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1. 发明授权

US07107910B2 Penetrator and method of using same 有权
标题翻译：穿刺器及其使用方法
公开(公告)号：US07107910B2
公开(公告)日：2006-09-19
申请号：US10988125
申请日：2004-11-12
申请人： David L. Hunn , Johnny E. Banks , Carlton B. Cowan
发明人： David L. Hunn , Johnny E. Banks , Carlton B. Cowan
IPC分类号： F42B12/06
CPC分类号： F42B10/06 , F42B10/02 , F42B10/08 , F42B12/06 , F42B12/60 , F42B12/64
摘要： A penetrator includes a fore body comprising a pin and having a center of aerodynamic pressure forward of a center of gravity and a stabilizing portion comprising a material of lower density than that of the fore body and a plurality of outwardly extending fins for improving an aerodynamic stability of the projectile and defining a bore in which the pin is received for removably attaching the fore body thereto such that, when attached to the fore body, a center of gravity for the penetrator is forward of a center of aerodynamic pressure for the penetrator.
摘要翻译：穿透器包括：前体，其包括销，并且具有中心重心的空气动力学压力中心，稳定部分包括密度低于前体密度的材料;以及多个向外延伸的翅片，用于改善空气动力学稳定性并且限定出一个孔，在该孔中可以将前体可拆卸地安装在其上，使得当附着到前体时，用于穿透器的重心位于穿透器的空气动力学压力中心的前方。

2. 发明授权

US06843179B2 Penetrator and method for using same 失效
标题翻译：穿刺器及其使用方法
公开(公告)号：US06843179B2
公开(公告)日：2005-01-18
申请号：US10251468
申请日：2002-09-20
申请人： David L. Hunn , Johnny E. Banks , Carlton B. Cowan
发明人： David L. Hunn , Johnny E. Banks , Carlton B. Cowan
IPC分类号： F42B10/02 , F42B10/08 , F42B12/06 , F42B12/64 , F42B10/06
CPC分类号： F42B10/06 , F42B10/02 , F42B10/08 , F42B12/06 , F42B12/60 , F42B12/64
摘要： A penetrator includes a fore body comprising a pin and having a center of aerodynamic pressure forward of a center of gravity and a stabilizing portion comprising a material of lower density than that of the fore body and a plurality of outwardly extending fins for improving an aerodynamic stability of the projectile and defining a bore in which the pin is received for removably attaching the fore body thereto such that, when attached to the fore body, a center of gravity for the penetrator is forward of a center of aerodynamic pressure for the penetrator.
摘要翻译：穿透器包括：前体，其包括销，并且具有中心重心的空气动力学压力中心，稳定部分包括密度低于前体密度的材料;以及多个向外延伸的翅片，用于改善空气动力学稳定性并且限定出一个孔，在该孔中可以将前体可拆卸地安装在其上，使得当附着到前体时，用于穿透器的重心位于穿透器的空气动力学压力中心的前方。

3. 发明授权

US06637699B2 Method and apparatus for controlling a trajectory of a projectile 失效
标题翻译：用于控制射弹轨迹的方法和装置
公开(公告)号：US06637699B2
公开(公告)日：2003-10-28
申请号：US10105666
申请日：2002-03-25
申请人： Johnny E. Banks , Brian C. Baker
发明人： Johnny E. Banks , Brian C. Baker
IPC分类号： F42B1002
CPC分类号： F42B10/64
摘要： An apparatus for controlling a trajectory of a projectile includes a planetary drive train, a yaw drive assembly engaged with the planetary drive train, and a pitch drive assembly engaged with the planetary drive train. The apparatus further includes a plurality of fin assemblies linked with the planetary drive train such that, as the planetary drive train is actuated by at least one of the yaw drive assembly and the pitch drive assembly, corresponding displacements are produced in the plurality of fin assemblies.
摘要翻译：用于控制射弹的轨迹的装置包括行星传动系，与行星传动系相啮合的偏转驱动组件，以及与行星传动系相配合的俯仰驱动组件。该装置还包括与行星传动系连接的多个翅片组件，使得当行星传动系由至少一个偏航驱动组件和俯仰驱动组件致动时，在多个翅片组件中产生相应的位移。

