| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 射弹的低特征发射系统和方法 | CN03121372.3 | 2003-03-26 | CN1447091A | 2003-10-08 | 泽夫·里特曼 |
| 本发明公开了一种射弹的低特征发射系统和方法。前板和后板与一具有轴的扩展容器联结。当扩展容器的容积增加时，活塞延轴朝相反方向移动。射弹按照可保证其通过前板的移动按既定方向发射出去的方式放置。板延轴向的移动是有限制的。两个板通过一可伸长联结结构而相互连接。 | ||||||
| 2 | 一种无污染液体平衡装置 | CN201180044171.9 | 2011-06-29 | CN103649670B | 2014-12-24 | 王生捷; 陈亚军; 邱旭阳; 陈爱锋; 唐玉龙; 韩书永 |
| 本发明公开了一种无污染液体平衡装置，包括：密封袋(1)、前盖(2)、后盖(3)和液体平衡物(4)，其中密封袋(1)、前盖(2)和后盖(3)都为塑料材料。密封袋(1)内部灌装液体平衡物(4)，两端高温塑封。前盖(2)和后盖(3)的直径与发射筒(5)内径匹配，密封袋(1)置于前盖(2)和后盖(3)之间。平时运输状态时，液体平衡物(4)在密封袋(1)中密封良好，发射时在火药推力作用下导弹向前运动，密封袋(1)、前盖(2)和后盖(3)瞬间碎裂，液体平衡物(4)高速向后喷出筒外，前后冲量相近或相等，从而减小或消除发射时对发射筒(5)的冲量。本装置结构简单，采用无污染液体平衡物(4)，发射后不污染环境。 | ||||||
| 3 | 一种无后坐力抛射装置 | CN201110001708.5 | 2011-01-06 | CN102141357B | 2013-03-06 | 王生捷; 邱旭阳; 陈爱锋; 唐玉龙; 迟克刚 |
| 本发明公开了一种无后坐力抛射装置，包括：前筒体(1)、前法兰(2)、中筒体(3)、后筒体(4)、后法兰(5)、平衡体(7)、制动环(8)、前活塞体(9)、支撑座(10)、后活塞(11)、点火管(12)和支耳(13)，还包括：插拔机构(14)。插拔机构(14)包括：壳体、可调节拉杆和电气插头。可调节拉杆一端与壳体销轴连接，另一端与电气插头销轴连接，壳体与前筒体(1)螺钉连接，电气插头沿弹(6)的发射方向斜插于弹(6)上。整个抛射过程燃气都封闭在前活塞体（9）、后活塞（11）与中筒体(3)之间的空腔中，做到抛射过程微声、微烟、微光，并消除了后坐力。 | ||||||
| 4 | 一种无后坐力抛射装置 | CN201110001708.5 | 2011-01-06 | CN102141357A | 2011-08-03 | 王生捷; 邱旭阳; 陈爱锋; 唐玉龙; 迟克刚 |
| 本发明公开了一种无后坐力抛射装置，包括：前筒体(1)、前法兰(2)、中筒体(3)、后筒体(4)、后法兰(5)、平衡体(7)、制动环(8)、前活塞体(9)、支撑座(10)、后活塞(11)、点火管(12)和支耳(13)，还包括：插拔机构(14)。插拔机构(14)包括：壳体、可调节拉杆和电气插头。可调节拉杆一端与壳体销轴连接，另一端与电气插头销轴连接，壳体与前筒体(1)螺钉连接，电气插头沿弹(6)的发射方向斜插于弹(6)上。整个抛射过程燃气都封闭在两个活塞与中筒体(3)之间的空腔中，做到抛射过程微声、微烟、微光，并消除了后坐力。 | ||||||
| 5 | 进入地下地层的方法和装置 | CN200480015324.7 | 2004-04-29 | CN1798902A | 2006-07-05 | 阿兰·L·纳克鲁德 |
| 为了激励多产地层，用于将至少一个炸药驱动的射弹(11，58)驱动到地下地层的开孔(H)或井孔(B)中的方法和设备(9，53)。为了以所希望的角度点火，该设备能够在该开孔或井孔中枢转，并且能够深深进入到地下地层中。该设备在水平钻井应用中也能够用管子(51)传输。 | ||||||
| 6 | Methods and counter mass firearm thereby manufactured to expand the usefulness of the counter mass firearms | JP2003564508 | 2003-01-15 | JP2005516178A | 2005-06-02 | ラルス アックス，; ラルス−アケ カルルクヴィスト，; アルネ フランゼン，; エジェ ランツ， |
| 本発明はカウンターマス火器の発射に関連して前記カウンターマス材料（１１）の前記カウンターマス包装体（１０）を開封することを可能とする方法と装置に関する。 本発明の基本概念は、カウンターマス火器（１）の銃身の後部出口端（１２）近くに銃身中に内向きに十分突出する多数の刃（１５）を出口の内部に形造り、これらの刃が前記火器（１）の発射時に前記刃（１５）を過ぎて押圧される前記カウンターマス容器（１０）中に切り込むことである。 | ||||||
| 7 | Method and device for launching free-flying projectile | JP2004303622 | 2004-10-19 | JP2005127704A | 2005-05-19 | REGEBRO CHRISTER |
