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11. 发明申请

US20230053512A1 TESTING AND DATA TRANSFER TO ARTILLERY GUIDING KITS 有权
公开(公告)号：US20230053512A1
公开(公告)日：2023-02-23
申请号：US17889435
申请日：2022-08-17
申请人： ELBIT SYSTEMS - ROKAR LTD
发明人： Gil WURZEL , Assaf Malul
IPC分类号： F42B10/04 , F42B15/01
摘要： Projectile guiding assemblies, caps and methods of delivering power for testing and optionally data over spring-mounted fin(s) of the guiding assembly are provided. The guiding assemblies are configured to have continuous electrically conductive path(s) from the fin(s), through the respective spring(s) on which the fin(s) are mounted, and into the electronics module, which may receive power for testing and guiding data from external source(s) over the electrically conductive path(s). In the testing state, cap mechanically secures the fin(s) to contact(s) thereupon to assure continuous power and data transfer, sparing surface area that was previously dedicated to power and data transfer and simplifying these processes, especially under field conditions.

12. 发明授权

US11143493B2 Ammunition cartridge 有权
公开(公告)号：US11143493B2
公开(公告)日：2021-10-12
申请号：US16769470
申请日：2018-12-04
申请人： Albert Gaide
发明人： Albert Gaide
IPC分类号： F42B5/16 , F42B5/10 , F42B5/285 , F42B10/04 , F42C19/08
摘要： Ammunition cartridge comprising a rigid casing including a tubular sleeve and a base closing an end of the casing, a projectile mounted at another end of the casing, a propellant charge contained inside the casing, and an ignition device. The ignition device comprises an ignition charge arranged to ignite the propellant charge at a point of ignition distal from the base and proximal the projectile.

13. 发明授权

US10845170B2 Morris 80 plastic tour bolt 有权
公开(公告)号：US10845170B2
公开(公告)日：2020-11-24
申请号：US16299353
申请日：2019-03-12
申请人： Elgie Allen Morris
发明人： Elgie Allen Morris
IPC分类号： F42B6/06 , F42B10/04 , F42B6/04
CPC分类号： F42B6/06 , F42B6/04 , F42B10/04
摘要： When combined with a metal point, this ten inch plastic pistol crossbow bolt is designed to extend past the barrel of a pistol crossbow so it can be used for recreational shooting, competition shooting, small game hunting, pistol crossbow fishing and pistol crossbow scuba fishing. The main fault of the standard pistol crossbow bolt is they are less than seven inches in length and do not extend past the end of a pistol crossbow barrel. Therefore, their use is limited to target points and recreational shooting only. Other faults of the standard short pistol crossbow bolts are their high travel speed. They are very difficult to be viewed in flight, causing most bolts to be lost after one use. Also, their irretrievability from any commonly used target. Therefore, they cannot be found and scored in any type of shooting competition. This ten inch bolt is a solid one piece unit made of a strong but, light weight plastic compound. It has a NOCK to securely hold the bow string in place. Most bolts do not have a nock. it has two FLAT WINGS for elevation stabilizing which creates an accurate and stable bolt flight. No other bolt has this type of flat wings. These features allow this bolt to be easily viewed in flight. This also allows this bolt to be used for competition shooting because these bolts can be easily located, scored and then retrieved from any type competition target. The shaft has a THREADED TIP to accept almost any type metal point.

14. 发明授权

US09587923B2 Low cost guiding device for projectile and method of operation 有权
标题翻译：射弹使用成本低的导向装置及操作方法
公开(公告)号：US09587923B2
公开(公告)日：2017-03-07
申请号：US15057215
申请日：2016-03-01
申请人： BAE SYSTEMS ROKAR INTERNATIONAL LTD
发明人： Gil Wurzel , Assaf Malul
IPC分类号： F42B10/06 , F42B15/01 , F42B10/64 , F42B10/04 , F42B10/26 , F42B15/10
CPC分类号： F42B15/01 , F42B10/04 , F42B10/26 , F42B10/64 , F42B15/10
摘要： A guiding assembly is adapted to be connected to a projectile and comprising a rear main unit adapted to be connected to the front end of the projectile, and a front main unit rotatably connected at its rear end to the front end of the rear main unit. The front main unit is adapted to rotate about a central longitudinal axis. A relative speed control unit is operable between the rear main unit and the front main unit and capable of providing spin braking force to slow the relative speed of rotation of the front main unit. An at least one guiding fin radially extends from the front main unit. The pitch angle of the fin is controllable by a return spring connected to the fin so that the pitch angle of the fin is growing as the aerodynamic pressure on the fin lowers and it is growing smaller as the aerodynamic pressure on the fin gets bigger.
摘要翻译：引导组件适于连接到射弹，并且包括适于连接到射弹前端的后主单元，以及在其后端可转动地连接到后主体前端的前主单元。前主体适于围绕中心纵向轴线旋转。相对速度控制单元可在后主单元和前主单元之间操作并且能够提供旋转制动力以减慢前主单元的相对旋转速度。至少一个引导翅片从前主单元径向延伸。翅片的俯仰角可以通过连接到翅片的复位弹簧来控制，使得当翅片上的空气动力压力降低时翅片的俯仰角度增加，并且随着翅片上的空气动力学压力变大，翅片的俯仰角变小。