4. 发明申请

US20080258065A1 Electromagnetic Energy Propagation Direction Sensor and Method of Using Same 审中-公开
标题翻译：电磁传播方向传感器及其使用方法
公开(公告)号：US20080258065A1
公开(公告)日：2008-10-23
申请号：US11739022
申请日：2007-04-23
申请人： Johnny E. Banks
发明人： Johnny E. Banks
IPC分类号： G01J5/00
CPC分类号： G01S3/781 , G01J5/023 , G01S3/043 , G01S3/28 , G01S3/783 , H01Q1/281 , H01Q1/368
摘要： A sensor for detecting a propagation direction of electromagnetic energy includes a plurality of receptors oriented in different directions for absorbing at least a portion of the electromagnetic energy, each of the plurality of receptors comprising a plurality of carbon nanotubes or nanofibers. The sensor further includes a processor electrically coupled with the plurality of receptors for determining the propagation direction of the electromagnetic energy based upon the electromagnetic energy absorbed by the plurality of receptors. A method for determining a propagation direction of electromagnetic energy includes the steps of providing a plurality of receptors oriented in different directions for absorbing at least a portion of the electromagnetic energy, each of the plurality of receptors comprising a plurality of carbon nanotubes or nanofibers, and determining the propagation direction of the electromagnetic energy with respect to the plurality of receptors based upon the amount of absorbed electromagnetic energy.
摘要翻译：用于检测电磁能的传播方向的传感器包括沿不同方向取向的多个受体，用于吸收至少一部分电磁能，多个受体中的每一个包括多个碳纳米管或纳米纤维。传感器还包括与多个受体电耦合的处理器，用于基于由多个受体吸收的电磁能确定电磁能的传播方向。一种用于确定电磁能的传播方向的方法包括以下步骤：提供沿不同方向定向的多个受体以吸收至少一部分电磁能，所述多个受体中的每一个包括多个碳纳米管或纳米纤维，以及基于吸收的电磁能量来确定电磁能相对于多个受体的传播方向。

5. 发明授权

US06682250B2 Position-adjustable fastening apparatus and method 失效
标题翻译：位置可调紧固装置及方法
公开(公告)号：US06682250B2
公开(公告)日：2004-01-27
申请号：US10045268
申请日：2001-11-07
申请人： Johnny E. Banks
发明人： Johnny E. Banks
IPC分类号： F16B218
CPC分类号： F16B5/0225 , Y10T403/125 , Y10T403/7049 , Y10T403/7064 , Y10T403/76
摘要： A position-adjustable fastening apparatus capable of maintaining a position of a first member with respect to a second member includes a cam receiver disposed in a bore of the first member, a cam disposed in a bore of the cam receiver, and a fastener disposed in the bore in the cam. A method for fastening a first member and a second member positioning the first member with respect to the second member, orienting a cam receiver with respect to a bore in the first member, and placing the cam receiver in the bore of the first member. The method further includes orienting a cam with respect to a bore in the cam receiver, placing the cam in the bore in the cam receiver, and engaging the fastener with the second member through the bore in the cam.
摘要翻译：能够保持第一构件相对于第二构件的位置的位置可调紧固装置包括设置在第一构件的孔中的凸轮接收器，设置在凸轮接收器的孔中的凸轮和布置在凸轮中的孔。一种用于紧固第一构件和第二构件的方法，所述第一构件和第二构件相对于所述第二构件定位所述第一构件，使凸轮接收器相对于所述第一构件中的孔定向，以及将所述凸轮接收器放置在所述第一构件的孔中。该方法还包括相对于凸轮接收器中的孔定位凸轮，将凸轮放置在凸轮接收器中的孔中，以及通过凸轮中的孔将紧固件与第二构件接合。

