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1. 发明公开

CN106068438A 无人水下航行器的远距离输送无效
公开(公告)号：CN106068438A
公开(公告)日：2016-11-02
申请号：CN201580010769.4
申请日：2015-01-15
申请人：波音公司
发明人：凯勒·斯托尔斯
IPC分类号： F41F1/00 , F41G7/00
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 , F41F1/00 , F41G7/00
摘要：一种射弹(100)包括引导飞行中的射弹的引导组件(102、103)。射弹进一步包括壳体和中空的鼻锥体(106)。壳体与引导组件配合并且鼻锥体与壳体耦合。鼻锥体包括被配置为容纳UUV(202)的内表面。射弹进一步包括控制器(108)，其识别用于部署飞行中的UUV的条件并且响应于确定条件满足使鼻锥体从壳体脱离。

2. 发明公开

EP2646321A1 AN AIR INTAKE SYSTEM FOR AN AIR VEHICLE 审中-公开
标题翻译：进气系统用于飞机
公开(公告)号：EP2646321A1
公开(公告)日：2013-10-09
申请号：EP11785696.3
申请日：2011-11-23
申请人： MBDA UK Limited
发明人： RICHARDS, Clifford, John
IPC分类号： B64D33/02 , F02C7/04 , F42B10/32 , F42B15/10
CPC分类号： B64D33/02 , B64C2201/084 , B64D2241/00 , F02C7/042 , F05D2250/411 , F05D2250/51 , F42B10/32 , F42B15/10 , Y10T137/0536
摘要： A missile comprises a propulsion system, a passageway for delivering air to the propulsion system and a ducting element associated with the passageway. The ducting element has a ducting surface for ducting air into the passageway, and the ducting element is rotatable, about an axis that is aligned, or more preferably co-axial, with the axis of the passageway, from a stowed position in which the ducting surface is received in the passageway, to a deployed position in which the ducting surface protrudes from the passageway to duct air into the passageway.

3. 发明授权

US09157713B1 Limited range rifle projectile 有权
标题翻译：有限范围步枪射弹
公开(公告)号：US09157713B1
公开(公告)日：2015-10-13
申请号：US14213061
申请日：2014-03-14
申请人： Alliant Techsystems Inc.
发明人： Bryan P. Peterson , Joshua L. Edel , Lawrence P. Head
IPC分类号： F42B10/32 , F42B8/00 , F42B8/12 , F42B12/36
CPC分类号： F42B10/32 , F42B8/00 , F42B8/14 , F42B10/48 , F42B12/36
摘要： Ammunition comprising bullets having destabilizing mechanisms that, under ballistic phase conditions, create instability in the bullets resulting in failure of the trajectory of the bullet and/or the sustainable velocity of the bullets.
摘要翻译：弹药包括具有不稳定机制的弹头，弹道机制在弹道相位条件下造成子弹的不稳定性导致子弹轨迹的失效和/或子弹的持续速度。

4. 发明申请

US20140230684A1 CHARGED PROJECTILES AND RELATED ASSEMBLIES, SYSTEMS AND METHODS 有权
标题翻译：收费项目及相关组织，系统和方法
公开(公告)号：US20140230684A1
公开(公告)日：2014-08-21
申请号：US13789147
申请日：2013-03-07
申请人： Alliant Techsystems Inc.
发明人： Otto S. Krauss , John W. Westbrook, III
IPC分类号： F42B10/38 , 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。

