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31. 发明授权

US07077072B2 Unmanned underwater vehicle turbine powered charging system and method 失效
公开(公告)号：US07077072B2
公开(公告)日：2006-07-18
申请号：US10822017
申请日：2004-04-08
申请人： Paul T. Wingett , Sharon K. Brault , Calvin C. Potter
发明人： Paul T. Wingett , Sharon K. Brault , Calvin C. Potter
IPC分类号： B63G8/00
CPC分类号： F03B13/00 , B63B22/18 , B63B2209/14 , B63B2209/18 , B63G8/001 , B63G8/08 , B63G2008/004 , B63G2008/008 , B63J3/04 , B63J2003/003 , B63J2003/046 , F03B17/06 , F05B2240/243 , F05B2240/97 , H02J7/1415 , Y02E10/28 , Y02T10/7005 , Y02T70/70 , Y02T90/38
摘要： A charging system for an unmanned underwater vehicle (UUV) is disposed within a submerged docking station. The charging system includes a battery, one or more generators, and a charge controller. The battery supplies electrical power to an electrical distribution bus in the docking station. The charge controller monitors the charge state of the battery and, when needed, activates one or more of the generators to recharge the battery. The charge controller also activates one or more of the generators when a UUV is docked in the docking station for recharging of its power plant.

32. 发明授权

US06921998B2 Energy storage flywheel auxiliary bearing system and method 失效
标题翻译：储能飞轮辅助轴承系统及方法
公开(公告)号：US06921998B2
公开(公告)日：2005-07-26
申请号：US10686874
申请日：2003-10-15
申请人： Todd R. Giles , Paul T. Wingett , Calvin C. Potter , Sharon K. Brault
发明人： Todd R. Giles , Paul T. Wingett , Calvin C. Potter , Sharon K. Brault
IPC分类号： H02K7/02
CPC分类号： H02K7/025 , H02J1/16 , Y02E60/16
摘要： An energy storage flywheel system includes a shaft, one or more primary bearing assemblies, and one or more secondary bearing assemblies. A secondary bearing control circuit determines the operability of the primary bearing assemblies and, based on this determination, selectively engages the secondary bearing assemblies to rotationally support the flywheel shaft.
摘要翻译：能量存储飞轮系统包括轴，一个或多个主要轴承组件和一个或多个次要轴承组件。次级轴承控制电路确定主轴承组件的可操作性，并且基于该确定，选择性地接合次级轴承组件以旋转地支撑飞轮轴。

33. 发明授权

US07251550B2 Aircraft accessory monitor 失效
标题翻译：飞机附件监视器
公开(公告)号：US07251550B2
公开(公告)日：2007-07-31
申请号：US10677567
申请日：2003-10-01
申请人： David M. Eschborn , Paul S. Evans , Casey Hanlon , Calvin C. Potter , Glenn H. Lane , Gary A. Farnsworth , Louie T. Gaines , David M. Mathis
发明人： David M. Eschborn , Paul S. Evans , Casey Hanlon , Calvin C. Potter , Glenn H. Lane , Gary A. Farnsworth , Louie T. Gaines , David M. Mathis
IPC分类号： G06F7/00
CPC分类号： G05B23/0254 , G07C5/008 , G07C5/0825 , G07C5/0858
摘要： Methods and apparatus are provided for monitoring an aircraft accessory. The apparatus comprises a processor associated with said aircraft accessory, a transducer coupled to said processor and operable to produce parametric data relating to said aircraft accessory and a memory coupled to said processor having baseline parametric data residing therein, wherein said baseline parametric data comprises the parametric data obtained during an acceptance test procedure. The method comprises installing a transducer configured to produce parametric data relating to said aircraft accessory, coupling said transducer to a processor associated with said aircraft accessory, coupling said processor to a memory associated with said aircraft accessory, recording baseline parametric data relating to said aircraft accessory in said memory during an acceptance test procedure for said aircraft accessory.
摘要翻译：提供了用于监视飞行器附件的方法和装置。所述设备包括与所述飞行器附件相关联的处理器，耦合到所述处理器并可操作以产生与所述飞行器附件相关的参数数据的传感器和耦合到所述处理器的存储器，其中驻留有驻留参考数据的基准参数数据，其中所述基准参数数据包括参数在验收测试程序中获得的数据。该方法包括安装一个被配置成产生与所述飞行器附件相关的参数数据的换能器，将所述换能器耦合到与所述飞机附件相关联的处理器，将所述处理器耦合到与所述飞行器附件相关联的存储器，记录与所述飞机附件相关的基准参数数据在所述飞机附件的验收测试程序期间在所述存储器中。

