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1. 发明申请

WO2018176157A3 IMPROVED BULLET, WEAPON PROVIDED WITH SUCH BULLETS, KIT FOR ASSEMBLING THE SAME, AND CORRESPONDING METHODS OF MANUFACTURING, OPERATING AND USE ASSOCIATED THERETO 审中-公开
公开(公告)号：WO2018176157A3
公开(公告)日：2018-10-04
申请号：PCT/CA2018/050398
申请日：2018-03-29
申请人： BINEK, Lawrence A. , ROMAGNOLO, Gabriel Idan , BINEK, Anthony A.
发明人： BINEK, Lawrence A. , ROMAGNOLO, Gabriel Idan , BINEK, Anthony A.
IPC分类号： F42B30/02 , F42B10/00 , F42B10/38 , F42B33/00 , F42B5/10
摘要： The present disclosure concerns a bullet (1) configured to be propelled by a blast of a cartridge, the bullet comprising a main body (3) provided with an internal body cavity (7) and having a frontward section and a rearward section provided with an opening in fluid communication with the internal body cavity, the internal body cavity by means of the opening being capable of recovering a portion of gun gas resulting from the blast of the cartridge. The present disclosure further comprises a weapon having such a bullet, and a method for reducing drag from a bullet propelled out of a barrel of a weapon.

2. 发明申请

WO2018022189A1 HYPERVELOCITY CANNON 审中-公开
标题翻译：超级无敌
公开(公告)号：WO2018022189A1
公开(公告)日：2018-02-01
申请号：PCT/US2017/035160
申请日：2017-05-31
申请人： AEROJET ROCKETDYNE, INC.
发明人： BULMAN, Melvin J.
IPC分类号： F41A1/04 , F42B14/08 , F42B5/10
CPC分类号： F41A1/02 , F41A1/04 , F42B5/105 , F42B14/08
摘要： A modified projectile includes a projectile, a container, and a liquid propellant in the container. The container is detachably attached to the projectile
摘要翻译：改进的射弹在容器中包括射弹，容器和液体推进剂。该容器可拆卸地连接到射弹上

3. 发明申请

WO2013052209A2 SHOTSHELL TYPE AMMUNITION, FIREARMS FOR FIRING SUCH SHOTSHELL TYPE AMMUNITION, AND METHODS OF MANUFACTURING SUCH SHOTSHELL TYPE AMMUNITION 审中-公开
公开(公告)号：WO2013052209A2
公开(公告)日：2013-04-11
申请号：PCT/US2012052023
申请日：2012-08-23
申请人： INTREPID TACTICAL SOLUTIONS LLC , DEJONG WILLIAM E
发明人： DEJONG WILLIAM E
IPC分类号： F42B5/02 , F42B5/10 , F42B33/02
CPC分类号： F41A21/12 , F41A5/00 , F41A9/64 , F41C7/00 , F42B5/30 , F42B7/04 , F42B7/06 , F42B8/10
摘要： Shotshell type ammunition includes a hull, a sabot disposed within the hull, and at least one projectile disposed within the sabot. The hull has a rimless first end that includes a primer for firing the ammunition. The hull also has a seat surface for seating the hull against a complementary seat surface in a firing chamber of a firearm. The seat surface is located a distance from an outer end surface of the hull at the rimless first end. The hull further includes an outer cylindrical side surface extending from the rimless first end of the hull to the seat surface of the hull. Methods of fabricating such ammunition includes forming such a hull, providing one or more projectiles within a sabot, and disposing the sabot with the one or more projectiles therein at least partially into the hull. Shotgun type firearms are configured for firing such ammunition.

4. 发明申请

WO2021161308A1 THERMOPLASTIC CANISTER 审中-公开
公开(公告)号：WO2021161308A1
公开(公告)日：2021-08-19
申请号：PCT/IL2021/050159
申请日：2021-02-10
申请人： RAFAEL ADVANCED DEFENSE SYSTEMS LTD.
发明人： PEREZ, Yatir , REDLICH, Yoav , BEN-ZVI, Itai
IPC分类号： F42B5/29 , F42B5/02 , F42B5/10 , F42B5/28 , F42B5/297 , F42B12/76 , F42B15/00 , C08J5/04
摘要： A canister for storing and launching a self-propelled projectile comprises: a) an inner layer comprising an aluminum foil; b) a top layer consisting of an injected thermoplastic polymer; and c) optionally, a primer and/or a topcoat.