6. 发明授权

US6092264A Single axis fold actuator and lock for member 失效
标题翻译：单轴折叠执行器和锁定成员
公开(公告)号：US6092264A
公开(公告)日：2000-07-25
申请号：US191492
申请日：1998-11-13
申请人： Johnny E. Banks
发明人： Johnny E. Banks
IPC分类号： E05D11/10 , E05F1/12 , F42B10/14 , F42B15/10
CPC分类号： F42B15/105 , F42B10/14 , E05D11/1007 , E05F1/1215 , Y10T16/53834 , Y10T16/53885 , Y10T16/5402
摘要： A mechanism (10, 100) is disclosed for deploying a mechanism, such as an air foil or antenna (14, 102, 104) which utilizes a pivot axle (16) and a torsion spring (18) to pivot the erectable surface to the erected position. A locking pin 22 can be provided to lock the erectable surface (14) in the erected position. In one embodiment, a wing (102) and a control fin (104) can be deployed about a single axis.
摘要翻译：公开了一种机构（10,100），用于展开机构，例如利用枢轴（16）和扭转弹簧（18）的空气箔或天线（14,102,104），以将可竖立的表面枢转到竖立位置可以设置锁定销22以将可竖立的表面（14）锁定在竖立位置。在一个实施例中，翼（102）和控制翼（104）可围绕单个轴展开。

7. 发明授权

US08468923B2 Apparatus and method for selectively affecting a launch trajectory of a projectile 有权
标题翻译：用于选择性地影响射弹发射轨迹的装置和方法
公开(公告)号：US08468923B2
公开(公告)日：2013-06-25
申请号：US11676209
申请日：2007-02-16
申请人： Umang R. Patel , Wayne K. Schroeder , Johnny E. Banks
发明人： Umang R. Patel , Wayne K. Schroeder , Johnny E. Banks
IPC分类号： F41F7/00
CPC分类号： F42B5/067 , F41F3/042 , F41F3/052 , F41F3/077 , F42B5/073
摘要： An apparatus for selectively affecting a launch trajectory of a projectile from a canister includes means for selectively positioning the projectile with respect to the canister and a sabot operably associated with the projectile and the means for selectively positioning the projectile. A projectile launch system includes a canister, a projectile disposed in the canister, and means for selectively positioning the projectile with respect to the canister. A method for affecting a launch trajectory of a projectile includes providing a canister and a projectile disposed in the canister and adjusting a position of the projectile with respect to the canister.
摘要翻译：用于选择性地影响来自罐的射弹的发射轨迹的装置包括用于相对于所述罐选择性地定位所述射弹的装置和与所述射弹可操作地相关联的炮弹以及用于选择性地定位所述射弹的装置。射弹发射系统包括罐，设置在罐中的抛射体，以及用于相对于罐选择性地定位射弹的装置。一种影响射弹发射轨迹的方法，包括提供一个放置在罐中的罐和一个抛射体，并相对于罐调节射弹的位置。

8. 发明申请

US20100269677A1 Apparatus and Method for Selectively Affecting a Launch Trajectory of a Projectile 有权
标题翻译：选择性地影响射弹发射轨迹的装置和方法
公开(公告)号：US20100269677A1
公开(公告)日：2010-10-28
申请号：US11676209
申请日：2007-02-16
申请人： Umang R. Patel , Wayne K. Schroeder , Johnny E. Banks
发明人： Umang R. Patel , Wayne K. Schroeder , Johnny E. Banks
IPC分类号： F41F7/00
CPC分类号： F42B5/067 , F41F3/042 , F41F3/052 , F41F3/077 , F42B5/073
摘要： An apparatus for selectively affecting a launch trajectory of a projectile from a canister includes means for selectively positioning the projectile with respect to the canister and a sabot operably associated with the projectile and the means for selectively positioning the projectile. A projectile launch system includes a canister, a projectile disposed in the canister, and means for selectively positioning the projectile with respect to the canister. A method for affecting a launch trajectory of a projectile includes providing a canister and a projectile disposed in the canister and adjusting a position of the projectile with respect to the canister.
摘要翻译：用于选择性地影响来自罐的射弹的发射轨迹的装置包括用于相对于所述罐选择性地定位所述射弹的装置和与所述射弹可操作地相关联的炮弹以及用于选择性地定位所述射弹的装置。射弹发射系统包括罐，设置在罐中的抛射体，以及用于相对于罐选择性地定位射弹的装置。一种影响射弹发射轨迹的方法，包括提供一个放置在罐中的罐和一个抛射体，并相对于罐调节射弹的位置。