34. 发明授权

US07556224B2 Distributed flight control surface actuation system 失效
标题翻译：分布式飞行控制面驱动系统
公开(公告)号：US07556224B2
公开(公告)日：2009-07-07
申请号：US11319869
申请日：2005-12-27
申请人： Andrew T. Johnson , Casey Hanlon , Calvin C. Potter
发明人： Andrew T. Johnson , Casey Hanlon , Calvin C. Potter
IPC分类号： B64C13/50
CPC分类号： B64C13/50 , B64C13/42
摘要： An aircraft flight control surface actuation system includes a plurality of flap actuators, and a plurality of slat actuators. The actuators receive actuator position commands from an actuator control unit and, in response, move flaps and slats between stowed and deployed positions. The flight control surface actuator control unit includes a plurality of independent actuator control channels. One or more of the independent actuator control channels is coupled to both a flap actuator and a slat actuator, and is configured to selectively supply the actuator position commands thereto.
摘要翻译：飞机飞行控制表面致动系统包括多个翼片致动器和多个板条致动器。执行器从致动器控制单元接收致动器位置命令，并且作为响应，在收起位置和展开位置之间移动襟翼和板条。飞行控制表面致动器控制单元包括多个独立的致动器控制通道。一个或多个独立的致动器控制通道联接到翼片致动器和板条致动器，并且被配置为选择性地向其提供致动器位置命令。

35. 发明授权

US07335999B2 Fluid actuated rotating device including a low power generator 失效
标题翻译：流体致动的旋转装置包括低功率发生器
公开(公告)号：US07335999B2
公开(公告)日：2008-02-26
申请号：US10869552
申请日：2004-06-15
申请人： Calvin C. Potter , David M. Eschborn
发明人： Calvin C. Potter , David M. Eschborn
IPC分类号： F03B13/12 , F03B13/00 , H02P9/04
CPC分类号： F03B13/00 , F02C7/27 , F05B2220/602 , F05B2270/404 , F05D2220/62 , F05D2270/44 , H02P9/04 , H02P9/307 , H02P2101/30 , H02P2207/03 , Y02B10/50
摘要： A fluid-powered actuator assembly is modified to include a low power generator. The low power generator rotates in response to a drive force received from the actuator assembly, and thus only generates electrical power when the actuator assembly is operating. The low power generator is used to supply electrical power to various sensors and circuits, which may be used to implement prognostic and health monitoring capabilities for the actuator assembly.
摘要翻译：流体动力致动器组件被修改为包括低功率发生器。低功率发生器响应于从致动器组件接收的驱动力而旋转，并且因此仅在致动器组件操作时产生电力。低功率发生器用于向各种传感器和电路供电，可用于实现致动器组件的预测和健康监测功能。

36. 发明授权

US07185857B2 Thrust vector actuation control system and method 失效
标题翻译：推力矢量驱动控制系统及方法
公开(公告)号：US07185857B2
公开(公告)日：2007-03-06
申请号：US10766994
申请日：2004-01-28
申请人： Calvin C. Potter , Paul S. Evans , Terry L. Keller
发明人： Calvin C. Potter , Paul S. Evans , Terry L. Keller
IPC分类号： B64G1/26
CPC分类号： B64G1/26 , B64G1/002 , F02K9/80 , F02K9/805 , F02K9/84 , F02K9/96 , F42B15/01
摘要： A thrust vector actuation control system and method is configured to allow self-testing of the entire actuation system and/or its individual system components. The control system also provides real-time, continuous monitoring of actuation system status, and allows system gain and compensation parameters to be changed during vehicle operation remote from its launch site.
摘要翻译：推力矢量致动控制系统和方法被配置为允许整个致动系统和/或其各个系统部件的自检。控制系统还提供对执行系统状态的实时，连续监控，并允许系统增益和补偿参数在远离其发射现场的车辆操作期间改变。

37. 发明授权

US06779759B1 Integrated power and attitude control system and method 有权
标题翻译：综合电力与姿态控制系统及方法
公开(公告)号：US06779759B1
公开(公告)日：2004-08-24
申请号：US10402493
申请日：2003-03-28
申请人： George J. Klupar , Stephen G. Abel , Calvin C. Potter
发明人： George J. Klupar , Stephen G. Abel , Calvin C. Potter
IPC分类号： B64G128
CPC分类号： B64G1/286 , B64G1/285 , B64G1/426
摘要： An integrated power and attitude control system that includes a plurality of flywheels and a controller. The controller receives power commands and attitude commands and determines the optimum set of flywheel acceleration and gimbal velocity commands to supply to each flywheel, to meet the commanded power and attitude. Flywheel rotational acceleration is controlled to provide the commanded power, and both flywheel acceleration and flywheel gimbal angular velocity are controlled to provide the commanded attitude.
摘要翻译：一种集成的动力和姿态控制系统，其包括多个飞轮和控制器。控制器接收功率命令和姿态指令，并确定飞轮加速度和万向节速度指令的最佳组合，以提供给每个飞轮，以满足指令的功率和姿态。控制飞轮旋转加速度以提供指令功率，并且控制飞轮加速度和飞轮万向角速度以提供指令态度。