15. 发明授权

US08499694B2 Two-fin stackable flechette having two-piece construction 失效
标题翻译：两片可堆叠式收割机具有两件式结构
公开(公告)号：US08499694B2
公开(公告)日：2013-08-06
申请号：US13249719
申请日：2011-09-30
申请人： David A. Bittle , Robert V. Weber , Julian L. Cothran
发明人： David A. Bittle , Robert V. Weber , Julian L. Cothran
IPC分类号： F42B10/04 , F42B12/02
CPC分类号： F42B12/362 , F42B6/003 , F42B10/08 , F42B39/007
摘要： A flechette has a forward body (20) containing its center of gravity which is connected to a tail section (24). The tail section has a pair of fins (24A, 24B) each having a preselected longitudinal angle and radial angle. When the two fins are viewed from the aft of the flechette, the pair of fins demonstrate a S-shaped orientation. The size, shape and orientation of the pair of fins provide aerodynamic stability to the flechette while allowing the flechette to be stacked with like-shaped flechettes. The two-piece assembly of the flechette easily accommodates the use of different density materials for the respective pieces.
摘要翻译：指示器具有包含其重心的前身（20），其连接到尾部（24）。尾部具有一对翅片（24A，24B），每个翼片具有预选的纵向角度和径向角度。当从收割机的后部观察两个翅片时，该对翅片呈现S形取向。一对翅片的尺寸，形状和方向为收割机提供空气动力学稳定性，同时允许卷帘纸以类似形状的薄膜堆叠。收割机的两件式组件可以容易地适应各种不同密度材料的使用。

16. 发明授权

US08375860B2 Stackable, easily packaged and aerodynamically stable flechette 失效
标题翻译：可堆叠，易于包装和空气动力学稳定的薄膜
公开(公告)号：US08375860B2
公开(公告)日：2013-02-19
申请号：US13101018
申请日：2011-05-04
申请人： David A. Bittle , Robert V. Weber , Julian L. Cothran
发明人： David A. Bittle , Robert V. Weber , Julian L. Cothran
IPC分类号： F42B10/04 , F42B12/02
CPC分类号： F42B12/362 , F42B10/08
摘要： A flechette has a forward section or body (12) containing its center of gravity. A quill (10) is connected to the forward section and is integrally connected to a pair of fins (15A, 15B) each having a longitudinal angle and a radial angle. When the two fins are viewed from the aft of the flechette, the pair of fins demonstrate an S-shaped orientation. The size, shape and orientation of the fins provide aerodynamic stability to the flechette while allowing the flechette to be stacked with like-shaped flechettes in rows and columns or in a radial, circular arrangement. When stacked in rows and columns or in a circular arrangement, each flechette has its nose oriented in the same forward direction.
摘要翻译：指示器具有包含其重心的前部或主体（12）。羽毛笔（10）连接到前部，并且一体地连接到每个具有纵向角度和径向角度的一对翅片（15A，15B）。当从收割机的后部观察两个翅片时，该对翅片呈现S形取向。散热片的尺寸，形状和方向为收割机提供空气动力学稳定性，同时允许收割机以行和列或径向圆形布置堆叠有类似形状的收敛片。当以行和列或圆形布置的方式堆叠时，每个收割机的鼻子朝向相同的向前方向。