| PROBLEM TO BE SOLVED: To solve a problem in using a transportable supporting weapon such as an antitank rifle or an antitank missile in a building wherein damage is inflicted upon a weapon operator, accompanied by toxic gas in addition to hydrochloric acid, lead powder, and heavy metal, and it is very dangerous. SOLUTION: The present invention relates to a method and a device by means of which it has been made possible, without gas discharge to the surrounding environment, to accelerate the speed of a powder-gas-driven projectile 4 from zero to a speed which gives the projectile free-flying characteristics. This has been made possible by utilizing at least some of the expansion force from the propellent powder charge 11, which discharges gas when it is initiated, for, by means of a displaceable piston 7, driving a countermass 8 out of the rear part 13 of the projectile in the direction opposite to the desired flying direction of the projectile 4. COPYRIGHT: (C)2005,JPO&NCIPI | ||||||
| 8 | Hama塞 device for low-recoil type firearms | JP375292 | 1992-01-13 | JP3142621B2 | 2001-03-07 | フォン ブラーヘル ヘルムート |
| 9 | Counter trout firearms | JP2003564509 | 2003-01-15 | JP4371820B2 | 2009-11-25 | ラルス アックス，; ラルス−アケ カルルクヴィスト，; アルネ フランゼン，; エジェ ランツ， |
| 10 | Counter trout firearms | JP2003564509 | 2003-01-15 | JP2005516179A | 2005-06-02 | ラルス アックス，; ラルス−アケ カルルクヴィスト，; アルネ フランゼン，; エジェ ランツ， |
| 本発明はカウンターマス火器を製造する一般的方法に関し、低圧室に対して作用するカウンターマス（１２，２６，２６′，３８）を持つ高圧システムと低圧システムの使用に基づいている。 高圧システム（７，２３，２３′，３６）は実際には火器発射薬装薬（８，２２，２２′,３５）のための燃焼室により形成され、一方低圧システム（２５，２５′）の主要部は始めの段階ではカウンターマスのための貯蔵及び加速室により形成されている。 本発明の利点は前記発明が射手周りに、火器（１，１３）の射程を減少することなく、かかる端部に対してより低い圧力水準を達成する可能性を提供することである。 | ||||||
| 11 | Casing for containing propellant and installation in barrel of recoilless weapon | JP26360093 | 1993-10-21 | JPH06201296A | 1994-07-19 | MARUKU RUSHIYU; BURUUNO RAN |
| PURPOSE: To simplify a structure and ensure airtightness without adding an additional seal, in a casing which contains propellant and which is to be installed in the barrel of a recoilless weapon. CONSTITUTION: A casing 3 contains propellant and is established in a barrel 2 of a recoilless weapon 1. The casing 3 is provided with a cylindrical enclosure 7 which is slidably fit into the barrel 2, and the enclosure 7 is defined by two sidewalls 8, 9. The enclosure 7 is integrally formed and has at least one annular break start portion 10. After the break start portion 10 breaks due to the action of the pressure of gases generated by the propellant, the casing 3 is divided into at least two elements that are move freely translationally relative to each other, while each of the elements carries enclosure parts 7a, 7b which ensure airtightness. COPYRIGHT: (C)1994,JPO | ||||||
