专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US6123289A Training projectile 失效
标题翻译：训练射弹
公开(公告)号：US6123289A
公开(公告)日：2000-09-26
申请号：US71453
申请日：1998-04-20
申请人： Leon Manole , William Rice , Stewart Gilman , John Dineen , Frank Renner , Mark Young , Anthony Farina
发明人： Leon Manole , William Rice , Stewart Gilman , John Dineen , Frank Renner , Mark Young , Anthony Farina
IPC分类号： F42B8/12 , F42B10/06 , F42B10/48 , F42B10/00 , F42B8/00 , F42B10/56
CPC分类号： F42B10/06 , F42B10/48 , F42B8/12
摘要： An aerodynamic device, such as a projectile includes an elongated forebody, and an aft section secured to the forebody. The aft section acts as a d control device, and includes a connecting member that extends integrally in a conically shaped flared section, for generating a lift force to help stabilize the projectile during forward flight. The aft section further includes a flange that extends from the flared section, and that provides velocity decay and optimal drag, in order to limit the projectile flight and descent within a predetermined safety or emergency range. The flared section is defined between an innermost edge positioned adjacent to the connecting member, and an outermost edge positioned adjacent to the flange. The flange includes a forward facing wall that extends from the outermost edge and that has a height "H" that controls the amount of drag on the projectile, such that the outer diameter of the aft section is less than, or equal to the inner diameter of the gun barrel from which the projectile is fired.
摘要翻译：诸如射弹的空气动力学装置包括细长的前体和固定到前体的后部。后部部分用作拖曳控制装置，并且包括连接构件，该连接构件一体地延伸在锥形扩张部分中，用于产生升力以帮助在向前飞行期间稳定射弹。后部段还包括从扩张部分延伸的凸缘，并且其提供速度衰减和最佳阻力，以便在预定的安全或紧急范围内限制射弹飞行和下降。扩口部分限定在邻近连接部件的最内边缘和邻近凸缘定位的最外边缘之间。凸缘包括从最外边缘延伸的具有高度“H”的向前壁，该高度“H”控制弹丸上的阻力量，使得后部的外径小于或等于内径枪弹被射击的枪管。

2. 发明申请

US20060065149A1 A FINLESS TRAINING PROJECTILE WITH IMPROVED FLIGHT STABILITY OVER AN EXTENDED RANGE 失效
标题翻译：在延长的范围内提高飞行稳定性的精细训练项目
公开(公告)号：US20060065149A1
公开(公告)日：2006-03-30
申请号：US10711714
申请日：2004-09-30
申请人： Stewart Gilman , Anthony Farina , Leon Manole
发明人： Stewart Gilman , Anthony Farina , Leon Manole
IPC分类号： F42B8/00 , F42B10/06
CPC分类号： F42B8/12 , F42B10/26 , F42B10/38
摘要： A finless cone-nosed, ogival-nosed, or combination ogive-cone nosed training projectile is statically stable, yet has adequate spin rate to compensate for aerodynamic or mass asymmetries. In addition, the training projectile can be fired from smooth bore or rifled cannons of various calibers, including 120 mm and 105 mm. Spin torque and stability augmentation are provided by a radially angled slotted tail flange attached to the rear of the training projectile, providing high performance and improved accuracy at low cost for use in training exercises. The training projectile has a higher static margin than conventional devices, and provides the ability to train personnel with a training projectile that achieves flight ranges similar to its matching tactical projectile, and has improved accuracy.
摘要翻译：无锥锥体，椭圆形或组合的ogive-cone nosed训练射弹是静态稳定的，但具有足够的旋转速率来补偿空气动力学或质量不对称性。此外，训练射弹可以从各种口径的平滑孔或膛线炮中射出，包括120毫米和105毫米。旋转扭矩和稳定性增加由附接到训练射弹后部的径向角度的开槽尾翼法兰提供，以低成本提供高性能和改进的准确性，用于训练练习。训练弹体具有比传统装置更高的静态裕度，并提供训练人员训练射弹的能力，实现与其匹配的战术射弹类似的飞行范围，并提高了准确性。

