子分类：
| 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 | 一种可重复装填的训练用非致命弹药 | CN201610933924.6 | 2016-10-27 | CN106440971A | 2017-02-22 | 汪送; 战仁军; 廖丹 |
| 本发明涉及一种非致命弹药，更具体地说涉及一种可重复装填的训练用非致命弹药，该可重复装填的训练用非致命弹药结构简单，弹壳体、药筒体、弹头和弹头底座可以重复使用，从而使得训练成本低廉，利于通过人装结合训练，促进非致命弹药战斗力的有效形成。可拆卸药筒体螺纹连接在弹壳上，底火设置在可拆卸药筒体的底部，发射药装填在可拆卸药筒体内部，药筒体喷火孔设置在可拆卸药筒体上侧面上，高压室设置在弹壳内部，卡环将弹壳与弹头底座之间固定连接，弹头的底端设置在弹头底座的内部，螺纹孔设置在弹头底座上，螺钉旋入螺纹孔的内部。 | ||||||
| 2 | 训练弹头和训练弹 | CN201380029897.4 | 2013-06-04 | CN104380031A | 2015-02-25 | 安德里亚斯·斯托弗 |
| 本发明涉及一种用于在短距离、特别是小于100米的距离使用的训练弹头(1)，其包括沿着中心轴(M)延伸并且包括弹头顶端(3)的前部区域(2)，和包括在中心轴(M)方向上邻接前部区域(2)并且包括弹头末端(5)的尾部区域(4)。尾部区域(4)设计用于使弹头(1)容纳在弹壳(6)中。弹头(1)包括由金属制成的弹头芯(7)，和包围弹头芯(7)、确定弹头(1)外形并且由塑料制成的被甲(8)。 | ||||||
| 3 | 충돌 지점 마킹을 구비하는 발사체 | KR1020137009106 | 2011-09-10 | KR1020140005153A | 2014-01-14 | 오,정혹; 정,분송; 칭,카힌; 고,춘강; 시에,렌지에 |
| 본 발명은 두 개의 발광 염료 성분들(123, 125) 및 염료 파우더(126)를 포함하는 발사체(100,100a, 100b, 100c, 100d)를 설명한다. 제 1 발광 염료 성분(123)은 앰플(122) 내에 포함되고 제 2 발광 염료 성분은 앰플(122) 내부에 배치된 작은 병(124) 내에 포함된다. 전방 분쇄기(120, 120a)는 앰플 및 작은 병 안으로 부서지도록 앰플의 전방에 제공되며, 그에 의해 염료 성분들이 반응하고 발광 글로우가 생기게 한다. 타켓에 충돌 시, 발사체(100, 100a, 100b, 100c, 100d)의 노즈 캡(110)은 깨지고 앰플 뒤에 후방 분쇄기(130)은 앰플(122)을 전방으로 쏟고 노즈 캡(110)의 밖으로 발광 염료를 스퍼터하며; 동시에, 앰플 주위의 염료 파우더(126)는 충돌 지점을 표시하기 위해 밖으로 스퍼터된다. 게다가, 열적 글로우 또한 충돌 지점을 표시하기 위해 제공된다. 발사체들은 또한 빛 추적을 허용한다.