5. 发明申请

WO01055665A1 ROCKET MOTOR ASSISTED GUN-LAUNCHED MUNITION 审中-公开
标题翻译： ROCKET电机辅助GUN-LUNCHED MUNITION
公开(公告)号：WO01055665A1
公开(公告)日：2001-08-02
申请号：PCT/US2001/002606
申请日：2001-01-26
IPC分类号： F42B5/10 , F42B15/00
CPC分类号： F42B5/10 , F42B15/00
摘要： A rocket powered gun launched munition that employs a sliding aft end closure (32) that forms the rocket propellant (34) into a force transmission column to transmit acceleration force onto the munition through the propellant rather than through the case of the rocket motor. This permits use of a thinner rocket motor case sidewall, provides more propellant and extends the operative range of the rocket motor. In other embodiments, portions of the munition case can be omitted which reduces weight, and expands the explosive charge cavity.
摘要翻译：火箭动力枪发射弹药，其使用形成火箭推进剂（34）的滑动后端封闭物（32）进入力传输塔，以通过推进剂而不是通过火箭发动机的情况将加速力传递到弹药上。这允许使用较薄的火箭发动机壳体侧壁，提供更多的推进剂并延长火箭发动机的操作范围。在其他实施例中，可以省略弹药盒的部分，这减少了重量，并且扩大了炸药装料腔。

6. 发明申请

WO0034731A3 GAS GENERATING EJECT MOTOR 审中-公开
标题翻译：燃气发电机
公开(公告)号：WO0034731A3
公开(公告)日：2000-10-12
申请号：PCT/US9926455
申请日：1999-11-10
申请人： CORDANT TECH INC , DOLL DANIEL W , LUND GARY K , HUGHES CRAIG D , HALL MARC A , MACON DAVID J
发明人： DOLL DANIEL W , LUND GARY K , HUGHES CRAIG D , HALL MARC A , MACON DAVID J
IPC分类号： C06D5/06 , F02K9/10 , F02K9/36 , F02K9/76 , F02K9/95 , F42B3/04 , F42B5/10
CPC分类号： C06D5/06 , F02K9/10 , F02K9/36 , F02K9/763 , F02K9/95 , F42B3/04 , F42B5/105
摘要： A gas generating eject motor (10) includes a case (12) containing an ignitable low temperature gas generant material (24) that does not produce toxic gases upon the combustion thereof. The gas generant material is generally contained with a screen enclosure (26, 30) housed within the case. An igniter (70) is disposed within the gas generant material for selectively igniting the gas generant to thereby generate combustion gases. A nozzle (40) is disposed within an open aft end of the case for focusing and directing the combustion gases generated by the ignited gas generant material. The case is constructed and arranged to be separaly attached to the aft end of a rocket (90) to be launched from a launch platform (80), so that, upon ignition of the gas generant, the combustion gases focused by the nozzle will apply a thrust to the rocket and thereby propel, or eject, the rocket from the launch platform, at which time the combustible propellant of the rocket motor will ignite and the eject motor will be separated from the rocket.
摘要翻译：气体发生喷射电动机（10）包括容纳可燃低温气体发生剂材料（24）的壳体（12），其在其燃烧时不产生有毒气体。气体发生剂材料通常包含容纳在壳体内的筛网外壳（26,30）。点火器（70）设置在气体发生剂材料内，用于选择性地点燃气体发生剂从而产生燃烧气体。喷嘴（40）设置在壳体的开口后端，用于聚焦和引导由点燃气体发生剂材料产生的燃烧气体。壳体被构造和布置成分离连接到从发射平台（80）发射的火箭（90）的后端，使得当燃气发生器点燃时，由喷嘴聚焦的燃烧气体将应用推动火箭从而推动或弹出火箭从发射平台，此时火箭发动机的可燃推进剂将点燃，弹出电机将与火箭分离。

