| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 41 | Rückstossfreie Flugkörper-Anlage | EP82810021.4 | 1982-01-19 | EP0056789B1 | 1984-08-29 | |
| 42 | Recoilless weapon | EP82810021 | 1982-01-19 | EP0056789A3 | 1982-09-08 | |
| 43 | VHS RIFLE | PCT/HR2006000010 | 2006-05-08 | WO2006120487A2 | 2006-11-16 | VUKOVIC MARKO |
| The VHS rifle shown on Figure 1 , among other, has a handgrip 30 that is placed in the rifle's centre of gravity, so it can be held in a single hand. The rifle has so called 'soft' opening and closing of the breech 12 that results in light recoil when a shot is being fired. At the front end of the handgrip 83 are the facilities for mounting of the bayonet 97, and in front of the front handgrip 83 is a swallowtail grove for attaching a lamp or an IR lamp 87. In the middle of the cover 19 is a handgrip for carrying the rifle. The rifle has integrated mount for attaching the grenade launcher 88, and mechanism for its firing, Figures 4. The bottom part of the handgrip 30 contains the feet 78 that can be folded into the groove on the handgrip 30. In the middle of the cover 19 is a mounting for attaching all sight types, Figure 1. This rifle, in spite of all accessories and contents, does not weigh more than 2 kilograms, without ammunition, bayonet, lamp and the grenade launcher barrel. | ||||||
| 44 | TRAINING WEAPON SYSTEM FOR RECOILLESS ANTITANK RIFLE WEAPONS | EP10851481 | 2010-05-11 | EP2569587A4 | 2017-06-21 | LIJEHOLM JOHNNY |
| The invention relates to a training weapon system (1) intended for a recoilless antitank rifle (2), the training weapon system (1) comprising a sub-caliber barrel (3) for firing sub-caliber practice projectiles (4) provided with base plates (5), the sub-caliber barrel (3) being arranged in a shell-like body (6) in the barrel (7) of the recoilless antitank rifle (2), the front part of the sub-caliber barrel (3) being fitted in a guide part (8) for centering the barrel (3), and a rear part of the barrel (3) being fitted in a breech (9), comprising a firing channel (10) and a nozzle screw thread (11) for fitting a nozzle screw (12), which is arranged in the rear part of the shell-like body (6). The invention is characterized in that the training weapon system (1) comprises at least one locking part (13, 14), the function of which is to prevent the nozzle screw (12) or the base plate (5) of the projectile (4) or part of the base plate (5) being expelled backwards through the nozzle funnel (21) of the antitank rifle (2) as loose flying projectiles. | ||||||
| 45 | RECOIL ATTENUATED PAYLOAD LAUNCHER SYSTEM | EP12823117.2 | 2012-08-03 | EP2739930B1 | 2016-10-12 | MENEFEE, James, Y., III |
| 46 | AKTIVE BREMSUNG EINES AUSSTOSSTRIEBWERKS | EP15190042.0 | 2015-10-15 | EP3015811A1 | 2016-05-04 | Hacker, Andreas; Bartinger, Franz |
Vorrichtung zur Beschleunigung und zum Ausstoss eines Haupttriebwerks (1) aus der Vorrichtung (2), in die ein Haupttriebwerk (1) aufnehmbar ist und die ein Ausstosstriebwerk (3) umfasst. Das Ausstosstriebwerk (3) ist zur Beschleunigung und zum Ausstoss des Haupttriebwerks (1) geeignet und umfasst Mittel (4) zu seiner Abbremsung nach der Initiierung der Beschleunigung des Haupttriebwerks (1), so dass das Ausstosstriebwerk (3) in der Vorrichtung (2) verbleibt.