3. 发明授权

US07150234B2 Finless training projectile with improved flight stability over an extended range 失效
标题翻译：无极训练抛射体，在更广泛的范围内具有改善的飞行稳定性
公开(公告)号：US07150234B2
公开(公告)日：2006-12-19
申请号：US10711714
申请日：2004-09-30
申请人： Stewart Gilman , Anthony Farina , Leon Manole
发明人： Stewart Gilman , Anthony Farina , Leon Manole
IPC分类号： F42B10/24
CPC分类号： F42B8/12 , F42B10/26 , F42B10/38
摘要： A finless cone-nosed, ogival-nosed, or combination ogive-cone nosed training projectile is statically stable, yet has adequate spin rate to compensate for aerodynamic or mass asymmetries. In addition, the training projectile can be fired from smooth bore or rifled cannons of various calibers, including 120 mm and 105 mm. Spin torque and stability augmentation are provided by a radially angled slotted tail flange attached to the rear of the training projectile, providing high performance and improved accuracy at low cost for use in training exercises. The training projectile has a higher static margin than conventional devices, and provides the ability to train personnel with a training projectile that achieves flight ranges similar to its matching tactical projectile, and has improved accuracy.
摘要翻译：无锥锥体，椭圆形或组合的ogive-cone nosed训练射弹是静态稳定的，但具有足够的旋转速率来补偿空气动力学或质量不对称性。此外，训练射弹可以从各种口径的平滑孔或膛线炮中射出，包括120毫米和105毫米。旋转扭矩和稳定性增加由附接到训练射弹后部的径向角度的开槽尾翼法兰提供，以低成本提供高性能和改进的准确性，用于训练练习。训练弹体具有比传统装置更高的静态裕度，并提供训练人员训练射弹的能力，实现与其匹配的战术射弹类似的飞行范围，并提高了准确性。

4. 发明授权

US5725179A Expansion wave spin inducing generator 失效
标题翻译：膨胀波自旋诱发发生器
公开(公告)号：US5725179A
公开(公告)日：1998-03-10
申请号：US743596
申请日：1996-11-04
申请人： Stewart Gilman , Andrew Gowarty , Anthony Farina
发明人： Stewart Gilman , Andrew Gowarty , Anthony Farina
IPC分类号： F42B10/24 , F42B10/00 , F42B5/24
CPC分类号： F42B10/24
摘要： A projectile to be, fired from a non-rifled tube includes an elongated foody and a stabilizer secured to the tail end of the forebody for enhancing the projectile flight stability and for imparting spin to the projectile. The stabilizer includes a threaded member that extends integrally into a forward section, a peripheral channel and a grooved aft section. The forward section has a generally smooth cylindrical shape. The peripheral channel extends along the entire peripheral contour of the stabilizer and has a generally semi-circular cross-section, for generating an expansion wave and for directing air flow toward the grooved aft section. The grooved aft section is cylindrically shaped relative to a longitudinal axis, and has a predetermined number of identical, equally spaced, circumferentially positioned grooves which traverse the entire axial length of the aft section, and which are angled relative to the longitudinal axis. Each angled groove is defined by two substantially parallel side walls.
摘要翻译：从非膛管发射的射弹包括细长的前体和固定到前体的尾端的稳定器，用于增强射弹飞行的稳定性并赋予射弹旋转。稳定器包括一体地延伸到前部的螺纹构件，周边通道和带槽的后部。前部具有大致平滑的圆柱形状。周边通道沿着稳定器的整个周边轮廓延伸，并且具有大致半圆形的横截面，用于产生膨胀波并用于引导空气流向开槽后部。开槽的后部段相对于纵向轴线是圆柱形的，并且具有预定数量的相同的等间距的周向定位的凹槽，其横过后段的整个轴向长度并且相对于纵向轴线成角度。每个成角度的凹槽由两个基本平行的侧壁限定。

5. 发明授权

US5328130A Stabilizer for a cannon projectile 失效
标题翻译：大炮射弹的稳定器
公开(公告)号：US5328130A
公开(公告)日：1994-07-12
申请号：US32
申请日：1993-01-04
申请人： Stewart Gilman , Anthony Farina
发明人： Stewart Gilman , Anthony Farina
IPC分类号： F42B20060101 , F42B10/04 , F42B10/26
CPC分类号： F42B10/26 , F42B10/04
摘要： A cylindrical device connected to the nose of a projectile for imparting n to the projectile fired from a non-rifled bore of a cannon. The device has at least two coaxial, adjacent, and integrally connected cylindrical segments of different diameter. The segment having the larger diameter is positioned most rearwardly of the projectile, relative to the nose of the projectile, and the periphery of this segment has circumferentially spaced angled slots for catching air moving past the projectile to spin the projectile. The segment with the smaller diameter attaches the cylindrical device to the aft end of the nose of the projectile and directs the flow of air to and through the angled slots of the segment having the larger diameter.
摘要翻译：连接到射弹的鼻子的圆柱形装置，用于从炮的非膛孔射出的射弹旋转。该装置具有不同直径的至少两个同轴，相邻和一体连接的圆柱形段。具有较大直径的段相对于射弹的鼻部位于抛射体的最后面，并且该段的周边具有周向间隔开的成角度的狭槽，用于捕捉通过射弹移动的空气以旋转射弹。具有较小直径的段将圆柱形装置附接到射弹的鼻部的后端，并将空气流引导并穿过具有较大直径的段的成角度的槽。

