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1. 发明授权

US08675183B1 Method and apparatus for target range determination 有权
标题翻译：目标范围确定方法和装置
公开(公告)号：US08675183B1
公开(公告)日：2014-03-18
申请号：US12700714
申请日：2010-02-04
申请人： James J. Jaklitsch
发明人： James J. Jaklitsch
IPC分类号： G01C3/22
CPC分类号： G06F17/5009 , F41F3/045 , F41G1/48 , F41G7/004 , F41G7/224 , G01C3/22 , G01S11/12 , G09B9/003
摘要： A system, method and computer program product provides for estimating the range of a target. An acquisition window of an imaging device is adjusted to fit a target at an unknown range in response to a user input. An angle subtended by the largest dimension of the target viewed from the acquisition window is determined. The range of the target is estimated from a largest dimension of the target and the angle subtended by the largest dimension of the target. The device may be a man-portable aircraft survivability equipment (ASE) system trainer (MAST), or any simulator simulating a man-portable air defense system (MANPADS).
摘要翻译：系统，方法和计算机程序产品用于估计目标的范围。调整成像装置的采集窗口以适应未知范围的目标以响应于用户输入。确定从采集窗口观看的目标的最大尺寸所对向的角度。目标的范围是从目标的最大维度和目标的最大尺寸所对的角度估计出来的。该装置可以是便携式飞机生存能力设备（ASE）系统训练器（MAST）或模拟便携式防空系统（MANPADS）的任何模拟器。

2. 发明申请

US20130280677A1 TRAINING WEAPON SYSTEM FOR RECOILLESS ANTITANK RIFLE WEAPONS 有权
标题翻译：训练武器系统，用于恢复反坦克制动武器
公开(公告)号：US20130280677A1
公开(公告)日：2013-10-24
申请号：US13697444
申请日：2010-05-11
申请人： Johnny Liljeholm
发明人： Johnny Liljeholm
IPC分类号： G09B25/00
CPC分类号： F41A33/00 , F41A1/08 , F41A21/10 , F41F3/045 , G09B25/00
摘要： The invention relates to a training weapon system (1) intended for a recoilless antitank rifle (2), the training weapon system (1) comprising a sub-calibre barrel (3) for firing sub-calibre practice projectiles (4) provided with base plates (5), the sub-calibre 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-calibre barrel (3) being fitted in a guide part (8) for centring 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.
摘要翻译：本发明涉及一种用于无后坐力的反坦克步枪（2）的训练武器系统（1），训练武器系统（1）包括用于发射子口径练习射弹（4）的子口筒（3）平板（5），副口径筒（3）布置在无后坐力的反坦克步枪（2）的筒体（7）中的壳体（6）中，子口筒（3）的前部）装配在用于使所述筒（3）定心的引导部分（8）中，并且所述筒体（3）的后部装配在后膛（9）中，包括击发通道（10）和喷嘴螺纹 11），用于安装布置在壳体（6）后部的喷嘴螺杆（12）。本发明的特征在于，训练武器系统（1）包括至少一个锁定部分（13,14），其功能是防止喷射器（12）或射弹（4）的基板（5））或基板（5）的一部分作为松散的飞行射弹通过反坦克步枪（2）的喷嘴漏斗（21）向后排出。

