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71. 发明申请

US20120216700A1 TIPPED PROJECTILES 有权
标题翻译：拖鞋项目
公开(公告)号：US20120216700A1
公开(公告)日：2012-08-30
申请号：US12199306
申请日：2008-08-27
申请人： Gregory A. Dennison
发明人： Gregory A. Dennison
IPC分类号： F42B12/78 , F42B10/02
CPC分类号： F42B10/46 , F42B10/02 , F42B10/42
摘要： A projectile is provided with a projectile tip having enhanced aerodynamic properties to improve accuracy of the projectile. The tip has a body having a base or lower end, an upper end and a curved, side wall between its upper and lower ends that defines an ogive tip length. The tip is received with a projectile jacket and also can have a series of aerodynamic features formed in its body to modify air flow about the body of the projectile in flight.
摘要翻译：射弹提供了具有增强的空气动力特性的抛射尖，以提高射弹的精度。尖端具有在其上端和下端之间具有底部或下端，上端和弯曲的侧壁的主体，其限定了尖端长度。尖端接收有射弹护套，并且还可以具有在其身体中形成的一系列空气动力学特征，以改变飞行中的射弹身体周围的气流。

72. 发明申请

US20120211592A1 MULTI-CALIBER FUZE KIT AND METHODS FOR SAME 有权
标题翻译：多校准FUZE套件及其方法
公开(公告)号：US20120211592A1
公开(公告)日：2012-08-23
申请号：US12469443
申请日：2009-05-20
申请人： Chris E. Geswender , Cesar Sanchez , Matthew A. Zamora
发明人： Chris E. Geswender , Cesar Sanchez , Matthew A. Zamora
IPC分类号： F42B15/01
CPC分类号： F42C19/02 , F42B10/02 , F42B10/04 , F42B10/64 , F42C19/00
摘要： A multi-caliber fuze kit includes a fuze housing configured for coupling with multiple projectiles. One or more canards are moveably coupled with the fuze housing. The one or more canards are adjustable between two or more canard configurations. In a first canard configuration, the one or more canards are at a first canard angle relative to a bore sight of the fuze housing, and the first canard angle is configured for use with a first projectile. In a second canard configuration, the one or more canards are at a second canard angle relative to the bore sight of the fuze housing, and the second canard angle is configured for use with a second projectile. The first and second canard angles are different. In another example, in the first canard configuration the one or more canards include a first canard shape configured to provide a first specified trajectory with the first projectile. In the second canard configuration the one or more canards include a second canard shape configured to provide a second specified trajectory with the second projectile. The first canard shape and the second canard shape are different.
摘要翻译：多口引信套件包括配置为与多个射弹耦合的引信外壳。一个或多个挡板与引信壳体可移动地联接。一个或多个挡板可以在两个或多个挡板配置之间调节。在第一个鸭子配置中，一个或多个胡须相对于引信壳体的孔眼位置处于第一个坎角，并且第一坎德角配置为与第一弹丸一起使用。在第二个鸭子结构中，一个或多个挡块相对于引信壳体的孔眼位置处于第二个角度，并且第二挡板角配置为与第二弹丸一起使用。第一和第二个角度是不同的。在另一个示例中，在第一坎达配置中，一个或多个挡块包括被配置为向第一弹丸提供第一指定轨迹的第一坎形形状。在第二个鸭子配置中，一个或多个小猫包括被配置为向第二弹丸提供第二指定轨迹的第二坎形。第一个鸭子形状和第二个鸭子形状是不同的。

73. 发明授权

US07750275B2 Folding control surface assembly and vehicle incorporating same 有权
标题翻译：折叠控制面组装和结合相同的车辆
公开(公告)号：US07750275B2
公开(公告)日：2010-07-06
申请号：US11474029
申请日：2006-06-23
申请人： Mark A. Turner
发明人： Mark A. Turner
IPC分类号： F42B15/01
CPC分类号： F42B10/14 , F42B10/02
摘要： A folding control surface assembly includes a torsion shaft, a base, and a control surface hingedly attached to the base via the torsion shaft, such that the torsion shaft biases the control surface toward an unfolded configuration with respect to the base. A vehicle includes a body and at least one folding control surface assembly. The at least one folding control surface assembly includes a torsion shaft, a base attached to the body, and a control surface hingedly attached to the base via the torsion shaft, such that the torsion shaft biases the control surface toward an unfolded configuration with respect to the base.
摘要翻译：折叠控制表面组件包括扭转轴，基座和通过扭转轴铰接地连接到基座的控制表面，使得扭转轴将控制表面朝向相对于基座的展开构造偏置。车辆包括主体和至少一个折叠控制表面组件。所述至少一个折叠控制表面组件包括扭转轴，附接到所述主体的基座以及通过所述扭转轴铰接地连接到所述基座的控制表面，使得所述扭转轴将所述控制表面朝向相对于的基地。

