| 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 | 无后坐力枪炮及其闭锁机构和自动方式 | CN201010269034.2 | 2010-08-22 | CN102374825A | 2012-03-14 | 柯兆宾 |
| 该无后坐力枪炮及其闭锁机构和自动方式。由枪管(1)、导气组件(2)、护木(3)、上机匣(4)、光学瞄准镜(5)、枪托(6)、液压式闭锁机构(7)、下机匣(8)、弹匣(9)、握把装置(10)、两脚架(11)等传统枪械零件组成；使枪炮易于士兵学习、操作；便于设计、制造。但本发明枪炮采用了全新的工作原理、自动方式和闭锁机构，均属于世界首创。通过将后坐力一分为二，转变成两个力作用在同一直线，方向相反的两个受力面积上，使其前后受力平衡，实现无后坐力。解决了几百年来枪炮的后坐力难题，使枪炮进入真真正正的无后坐力时代。使枪炮实现：高精度射击、高-低射速、高初速、大威力、远射程、低故障、等众多优点。 | ||||||
| 2 | 无后坐力枪炮液压闭锁机自动原理 | CN200910207796.7 | 2009-11-05 | CN102207358A | 2011-10-05 | 柯兆宾 |
| 无后坐力枪炮液压闭锁机自动原理，该无后坐力枪炮液压闭锁机含有蓄能器(1)、高压软管(2)、阀座体(3)、截止阀(4)、流量控控制阀(5)、压力控制阀(6)、高压软管(7)、液压缸(8)、机头(14)。解决了枪械射击时后坐力大、射击精度差、连发散布大、故障率高、可靠性差、维修困难。使枪械具有：高射击精度、高射速、高初速、大威力、远射程、无后坐力、低故障、等众多优点。用于提高枪械性能、提高射击精度。增强国防实力、减轻射击培训费用、减轻狙击手的培训费用、具有显著的效果。 | ||||||
| 3 | 便携式多用途武器 | CN200880007281.6 | 2008-01-09 | CN101652624A | 2010-02-17 | P·费希尔 |
| 本发明提出一种便携、无后坐力或低后坐力的武器系统(11)，该武器系统对静止和运动的目标都是有效的，并且在日间和夜间都可以发射优选可编程的高性能的弹药。所述武器系统(11)自身具有火控系统。 | ||||||
| 4 | 가스 발생기를 이용한 미사일 발사 시스템 | KR1019900011679 | 1990-07-31 | KR1019940004642B1 | 1994-05-27 | 드중브이.판; 케빈에스.마인즈 |
| 내용 없음. | ||||||
| 5 | 잠수함 및 이 잠수함에 사용하기 위한 접개들이 장치 | KR1020040050487 | 2004-06-30 | KR1020050004048A | 2005-01-12 | 샤르프볼프강; 로이터요아킴; 쾰베르롤프 |
| PURPOSE: A submarine is provided to expand a machine gun according to the arrangement and design of adjacent retractable instruments while inserting and expanding completely the retractable instruments. CONSTITUTION: In a submarine having at least one retractable instrument(3), a pressure-resistance submarine container(4) in which a recoilless rifle(5) is disposed is installed at the end of the retractable instrument. The retractable instruments for supporting the container are mounted in a tower area(2). The rifle extends from the container to orbit and is a machine gun. The rifle is integrated in a weapon control system of the submarine. The retractable instrument for the container has at least one guide profile(6) and a lifting cylinder(9). Devices for expanding and inserting weapons, adjusting the position, and controlling operations are mounted and operated in an airtight chamber(1). | ||||||
| 6 | Projectile launching device | JP5460889 | 1989-03-07 | JP2718745B2 | 1998-02-25 | 直人 中川 |
| 7 | Method and apparatus for burning gunpowder | JP12355793 | 1993-04-26 | JPH06307796A | 1994-11-01 | ENDO YOSHITERU; SHIMOZAKI ISAO |
| PURPOSE: To eliminate a flame from a tail of a gun barrel at the time of shooting a bullet and to reduce danger of discovering by an opponent by mixing gas of high temperature generated by igniting gunpowder in the barrel with unburned gunpowder forcibly by a turbine. CONSTITUTION: When a bullet 20 is charged in a gun barrel 10, gunpowder 22 is supplied to a charging chamber 10a, and then ignited by an igniter, the gunpowder 22 is burned to generate high temperature gas 24. In this case, since an irregularity in burning due to natural burning, partial gunpowder 22 is fed together with gas 24 without burning from the chamber 10a to a turbine chamber 10b. First-third turbines 14, 16, 18 are forcibly rotated by a force based on the flow of the gas 24. Thus, the unburned gunpowder 22 and the gas 24 are forcibly mixed, and completely burned. Accordingly, only the gas 24 is injected externally from a vent hole 10dl of a wall 10d to eliminate flame from rear of the barrel 10. COPYRIGHT: (C)1994,JPO | ||||||
| 8 | Gas generator missile launch system | JP20495890 | 1990-08-01 | JPH0672755B2 | 1994-09-14 | ZUNGU BUI FUAN; KEBIN ESU MAINZU |
| 9 | JPS63142597U - | JP3456187 | 1987-03-10 | JPS63142597U | 1988-09-20 | |
| 10 | JPS60139197U - | JP19517684 | 1984-12-21 | JPS60139197U | 1985-09-14 | |
| 11 | Rear injection induction device for recoilless firearm | JP12073781 | 1981-08-03 | JPS5822900A | 1983-02-10 | IKOMA KIYUUZABUROU |
| 12 | Shooter connector for nonnreaction arm | JP1840376 | 1976-02-20 | JPS51132700A | 1976-11-17 | ANDORESU HAAKAN ANDERUSON; KURAESU GUSUTAFU ERIKU YUNGUFU; RUNE FUERUNERU AKUHAAGEN |