3. 发明授权

US07237488B2 Fireworks bottle rocket launcher 失效
标题翻译：烟花瓶火箭发射器
公开(公告)号：US07237488B2
公开(公告)日：2007-07-03
申请号：US11066916
申请日：2005-02-25
申请人： Cameron Michael Duescher , Kent Wayne Duescher
发明人： Cameron Michael Duescher , Kent Wayne Duescher
IPC分类号： F42B4/06 , F42B4/20
CPC分类号： F41A3/06 , F41F3/045 , F42B4/20
摘要： A bottle rocket launcher comprises a long hollow tube barrel having an tube-axial sealing valve that has a rotary cylindrical or spherical valve member where the valve is attached at the breech end of the launcher barrel. The rocket launcher can be angled up to a near vertical position with support legs. In use, a bottle rocket can be partially inserted into the valve passageway that is held open. The flammable rocket fuse is lit and the bottle rocket is dynamically inserted by hand contact with the rocket stick into the barrel inside chamber body to a position that is beyond the valve member. The valve is rotated into a valve-closed position while the rocket fuse is burning. When the bottle rocket powder is ignited by the burning fuse, the burning exhaust gases thrusts the bottle rocket along the inside of the barrel tube and propels it into the sky in the direction that the launcher barrel is pointed. The rocket exhaust gasses are all restricted to the valve sealed interior confirms of the launch barrel, which protects the operator from the gases or from a premature explosion of the rocket. The launch tube may be independently supported on the surface of the ground or the launch tube may be used as a hand-held device.
摘要翻译：瓶式火箭发射器包括具有管轴向密封阀的长的中空管筒，其具有旋转圆柱形或球形阀构件，其中阀安装在发射筒的后端。火箭发射器可以与支撑腿成一个垂直的垂直位置。在使用中，瓶火箭可以部分地插入被保持打开的阀通道中。可燃火箭保险丝点亮，并且通过与火箭棒手枪接触到腔室内的枪管中动态地插入瓶火箭至超过阀构件的位置。当火箭保险丝燃烧时，阀门旋转到阀门关闭位置。当燃烧的保险丝点燃瓶火箭粉末时，燃烧的废气沿着枪管的内部推动瓶火箭，并沿着发射筒指向的方向将其推入天空。火箭废气都限于发射筒的阀门密封内部确认，这保护了操作者免受气体或火箭的过早爆炸。发射管可以独立地支撑在地面上，或者发射管可以用作手持装置。

4. 发明申请

US20050217529A1 Projectile and method for sealing a projectile in a barrel 审中-公开
标题翻译：用于将炮弹中的弹丸密封的弹丸和方法
公开(公告)号：US20050217529A1
公开(公告)日：2005-10-06
申请号：US11112480
申请日：2005-04-22
申请人： James O'Dwyer
发明人： James O'Dwyer
IPC分类号： F41A21/06 , F41A21/00 , F41A21/28 , F41A25/12 , F41F1/00 , F41F3/045 , F42B5/03 , F42B14/00
CPC分类号： F41A25/12 , F41F1/00 , F41F3/045 , F42B5/035
摘要： A weapon (104) including a stock, a barrel assembly (105) slidably mounted on said stock whereby, on discharging said weapon, the barrel assembly (105) slidably recoils relative to said stock, and a damper (107) for decelerating the recoiling barrel assembly, wherein said barrel assembly (105) includes a plurality of projectiles axially disposed within a barrel (108) wherein each of said projectiles is associated with a discrete propellant charge for propelling said projectile from the barrel. Suitably the weapon further includes a breech block (109) which slidably recoils relative to said stock and a further damper (106) for decelerating the recoiling breech block.
摘要翻译：一种包括库存的武器（104），可滑动地安装在所述库存上的桶组件（105），其中在排出所述武器时，所述桶组件（105）相对于所述坯料可滑动地回缩;以及阻尼器（107），用于减速所述回卷其中所述枪管组件（105）包括轴向设置在枪管（108）内的多个射弹，其中每个所述射弹与用于将炮弹从枪管推进的离散推进剂装料相关联。适当地，武器还包括相对于所述坯料滑动地回缩的后膛块（109）和用于减速回弹后膛块的另外的阻尼器（106）。