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| 4 | 연습용 축사탄 | KR2020090003887 | 2009-04-03 | KR2020100010026U | 2010-10-13 | 조효식 |
| 본 고안은 연습용 축사탄에 관한 것으로, 낮은 납 함유량의 연막제를 포함하여 환경오염을 낮출수 있으며, 둥근 표면 프로파일의 후방 내측을 가지는 격발몸체를 포함하여 격발몸체의 내구성을 증가시킬 수 있다. 또한 분사부가 오목한 표면의 후방부를 가져 안전성을 증가시킬 수 있다. 연습용 축사탄 | ||||||
| 5 | 銃器のための生分解性弾薬 | JP2018501982 | 2015-07-10 | JP2018522196A | 2018-08-09 | ロペス−ポザス ラヌーザ, ルイス エンリケ |
| ガス発生手段を備えるカートリッジケース、ケース基部、および発射体によって形成された、銃器のための生分解性で非致死性の生分解性弾薬であって、前記発射体の組成物が、ISO 14855: 1999の分析方法に従ったUNE-EN-ISO 14855: 2005規格に従う少なくとも30%の生分解性バイオプラスチックと、70%までの1つ以上の不活性で無毒の鉱物充填剤であって、各々が炭酸塩または鉱物塩のグループから選択される、鉱物充填剤とを備えることを特徴とする、弾薬。 | ||||||
| 6 | Practice ammunition | JP2001500184 | 2000-05-11 | JP3817626B2 | 2006-09-06 | ハエセリッヒ，テッド |
| 7 | Practice ammunition | JP2001500184 | 2000-05-11 | JP2003529034A | 2003-09-30 | ハエセリッヒ，テッド |
| (57)【要約】 【課題】 練習弾が標的に当たった時に破裂して衝突場所を光学的にマークするためのマーキング剤を収容したヘッドを有する演習弾。 【解決手段】 マーキング剤が複数の化学薬品成分（7、8、11、12）から成り、各成分が別々の脆い区画（4、5、10、12）内に収容されている。 各区画（4、5、10、12）が破断した時に２つの成分（7、8、11、12）が混合し、互いに化学反応して光学的にマーキングされる。 | ||||||
| 8 | Training ammunition | JP23931386 | 1986-10-09 | JPH0833289B2 | 1996-03-29 | ARIZONO YUKIMICHI; KANEKO TAKESHI; YOSHIKAWA HIDEKAZU |
| 9 | Training ammunition | JP2179688 | 1988-02-23 | JPH0711356Y2 | 1995-03-15 | 孝昇 松浦; 光雄 森; 英孝 河西 |
| 10 | High speed airframe | JP13198893 | 1993-06-02 | JPH06341794A | 1994-12-13 | KEMA TAISEI; KAWAZOE MASANORI; TAKAOKA YASUTO; MIYOSHI HIDEKI |
| PURPOSE: To diffuse the air from a vent hole at the time of flying a high speed airframe at a high speed, and to limit flying speed and distance of the airframe to specific ranges by forming the hole opened at one end at a front surface and at the other at a side at a wing of the airframe. CONSTITUTION: A wing member of a high speed airframe is formed of a columnar body 1A which is long in a longitudinal direction, and a plurality of wings 1B radially symmetrically stood on a rear part of the body. In this case, vent holes 3 are asymmetrically arranged at the body 1A. That is, the holes 3 are formed of a first hole 3a opened at a center of a front surface of a wing member and extended rearward, and a second hole 3b opened at a side of the body 1A inclined toward a rear side at outer side. At the time of flying the airframe at a high speed, the air is fed to be diffused from the hole 3a to the hole 3b. Thus, a radial load is operated at the member, and an aerodynamic resistance is increased by a shock wave W generated at a diffusing forward side of the air. COPYRIGHT: (C)1994,JPO | ||||||
| 11 | Tank shells for training | JP22037386 | 1986-09-18 | JPH0695000B2 | 1994-11-24 | 了 小路; 憲一 山本; 修 明石; 促通 有薗; 武 金子 |
| 12 | Tank shells for training | JP22037086 | 1986-09-18 | JPH0694997B2 | 1994-11-24 | 了 小路; 憲一 山本; 修 明石; 促通 有薗; 武 金子 |
| 13 | JPH0277496U - | JP15675488 | 1988-11-30 | JPH0277496U | 1990-06-14 | |
| 14 | Training projectile | JP26257687 | 1987-10-20 | JPH01107099A | 1989-04-24 | ARAKAWA HARUHIKO |
| PURPOSE: To reduce a carry after reaching a target of a projectile by a method wherein a liquid is sealed into a body, a seal for blocking a liquid draining hole provided at the front section is pulled to open the liquid draining hole by a spring as the velocity of a projectile body is decreased so as to suddenly decrease the velocity thereof. CONSTITUTION: A liquid 22 is sealed in the inside of a body 2 of a projectile, and a liquid draining hole 15 is formed in the front section thereof. The liquid draining hole 15 is blocked by a seal 16, and the seal 16 is pulled by a spring 19 to a specified force. When a projectile body is fired and a sabot 5 breaks up from the projectile body, the pin 15 pulls out from the seal, allowing it to move, but since the tensile force of the spring 19 is weakened by the speed reducing force applied to the projectile body at such a point in time, the seal 16 holds the liquid draining hole 15 being blocked. When the projectile flies near the target position and the velocity is decreased, the tensile force increases further, and the seal 16 is pulled to open the liquid draining hole 15, so that the projectile body becomes light, the velocity is suddenly dropped, and the range is shortened. COPYRIGHT: (C)1989,JPO | ||||||