6. 发明授权

US09540029B1 Cooler sled device 有权
标题翻译：冷却器雪橇装置
公开(公告)号：US09540029B1
公开(公告)日：2017-01-10
申请号：US14743282
申请日：2015-06-18
申请人： Anthony Farina
发明人： Anthony Farina
IPC分类号： B62B19/00 , B62B13/18
CPC分类号： B62B13/18 , B62B15/007 , B62B19/02 , B62B2203/44 , B62B2204/06
摘要： A cooler sled device for facilitating transport of a cooler over surfaces such as gravel, loose terrain, and sand includes a panel. A bottom surface of the panel is convexly curved between outer sides of a perimeter edge of the panel and extending rearwardly from a front side of the perimeter edge defining an upwardly turned front section of the bottom surface. Each of a pair of wells is positioned on an upper surface of the panel and proximate a respective one of the outer sides of the perimeter edge for receiving wheels coupled to a cooler positioned on the panel. A strap is positionable to extends across the upper surface of the panel for securing the cooler on the panel.
摘要翻译：用于便于在诸如砾石，松散地形和沙子的表面上的冷却器的运输的冷却器滑板装置包括面板。面板的底面在面板的周边边缘的外侧之间凸出地弯曲，并且从周边边缘的前侧向后延伸，限定底面的向上转动的前部。一对孔中的每一个都位于面板的上表面上并且靠近周边边缘的相应一个外侧边缘，用于接收连接到位于面板上的冷却器的轮。带可定位以延伸穿过面板的上表面以将冷却器固定在面板上。

7. 发明授权

US06402087B1 Fixed canards maneuverability enhancement 失效
标题翻译：固定式机动性增强
公开(公告)号：US06402087B1
公开(公告)日：2002-06-11
申请号：US09613147
申请日：2000-07-11
申请人： Anthony Farina , Michael J. Amoruso , Wilfredo Toledo
发明人： Anthony Farina , Michael J. Amoruso , Wilfredo Toledo
IPC分类号： F42B1060
CPC分类号： F42B10/661 , F42B10/64
摘要： A guidance device for projectiles has stationary canards (40) and thrusters (50) positioned on the nose (20) of the projectile (10). The thrusters (50) are initiated from remote or local sensor to provide flight maneuverability to a target.
摘要翻译：用于射弹的引导装置具有定位在射弹（10）的鼻部（20）上的固定的门（40）和推进器（50）。推进器（50）从远程或本地传感器启动，以向目标提供飞行机动性。

8. 发明授权

US08640625B1 Kinetic energy training projectile 有权
标题翻译：动能训练射弹
公开(公告)号：US08640625B1
公开(公告)日：2014-02-04
申请号：US13211624
申请日：2011-08-17
申请人： Brian Wong , Andrew Gowarty , Francis Donlon , Francis Renner , Robert Sayer , Carlton Adam , Daniel Vo , John Dineen , Anthony Farina
发明人： Brian Wong , Andrew Gowarty , Francis Donlon , Francis Renner , Robert Sayer , Carlton Adam , Daniel Vo , John Dineen , Anthony Farina
IPC分类号： F42B14/06 , F42B8/14
CPC分类号： F42B8/14 , F42B10/06 , F42B10/26 , F42B12/06 , F42B14/061 , F42B14/062
摘要： A kinetic energy training cartridge simulates the performance, weight, length, and external geometry of a tactical cartridge. The training cartridge includes a cartridge case and a projectile that is secured to cartridge case by means of a sabot. The sabot includes a rearward extension that encapsulates part of the projectile, to add weight and to increase a length to diameter ratio of the projectile, so as to decrease an intrusion volume of the projectile within the cartridge case. In a preferred embodiment, the length to diameter ratio of the projectile is at least 15.
摘要翻译：动能训练筒模拟战术弹药筒的性能，重量，长度和外部几何形状。训练筒包括一个盒壳体和一个通过一个破碎机固定到盒壳体上的射弹。该装置包括一个向后延伸部分，其包封部分弹丸，以增加重量并增加弹丸的长度与直径之比，从而减小弹药筒内的入射体积。在优选实施例中，射弹的长径比为至少15。

9. 外观设计

USD448658S1 Right angle drive hose clamp 失效
标题翻译：直角驱动软管夹
公开(公告)号：USD448658S1
公开(公告)日：2001-10-02
申请号：US29127156
申请日：2000-07-31
申请人： Anthony Farina
设计人： Anthony Farina

10. 发明授权

US5498160A Training projectile 失效
标题翻译：训练射弹
公开(公告)号：US5498160A
公开(公告)日：1996-03-12
申请号：US273032
申请日：1994-07-07
申请人： Anthony Farina , Mark Young
发明人： Anthony Farina , Mark Young
IPC分类号： F41A33/00 , F42B8/00 , F42B8/12 , F42B10/06
CPC分类号： F42B8/12 , F42B10/06
摘要： The disclosure is of a projectile having a main body, a nose and a tail iuding a flared tail member, the projectile having its center of gravity close to the nose thereof.
摘要翻译：本发明公开的是具有主体，鼻子和尾部的射弹，其包括扩口尾部件，该弹丸的重心靠近其鼻部。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式