| 12 | Filling apparatus for low reaction type gun | JP375292 | 1992-01-13 | JPH04313696A | 1992-11-05 | HERUMUUTO FUON BURAAHERU |
| PURPOSE: To ensure a filling apparatus capable of maintaining high dimensional accuracy and shape accuracy, and securely being decomposed into many small pieces upon leaving a launcher. CONSTITUTION: There are provided a sleeve (11) in which a cylindrical filling agent (13) is contained, and a gas guide passage (21) that extends in the longitudinal direction of the sleeve (11) and generates the filling agent (13). In a filling apparatus for propulsion and powder loading of a low reaction type gun, the sleeve (11) includes a plurality of longitudinal grooves (23) extending longitudinally and including a flat or bent groove base (31) that is disposed and distributed over the entire periphery of the sleeveperipheral wall surface (25) of the sleeve (11). COPYRIGHT: (C)1992,JPO | ||||||
| 13 | 無公害液体バランス装置 | JP2014515030 | 2011-06-29 | JP5860956B2 | 2016-02-16 | 王 生▲ジエ▼; ▲陳▼ ▲亜▼▲軍▼; ▲チュウ▼ 旭▲陽▼; ▲陳▼ ▲愛▼▲鋒▼; 唐 玉▲龍▼; ▲韓▼ ▲書▼永 |
| 14 | Pollution-free liquid balance device | JP2014515030 | 2011-06-29 | JP2014519593A | 2014-08-14 | 生▲ジエ▼ 王; ▲亜▼▲軍▼ ▲陳▼; 旭▲陽▼ ▲チュウ▼; ▲愛▼▲鋒▼ ▲陳▼; 玉▲龍▼ 唐; ▲書▼永 ▲韓▼ |
| 【解決手段】無公害液体バランス装置であって、プラスチック製の密封袋（１）と、プラスチック製の前面カバー（２）と、プラスチック製の背面カバー（３）と、液体バランス材料（４）と、を含む。 液体バランス材料（４）を、両端がプラスチックで高温密封される密封袋（１）の内部に入れる。 前面カバー（２）および背面カバー（３）の直径は発射管（５）の内径と合わせて、密封袋（１）を前面カバー（２）と背面カバー（３）の間に配置する。 常時の輸送される状況で、液体バランス材料（４）が密封袋（１）の中に良好に密封されて、発射する際に火薬の推力の作用でミサイルが前進すると、密封袋（１）、前面カバー（２）および背面カバー（３）を瞬時に断片化して、液体バランス材料（４）は高速で後方に向けて発射管外に排出される。 前部と後部のインパルスは類似または等しいことで、発射する際の発射管（５）に対するインパルスを低減または解消する。 この装置は、簡単な構造を有し、無公害液体バランス材料（４）を採用することにより、発射後に、環境を汚染しないことになる。 | ||||||
| 15 | JPH05504614A - | JP50392791 | 1991-01-29 | JPH05504614A | 1993-07-15 | |
| 16 | JPH05504613A - | JP50392691 | 1991-01-29 | JPH05504613A | 1993-07-15 | |
| 17 | 발사체의 저식별 신호 발사를 위한 시스템 및 방법 | KR1020030018371 | 2003-03-25 | KR1020030077415A | 2003-10-01 | 리트만지브 |
| 발사체의 발사를 위한 방법 및 장치가 개시된다. 전방 및 후방 플레이트는 축을 갖는 확장 용기에 결합되어, 확장 용기의 용적이 증가하면, 피스톤이 축을 따라 대향방향으로 이동한다. 발사체는 전방 플레이트의 동작에 의해 소망의 방향으로 발사되도록 배치된다. 2개의 플레이트는 신축가능한 결합 구조체에 의해 서로 연결되어 있어서, 플레이트들의 축을 따른 동작이 제한된다. | ||||||
| 18 | 저반동 무기용 충전부재 | KR1019920000520 | 1992-01-16 | KR100210112B1 | 1999-07-15 | 헬무트폰브라헬 |
| 저 반동총의 추진 장약을 위한 탬핑은 원통형 탬핑 매스(13)를 포함하는 케이싱(11)을 갖고, 이 케이싱은 축상으로 연장되는 몇 개의 약해지는 부분홈이 있으며 또 케이싱(11)의 주변에 배열되어 있다. 약해지는 부분들은 평평하거나 곡선을 이루는 홈기부를 갖는 종방향 홈으로써 이루어져 있다. 홈기부에서, 개방부는 종방향으로 케이싱 벽위에 마련되어 있다. 발사튜브를 떠났을 때, 탬핑의 케이싱(11)은 종방향 홈에 따라 파열되며 좁은 스트립으로 나뉘어진다. 천공된 종방향 홈들은 그 홈들의 부분에서 재료의 약화 때문에 오랜 저장이나 부적합한 운반 도중에 변형될지도 모른다는 위험이 없이 케이싱의 신뢰할 수 있는 파열을 보장해 준다. | ||||||