5. 发明授权

US4593602A Rocket weapon system and method therefor 失效
标题翻译：火箭武器系统及其方法
公开(公告)号：US4593602A
公开(公告)日：1986-06-10
申请号：US678198
申请日：1984-12-04
申请人： John J. Faix
发明人： John J. Faix
IPC分类号： F41A19/27 , F41A19/57 , F41F1/08 , F41F3/045 , F41F3/04
CPC分类号： F41A19/27 , F41A19/57 , F41F1/08 , F41F3/045
摘要： An improved rifle-actuated rocket weapon system and an improved method foriming the system in relation to a short range target by firing one or more tracer bullets until it is aimed at the target for launching the rocket weapon. The system is generally made up of a spotting rifle and a rocket weapon launch tube subassembly. The rifle is provided with a magazine for carrying one or more tracer bullets. Fluid passageway means are provided in the launch tube subassembly, rocket weapon fuse device, and rifle. Interconnection of the passageway means with the bullet accelerating and guiding passageway of the rifle is effected by a manually operated normally closed valve. The valve is disposed in the rifle and is operatively associated with the passageway means. When the system is aimed at the target, the valve is opened and a final bullet is fired such that the high temperature, pressurized gases of the bullet are directed via the passageway means to ignite the rocket fuel and arm the rocket weapon fuse device as the weapon is launched to strike the target. The rocket weapon can be positively secured to the launch tube subassembly by a gas-releasable pin that is inserted in the passageway means and that is disposed between the weapon and the subassembly. Since the system is portable and shoulder-held, it is easily maneuverable for progressively aiming the system in relation to a short-range target to be destroyed by a system-launched rocket weapon.
摘要翻译：改进的步枪致动火箭武器系统和改进的方法，用于通过发射一个或多个示踪子弹直到瞄准目标以发射火箭武器来瞄准系统与短距离目标。该系统通常由点样步枪和火箭发射管子组件组成。步枪设有一个用于携带一个或多个示踪器子弹的杂志。流体通道装置设置在发射管子组件，火箭武器保险丝装置和步枪中。通道装置与步枪的子弹加速和引导通道的互连通过手动操作的常闭阀来实现。阀设置在步枪中并且与通道装置可操作地相关联。当系统瞄准目标时，阀打开，并且发射最后的子弹，使得子弹的高温加压气体经由通道装置引导以点燃火箭燃料并且将火箭武器保险丝装置作为武器发动袭击目标。火箭武器可以通过插入在通道装置中并且设置在武器和子组件之间的可气体释放的销子牢固地固定到发射管子组件。由于该系统是便携式和肩托式的，因此可以轻松地机动地将系统逐渐瞄准由系统发射的火箭武器销毁的短距离目标。

6. 发明授权

US4584925A Underwater rocket launcher and rocket propelled missile 失效
标题翻译：水下火箭发射器和火箭推进导弹
公开(公告)号：US4584925A
公开(公告)日：1986-04-29
申请号：US535814
申请日：1983-09-26
申请人： Kenneth W. Culotta , Anthony J. Culotta
发明人： Kenneth W. Culotta , Anthony J. Culotta
IPC分类号： F41A19/58 , F41C9/06 , F41F3/045 , F41B11/10 , F41C1/00 , F41F3/04
CPC分类号： F41F3/045 , F41A19/58 , F41C9/06
摘要： Our invention comprises a launcher which takes the form of a holster carried firearm and a rocket propelled missile slidably mounted within the launcher. Features of our invention include electrical ignition of the rocket propelled missile, waterproof electrical connectors and switches, an impact actuated warhead, a warhead firing mechanism, electrical and mechanical safety devices, and automatic warhead arming upon rocket motor ignition. Additional features include rapid reload capability, illuminated sight lights, ease of carry and one hand operation. Our design incorporates only two moving parts in the launcher, and one moving part sealed within the missile body. Advantageously, none of the components are subject to corrosion or contamination, and no special materials are necessary in its fabrication.
摘要翻译：我们的发明包括一个发射器，其采用携带枪支的皮套和可滑动地安装在发射器内的火箭推进导弹。我们的发明的特征包括火箭推进导弹的电气点火，防水电气连接器和开关，冲击致动的弹头，弹头击发机构，电气和机械安全装置以及在火箭发动机点火时布置的自动弹头。附加功能包括快速重新载入能力，照明瞄准灯，便于携带和单手操作。我们的设计在发射器中仅包含两个运动部件，一个运动部件在导弹体内密封。有利的是，没有一个组件遭受腐蚀或污染，并且在其制造中不需要特殊的材料。