| 13 | Portable multi-purpose weapon | JP2009547563 | 2008-01-09 | JP2010518345A | 2010-05-27 | フィッシェル，ピエール |
| 本発明は、携帯可能な、反動のない、又は反動の少ない兵器システム（１）を提供するものであり、兵器システム（１）は、静的及び動的の標的に対して有効であって、昼と夜とにおいて高性能な発射体を発射することができ、発射体はプログラム可能であることが好ましい。 兵器システム（１）は、専用の発射制御装置を備えている。
【選択図】図１ |
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| 14 | Cannon barrel with low reaction | JP24006092 | 1992-08-18 | JPH0666496A | 1994-03-08 | ENDO YOSHITERU; SHIMOZAKI ISAO |
| PURPOSE:To cause a position of a cannon barrel to be hardly discovered by a method wherein when a bullet is launched, a discharging of launching gas is delayed. CONSTITUTION:When a launching bullet 3a completes its combustion, a main body 1a of a cannon near a rear end of a bullet 2 is formed with a launching gas discharging part 1b. The launching gas discharging part 1b is covered by an outer cylinder having a front end fixed to an outer surface of the main body 1a of the cannon so as to define a launching gas glowing passage 4a communicating from a launching gas discharging part 1b reawardly and having its rear end opened. Due to this fact, combustion of not-yet ignited launching gas outside the bullet is restricted when the bullet 2 is launched. Along with this operation, explosion wind is reduced and its safety characteristic is improved, resulting in that a degree of freedom of arranging of army groups can be increased and a position of the cannon can be hardly discovered by enemy. | ||||||
| 15 | Flying object launcher | JP5460889 | 1989-03-07 | JPH02233998A | 1990-09-17 | NAKAGAWA NAOTO |
| PURPOSE: To obtain a stable repulsion force and its offset force by providing a friction adjusting device which adjusts the friction forces between an outer launcher tube and a front inner-launcher tube of an inner launcher tube, and between the outer launcher tube and a rear inner launcher tube, and top and bottom covers which are respectively attached on the top and bottom of the outer launcher tube. CONSTITUTION: When a launching instruction is given to a flying object 25, and a rocket motor is ignited, a bottom cover 27 is blown off by a blast discharged from the rocket motor. Simultaneously, a rear inner-launcher tube 212 is pushed forward by the blast force, and breaks a top cover 26. When the flying object 25 gets out of an outer launcher tube 22, a front inner-launcher tube 211 is split into pieces and dispersed away from the flying object as it receives a circumferential direction wind pressure of the flying object 25. At this time, the change in the repulsion force exerted on a shooter is a plus direction repulsion force as shown on Fig. a, for example, during a period from t 1 at which the blast of the rocket motor is started till t 2 at which the top cover 26 is broken, and at the same time, a minus direction repulsion force is generated as shown on Fig. b during a period from t 1 at which the blast is started till t 2 at which the bottom cover 27 is broken, cancelling said plus direction reaction force. COPYRIGHT: (C)1990,JPO&Japio | ||||||
| 16 | Missile shooting device without reaction | JP5699577 | 1977-05-16 | JPS52141100A | 1977-11-25 | KURAESU ROJIYAA ANDAASON |
| 17 | Projectile shooting assembly | JP7797376 | 1976-07-02 | JPS527200A | 1977-01-20 | EMIIRU SUTOUFU |
| 18 | Jushinnofure shogekiboshiho | JP7777874 | 1974-07-09 | JPS516400A | 1976-01-19 | ABE TOSHIHIRO |
| 19 | JPS501320B1 - | JP12201970 | 1970-12-29 | JPS501320B1 | 1975-01-17 | |
| 20 | Tank Muzori recoil energy turret | JP958097 | 1997-10-15 | JP3048049U | 1998-05-06 | 自遜 賈; 徳菱 趙 |
| (57)【要約】 【課題】 戦車用無反跳エネルギー砲塔の提供。 【解決手段】 砲塔１内部にあって、滑車装置３がスライドレール３上を懸吊アーム１１及び砲管２と一体にスライド可能とされ且つ位置決めブロック１７により位置決め可能とされ、砲管２前端が前板１２より突出し、前板１２に高さ調整器１４が設けられ、砲塔１の背面に排気孔が砲管２の後端に対向する位置に設けられ、発射時に発生する気体を排気孔より排出して反跳エネルギーを発生しないようにしてある。 | ||||||
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