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| 47 | WAFFE MIT RÜCKLAUF UND EINER DIESEN DÄMPFENDEN BREMSEINRICHTUNG | EP09737351.8 | 2009-10-13 | EP2344831B1 | 2015-08-12 | KOHNEN, Norbert |
| 48 | HÜLSENLOSE MUNITION | EP10722955.1 | 2010-06-01 | EP2440881B1 | 2014-07-02 | SCHNEIDER, Hubert |
| 49 | TRAINING WEAPON SYSTEM FOR RECOILLESS ANTITANK RIFLE WEAPONS | EP10851481.1 | 2010-05-11 | EP2569587A1 | 2013-03-20 | LIJEHOLM, Johnny |
| The invention relates to a training weapon system (1) intended for a recoilless antitank rifle (2), the training weapon system (1) comprising a sub-caliber barrel (3) for firing sub-caliber practice projectiles (4) provided with base plates (5), the sub-caliber barrel (3) being arranged in a shell-like body (6) in the barrel (7) of the recoilless antitank rifle (2), the front part of the sub-caliber barrel (3) being fitted in a guide part (8) for centering the barrel (3), and a rear part of the barrel (3) being fitted in a breech (9), comprising a firing channel (10) and a nozzle screw thread (11) for fitting a nozzle screw (12), which is arranged in the rear part of the shell-like body (6). The invention is characterized in that the training weapon system (1) comprises at least one locking part (13, 14), the function of which is to prevent the nozzle screw (12) or the base plate (5) of the projectile (4) or part of the base plate (5) being expelled backwards through the nozzle funnel (21) of the antitank rifle (2) as loose flying projectiles. | ||||||
| 50 | HÜLSENLOSE MUNITION | EP10722955.1 | 2010-06-01 | EP2440881A1 | 2012-04-18 | SCHNEIDER, Hubert |
| The invention relates to a caseless munition (1, 10) having a bullet (2) enclosed by a combustible casing (3, 13), wherein the bullet (2) comprises a hollow space (4, 14) at the tail thereof for receiving an additional charge (6, 16). The hollow space (4, 14) itself opens into a nozzle-like expansion (5, 15). The bullet (2) thus bites into the weapon barrel (25) in a timely manner before the combustible casing (3, 13) releases the bullet (2). | ||||||
| 51 | Recoil dampening mechanism | EP08445021.2 | 2008-05-27 | EP2128552B1 | 2011-09-07 | Strömberg, Håkan |
| 52 | Recoil dampening mechanism | EP08445021.2 | 2008-05-27 | EP2128552A1 | 2009-12-02 | Strömberg, Håkan |
The invention concerns a recoilless weapon (1) comprising a launch tube (3) for launching a projectile and a recoil dampener (2) for dampening recoil forces from the projectile, characterised in that the recoil dampener (2) comprises at least two recoil dampening mechanisms (8) comprising dampening means (11, 13, 14, 15) and that the recoil dampener (2) is adjustable in regard to a gunner and/or to projectile.
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| 53 | Munitionsprüfgerät | EP07004907.7 | 2007-03-09 | EP1843121B1 | 2008-08-27 | Schneider, Hubert |
| 54 | Unterseeboot | EP04014657.3 | 2004-06-23 | EP1493657B1 | 2007-01-10 | Scharf, Wolfgang; Reuter, Joachim; Körver, Rolf |
| 55 | BOTTOM PLATE MEMBER | EP96910281.3 | 1996-04-10 | EP0870165B1 | 2002-07-24 | JOHANSSON, Ingemar; LAGER, Tomas; LINDERHOLT, Leif; SUNDELL, Christer |
| The invention relates to a bottom plate member (6) which is designed and made for initially tightening a chamber in which a high gas pressure is generated, for example the propellant charge chamber (4) in an ammuniton round for a recoilless weapon system or in pipes or containers within the process industry. The plate member (6) is breakable and opens for the gases to exit when the gas pressure within the chamber exceeds a certain level. The plate member has a through hole (12) in the center which gives an effective starting point for the cracking process as well as fractural impressions (10) to control the cracking process so that the plate is divided into a number of well defined parts of flaps (11) which are connected to each other. The plate member (6) further comprises a number of straight edges (16), which number corresponds to the number of flaps (11), against which edges the base of the flaps are arranged to be folded when the plate member opens due to the gas pressure. | ||||||
| 56 | PRACTICE WEAPON FOR A CARRIED RECOILLESS ANTI-TANK WEAPON | EP95906573.0 | 1994-12-27 | EP0739473A1 | 1996-10-30 | ASBRINK, Mats |
| The present invention relates to a practice weapon for a hand-held recoilless anti-armour weapon. Hitherto practice weapons with sub-calibre barrels (2) mounted in full calibre barrels (1) have been used. To enable the marksman to repeatedly train to be subejected to the powerful noise and pressure effects of a full calibe weapon, the practice weapon according to the invention includes a marker charge (3), which is arranged to be ignited at the firing of a sub-calibre round. In order to transfer the ignition sequence in a simple fashion with few moving parts, the marker charge (3) is arranged to be ignited by the jet of flame of the charge of the practice projectile. | ||||||
