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1. 发明申请

US20220163304A1 Remotely Controllable Aeronautical Ordnance 有权
公开(公告)号：US20220163304A1
公开(公告)日：2022-05-26
申请号：US17378765
申请日：2021-07-19
申请人： Overwerx Ltd
发明人： Jeffrey Hill
IPC分类号： F42B15/01 , G05D1/00 , F42B10/38 , F42C13/04 , F42B12/02 , F42B15/10 , H04N7/18 , F42C1/00 , G06V20/13
摘要： An ordnance for air-borne delivery to a target under remotely controlled in-flight navigation. In one embodiment, self-powered aerial ordnance includes upper and lower cases. A plurality of co-axial, deployable blades is powered by a motor positioned in the upper case. When deployed, the blades are rotatable about the upper case to impart thrust and bring the vehicle to a first altitude above a target position. An explosive material and a camera are positioned in a lower case which is attached to the upper case. The camera generates a view along the ground plane and above the target when the ordinance is in flight. When the vehicle is deployed it is remotely controllable to deliver the vehicle to the target to detonate the explosive at the target. The ordnance may drop directly on a target as a bomb does.

2. 发明申请

US20180023931A1 AERODYNAMIC PROJECTILE 审中-公开
公开(公告)号：US20180023931A1
公开(公告)日：2018-01-25
申请号：US15693615
申请日：2017-09-01
申请人： United Tactical Systems, LLC
发明人： Gary E. Gibson , Michael A. Varacins , Jon Willson
IPC分类号： F42B10/38 , F42B10/26 , F42B10/24
CPC分类号： F42B10/38 , F42B10/24 , F42B10/26 , F42B10/44 , F42B12/40
摘要： A projectile has a front portion and a cylindrical portion. The cylindrical portion comprises a cylindrical sidewall having an outer surface and an inner surface. The projectile also has a plurality of depressions in the cylindrical sidewall. The depressions have an outlet adjacent the second end, an inlet toward the first end and a neck area between the inlet and the outlet. A width of the inlet is smaller than a width of the outlet. The depressions at the neck area have a curved sidewall, but a generally straight sidewall between the neck area and the outlet. The surface of the depression extends at a ramp angle from the outer surface of the sidewall at the inlet of the depression toward the inner surface of the sidewall at the outlet.

3. 发明授权

US09488453B2 Structuring of the ogive surface of a projectile 有权
标题翻译：弹丸表面的构造
公开(公告)号：US09488453B2
公开(公告)日：2016-11-08
申请号：US14237639
申请日：2012-08-07
申请人： Hannes Dikhoff , Karlheinz Muss , Vasile Papet , Frank Mönius
发明人： Hannes Dikhoff , Karlheinz Muss , Vasile Papet , Frank Mönius
IPC分类号： F42B5/24 , F42B12/02 , F42B10/38 , F42B10/42
CPC分类号： F42B12/02 , F42B10/38 , F42B10/42
摘要： The invention relates to a projectile with a projectile tip (9) at the front as viewed in the direction of the shot, which transforms via an ogive (1) into a rear cylindrical area (7). To reduce the air resistance and optimize precision, it is proposed according to the invention that the surface of the ogive (1) be structured.
摘要翻译：本发明涉及一种在射击方向观察时在前方具有射弹尖（9）的射弹，其通过一个凹陷（1）转变成后圆柱形区域（7）。为了降低空气阻力并优化精度，根据本发明提出，构造了（1）的表面。

4. 发明授权

US09404721B2 Ring airfoil glider with augmented stability 有权
标题翻译：环形翼型滑翔机具有增强的稳定性
公开(公告)号：US09404721B2
公开(公告)日：2016-08-02
申请号：US14193855
申请日：2014-02-28
申请人： Kimball Rustin Scarr
发明人： Kimball Rustin Scarr
IPC分类号： F42B10/36 , F42B10/38
CPC分类号： F42B10/36 , F42B10/38
摘要： In one embodiment, a less lethal munition including a ring airfoil projectile. The flight trajectory of the projectile has increased accuracy resulting from the aerodynamic stabilization of the projectile. In some embodiments, the projectile is both aerodynamically stabilized and spin stabilized.
摘要翻译：在一个实施例中，一种不太致命的弹药，包括环形翼型弹丸。弹丸的飞行轨迹由于弹丸的气动稳定性而提高了精度。在一些实施例中，射弹既是空气动力学稳定又自旋稳定。