5. 发明申请

US20130284279A1 AIR INTAKE SYSTEM FOR AN AIR VEHICLE 审中-公开
标题翻译：用于空气车辆的空气进气系统
公开(公告)号：US20130284279A1
公开(公告)日：2013-10-31
申请号：US13976235
申请日：2011-11-23
申请人： Clifford John Richards
发明人： Clifford John Richards
IPC分类号： B64D33/02
CPC分类号： B64D33/02 , B64C2201/084 , B64D2241/00 , F02C7/042 , F05D2250/411 , F05D2250/51 , F42B10/32 , F42B15/10 , Y10T137/0536
摘要： A missile comprises a propulsion system, a passageway for delivering air to the propulsion system and a ducting element associated with the passageway. The ducting element has a ducting surface for ducting air into the passageway, and the ducting element is rotatable, about an axis that is aligned, or more preferably co-axial, with the axis of the passageway, from a stowed position in which the ducting surface is received in the passageway, to a deployed position in which the ducting surface protrudes from the passageway to duct air into the passageway.
摘要翻译：导弹包括推进系统，用于将空气输送到推进系统的通道和与通道相关联的管道元件。管道元件具有用于将空气引导到通道中的管道表面，并且管道元件围绕与通道的轴线对准，或更优选地同轴地从收起位置旋转的管道元件，其中管道表面被容纳在通道中，到达展开位置，其中管道表面从通道突出到管道空气进入通道。

6. 发明公开

EP2203708A4 METHOD OF VARYING FIRING RANGE AND EFFECT IN TARGET FOR SHELL AND SHELL CONFIGURED FOR THIS PURPOSE 有权
标题翻译： SHOT范围变化的方法和目标效果FOR A GRENADE并且为此CONFIGURED GRENADE
公开(公告)号：EP2203708A4
公开(公告)日：2013-05-01
申请号：EP08839565
申请日：2008-10-16
申请人： BAE SYSTEMS BOFORS AB
发明人： JOHANSSON NILS
IPC分类号： F42B15/36 , F42B10/32 , F42B12/02 , F42B15/38 , F42B30/00
CPC分类号： F42B15/36 , F42B10/32

7. 发明公开

EP2460729A1 An air intake system for an air vehicle 审中-公开
标题翻译： Lufteinlasssystemfürein Luftfahrzeug
公开(公告)号：EP2460729A1
公开(公告)日：2012-06-06
申请号：EP11275081.5
申请日：2011-05-12
申请人： MBDA UK Limited
发明人： The designation of the inventor has not yet been filed
IPC分类号： B64D33/02 , F02C7/042 , F42B10/32 , F42B15/10
CPC分类号： B64D33/02 , B64C2201/084 , B64D2241/00 , F02C7/042 , F05D2250/411 , F05D2250/51 , F42B10/32 , F42B15/10 , Y10T137/0536
摘要： A missile comprises a propulsion system, a passageway (1) for delivering air to the propulsion system and a ducting element (9) associated with the passageway (1). The ducting element (9) has a ducting surface for ducting air into the passageway (1), and the ducting element (9) is rotatable, about an axis (13) that is aligned, or more preferably co-axial, with the axis (19) of the passageway (1), from a stowed position in which the ducting surface is received in the passageway (1), to a deployed position in which the ducting surface protrudes from the passageway (1) to duct air into the passageway.
摘要翻译：导弹包括推进系统，用于将空气传送到推进系统的通道（1）和与通道（1）相关联的管道元件（9）。管道元件（9）具有用于将空气引导到通道（1）中的管道表面，并且管道元件（9）可绕轴线（13）旋转，该轴线（13）与轴线（1）的管道表面被收纳在通道（1）中的收起位置处的通道（19）到管道表面从通道（1）突出到管道空气进入通道的通道位置。

