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11. 发明申请

US20150375840A1 STAND-OFF DELIVERY OF UNMANNED UNDERWATER VEHICLES 审中-公开
标题翻译：未经规定的水下车辆的交付
公开(公告)号：US20150375840A1
公开(公告)日：2015-12-31
申请号：US14228686
申请日：2014-03-28
申请人： The Boeing Company
发明人： Kyle Stowers
IPC分类号： B63G8/00 , F41G7/34 , B63G8/08 , F42B10/32 , B64D17/62
CPC分类号： B63G8/001 , B63G8/08 , B63G2008/004 , B63G2008/005 , B64D17/62 , F41G7/346 , F42B10/32 , F42B15/22 , F42B17/00 , F42B19/46 , F42B22/44
摘要： Embodiments described herein provide apparatus and method for stand-off deployment of UUVs utilizing self-directed projectiles that include guidance kits. One embodiment is a projectile that includes a guidance kit that directs the projectile in flight. The projectile further includes a shell and a hollow nose cone. The shell mates with the guidance kit and the nose cone couples with the shell. The nose cone includes an interior surface configured to house a UUV. The projectile further includes a controller that identifies a condition for deploying the UUV in flight, and detaches the nose cone from the shell in response to determining that the condition is satisfied.
摘要翻译：本文描述的实施例提供了使用包括指导套件的自导弹丸的UUV的对立部署的装置和方法。一个实施例是一种抛射体，其包括指导飞行中的弹丸的引导工具。射弹还包括一个外壳和一个空心鼻锥。外壳与指导套件配合，鼻锥与外壳配合。鼻锥包括配置成容纳UUV的内表面。弹丸还包括控制器，其识别在飞行中部署UUV的条件，并且响应于确定条件得到满足而将鼻锥从壳体分离出来。

12. 发明授权

US09534858B2 Cartridge and system for generating a projectile with a selectable launch velocity 有权
标题翻译：用于产生具有可选发射速度的弹丸的弹药筒和系统
公开(公告)号：US09534858B2
公开(公告)日：2017-01-03
申请号：US14351724
申请日：2012-10-15
申请人： The Commonwealth of Australia
发明人： Stephen Forbes , Edmond Almond , Shaun McCormack , Jeffery Ackers , Robert Reichstein , Michael Chatwin
IPC分类号： F41A1/06 , F42B5/08 , F41A19/58 , F41A19/69 , F42C19/08 , F41C27/06 , F41G1/473 , F41G3/06 , F42B10/32 , F42B12/02 , F41H9/10 , F42B5/145 , F42B5/02
CPC分类号： F41A1/06 , F41A19/58 , F41A19/69 , F41C27/06 , F41G1/473 , F41G3/06 , F41H9/10 , F42B5/02 , F42B5/08 , F42B5/145 , F42B10/32 , F42B12/02 , F42C19/0834
摘要： A weapon system includes a cartridge and a fire control apparatus have been developed for generating a projectile with a selectable launch velocity. The cartridge includes multiple primers and propellant chambers which may be individually selected by the fire controller so as to fire the projectile at a selected launch velocity. Additionally after firing the selected primers and propellant charges, the fire controller sends a second firing signal to all remaining primers after a suitable delay. The second firing signal ensures that all remaining propellant is initiated and consumed, thus rendering the cartridge safe to eject. The delay between the first firing signal and the second firing signal is sufficient to allow the projectile to be expelled from the cartridge so that the launch velocity is not affected by the combustion of the remaining propellant.
摘要翻译：已经开发了一种武器系统，其包括用于产生具有可选发射速度的射弹的筒和消防控制装置。所述筒包括多个底漆和推进剂室，其可以由所述防火控制器单独选择，以便以选定的发射速度对所述射弹起火。另外在烧制所选择的引物和推进剂电荷之后，火灾控制器在合适的延迟之后向所有剩余的引物发送第二次发射信号。第二个发射信号确保所有剩余的推进剂被启动和消耗，从而使墨盒安全地弹出。第一发射信号和第二发射信号之间的延迟足以允许射弹从盒中排出，使得发射速度不受剩余推进剂燃烧的影响。