17. 发明申请

US20120199034A1 Aerodynamic projectile 有权
标题翻译：气动弹丸
公开(公告)号：US20120199034A1
公开(公告)日：2012-08-09
申请号：US12317868
申请日：2008-12-29
申请人： Gary E. Gibson , Michael A. Varacins
发明人： Gary E. Gibson , Michael A. Varacins
IPC分类号： F42B12/40 , F42B12/72 , F42B10/04
CPC分类号： F42B10/06 , F42B12/40
摘要： An aerodynamic projectile is provided having a shell with an aerodynamic structure and a controlled center of gravity, and which exhibits improved aerodynamics and resulting accuracy, and which is suitable for less lethal uses. The projectile shell has a closed front cavity housing a payload, such as a marking agent, therein. The projectile shell also has an open rear portion to provide access to the open rear cavity, and to decrease the weight of the projectile and appropriately locate the center of gravity. The projectile shell also includes a plurality of fins on a sidewall member to enhance the accuracy of the projectile.
摘要翻译：提供了具有空气动力学结构和受控重心的外壳的空气动力学抛射体，其具有改善的空气动力学和所得精度，并且适用于较少致命的用途。抛射体壳体具有封闭的前腔，其中容纳有效载荷，例如标记剂。抛射体壳体还具有敞开的后部部分，以提供进入开放的后腔，并且减少弹丸的重量并适当地定位重心。抛射体壳体还包括在侧壁构件上的多个翅片以增强射弹的精度。

18. 发明申请

US20110272518A1 Stackable, Easily Packaged and Aerodynamically Stable Flechette 失效
标题翻译：可堆叠，易于包装和空气动力学稳定的指南针
公开(公告)号：US20110272518A1
公开(公告)日：2011-11-10
申请号：US13101018
申请日：2011-05-04
申请人： David A. Bittle , Robert V. Weber , Julian L. Cothran
发明人： David A. Bittle , Robert V. Weber , Julian L. Cothran
IPC分类号： F42B10/04 , F42B12/02
CPC分类号： F42B12/362 , F42B10/08
摘要： A flechette has a forward section or body (12) containing its center of gravity. A quill (10) is connected to the forward section and is integrally connected to a pair of fins (15A, 15B) each having a longitudinal angle and a radial angle. When the two fins are viewed from the aft of the flechette, the pair of fins demonstrate an S-shaped orientation. The size, shape and orientation of the fins provide aerodynamic stability to the flechette while allowing the flechette to be stacked with like-shaped flechettes in rows and columns or in a radial, circular arrangement. When stacked in rows and columns or in a circular arrangement, each flechette has its nose oriented in the same forward direction.
摘要翻译：指示器具有包含其重心的前部或主体（12）。羽毛笔（10）连接到前部，并且一体地连接到每个具有纵向角度和径向角度的一对翅片（15A，15B）。当从收割机的后部观察两个翅片时，该对翅片呈现S形取向。散热片的尺寸，形状和方向为收割机提供空气动力学稳定性，同时允许收割机以行和列或径向圆形布置堆叠有类似形状的收敛片。当以行和列或圆形布置的方式堆叠时，每个收割机的鼻子朝向相同的向前方向。

19. 发明授权

US5518567A Process for the production of a composite material part constituted by a central body and ailerons 失效
标题翻译：用于生产由中心体和副翼构成的复合材料部件的方法
公开(公告)号：US5518567A
公开(公告)日：1996-05-21
申请号：US265725
申请日：1994-06-24
申请人： Jacques Fages
发明人： Jacques Fages
IPC分类号： F42B15/00 , B29C53/58 , B29C69/00 , B29C70/06 , B29C70/30 , B29C70/54 , B29D99/00 , F42B10/06 , B32B5/00 , B65H81/00 , F42B10/04
CPC分类号： F42B10/06 , B29C69/003 , B29C70/30 , B29C70/545 , B29C53/58 , Y02T50/433
摘要： A process for producing a composite material part having a central hollow body with edge ailerons extending outwardly therefrom in which peripheral mandrels 1 are joined and a peripheral mandrels 1 then being turned round and pressed against a central mandrel 16 on which another filament has been wound. The filaments are impregnated and polymerized to form the desired part.
摘要翻译：一种制造复合材料部件的方法，所述复合材料部件具有中心空心体，所述中空中空体具有从其向外延伸的边缘副翼，其中周向心轴1连接在一起，并且周向心轴1然后被转动并压靠在其上缠绕另一个细丝的中心心轴16上。将长丝浸渍并聚合以形成所需的部分。

20. 发明公开

US20240310155A1 PROJECTILE 审中-公开
公开(公告)号：US20240310155A1
公开(公告)日：2024-09-19
申请号：US18574011
申请日：2022-06-25
申请人： BAE SYSTEMS BOFORS AB
发明人： Fredrik THUVANDER , David MALMSTRÖM
IPC分类号： F42B14/06 , F42B10/04 , F42B27/00
CPC分类号： F42B14/06 , F42B10/04 , F42B27/00
摘要： A projectile for launching from a launching device with a propellant charge in a barrel is arranged with a cross-section in the shape of a curve of constant width.

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