9. 发明授权

US07752976B2 Warhead and method of using same 有权
标题翻译：弹头和使用方法
公开(公告)号：US07752976B2
公开(公告)日：2010-07-13
申请号：US11140131
申请日：2005-05-27
申请人： Johnny E. Banks
发明人： Johnny E. Banks
IPC分类号： F42B12/58 , F42B12/64
CPC分类号： F42B12/64 , F42B12/06 , F42B12/60 , F42B12/62 , F42B14/065
摘要： A warhead includes a barrel operatively associated with the vehicle, the barrel being extendable from and retractable into the vehicle; a penetrator disposed in the barrel; and means for expelling the penetrator from the barrel. A vehicle includes a barrel extendable from and retractable into the vehicle; a penetrator disposed in the barrel; and means for expelling the penetrator from the barrel. A method includes transporting a warhead to a position proximate a target; angularly or translationally positioning a barrel of the warhead; and expelling at least one penetrator from the barrel toward the target. A vehicle includes an airfoil; a barrel operably associated with the airfoil; a penetrator disposed in the barrel; and means for expelling the penetrator from the barrel.
摘要翻译：弹头包括与车辆可操作地相关联的桶，所述筒可从车辆延伸并可缩回到车辆中; 设置在筒体中的穿透器; 以及用于将穿透器从筒体排出的装置。车辆包括可从车辆延伸并可收回的车桶; 设置在筒体中的穿透器; 以及用于将穿透器从筒体排出的装置。一种方法包括将弹头运送到靠近目标的位置; 角度地或平移地定位弹头的枪管; 并将至少一个穿透器从桶朝向目标排出。车辆包括翼型件; 与机翼可操作地连接的桶; 设置在筒体中的穿透器; 以及用于将穿透器从筒体排出的装置。

10. 发明授权

US07097132B2 Apparatus and method for selectivity locking a fin assembly 有权
标题翻译：用于选择性地锁定翅片组件的装置和方法
公开(公告)号：US07097132B2
公开(公告)日：2006-08-29
申请号：US10244323
申请日：2002-09-16
申请人： Johnny E. Banks , Brian C. Baker
发明人： Johnny E. Banks , Brian C. Baker
IPC分类号： F42B15/01
CPC分类号： F42B10/64 , F42B10/14
摘要： A fin assembly includes a fin base, a fin tip rotatably connected with the fin base, and means for selectively locking the fin tip in a chosen configuration. A vehicle includes a body defining a cavity therein and defining an opening through a wall thereof, a fin control mechanism disposed within the cavity, and a fin base having an axle extending through the opening and engaged with the fin control mechanism. The vehicle further comprises a fin tip rotatably connected with the fin base, and means for selectively locking the fin tip in a chosen configuration. A method for configuring a fin assembly on a vehicle includes providing a fin tip rotatably connected with a fin base being operably coupled with the vehicle and selectively locking the fin tip in a first position relative to the fin base.
摘要翻译：翅片组件包括翅片基座，与翅片基部可旋转地连接的翅片尖端以及用于以选定构造选择性地锁定翅片尖端的装置。车辆包括在其中限定空腔并且通过其壁限定开口的主体，设置在腔内的翅片控制机构和具有延伸穿过开口并与翅片控制机构接合的轴的翅片底座。车辆还包括与翅片基座可旋转地连接的翅片尖端，以及用于以选定的构造选择性地锁定翅片尖端的装置。一种用于在车辆上构造翅片组件的方法包括提供可转动地连接到翅片底座的翅片头部，该翅片底座可操作地与车辆联接并且相对于翅片底座选择性地将翅片尖端锁定在第一位置。

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