13. 发明授权

US09329007B2 Charged projectiles and related assemblies, systems and methods 有权
标题翻译：装弹和相关装配，系统和方法
公开(公告)号：US09329007B2
公开(公告)日：2016-05-03
申请号：US13789147
申请日：2013-03-07
申请人： Orbital ATK, Inc.
发明人： Otto S. Krauss , John W. Westbrook, III
IPC分类号： F42B10/38 , F42B10/32 , F42B5/02 , F42B30/00 , F42B12/00
CPC分类号： F42B10/38 , F42B5/02 , F42B10/32 , F42B12/00 , F42B30/00
摘要： Charged projectile assemblies include a housing and an electronic assembly configured to produce an electric field about at least a portion of the housing of the projectile. Cartridge assemblies for use with firearms include charged projectiles. Methods of charging a projectile include forming an electric field about at least a portion of a projectile and extending the electric field at least partially between a forward portion of the projectile and an aft portion of the projectile.
摘要翻译：带电弹丸组件包括壳体和电子组件，其被配置为在射弹的壳体的至少一部分周围产生电场。与火器一起使用的墨盒组件包括带电弹丸。对弹丸进行充电的方法包括在射弹的至少一部分周围形成电场，并至少部分地在射弹的前部与射弹的后部之间延伸电场。

14. 发明申请

US20150159981A1 Cartridge and System for Generating a Projectile with a Selectable Launch Velocity 有权
标题翻译：用于生成具有可选发射速度的弹丸的弹药筒和系统
公开(公告)号：US20150159981A1
公开(公告)日：2015-06-11
申请号：US14351724
申请日：2012-10-15
申请人： The Commonwealth of Australia
发明人： Stephen Forbes , Edmond Almond , Shaun McCormack , Jeffery Ackers , Robert Reichstein , Michael Chapman
IPC分类号： F42B5/145 , F41H9/10
CPC分类号： F41A1/06 , F41A19/58 , F41A19/69 , F41C27/06 , F41G1/473 , F41G3/06 , F41H9/10 , F42B5/02 , F42B5/08 , F42B5/145 , F42B10/32 , F42B12/02 , F42C19/0834
摘要： A weapon system includes a cartridge and a fire control apparatus have been developed for generating a projectile with a selectable launch velocity. The cartridge includes multiple primers and propellant chambers which may be individually selected by the fire controller so as to fire the projectile at a selected launch velocity. Additionally after firing the selected primers and propellant charges, the fire controller sends a second firing signal to all remaining primers after a suitable delay. The second firing signal ensures that all remaining propellant is initiated and consumed, thus rendering the cartridge safe to eject. The delay between the first firing signal and the second firing signal is sufficient to allow the projectile to be expelled from the cartridge so that the launch velocity is not affected by the combustion of the remaining propellant.
摘要翻译：已经开发了一种武器系统，其包括用于产生具有可选发射速度的射弹的筒和消防控制装置。所述筒包括多个底漆和推进剂室，其可以由所述防火控制器单独选择，以便以选定的发射速度对所述射弹起火。另外在烧制所选择的引物和推进剂电荷之后，火灾控制器在合适的延迟之后向所有剩余的引物发送第二次发射信号。第二个发射信号确保所有剩余的推进剂被启动和消耗，从而使墨盒安全地弹出。第一发射信号和第二发射信号之间的延迟足以允许射弹从盒中排出，使得发射速度不受剩余推进剂燃烧的影响。