7. 发明申请

WO9932780A3 MISSILE WITH SAFE ROCKET IGNITION SYSTEM 审中-公开
标题翻译：具有安全的点火点火系统
公开(公告)号：WO9932780A3
公开(公告)日：1999-10-07
申请号：PCT/US9824720
申请日：1998-11-19
申请人： RAYTHEON CO
发明人： ATKINSON BOBBY G
IPC分类号： F02K9/38 , F02K9/95 , F41A19/58 , F41G7/00 , F42B5/10 , F42B15/00 , F42C15/40
CPC分类号： F02K9/38 , F41A19/58 , F41G7/007 , F42B5/105 , F42B15/00 , F42C15/40
摘要： A rocket ignition system (32) adapted for use with a missile (30) having a rocket motor (24). The system (32) includes detectors (34, 36) and circuitry (22, 34, 36, 38, 40) for detecting an optical impulse and a pressure wave, both of them being components of a launch signal. In the illustrative embodiment, the system (30) includes a primer for generating the launch signal having. A processor (38, 40) computes the difference between the time elapsed between the receipt of both of the signal components and provides an ignition signal to the pyrotechnic rocket motor igniter (22) if the difference is within a predetermined valid time range. The predetermined valid time difference is computed based on the difference in position between both if the detectors, and the difference in velocities of said signal components. A safety switch (48) blocks the ignition signal when the missile (30) is not ready for use.
摘要翻译：一种适于与具有火箭发动机（24）的导弹（30）一起使用的火箭点火系统（32）。系统（32）包括用于检测光脉冲和压力波的检测器（34,36）和电路（22,34,36,38,40），它们都是发射信号的组成部分。在说明性实施例中，系统（30）包括用于产生具有发射信号的引导器。处理器（38,40）计算在两个信号分量的接收之间经过的时间之间的差异，并且如果该差值在预定的有效时间范围内，则向烟火火箭发动机点火器（22）提供点火信号。基于检测器之间的位置差和所述信号分量的速度差来计算预定的有效时间差。当导弹（30）不准备使用时，安全开关（48）阻挡点火信号。

8. 发明申请

WO99006276A3 ROCKET LAUNCHING SYSTEM EMPLOYING THERMAL-ACOUSTIC DETECTION FOR ROCKET IGNITION 审中-公开
标题翻译：火箭发射器系统使用热声检测火箭发射
公开(公告)号：WO99006276A3
公开(公告)日：1999-08-12
申请号：PCT/US1998/015255
申请日：1998-07-23
IPC分类号： B64G1/00 , F41A19/58 , F42B5/10 , F42B15/00 , F41F3/04 , F02K9/38 , F02K9/95
CPC分类号： F41A19/58 , B64G1/002 , F42B5/10 , F42B15/00
摘要： A rocket launching system (40) employing ignition apparatus (12, 13, 14, 18) that is used with a small rocket (10) to launch the rocket from a gun (30). The rocket is equipped with acoustic (pressure) and optical (thermal) sensors (13, 14) that detect a pressure pulse and light flash of a primer charge (35) used to fire the gun. The simultaneous detection of the pressure pulse and light flash by the sensors generates output signals that are used to complete an electrical circuit in an electronic ignition circuit (12) that activates an igniter (18) that ignites a rocket motor (16).
摘要翻译：火箭发射器系统（40）使用用于小火箭（10）的发射装置（12,13,14,18）从火炮（30）发射火箭。。火箭装备有声学（压力）和光学（热）传感器（13,14），其检测压力脉冲和来自用于点燃枪的起爆药（35）的闪光。传感器同时检测压力脉冲和闪电产生的输出信号用于完成电子点火电路（12）的电路，该电路启动启动器（ 18），它点燃火箭发动机（16）。