| 19 | Cooling device for cooling combustion gases from recoilless anti-tank weapons | US13811036 | 2010-07-22 | US09291410B2 | 2016-03-22 | Lars Nilsson |
| The present invention relates to a cooling device (2) for cooling combustion gases from a rocket motor (1) in an antitank weapon. The cooling device (2) comprises a coolant reservoir (3, 21) containing a coolant (4). The coolant reservoir (3, 21) is arranged such that the coolant (4) is transferred from the coolant reservoir (3, 21) to the combustion gases in the gas outlets (6) of the rocket motor (1) in response to a pressure increase in the rocket motor (1). The coolant reservoir (3, 21) constitutes an integral part of the rocket motor (1) and is connected to the combustion chamber (7) by at least two gas inlets (8) for pressurization of the coolant (4). The coolant reservoir is furthermore connected to the rocket motor nozzle (9) by at least two coolant outlets (10) for transfer of coolant (4) from the coolant reservoir (3, 21) to the rocket motor nozzle (9). | ||||||
| 20 | Pollution-free liquid balancing device | US14011729 | 2013-08-27 | US08707847B2 | 2014-04-29 | Shengjie Wang; Yajun Chen; Xuyang Qiu; Aifeng Chen; Yulong Tang; Shuyong Han |
| A pollution-free liquid balancing device comprises a sealing bag (1), a front cover (2), a rear cover (3) and liquid balancing matter (4), wherein the sealing bag (1), the front cover (2) and the rear cover (3) are all plastic material. The sealing bag (1) is filled with the liquid balancing matter (4) inside, and plastically sealed under high temperature at both ends. The diameters of the front cover (2) and the rear cover (3) are matched with the inner diameter of a launch barrel (5), and the sealing bag (1) is provided between the front cover (2) and the rear cover (3). In an ordinary transportation state, the liquid balancing matter (4) is well sealed in the sealing bag (1), and a missile is launched forward by the propulsion of powder during launch, the sealing bag (1), the front cover (2) and the rear cover (3) crack instantaneously, and the liquid balancing matter (4) is ejected backward outside the barrel at high speed. The forward and backward impulses are similar or equal, thereby reducing or eliminating the impulse to the launch barrel (5) during launch. The device has a simple structure and uses the pollution-free liquid balancing matter (4), thus there is no pollution after launch. | ||||||
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