74. 发明授权

US07428871B2 Pellet for pneumatic and spring-piston operated weapons 失效
标题翻译：用于气动和弹簧活塞操作的武器的颗粒
公开(公告)号：US07428871B2
公开(公告)日：2008-09-30
申请号：US11483579
申请日：2006-07-10
申请人： L. Carl Dodson , David Phillips
发明人： L. Carl Dodson , David Phillips
IPC分类号： F42B10/00
CPC分类号： F42B6/10 , F42B10/02
摘要： A pellet for at least one of a compressed gas and spring operated weapon includes a forward head portion and a cylindrical rearward tail portion which is disposed about a common centerline with the head portion and which has an air pocket formed therein. A frustoconical middle portion connects the tail portion to the head portion. The pellet design is adaptable for use with various commonly available caliber weapons.
摘要翻译：用于压缩气体和弹簧操作的武器中的至少一个的颗粒包括前头部分和圆柱形后尾部分，其围绕与头部部分共同的中心线设置并且具有形成在其中的气穴。截头圆锥形的中间部分将尾部连接到头部。颗粒设计适用于各种常用的口径武器。

75. 发明申请

US20080148986A1 Kinetic energy penetrator and method of using same 有权
公开(公告)号：US20080148986A1
公开(公告)日：2008-06-26
申请号：US11231679
申请日：2005-09-21
申请人： Mark A. Turner , William R. Greisser
发明人： Mark A. Turner , William R. Greisser
IPC分类号： F42B30/00
CPC分类号： F42B12/06 , F42B5/045 , F42B10/02 , F42B10/38
摘要： A kinetic energy penetrator includes a plurality of penetrator segments, a penetrator segment sleeve for storing the plurality of penetrator segments, and means for moving the plurality of penetrator segments from the penetrator segment sleeve to locations substantially aligned along an axis of attack. A method includes storing a plurality of penetrator segments away from an axis of attack and moving the plurality of penetrator segments to locations substantially aligned along the axis of attack. A vehicle includes a body and a kinetic energy penetrator disposed in a forward portion of the vehicle. The kinetic energy penetrator includes a plurality of penetrator segments, a penetrator segment sleeve for storing the plurality of penetrator segments, and means for moving the plurality of penetrator segments from the penetrator segment sleeve to locations substantially aligned along an axis of attack.

76. 发明申请

US20060096492A1 Ring airfoil style paintball and launcher 失效
公开(公告)号：US20060096492A1
公开(公告)日：2006-05-11
申请号：US11271052
申请日：2005-11-09
申请人： Abraham Flatau , Chester Vanek
发明人： Abraham Flatau , Chester Vanek
IPC分类号： F42B14/06
CPC分类号： F41B11/62 , F42B6/10 , F42B10/02 , F42B10/36 , F42B12/40
摘要： A ring airfoil style paintball comprises a ring airfoil carrying a visible marking agent. The marking agent is located in one more compartments in a nose portion of a body of the ring airfoil, or within one or more containers located in those compartments. The nose portion of the body of the airfoil is configured to rupture upon impacting a target, releasing the marking agent into contact with the target. Cartridges comprising a sabot containing the ring airfoil style paintball are launched from a launcher. The launcher includes a magazine for sequentially delivering cartridges for launch. A stripper associated with the launcher strips the sabot from the ring airfoil paintball, and an ejector ejects the stripped sabot from the launcher.