9. 发明申请

WO9915850A3 SEMIAUTOMATIC POCKET GUN AND AMMUNITION 审中-公开
标题翻译：半自动口袋枪和弹药
公开(公告)号：WO9915850A3
公开(公告)日：1999-07-29
申请号：PCT/US9820255
申请日：1998-09-25
申请人： MORGADO RALPH GORDON
发明人： MORGADO RALPH GORDON
IPC分类号： F41A3/04 , F41A9/17 , F41A11/04 , F41A19/50 , F41C3/00 , F42B5/18 , F42B5/10
CPC分类号： F41A3/04 , F41A9/17 , F41A9/45 , F41A11/04 , F41A19/50 , F41C3/00 , F41C9/02 , F42B5/18
摘要： Semiautomatic pistol which is small enough to be carried in a pocket or otherwise concealed on the body of a person, and caseless ammunition (163) for use in the pistol. The pistol has a grip (29) adapted to be held in the hand of a shooter, a barrel (22) extending in a forward direction from the grip (29) a closed chamber at the rear of the barrel (22), means for firing a caseless cartridge in the chamber with the entire cartridge (163) being discharged through the barrel (22) and means responsive to the firing of the cartridge (163) for opening the chamber and loading another cartridge (163) into the chamber. The caseless cartridge (163) consists of a hollow projectile filled with gunpowder (177), and a primer (174) for igniting the powder (177). The primer (174) is mounted directly to the projectile, and there is no casing or other material to be ejected from the chamber before another round is loaded.
摘要翻译：半自动手枪足够小，可携带在口袋中或以其他方式隐藏在人身上，以及无弹药（163）用于手枪。手枪具有适于保持在射手的手中的手柄（29），从手柄（29）向前方向延伸的在枪管（22）的后部处的封闭腔室的枪管（22），用于在整个筒体（163）通过筒体（22）排出的情况下，在室内发射无盒式药筒，以及响应于用于打开腔室并将另一个药筒（163）装入腔室中的药筒（163）的点燃的装置。无烟筒（163）由填充有火药（177）的中空射弹和用于点燃粉末（177）的底漆（174）组成。底漆（174）直接安装在抛射体上，在另一轮装载之前，没有外壳或其他材料从腔室中弹出。

10. 发明申请

WO2015116017A1 ПАТРОН С РЕАКТИВНОЙ ПУЛЕЙ 审中-公开
标题翻译：带箭头的卡特彼勒
公开(公告)号：WO2015116017A1
公开(公告)日：2015-08-06
申请号：PCT/UA2014/000024
申请日：2014-02-17
申请人： КАЛАЧЕВ, Александр Иванович , КАРПЕНКО, Роман Валериевич , ХАБИБУЛЛИН, Халит Гибадуллович
发明人： КАЛАЧЕВ, Александр Иванович , КАРПЕНКО, Роман Валериевич , ХАБИБУЛЛИН, Халит Гибадуллович
IPC分类号： F42B5/10 , F42B30/02
CPC分类号： F42B5/10 , F42B12/06 , F42B12/74 , F42B30/02
摘要： Изобретение относится к области боеприпасов, предназначенных для стрельбы из гладкоствольного или нарезного оружия любой конструкции, где в качестве поражающего элемента используется реактивная пуля или снаряд. Патрон содержит гильзу с капсюлем, реактивную пулю с внутренней полостью, в которой размещен метательный заряд, и соплом. Реактивная пуля состоит из оболочки, имеющей головную и донную части, и сердечника или рубашки и сердечника, при этом в головной части оболочки реактивной пули выполнено углубление, в котором размещены сердечник или рубашка и сердечник. Увеличено надежное поражение цели с одновременным повышением меткости и кучности стрельбы.
摘要翻译：本发明涉及从任何设计的平滑孔或膛膛武器进行射击的弹药领域，其中破坏性元件是火箭弹或导弹。本筒包括具有底漆的壳体和具有包含推进剂装料的内腔的火箭弹和喷嘴。火箭弹由具有鼻部和尾部的壳体以及芯或套筒和芯组成，其中火箭弹的壳的头部设置有凹部，芯或套和芯是处置。结果是更可靠地破坏了目标，提高了射击精度和命中次数。

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