| 57 | Recoilless missile launch system | EP90307413.6 | 1990-07-06 | EP0414359A2 | 1991-02-27 | Phan, Dzung V.; Minds, Kevin S. |
A missile launching system with an open-ended cylindrical container (10) having a bore in which a slidable piston (20) is located between the missile (12) and a gas generator (14) adjacent the container aft end (16). The piston (20) area is substantially the same as the container bore at the aft end (16). An internal ring (42) forms a reduced area throat for gas exiting via the aft end of the container (10) with the ratio of the piston area to the throat area, Ap/At, being functionally related to the propellant physical characteristics. |
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| 58 | Geschosswaffe, insbesondere panzerbrechende Waffe | EP84890153.4 | 1984-08-13 | EP0145696A1 | 1985-06-19 | Schabelreiter, Johann, Dr. |
Die Erfindung betrifft eine, insbesondere rückstossgebremste, Geschosswaffe, wobei eine Treibladung (5') in einem bei Zündung im wesentlichen axial voneinander weg verschiebbare Wandelemente aufweisenden Raum (4) im Waffenrohr (1) angeordnet ist, aus dem vermittels mündungsseitigem Wandelement (310) ein Geschoss (2) austreibbar ist, wobei im Waffenrohr (1) mindestens zwei teleskopartig ineinander verschiebbare Hohlzylinder bzw. -prismen (30, 31) angeordnet sind, und sich eine mit Zündeinrichtung (7,70), zündbare Treibladung (5') in einem Raum (4) befindet, der begrenzt ist von einem im äussersten Hohlzylinder bzw. -prisma (30) bis höchstens zu dessen rückseitigem Ende verschiebbaren, dessen Hohlraumquerschnitt deckenden oder ihn bzw. es an seinem rückseitigen Ende schliessenden Wandelement (300) und einem im innersten Hohlzylinder bzw. -prisma (31) bei Zündung bis höchstens zu dessen mündungsseitigem Ende verschiebbaren, dessen Hohlraumquerschnitt deckenden oder ihn bzw. es an seinem mündungsseitigen Ende schliessenden Wandelement (310) und Stirn- und gegebenenfalls Anschlagflächen (305, 315, 316,310') innerer Hohlzylinder bzw. -prismen (31), und gegebenenfalls deren Wandelement (310) sowie gegebenenfalls Mantelteilen zumindest des äusseren Hohlzylinders bzw. -prismas (30). |
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| 59 | Rückstossfreie Flugkörper-Anlage | EP82810021.4 | 1982-01-19 | EP0056789A2 | 1982-07-28 | |
Die Anlage enthält ein Rohr (1), das zwei Kammern (2,3) zur Aufnahme von Treibladungen (4, 5) aufweist und das als Brennkammer dient. Das beispielsweise zweistufige Geschoss (7) weist ein Leitwerk (12) mit drei Flügeln (13) auf, die von den austretenden Gasen umströmt werden, die das Geschoss in Drehung versetzen, wodruch eine Zielabweichung infolge dessen Unwucht beseitigt wird, die durch den Abbrand der Treibladungen und durch den Bau hervorgerufen wird. Der Schub der zweiten Stufe (10) ist derart bemessen, dass er ungefähr dem Luftwiderstand des fliegenden Geschosses entspricht, wodurch der Einfluss des Seitenwindes auf das Geschoss ausgeschaltet wird. Die Verwendung von stationären Treibladungen einerseits und einer Treibladung zur Ausschaltung des Einflusses des Seitenwindes am Raketengeschoss andererseits ergibt ohne grossen Aufwand ein Geschoss mit hoher Anfangsgeschwindigkeit und grosser Zielgenauigkeit, wobei solche Raketen für die Panzer- und Flugabwehr verwendet werden können. |
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| 60 | Grenade and grenade launching apparatus | US12976434 | 2010-12-22 | US09488422B2 | 2016-11-08 | Helmut Hammer; Axel Pfersmann |
| The present invention relates to a grenade that can be fired from a barrel, for recoilless firing. The barrel is open at both ends and is without any flow cross-section constrictions. The grenade is formed of a grenade base body which surrounds at least one explosive charge, and a flow cross-section reduction device for reducing the flow cross-section of the barrel. The device is arranged in the opposite direction to the firing direction X with respect to the grenade base body. The flow cross-section reduction device is connected to the grenade base body, separated from it, via a connecting device, and is connected to it such that it is stable during firing. A grenade launcher or shell firing apparatus has a grenade such as this, and the grenade firing apparatus has a barrel which is open at both ends and does not have any flow cross-section constrictions. | ||||||