8. 再颁专利

USRE47187E1 Projectile body and corresponding ammunition round for small arms or a light firearm 有权
公开(公告)号：USRE47187E1
公开(公告)日：2019-01-01
申请号：US15425458
申请日：2017-02-06
申请人： TECHVENTURE INVESTMENTS PTY LTD
发明人： Dale Harrison
IPC分类号： F42B5/10 , F42B14/02 , F42B14/00 , F42B10/44 , F42B10/38 , F42B12/02 , F42C19/08 , F42B5/18 , F42B10/32
CPC分类号： F42B14/00 , F42B5/10 , F42B10/38 , F42B10/44 , F42B12/02 , F42B14/02 , F42C19/0823 , F42B5/18 , F42B10/32
摘要： A projectile (14) for an ammunition round (10) for use with a small arms or light firearm comprises an elongated projectile body (16). The projectile body (16) has first and second axially opposed ends (18, 20) respectively and a cavity (20) extending there between. The cavity is able to hold a quantity of propellant (24). A plurality of seals (26) extend about an outer surface of the body (16). The seals (26) protrude radially from the body (16) and operate to form a substantial seal against an inner circumferential surface of a barrel (12) of the firearm. Two of the seals (26b and 26c) are mutually adjacent and spaced apart in a direction of a longitudinal axis of the body to form a seal bound outer surface portion (36) of the body (16). One or more holes (38) are formed in the body (16) enabling fluid communication between the cavity (22) and the seal bound outer surface portion (36) of the body (16). This enables pressure equalization inside and outside of the cavity (22) about the seal bound outer surface portion (36) when the projectile (14) is travelling through the barrel (12).

9. 发明授权

US09879963B2 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：US09879963B2
公开(公告)日：2018-01-30
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： G06F19/00 , F42B35/00 , F42B12/22 , F42B12/38
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.

10. 发明申请

US20160131465A1 A PROJECTILE BODY AND CORRESPONDING AMMUNITION ROUND FOR SMALL ARMS OR A LIGHT FIREARM 有权
标题翻译：小型武器或轻型火箭的弹道身体和相应的弹道导弹
公开(公告)号：US20160131465A1
公开(公告)日：2016-05-12
申请号：US14422451
申请日：2014-07-25
申请人： Techventure Investment Pty Ltd
发明人： Dale Harrison
IPC分类号： F42B14/00 , F42B12/02 , F42C19/08
CPC分类号： F42B14/00 , F42B5/10 , F42B5/18 , F42B10/32 , F42B10/38 , F42B10/44 , F42B12/02 , F42B14/02 , F42C19/0823
摘要： A projectile (14) for an ammunition round (10) for use with a small arms or light firearm comprises an elongated projectile body (16). The projectile body (16) has first and second axially opposed ends (18, 20) respectively and a cavity (20) extending there between. The cavity is able to hold a quantity of propellant (24). A plurality of seals (26) extend about an outer surface of the body (16). The seals (26) protrude radially from the body (16) and operate to form a substantial seal against an inner circumferential surface of a barrel (12) of the firearm. Two of the seals (26b and 26c) are mutually adjacent and spaced apart in a direction of a longitudinal axis of the body to form a seal bound outer surface portion (36) of the body (16). One or more holes (38) are formed in the body (16) enabling fluid communication between the cavity (22) and the seal bound outer surface portion (36) of the body (16). This enables pressure equalisation inside and outside of the cavity (22) about the seal bound outer surface portion (36) when the projectile (14) is travelling through the barrel (12).
摘要翻译：用于与小武器或轻型枪支一起使用的弹药弹（10）的弹药（14）包括细长的射弹体（16）。射弹体（16）分别具有第一和第二轴向相对的端部（18,20）和在其间延伸的空腔（20）。空腔能够容纳一定数量的推进剂（24）。多个密封件（26）围绕主体（16）的外表面延伸。密封件（26）从主体（16）径向突出并且操作以形成抵靠火器枪管（12）的内圆周表面的实质密封。两个密封件（26b和26c）相互相邻并且在主体的纵向轴线的方向上间隔开以形成主体（16）的密封结合外表面部分（36）。一个或多个孔（38）形成在主体（16）中，使得空腔（22）和主体（16）的密封结合的外表面部分（36）之间能够流体连通。这使得当抛射体（14）行进通过枪管（12）时，围绕密封结合的外表面部分（36）在空腔（22）的内部和外部压力平衡。

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