38. 发明授权

US07407137B2 Dual voltage integrated power and attitude control system and method 失效
标题翻译：双电压综合电源与姿态控制系统及方法
公开(公告)号：US07407137B2
公开(公告)日：2008-08-05
申请号：US11418798
申请日：2006-05-05
申请人： George J. Klupar , Calvin C. Potter , Sharon K. Brault , Robert J. Pinkerton , Norman Stanley Kolecki
发明人： George J. Klupar , Calvin C. Potter , Sharon K. Brault , Robert J. Pinkerton , Norman Stanley Kolecki
IPC分类号： B64G1/28
CPC分类号： B64G1/428 , B64G1/285 , B64G1/286 , B64G1/426 , B64G1/44
摘要： An integrated power and attitude control system and method for a vehicle efficiently supplies electrical power to both low voltage and high voltage loads, and does not rely on relatively heavy batteries to supply power during the vehicle initialization process. The system includes an energy storage flywheel, and a solar array that is movable between a stowed position and a deployed position. The energy storage flywheel is spun up, using electrical power supplied from a low voltage power source, to a rotational speed sufficient to provide attitude control. Then, after the solar array is moved to its deployed position, the energy storage flywheel is spun up, using electrical power supplied from a second power source, to a rotational speed sufficient to provide both attitude control and energy storage.
摘要翻译：用于车辆的集成电力和姿态控制系统和方法有效地向低压和高压负载提供电力，并且在车辆初始化过程中不依赖于相对较重的电池供电。该系统包括能量存储飞轮和可在收起位置和展开位置之间移动的太阳能阵列。使用从低压电源供应的电力将能量存储飞轮旋转到足以提供姿态控制的转速。然后，在太阳能电池阵列移动到其展开位置之后，使用从第二电源供应的电力将能量存储飞轮旋转到足以提供姿态控制和能量存储的转速。

39. 发明授权

US07400110B2 Smart power converter 失效
标题翻译：智能电源转换器
公开(公告)号：US07400110B2
公开(公告)日：2008-07-15
申请号：US11345161
申请日：2006-01-31
申请人： Calvin C. Potter , Andrew J. Brackenbury , Gene H. Nishikida
发明人： Calvin C. Potter , Andrew J. Brackenbury , Gene H. Nishikida
IPC分类号： H02P27/04
CPC分类号： H02J3/01 , Y02E40/40
摘要： A smart power conversion and control system and method converts source AC power at a first voltage level to DC power at a second voltage level that is less than the first voltage level. Upon receipt of a command signal, a portion of the system is enabled to further convert the source AC power to regulated DC power at a voltage level that is less than the first voltage level and greater than the second voltage level. One or more relatively high voltage DC loads are then energized with the regulated DC power. When the portion of the system is not enabled, the source AC power is not converted.
摘要翻译：智能电力转换和控制系统和方法将第一电压电平的源AC电力转换为小于第一电压电平的第二电压电平的DC电力。在接收到命令信号时，系统的一部分能够进一步将源AC电力转换为小于第一电压电平且大于第二电压电平的电压电平的稳压DC电力。一个或多个相对高压的直流负载然后用调节的直流电力通电。当系统的部分未启用时，源AC电源不被转换。

40. 发明授权

US07078880B2 Energy storage flywheel voltage regulation and load sharing system and method 失效
标题翻译：储能飞轮电压调节和负载共享系统及方法
公开(公告)号：US07078880B2
公开(公告)日：2006-07-18
申请号：US10641509
申请日：2003-08-15
申请人： Calvin C. Potter , Stephen G. Abel , George J. Klupar
发明人： Calvin C. Potter , Stephen G. Abel , George J. Klupar
IPC分类号： H02K7/02 , H02P9/10 , H02P9/14 , H02P9/00 , B64G1/28
CPC分类号： H02J3/30 , H02K7/025 , Y02E60/16
摘要： A system for regulating the voltage in an electrical distribution system includes a plurality of flywheels, motor/generators, and controllers. Each of the motor/generators is coupled to one of the energy storage flywheels and to the electrical supply system. The motor/generators each supply one or more signals representative of motor/generator operational parameters, and each motor/generator controllers receive one or more of the motor/generator operational parameter signals from each of the motor/generators. In response to the operational parameter signals, the motor/generator controllers each control the operation of one of the motor/generators in either a motor mode or a generate mode, to thereby regulate the electrical supply system voltage and equally share the electrical load between the motor/generators.
摘要翻译：用于调节配电系统中的电压的系统包括多个飞轮，电动机/发电机和控制器。每个电动机/发电机耦合到能量存储飞轮之一和电力供应系统。电动机/发电机各自提供表示电动机/发电机操作参数的一个或多个信号，并且每个电动机/发电机控制器从每个电动机/发电机接收一个或多个电动机/发电机操作参数信号。响应于操作参数信号，电动机/发电机控制器各自以电动机模式或发电模式来控制电动机/发电机中的一个的运行，从而调节供电系统电压并且平均地共享电力系统电机/发电机。

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