5. 发明申请

US20160131462A1 Long-Range Aerodynamic Pellet for Airsoft and Military Training 审中-公开
标题翻译：用于气枪和军事训练的长程气动颗粒
公开(公告)号：US20160131462A1
公开(公告)日：2016-05-12
申请号：US14769918
申请日：2014-01-13
申请人： BIOPLAST FUTURE, S.L.
发明人： Luis Henrique LÓPEZ-POZAS LANUZA
IPC分类号： F42B6/10 , F42B10/38 , F42B8/12
CPC分类号： F42B6/10 , F42B8/12 , F42B10/38
摘要： The invention relates to a variety of pellets for using in the sport Airsoft and for military training, said pellets being novel in that they have a more aerodynamic design based on a surface that reduces the air friction and allows a longer range. Said pellets are characterized in that they have a surface forming different geometric figures such as a hexagon, pentagon, triangle, circle or square, that create a turbulent flow in the surrounding air layers, thereby obtaining a longer range and improved shooting precision.
摘要翻译：本发明涉及用于运动Airsoft和军事训练中的各种粒料，所述丸是新颖的，因为它们具有基于表面的更空气动力学设计，其减少空气摩擦并允许更长的范围。所述颗粒的特征在于它们具有形成不同几何图形的表面，例如六边形，五边形，三角形，圆形或正方形，其在周围空气层中产生湍流，从而获得更长的范围并提高了拍摄精度。

6. 发明授权

US08985518B2 Air guiding means for a dispenser 有权
标题翻译：用于分配器的空气引导装置
公开(公告)号：US08985518B2
公开(公告)日：2015-03-24
申请号：US13377299
申请日：2009-06-11
申请人： Christer Zätterqvist
发明人： Christer Zätterqvist
IPC分类号： B64D1/00 , F42B5/155 , F42B12/70 , F42B4/26 , F42B10/38 , F42B12/62
CPC分类号： F42B5/155 , F42B4/26 , F42B10/38 , F42B12/62 , F42B12/70
摘要： An air guide for a dispenser. At least one air scoop is configured to guide an air stream to a feeding out opening for chaffs on the dispenser in order to facilitate packages of chaffs to be released from the dispenser. A control unit is configured to control the air stream through the at least one air scoop.
摘要翻译：一个分配器的导航器。至少一个空气铲斗构造成将空气流引导到分配器上的谷壳的送出开口，以便于将包装盒从分配器中释放出来。控制单元构造成通过至少一个空气勺来控制空气流。

7. 发明授权

US08915806B2 Arrow shaft 有权
标题翻译：箭轴
公开(公告)号：US08915806B2
公开(公告)日：2014-12-23
申请号：US13333683
申请日：2011-12-21
申请人： Richard Asherman
发明人： Richard Asherman
IPC分类号： F42B6/04 , F42B10/38
CPC分类号： F42B6/04 , F42B10/38
摘要： An arrow includes an elongate shaft, a plurality of vanes located proximate a proximal end of the shaft, and a point located proximate a distal end of the shaft. The shaft may have a dimpled outer surface. The shaft may also or alternatively have an internal supporting structure.
摘要翻译：箭头包括细长轴，位于轴的近端附近的多个叶片以及位于轴的远端附近的点。轴可以具有凹陷的外表面。轴也可以或者可选地具有内部支撑结构。

8. 发明申请

US20110290140A1 System and Method for Powered Bomb Guidance 审中-公开
标题翻译：动力炸弹指导系统和方法
公开(公告)号：US20110290140A1
公开(公告)日：2011-12-01
申请号：US12788424
申请日：2010-05-27
申请人： David G. Howard , Robert A. Bailey
发明人： David G. Howard , Robert A. Bailey
IPC分类号： F42B10/00 , F42B10/38
CPC分类号： F42B10/64 , F42B15/01
摘要： According to one embodiment, a system of powered bomb guidance includes a munition and a guidance system operable to detect a relative position of a target. The guidance system determines course corrections to direct the munition to the target and generates a control signal reflective of the course corrections. One or more explosive guidance units are disposed at one or more control surfaces disposed along an outer surface of the munition. Each explosive guidance unit is mechanically coupled to one of a plurality of control surfaces and in electrical communication with the guidance system. Each explosive guidance unit is configured to detonate in response to receiving the control signal from the guidance system and is further configured to apply force upon detonation to the control surface to which it is coupled.
摘要翻译：根据一个实施例，动力炸弹引导系统包括可操作以检测目标的相对位置的弹药和引导系统。引导系统确定课程校正以将弹药引导到目标，并产生反映课程校正的控制信号。一个或多个爆炸引导单元设置在沿着弹药的外表面设置的一个或多个控制表面上。每个爆炸引导单元机械地联接到多个控制表面之一并与引导系统电连通。每个爆炸引导单元被配置为响应于从引导系统接收到控制信号而引爆，并且还被配置成在引爆时将力施加到与其联接的控制表面。