7. 发明授权

US4010688A Weapon arrangement 失效
公开(公告)号：US4010688A
公开(公告)日：1977-03-08
申请号：US307444
申请日：1972-11-17
申请人： Matthew S. Smith , Ernest A. Filippi
发明人： Matthew S. Smith , Ernest A. Filippi
IPC分类号： F41A23/12 , F41F3/045 , F41F7/00 , F42B10/48 , F42B15/00 , F42B11/42
CPC分类号： F42B10/48 , F41A23/12 , F41F3/045 , F41F7/00 , F42B15/00
摘要： A rocket boosted and/or sustained round for launching from a firearm, recoilless rifle, mortar or any other type of closed breech launcher and an adjustable, recoiling tripod support for the firearm or other type of closed breech launcher. The tripod supports the launcher during launch of the rocket boosted and/or sustained round. The rocket boosted round, which may be launched, for example, from the conventional M-16 rifle, is aero-gyro stabilized and is provided with a tubular tailpipe that slidingly fits over the end of the firearm barrel. A rocket motor which is ignited during or after launch is coupled to the tailpipe and a warhead having a predetermined ogive configuration is coupled to the rocket motor. An ignition delay means in the round such as a pyrotechnic delay may be provided to allow a predetermined time delay between launch of the round and the ignition of the rocket motor. Other round configurations incorporate a progressive burning rocket motor grain instead of a pyrotechnic delay. The low thrust and negligible back blast from the initial burn of the rocket allows the elimination of the time delay from launch to rocket motor ignition. The round is launched by firing a grenade launcher cartridge in the launcher. The hot, gaseous products of combustion from the cartridge enter the tailpipe of the round and launch the round from the launcher. The ignition delay means if utilized, initiates ignition of the rocket motor after a predetermined time interval has elapsed from launch. In the progressive burn configuration the rocket motor ignites while on the launcher. In order to achieve zone firing, various shrouds may also be provided. For example, to achieve the longest range firing, a streamlined fairing maybe coupled between the warhead and the tailpipe to provide minimum drag configuration for maximum ranging. If shorter ranges are desired one or more drag shrouds may be coupled to the round to decrease the range. For minimum range, a plug is inserted in the tailpipe to prevent ignition of the rocket motor and the round follows a ballistic trajectory after launch. The tripod support is a recoil energy dissipating type of support and is detachably mountable on the launcher, preferably without modification or change to the launcher. During firing the tripod support time to full recoil is considerably greater than the time required for the rocket round to leave the launcher. Thus the rocket round starts free flight without the introduction of launch perturbations. The tripod support is adjustable to provide a plurality of different launch angles for launching of the round from the launcher and is foldable from the firing positions to a folded position providing a minimum package configuration for convenience in transportation thereof.

8. 发明授权

US3421410A Missile and hand held launcher 失效
标题翻译：小型和手持式发动机
公开(公告)号：US3421410A
公开(公告)日：1969-01-14
申请号：US3421410D
申请日：1967-08-25
申请人： GEORGE KAYAIAN
发明人： KAYAIAN GEORGE
IPC分类号： F41A19/59 , F41F3/045 , F41F3/052 , F42C15/184 , F41F3/04
CPC分类号： F41F3/052 , F41A19/59 , F41F3/045 , F42C15/184

9. 发明授权

US3398640A Rocket launcher device 失效
标题翻译：火箭发射装置
公开(公告)号：US3398640A
公开(公告)日：1968-08-27
申请号：US60168966
申请日：1966-12-14
申请人： OERLIKON BUEHRLE HOLDING AG
发明人： ROBERT APOTHELOZ , HANSPETER SCHENK , ALEX GELBERT
IPC分类号： F41A19/29 , F41F3/04 , F41F3/042 , F41F3/045 , F41F3/077 , F42B4/22 , F42C7/12
CPC分类号： F42B4/22 , F41A19/29 , F41F3/04 , F41F3/042 , F41F3/045 , F41F3/077 , F42C7/12

10. 发明授权

US1332716A Holder for rocket-bombs 失效
标题翻译：火箭弹持有人
公开(公告)号：US1332716A
公开(公告)日：1920-03-02
申请号：US24545018
申请日：1918-07-18
申请人： DE SHERBININ ERIC M
发明人： DE SHERBININ ERIC M
IPC分类号： F41F3/045
CPC分类号： F41F3/045

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