| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 用于保持和部署鸭翼的系统和方法 | CN201410032606.3 | 2014-01-23 | CN103968717A | 2014-08-06 | M.普卢默; J.吉布森; J.拜尔恩; B.理查森 |
| 本发明公开了用于将多个鸭翼和鸭翼盖保持和部署在弹丸上的系统和方法。所述弹丸包括：弹丸外壳，其界定内腔和纵轴；鸭翼，其可旋转地安装到所述外壳；鸭翼盖；筒管，其沿着所述纵轴可移动地安置在所述外壳的所述内腔中；和摇臂。所述鸭翼被安装来从收纳位置移动到部署位置。所述鸭翼盖具有钩元件，且适于覆盖形成于所述外壳中的各自的槽。所述筒管具有第一端和第二端和邻近所述第二端的保持面。摇臂具有第一臂端和第二臂端，其中鸭翼保持槽被界定于其间。所述第一臂端包括用于与所述鸭翼盖元件接合的闩锁元件，且所述第二臂端定位为邻近所述保持面。 | ||||||
| 2 | 用于保持和部署鸭翼的系统和方法 | CN201410032606.3 | 2014-01-23 | CN103968717B | 2017-06-23 | M.普卢默; J.吉布森; J.拜尔恩; B.理查森 |
| 公开了用于将多个鸭翼和鸭翼盖保持和部署在弹丸上的系统和方法。所述弹丸包括：弹丸外壳，其界定内腔和纵轴；鸭翼，其可旋转地安装到所述外壳；鸭翼盖；筒管，其沿着所述纵轴可移动地安置在所述外壳的所述内腔中；和摇臂。所述鸭翼被安装来从收纳位置移动到部署位置。所述鸭翼盖具有钩元件，且适于覆盖形成于所述外壳中的各自的槽。所述筒管具有第一端和第二端和邻近所述第二端的保持面。摇臂具有第一臂端和第二臂端，其中鸭翼保持槽被界定于其间。所述第一臂端包括用于与所述鸭翼盖元件接合的闩锁元件，且所述第二臂端定位为邻近所述保持面。 | ||||||
| 3 | 一种大质量弹丸高速撞击下弹丸弹托分离装置 | CN201610297918.6 | 2016-05-06 | CN105973078A | 2016-09-28 | 屈可朋; 沈飞; 李亮亮; 何超; 王辉; 肖玮 |
| 本发明公开了一种大质量弹丸高速撞击下弹丸弹托分离装置，包括支架、分离器、减速环、垫板、缓冲胶垫、惰性体和挡板。支架为两端带有法兰盘、内壁加工有凸台的圆筒体，支架通过法兰盘分别与炮管上的法兰盘以及挡板连接；支架内部安装有分离器、垫板、缓冲胶垫和惰性体。分离器朝向炮管的一端为圆锥形，另一端为圆柱形，且有贯通的台阶式中心通孔，分离器圆锥形一端的外圆周上套有减速环，圆柱形一端由垫板上的中心通孔定位。本发明优点在于能够承受较强的冲击载荷并可以延长反向冲击载荷作用于弹托的时间，满足大质量弹丸在高撞击速度下的弹丸弹托分离要求，有效避免弹托撞击到目标靶板造成目标靶的附加损伤，且能够重复使用。 | ||||||
| 4 | 一种适用于回转体箭体结构的组合配平方法 | CN201610207328.X | 2016-04-05 | CN105890466A | 2016-08-24 | 刘志伟; 唐颀; 张群; 杨自鹏; 王猛; 杨勇; 林宏; 彭慧莲; 张新宇; 杨虎军; 刘建忠; 杨炜平; 周佑君 |
| 一种适用于回转体箭体结构的组合配平方法，首先以任一箭体截面的圆心为坐标原点，箭体截面上任意两垂直直径为y、z轴，建立yoz坐标系，然后获取箭体质心在坐标系中的横移坐标，当横移坐标对应对接孔具备安装条件时，计算得到单一配平块质量，当横移坐标对应对接孔不具备安装条件时，计算得到分布的配平块质量，最后将配平砝码进行组合得到对应质量及数量的配平块，并利用紧固件紧固，完成质心配平。本发明配平方法通过利用回转体箭体环形框上的一个或者多个对接孔安装紧固配平块，克服了现有技术需要在箭体结构上额外开孔或者预留安装孔的缺陷，保证了箭体的产品质量，具有较好的配平效率和适应性。 | ||||||
| 5 | 格納状態にあるミサイルの折畳み翼を保護するための方法およびシステム | JP2017524416 | 2014-11-07 | JP6423531B2 | 2018-11-14 | ソールベルグ,アンシュタイン; イェストヴァング,イェンス,アー.; スレーヴェランド,トロン,ヘンニング; イェンスルード,クリスティアン; ホーイルセーテル,イーヴァル,トムレ |
| 6 | 格納状態にあるミサイルの折畳み翼を保護するための方法およびシステム | JP2017524416 | 2014-11-07 | JP2017534042A | 2017-11-16 | ソールベルグ，アンシュタイン; イェストヴァング，イェンス，アー．; スレーヴェランド，トロン，ヘンニング; イェンスルード，クリスティアン; ホーイルセーテル，イーヴァル，トムレ |
| 格納した翼を持ちそれを搬送する運搬体に接続されたミサイル(15)を保護するためのカバー(10)および方法。カバー(10)は、ミサイル(15)の翼(20)とミサイル(15)の胴体との間の間隙を覆い空気力学的な力を最小化するための、スポイラー形状の前部(25)を含む。 | ||||||
| 7 | Rotational control actuation system for guiding projectiles | US12942995 | 2010-11-09 | US09939238B1 | 2018-04-10 | Zak Sowle; Srikanth Vasudevan; Matthew C. Birch |
| A projectile incorporates one or more spoiler-tabbed spinning disks to effect flow around the projectile and thus impart steering forces and/or moments. The spoiler tabs may be deployed only during steering phases of travel thus minimizing the drag penalty associated with steering systems. The disks are driven by motors and informed and controlled by sensors and electronic control systems. The spoiler tabs protrude through the surface of the projectile only for certain angles of spin of the spinning disk. For spin-stabilized projectiles, the disks spin at substantially the same rate as the projectile, but the disks may function in fin-stabilized projectiles as well. Any number of such spinning flow effector disks may be incorporated in a projectile, with the manner of functional coordination differing slightly for even and odd numbers of disks. | ||||||
| 8 | 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 | US15200023 | 2016-07-01 | US09879963B2 | 2018-01-30 | Kevin Michael Sullivan |
| 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. | ||||||
| 9 | Less than lethal cartridge | US13472198 | 2012-05-15 | US09021959B2 | 2015-05-05 | John Hayes |
| A less than lethal cartridge for a projectile which when fired has a velocity which will not kill an individual struck by the projectile. The less than lethal cartridge has a rim which is deeper or thicker than a rim on a conventional lethal cartridge. The caliber of the cartridge is also selected so that regular lethal ammunition is not available in this caliber. The preferred caliber of the less than lethal cartridge is .490. The less than lethal cartridge contains a polymeric projectile or alternatively, a sealed filled polymeric pouch containing shot therein. | ||||||
| 10 | Multiple cartridge assembly for less than lethal cartridge | US13651870 | 2012-10-15 | US20130111797A1 | 2013-05-09 | John Hayes |