15. 发明授权

US08729443B2 Projectile and method that include speed adjusting guidance and propulsion systems 有权
标题翻译：包括速度调节引导和推进系统的抛射和方法
公开(公告)号：US08729443B2
公开(公告)日：2014-05-20
申请号：US13020276
申请日：2011-02-03
申请人： Andrew B. Facciano , James A. Ebel , Michael Alkema , Robert D. Travis , Mike J. Saxton
发明人： Andrew B. Facciano , James A. Ebel , Michael Alkema , Robert D. Travis , Mike J. Saxton
IPC分类号： F42B15/01 , F42B10/32 , F42B15/00 , F42B10/00
CPC分类号： B64G1/002 , B64G1/401 , B64G1/403 , F42B10/32 , F42B15/01 , F42B15/10
摘要： Some embodiments pertain to a projectile and method that includes a flight vehicle and a propulsion system attached to the flight vehicle. The propulsion system includes a plurality of motors that propel the projectile. A guidance system is connected to the propulsion system. The guidance system ignites an appropriate number of the motors to adjust the speed of the projectile based on the location of the projectile relative to a desired destination for the flight vehicle. In some embodiments, the flight vehicle is a kinetic warhead. The projectile may be an interceptor that includes a first propulsion stage, a second propulsion stage and a third propulsion stage that includes the third propulsion system. The number of booster motors that will be ignited by the guidance system depends on the speed that the projectile needs to be adjusted to in order to maneuver the projectile to a desired location.
摘要翻译：一些实施例涉及包括飞行车辆和附接到飞行器车辆的推进系统的射弹和方法。推进系统包括推动射弹的多个马达。引导系统连接到推进系统。引导系统点燃适当数量的电机，以根据飞弹相对于飞行器的所需目的地的位置来调整射弹的速度。在一些实施例中，飞行器是动力弹头。抛射体可以是包括第一推进阶段，第二推进阶段和包括第三推进系统的第三推进阶段的拦截器。引导系统将引燃的助力马达的数量取决于弹丸需要调整的速度，以便将弹丸操纵到所需的位置。

16. 发明申请

US20100224719A1 METHOD OF VARYING FIRING RANGE AND EFFECT IN TARGET FOR SHELL AND SHELL CONFIGURED FOR THIS PURPOSE 有权
标题翻译：改变针对本目的配置的外壳和外壳目标的闪光范围和效果的方法
公开(公告)号：US20100224719A1
公开(公告)日：2010-09-09
申请号：US12682849
申请日：2008-10-16
申请人： Nils Johansson
发明人： Nils Johansson
IPC分类号： F42B10/38
CPC分类号： F42B15/36 , F42B10/32
摘要： The present invention relates to a method and a shell (1) for achieving variable firing range and effect when firing from a launcher, which shell (1) contains a firing charge (10), a rocket motor charge (6) with gas outlet (8), a rocket motor nozzle (9) and an active part (5). According to the invention, this is achieved by virtue of the fact that the shell (1) also contains a release mechanism (15) for releasing the rocket motor nozzle (9) from the rocket motor charge (6) after a time delay determined with regard to firing range and effect, and that the rocket motor charge (6) comprises a propellant which is detonable.
摘要翻译：本发明涉及一种用于实现可变点火范围的方法和壳体（1），其用于从发射器进行燃烧时，该发射器（1）包含点火装置（10），具有气体出口的火箭发动机充电器（6） 8），火箭发动机喷嘴（9）和活动部件（5）。根据本发明，这是通过以下事实来实现的：壳体（1）还包含用于在火箭发动机喷嘴（9）与火箭发动机电荷（6）之间释放时间延迟之后释放火箭发动机喷嘴（9）的释放机构（15）关于射程和效果，并且火箭发动机充电（6）包括可引爆的推进剂。

17. 发明授权

US1509178A Projectile 失效
公开(公告)号：US1509178A
公开(公告)日：1924-09-23
申请号：US62486223
申请日：1923-03-13
申请人： RATCLIFF HILERY M
发明人： RATCLIFF HILERY M
IPC分类号： F42B10/32
CPC分类号： F42B10/32

18. 发明授权

US09752858B2 Methods of utilizing projectiles 有权
公开(公告)号：US09752858B2
公开(公告)日：2017-09-05
申请号：US15141630
申请日：2016-04-28
申请人： Orbital ATK, Inc.
发明人： Otto S. Krauss , John W. Westbrook, III
IPC分类号： F42B10/38 , F42B10/32 , F42B5/02 , F42B12/00 , F42B30/00
CPC分类号： F42B10/38 , F42B5/02 , F42B10/32 , F42B12/00 , F42B30/00
摘要： Charged projectile assemblies include a housing and an electronic assembly configured to produce an electric field about at least a portion of the housing of the projectile. Cartridge assemblies for use with firearms include charged projectiles. Methods of charging a projectile include forming an electric field about at least a portion of a projectile and extending the electric field at least partially between a forward portion of the projectile and an aft portion of the projectile.

