneurs sont mis en place dans une chambre d'une arme. Application au domaine de l'artillerie de gros calibre ou de char. |
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| 158 | CONTENEUR POUR CHARGE PROPULSIVE POUVANT ETRE RENDU SOLIDAIRE D'UN AUTRE CONTENEUR | EP95902159.0 | 1994-11-22 | EP0681679A1 | 1995-11-15 | CAPPY, Yves; HOSSARD, Michel |
| A propellant charge container securable to a second container via one of its front surfaces, and comprising a ring (12) slidably arranged in a first necked portion whereby it can partially cover a second necked portion on the second container. Said ring (12) has an internal thread (16) provided on a front end (15) and engageable with a thread (18) on the second container. Said container is useful for producing ammunition. | ||||||
| 159 | Conteneur muni de moyens de liaison électrique | EP92400170.4 | 1992-01-22 | EP0499500A1 | 1992-08-19 | Brion, Bernard; Eches, Nicolas; Brule, Michel; Laurensou, René |
Le secteur technique de l'invention est celui des conteneurs pour un chargement propulsif en au moins deux fardeaux. Le conteneur (1a-1b) selon l'invention comprend une enveloppe (9a-9b) délimitant un volume interne, dans lequel peut être mis en place en particulier un chargement propulsif, et il est destiné à être rendu solidaire d'un deuxième conteneur au niveau d'une de ses faces frontales (10a-10b), il est caractérisé en ce qu'il comporte des moyens de conduction de l'électricité, destinés à recevoir et à transmettre un signal provenant d'une arme, ainsi que des moyens de connexion permettant d'assurer, après solidarisation avec le deuxième conteneur, une connexion électrique entre ces moyens de conduction et d'autres moyens de conduction portés par le deuxième conteneur. Application aux munitions de char. |
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| 160 | STECKVERBINDUNG FÜR TREIBLADUNGSMODULE | EP88907265.0 | 1988-07-27 | EP0341270A1 | 1989-11-15 | RAHNENFÜHRER, Eckhard; SCHULZE, Albert; JASKOLKA, Heinz |
| 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 zusammengesteckt werden sollen. Abhilfe schafft hier eine Steckverbindung (1) für wenigstens zwei rotations- und axialsymmetrisch 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. Abstract 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 interconnected as desired in various graduations corresponding to their range. | ||||||