9. 发明申请

US20050133668A1 METHODS AND APPARATUS FOR INCREASING AERODYNAMIC PERFORMANCE OF PROJECTILES 失效
标题翻译：增加项目空气动力性能的方法和装置
公开(公告)号：US20050133668A1
公开(公告)日：2005-06-23
申请号：US10833475
申请日：2004-04-26
申请人： Jahangir Rastegar , Richard Pelz
发明人： Jahangir Rastegar , Richard Pelz
IPC分类号： F42B10/14 , F42B10/38 , F42B10/40 , F42B10/42 , F42B10/44 , B64C1/38
CPC分类号： F42B10/146 , F42B10/38 , F42B10/40 , F42B10/42 , F42B10/44
摘要： A method for enhancing an aerodynamic performance of an unmanned projectile. The method including at least one of the following: (a) morphing a cross-sectional shape of the projectile after launch thereof; (b) morphing a longitudinal shape of the projectile after launch thereof; (c) bleeding a fluid at a base of the projectile during flight thereof: (d) varying a base cone angle of the projectile as a function of speed thereof; (e) deploying at least one wing from a body of the projectile after launch thereof; and (f) deploying a fin from the body of the projectile after launch thereof.
摘要翻译：一种提高无人射弹空气动力学性能的方法。该方法至少包括以下之一：（a）在发射后变形射弹的横截面形状; （b）在发射后变形射弹的纵向形状; （c）在其飞行期间在射弹的基部处流出液体：（d）作为其速度的函数改变射弹的基底锥角; （e）在发射之后，从射弹的身体部署至少一个翼; 和（f）在发射之后从射弹的身体部署翅片。

10. 发明授权

US6138945A Neural network controller for a pulsed rocket motor tactical missile system 失效
标题翻译：用于脉冲火箭发动机战术导弹系统的神经网络控制器
公开(公告)号：US6138945A
公开(公告)日：2000-10-31
申请号：US004993
申请日：1998-01-09
申请人： James E. Biggers , Kevin P. Finn , Homer H. Schwartz, II
发明人： James E. Biggers , Kevin P. Finn , Homer H. Schwartz, II
IPC分类号： F42B10/38 , F42B10/66 , F42B15/00 , F41G7/00
CPC分类号： F42B10/38 , F42B10/66 , F42B15/00
摘要： A neural network controller for a pulsed rocket motor tactical missile. The missile includes a fuselage or body, with a propulsion system. The pulsed propulsion system has a need for a logical control of the application of propulsion energy throughout the missile's flight. The controller is trained to provide optimal initiation of individual rocket motor thrust pulses based on tactical information available at various points/times in the missile's flight. The controller training is through use of training cases, in which the network learns to output a specific target value(s) when specific values are input. When trained with a large sample of training cases selected from the multidimensional population of interest, the neural network effectively learns the correlations between inputs and outputs and can predict input/output relationships not previously seen in any training case.
摘要翻译：一种用于脉冲火箭发动机战术导弹的神经网络控制器。导弹包括机身或机身，带有推进系统。脉冲推进系统需要对整个导弹飞行中推进能量的应用进行逻辑控制。根据导弹飞行中不同点/次的战术信息，对控制器进行训练，以提供单个火箭发动机推力脉冲的最佳启动。控制器培训是通过使用培训案例，当具体值被输入时，网络学习输出特定的目标值。在从多维感兴趣群体中挑选的大量培训案例进行培训时，神经网络有效地学习了输入和输出之间的相关性，并且可以预测任何培训案例中以前没有的输入/输出关系。

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