| 15 | Cannonball for training | JP23253887 | 1987-09-18 | JPS6475897A | 1989-03-22 | TANEDA YUJI |
| PURPOSE: To get a shell which flies with conventional performance for a necessary distance and thereafter lands on the earth with the shortest possible distance, by providing the shell with a hole piercing it from the tip of the body to the side of the body, within the body of the shell, and further, providing it with a cover which melts by the aerodynamic heating by the flying of the shell, at the inlet of the hole at the tip of the body. CONSTITUTION: A shell is equipped with a body 1 and a fin 2, and the external form is made similar to a conventional one. The body 1 is provided with a hole 4 bent at the bend 5 piercing it from the tip to the topside. This shell is provided with a cover 3 made of, for example, synthetic resin or the like, at the inlet of that hole 4. For that cover 3, the thickness, etc., are set in advance so that the cover may melt enough to let the hole through about the time when it gets over the range from the quantity of aerodynamic heating being settled by the flying velocity and the planned range. Accordingly, it follows that the shell flies the specified trajectory until the shell reaches the target and looses it balance after a specified time after a specified time and lands on the earth, by selecting the material of the cover, the thickness, etc. | ||||||
| 16 | Training ammunition | JP23931386 | 1986-10-09 | JPS6396499A | 1988-04-27 | ARIZONO YUKIMICHI; KANEKO TAKESHI; YOSHIKAWA HIDEKAZU |
| 17 | Tank cannonball for training | JP22037486 | 1986-09-18 | JPS6375499A | 1988-04-05 | AKASHI OSAMU; SHOJI SATORU; YAMAMOTO KENICHI; ARIZONO YUKIMICHI; KANEKO TAKESHI |
| 18 | LESS LETHAL PROJECTILE AND METHOD OF MANUFACTURE | US16225020 | 2018-12-19 | US20190204053A1 | 2019-07-04 | John M. Klein |
| A less lethal projectile for use with a shotgun shell is manufactured from a tubular sleeve, having a quantity of pellets contained therein and which is separated from any remaining volume of the sleeve. The remaining volume of the sleeve is folded over the quantity of pellets to provide a double walled projectile which is suitable for use with a shotgun shell to provide a less lethal projectile. | ||||||
| 19 | 40 mm extended range high performance projectile with rocket and guidance navigation control capability and decoupling device | US14870712 | 2015-09-30 | US09746295B1 | 2017-08-29 | Leon Manole; Wilfredo Toledo; Arthur Ricardo Pizza; Ronny Alzamora; Gary Anthony Pacella |
| An extended range, enhanced lethality 40 mm ammunition round. The round features controlled guidance and camera front end, which can be fired as fin stabilized with no appreciable spin, from an M320 grenade launcher. The round has a launching sleeve with an oversized propellant cup, to essentially double or triple conventional range, with sharp accuracy provided by the guidance system. | ||||||
| 20 | Bullet and practice cartridge for use on a shooting range | US14426575 | 2013-09-05 | US09644928B2 | 2017-05-09 | Bernd Krause; Claus Reuther; Martin Liebl |
| Disclosed is a bullet and practice cartridge for use on a shooting range having a cylindrical rear part and an ogive region at the nose end. The ogive region has a rear end and a bullet tip. In order that the bullet behaves like a conventional full metal jacket round nose bullet in a soft target, and moreover has a low energy output in the soft target, that the bullet does not deform or splinter in soft materials, and that the bullet does not puncture protective materials of bullet catchers, the bullet is constructed in one piece, the ogive region is closed all round a cavity and the wall thickness of the ogive region decreases constantly from the rear end to the tip. | ||||||
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