19. 发明授权

US09677864B1 Closed, self-contained ballistic apogee detection module and method 有权
公开(公告)号：US09677864B1
公开(公告)日：2017-06-13
申请号：US14547972
申请日：2014-11-19
申请人： Michael Jankowski , Anthony Opperman , Gerard Skebe
发明人： Michael Jankowski , Anthony Opperman , Gerard Skebe
IPC分类号： G05D1/00 , F42B10/00 , F42B15/01 , F42B10/14 , F41G7/30 , F41G7/22 , F42B10/62 , G05D1/12 , B64C13/16
CPC分类号： F42B15/01 , B64C13/16 , F41G7/008 , F41G7/22 , F41G7/30 , F41G7/306 , F42B10/14 , F42B10/32 , F42B10/62 , F42B30/10 , F42C15/00 , G05D1/0033 , G05D1/0094 , G05D1/12
摘要： A closed, self-contained ballistic apogee detection module for use in a projectile, such as a rocket, mortar round, or artillery round, fuses data from multiple built-in sensors, such as an accelerometer, a magnetometer, and a gyroscope, and processes the data using a microprocessor through a custom quaternion extended Kalman filter to provide accurate state and orientation information about the projectile so as to accurately predict apogee. The module outputs a signal indicating apogee detection or prediction which they projectile uses to initiate fuze arming, targeting control, airbody transformation, maneuvering, flow effector deployment or activation, payload exposure or deployment, and/or other mission activity. Because the system and method of the invention does not rely on external environmental data to detect apogee, it need not use a pressure sensor and can be completely sealed in and closed without requiring access to air from outside the projectile for barometric readings.

20. 发明申请

US20170097216A1 SYSTEMS TO MEASURE YAW, SPIN AND MUZZLE VELOCITY OF PROJECTILES, IMPROVE FIRE CONTROL FIDELITY, AND REDUCE SHOT-TO-SHOT DISPERSION IN BOTH CONVENTIONAL AND AIRBURSTING PROGRAMMABLE PROJECTILES 有权
公开(公告)号：US20170097216A1
公开(公告)日：2017-04-06
申请号：US15200023
申请日：2016-07-01
申请人： NOSTROMO HOLDINGS, LLC
发明人： KEVIN MICHAEL SULLIVAN
IPC分类号： F42B35/00 , F42B12/38 , F42B12/22
CPC分类号： F42B35/00 , F41A21/30 , F41A21/32 , F41A21/34 , F42B10/00 , F42B10/32 , F42B12/02 , F42B12/22 , F42B12/387 , F42B12/72 , F42B12/76 , F42C17/00 , G01P3/38 , G01P3/685 , H04N5/2256
摘要： Kits or sub-systems that include sensors to measure a projectile's condition at muzzle exit. The kits or sub-systems are coupled to ballistic calculators or fire control systems that calculate aiming and programming solutions to improve shot placement, reduced dispersion and improve terminal performance. Where airburst munitions are used, the projectile is programmed when reaching a programming station beyond the barrel and the projectile is programmed with a solution that adjusts the burst location based on the measured muzzle velocity. Sub-systems, processes and sub-routines optimize “post-shot” programming using certain non-linear methods that are incorporated into fire control systems and ballistic calculators. These non-linear sub-routines are useful in establishing the optimum terminal effect of such airburst projectiles. The sub-systems are used separately or are incorporated into the weapons, to reduce dispersion and improve the terminal effects of the projectiles.

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