| A multiple cartridge assembly is described which facilitates speed loading of a four barrel less than lethal gun. Four less than lethal cartridges are attached to the multiple cartridge assembly and arranged to correspond with the breech of a four barrel less than lethal gun. Each less than lethal cartridge is constructed with a projectile which when fired has a velocity which will not kill an individual struck by the projectile. The less than lethal cartridge has a rim which is deeper or thicker than a rim on a conventional lethal cartridge. The caliber of the cartridge is also selected so that regular lethal ammunition is not available in this caliber. The preferred caliber of the less than lethal cartridge is 0.490. The less than lethal cartridge contains a polymeric projectile or alternatively, a sealed filled polymeric pouch containing shot therein. | ||||||
| 11 | Telescoped projectile | US11204575 | 2005-08-16 | US07380504B2 | 2008-06-03 | Richard Dryer |
| A projectile reconfigures in flight from a launch configuration, in which the center of gravity is aft of the center of pressure, to a flight configuration, in which the center of gravity is forward of the center of pressure. The projectile includes a forward portion and an aft portion, and the reconfiguration involves movement of at least part of one of the portions relative to the other portion. The projectile may have an overall substantially conical shape when in the launch configuration. The forward portion may include a substantially conical nose, and a cylindrical central body attached to the nose. In the launch configuration, at least part of the central body may be located within a hollow in a base of the aft portion. The base may be slidable relative to the central body. | ||||||
| 12 | borchardt | US258528D | US258528A | 1882-05-23 | ||
| 13 | Improvement in bullet-patching machines | US159748D | US159748A | 1875-02-16 | ||
| 14 | Archery arrow having improved flight characteristics | US15181326 | 2016-06-13 | US09644927B2 | 2017-05-09 | Martin Connolly |
| The archery arrow having improved flight characteristics of the present invention is designed to improve the accuracy of the arrow which is equipped with a dampening medium within the central bore of the arrow shaft. The dampening materials in an embodiment may include, but not be limited to, silicon, epoxies or urethanes and selection of various dampening materials may provide for varying degrees of stiffness. The dampening effects of internal dampening materials decrease the initial deflection distance of the arrow and also serves to decrease the deflection with each oscillation. In addition, the dampening medium adopted in the present invention provides for an arrow having a selectable center of gravity location that has improved flight characteristics. Thus, the dampening materials adopted in the present invention provide for a selected location of center of gravity and a desired attnuation of oscillations. | ||||||
| 15 | ARCHERY ARROW HAVING IMPROVED FLIGHT CHARACTERISTICS | US15181326 | 2016-06-13 | US20170023340A1 | 2017-01-26 | Martin Connolly |
| The archery arrow having improved flight characteristics of the present invention is designed to improve the accuracy of the arrow which is equipped with a dampening medium within the central bore of the arrow shaft. The dampening materials in an embodiment may include, but not be limited to, silicon, epoxies or urethanes and selection of various dampening materials may provide for varying degrees of stiffness. The dampening effects of internal dampening materials decrease the initial deflection distance of the arrow and also serves to decrease the deflection with each oscillation. In addition, the dampening medium adopted in the present invention provides for an arrow having a selectable center of gravity location that has improved flight characteristics. Thus, the dampening materials adopted in the present invention provide for a selected location of center of gravity and a desired attnuation of oscillations. | ||||||
| 16 | Modular adjustable weight arrow tip | US14803593 | 2015-07-20 | US09494394B1 | 2016-11-15 | Thomas Andrew Addleman |