77. 发明授权

US06983700B1 Variable drag projectile stabilizer for limiting the flight range of a training projectile 失效
标题翻译：用于限制训练射弹的飞行范围的可变阻力弹丸稳定器
公开(公告)号：US06983700B1
公开(公告)日：2006-01-10
申请号：US10709401
申请日：2004-05-03
申请人： Gregory Malejko , Anthony Vella , Eric P. Scheper , Philip M. Donadio
发明人： Gregory Malejko , Anthony Vella , Eric P. Scheper , Philip M. Donadio
IPC分类号： F42B8/00
CPC分类号： F42B10/48 , F42B10/02
摘要： A variable drag projectile stabilizer is utilized by a training projectile to match the trajectory of a tactical projectile for up to 3 km while having a range limitation of 8 km. The stabilizer applies supersonic flow phenomena to alter the aerodynamic characteristics of a training projectile while in free flight to fulfill this requirement. The stabilizer uses a cowling supported by struts to provide tail lift and ensure a stable flight path. Supersonic flow is established through ducts formed by the cowling and struts when launched from a weapon. The flow remains supersonic until the projectile reaches the desired range but then quickly becomes subsonic (choked) due to shock waves emanating from interior angles in the ducts. The geometry of the ducts can be designed to create different shock wave patterns within the ducts. The variance of leading edge location, leading edge angle, cowling intake angle, and flight Mach number influences the shock patterns within the ducts and consequently, the range of the projectile.
摘要翻译：训练射弹使用可变拖弹弹稳定器，将战术射弹的轨迹与距离限制为8公里相距3公里。稳定器采用超音速流动现象来改变训练射弹的空气动力特性，同时在自由飞行中满足这一要求。稳定器使用由支柱支撑的整流罩来提供尾部提升，并确保稳定的飞行路径。超音速流动通过从武器发射时由罩和支柱形成的管道建立。流体保持超音速，直到弹丸达到所需的范围，然后由于管道内角发出的冲击波，迅速变为亚音速（窒息）。管道的几何形状可以设计成在管道内产生不同的冲击波形图案。前缘位置，前缘角，整流罩角度和飞行马赫数的变化影响管道内的冲击模式，从而影响射弹的射程。

78. 发明授权

US06968785B2 Locking and stabilizing device for grenades 失效
公开(公告)号：US06968785B2
公开(公告)日：2005-11-29
申请号：US10666824
申请日：2003-09-22
申请人： Lamar M. Auman , Douglas J. Love , Brad L. Bachelor
发明人： Lamar M. Auman , Douglas J. Love , Brad L. Bachelor
IPC分类号： F42B10/02 , F42C15/23 , F42B10/56 , F42C15/184
CPC分类号： F42B10/02
摘要： The locking and stabilizing device for grenades utilizes a solid nylon ring and multiple nylon ribbons that are attached to the ring at regular intervals around its circumference. During storage, the ring surrounds and locks the slider of the grenade in its storage position. But upon deployment, under aerodynamic forces the ring moves away from the slider, releasing the slider. When the slider is thusly released, it slides out and brings the detonator in place to be impacted upon by the pin when the grenade hits the target, thus detonating the grenade. The multiple ribbons extending from the ring unfurl due to the aerodynamic forces and provide stability to the grenade flight.

79. 发明授权

US06862996B2 Projectile for rapid fire gun 失效
标题翻译：射弹快速火炮
公开(公告)号：US06862996B2
公开(公告)日：2005-03-08
申请号：US10270812
申请日：2002-10-15
申请人： Mark Key
发明人： Mark Key
IPC分类号： F42B5/03 , F42B5/18 , F42B5/184 , F42B10/02 , F42B10/44 , F42B10/46 , F42B10/00 , F42B10/32 , F42B30/02
CPC分类号： F42B10/46 , F42B5/035 , F42B5/18 , F42B10/02 , F42B10/44
摘要： An ammunition system for a rapid fire gun. The ammunition system includes a bullet having a tip that is stored in a retracted position and during flight is deployed create an aerodynamic shape. Another aspect of the ammunition system is that the bullet has a cylindrical body having a first length in storage and a second longer length after ignition of the propellant.
摘要翻译：用于快速消防枪的弹药系统。弹药系统包括一个子弹，其具有存储在缩回位置并且在飞行期间被部署的尖端产生空气动力学形状。弹药系统的另一个方面是子弹具有一个具有第一长度在储存中的圆柱体，并且在该推进剂着火之后的第二个更长的长度。

80. 发明申请

US20040069173A1 Projectile for rapid fire gun 失效
标题翻译：射弹快速火炮
公开(公告)号：US20040069173A1
公开(公告)日：2004-04-15
申请号：US10270812
申请日：2002-10-15
发明人： Mark Key
IPC分类号： F42B005/18
CPC分类号： F42B10/46 , F42B5/035 , F42B5/18 , F42B10/02 , F42B10/44
摘要： An ammunition system for a rapid fire gun. The ammunition system includes a bullet having a tip that is stored in a retracted position and during flight is deployed to create an aerodynamic shape. Another aspect of the ammunition system is that the bullet has a cylindrical body having a first length in storage and a second longer length after ignition of the propellant.
摘要翻译：用于快速消防枪的弹药系统。弹药系统包括具有尖端的子弹，该尖端存储在缩回位置并且在飞行期间被部署以产生空气动力学形状。弹药系统的另一个方面是子弹具有一个具有第一长度在储存中的圆柱体，并且在该推进剂着火之后的第二个更长的长度。

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