| A modular, adjustable weight arrow tip is disclosed. The arrow tip has a body and one or more blades in various configurations. The arrow tip utilizes one more modular weights, preferably seated between the body rear end and the arrow shaft, to allow the user to be able to selectably adjust an incrementally stepped array of weights to achieve the desired flight and “front of center” for their application. The modular weights can be threaded or unthreaded, can utilize a modular weight seating collar, can have varying weights, and may be utilized with any type of archery tip. | ||||||
| 17 | Multiple cartridge assembly for less than lethal cartridge | US13651870 | 2012-10-15 | US09103613B2 | 2015-08-11 | John Hayes |
| A multiple cartridge assembly is described which facilitates speed loading of a four barrel less than lethal gun. Four less than lethal cartridges are attached to the multiple cartridge assembly and arranged to correspond with the breech of a four barrel less than lethal gun. Each less than lethal cartridge is constructed with a projectile which when fired has a velocity which will not kill an individual struck by the projectile. The less than lethal cartridge has a rim which is deeper or thicker than a rim on a conventional lethal cartridge. The caliber of the cartridge is also selected so that regular lethal ammunition is not available in this caliber. The preferred caliber of the less than lethal cartridge is 0.490. The less than lethal cartridge contains a polymeric projectile or alternatively, a sealed filled polymeric pouch containing shot therein. | ||||||
| 18 | Modular adjustable weight arrow tip | US14170815 | 2014-02-03 | US09097500B1 | 2015-08-04 | Thomas Andrew Addleman |
| A modular, adjustable weight arrow tip is disclosed. The arrow tip has a body and one or more blades in various configurations. The arrow tip utilizes one more modular weights, preferably seated between the body rear end and the arrow shaft, to allow the user to be able to selectably adjust an incrementally stepped array of weights to achieve the desired flight and “front of center” for their application. The modular weights can be threaded or unthreaded, can utilize a modular weight seating collar, can have varying weights, and may be utilized with any type of archery tip. | ||||||
| 19 | Systems and methods for retaining and deploying canards | US13748250 | 2013-01-23 | US09012825B2 | 2015-04-21 | Matt Plumer; Jeff Gibson; Jim Byrne; Brian Richardson |
| Disclosed are systems and methods for retaining and deploying a plurality of canards and canard covers on a projectile. The projectile includes a projectile housing defining an interior chamber and a longitudinal axis, canards rotatably mounted to the housing, canard covers, a bobbin movably disposed in the interior chamber of the housing along the longitudinal axis, and rocker arms. The canards mounted for movement from a stowed position to a deployed position. The canard covers have a hook element and are adapted to cover respective slots formed in the housing. The bobbin has first and second ends and a retaining surface proximate the second end. Rocker arms have a first and second arm end, with a canard retaining slot defined therebetween. The first arm end includes a latch element for engaging with the canard cover element, and the second arm end is positioned proximate the retaining surface. | ||||||
| 20 | Archery Arrow Having Improved Flight Characteristics | US14531063 | 2014-11-03 | US20150051030A1 | 2015-02-19 | Martin Connolly |
| The archery arrow having improved flight characteristics of the present invention is designed to improve the accuracy of the arrow which is equipped with a dampening medium within the central bore of the arrow shaft. The dampening materials in an embodiment may include, but not be limited to, silicon, epoxies or urethanes and selection of various dampening materials may provide for varying degrees of stiffness. The dampening effects of internal dampening materials decrease the initial deflection distance of the arrow and also serves to decrease the deflection with each oscillation. In addition, the dampening medium adopted in the present invention provides for an arrow having a selectable center of gravity location that has improved flight characteristics. Thus, the dampening materials adopted in the present invention provide for a selected location of center of gravity and a desired attenuation of oscillations. | ||||||
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