公开(公告)号：US20070022936A1

公开(公告)日：2007-02-01

申请号：US11170862

申请日：2005-06-30

Applicant: Calvin Potter ,  Dennis Alexander ,  Paul Wingett

Inventor： Calvin Potter ,  Dennis Alexander ,  Paul Wingett

IPC: B63G8/28

CPC classification number: B63G8/32 ,  F41F3/10

Abstract: A submersible vehicle object ejection control system stores a plurality of pump speed command profiles. Each pump speed command profile is based on vehicle depth, vehicle speed, type of object being ejected, maximum noise emission magnitude during object ejection, and object exit velocity. The system also receives data representative of current vehicle depth, current vehicle speed, and the type of object being ejected. In response to these data, the system retrieves one of the plurality of pump speed command profiles and supplies pump speed commands representative of the retrieved pump speed command profile.

Abstract translation: 潜水车辆物体喷射控制系统存储多个泵速度指令轮廓。 每个泵速指令轮廓基于车辆深度，车辆速度，被排出的物体的类型，物体喷射期间的最大噪声发射幅度和物体离开速度。 该系统还接收代表当前车辆深度，当前车辆速度和被弹出物体的类型的数据。 响应于这些数据，系统检索多个泵速指令轮廓中的一个，并提供表示检索的泵速命令轮廓的泵速指令。

公开(公告)号：US20070018040A1

公开(公告)日：2007-01-25

申请号：US11192625

申请日：2005-07-28

Applicant: Paul Wingett ,  Calvin Potter ,  Casey Hanlon ,  Dwayne Benson

Inventor： Paul Wingett ,  Calvin Potter ,  Casey Hanlon ,  Dwayne Benson

IPC: B64C13/00

CPC classification number: B64C13/42 ,  B64C13/00

Abstract: A flight control surface actuator assembly includes a pair of flight control surface actuators and a pivot arm. One of the flight control surface actuators is coupled to a flight control surface and a static airframe structure, the other flight control surface actuator is coupled to the flight control surface and the pivot arm. The pivot arm coupled to the static airframe structure and is configured to pivot relative to the second flight control surface actuator and the static airframe structure.

Abstract translation: 飞行控制表面致动器组件包括一对飞行控制表面致动器和枢转臂。 飞行控制表面致动器中的一个联接到飞行控制表面和静态机身结构，另一个飞行控制表面致动器联接到飞行控制表面和枢转臂。 枢转臂联接到静态机身结构并且构造成相对于第二飞行控制表面致动器和静止机身结构枢转。

公开(公告)号：US20070007385A1

公开(公告)日：2007-01-11

申请号：US11192817

申请日：2005-07-29

Applicant: Calvin Potter ,  Casey Hanlon ,  Paul Wingett

Inventor： Calvin Potter ,  Casey Hanlon ,  Paul Wingett

IPC: B64D33/00

CPC classification number: B64C13/505

Abstract: An electric flight control surface actuation system is implemented using a low level control section and a high power section. The low level control section is disposed within an electronics bay within the aircraft, and is in operable communication with one or more flight computers via a communication bus. The flight computers supply flight control surface position commands to the low level control section, which in turn transmits actuator commands to the high power section via a plurality of redundant communication links. The high power section is disposed remotely from the low level control section and, in addition to being in operable communication with the low level control section, is coupled to an aircraft power bus and to each of the actuators. The high power section receives the actuator position commands transmitted from the low level control section and, in response, selectively energizes the actuators from the aircraft power bus.

Abstract translation: 使用低电平控制部分和高功率部分实现电动飞行控制表面致动系统。 低级控制部分设置在飞行器内的电子设备舱内，并且经由通信总线与一个或多个飞行计算机可操作地通信。 飞行计算机向低级控制部分提供飞行控制表面位置命令，该低级控制部分又通过多个冗余通信链路将致动器命令传送到高功率部分。 高功率部分远离低电平控制部分设置，并且除了与低电平控制部分可操作地通信之外，还耦合到飞行器电源总线和每个致动器。 高功率部分接收从低电平控制部分发送的致动器位置命令，并且作为响应，从飞行器电力总线选择性地激励致动器。

公开(公告)号：US20050206351A1

公开(公告)日：2005-09-22

申请号：US10793545

申请日：2004-03-03

Applicant: Paul Wingett ,  Sharon Brault ,  George Klupar ,  Calvin Potter

Inventor： Paul Wingett ,  Sharon Brault ,  George Klupar ,  Calvin Potter

IPC: F03G3/08 ,  H02P9/00

CPC classification number: F03G3/08

Abstract: A system and method for removing energy from the rotating group in an energy storage flywheel system during flywheel system testing includes one or more sensors is operable to sense operational parameters of the energy storage flywheel and to supply a sensor signals representative thereof. A primary control circuit is coupled to receive the sensor signals and, in response thereto, selectively supplies a primary brake activation signal to a brake. The brake, in response to the brake activation signal, selectively supplies a brake force to the energy storage flywheel.

Abstract translation: 用于在飞轮系统测试期间从能量存储飞轮系统中的旋转组中去除能量的系统和方法包括一个或多个传感器可操作以感测能量存储飞轮的操作参数并且提供代表其的传感器信号。 主控制电路被耦合以接收传感器信号，并且响应于此，选择性地向制动器提供初级制动器启动信号。 制动器响应于制动器启动信号选择性地向储能飞轮提供制动力。

公开(公告)号：US20050149236A1

公开(公告)日：2005-07-07

申请号：US10953985

申请日：2004-09-28

Applicant: Calvin Potter ,  Sharon Brault ,  Paul Wingett

Inventor： Calvin Potter ,  Sharon Brault ,  Paul Wingett

IPC: G05D1/00

CPC classification number: G05D1/0022

Abstract: A communication system for an unmanned underwater vehicle (UUV) is disposed at least partially within a submerged docking station. The communication system receives communication requests from a remote station, and transmits requested data to and from the remote station. The data transmitted from the remote station may be further transmitted to a submerged UUV, either via a data port or wirelessly, depending on whether the UUV is docked in the docking station.

Abstract translation: 用于无人水下航行器（UUV）的通信系统至少部分地设置在淹没坞站内。 通信系统从远程站接收通信请求，并向远程站发送请求的数据。 根据UUV是否对接在对接站中，从远程站发送的数据可以经由数据端口或无线地进一步发送到浸没的UUV。

公开(公告)号：US20050120807A1

公开(公告)日：2005-06-09

申请号：US10730410

申请日：2003-12-08

Applicant: Paul Wingett ,  Calvin Potter ,  Brent Bristol

Inventor： Paul Wingett ,  Calvin Potter ,  Brent Bristol

IPC: G01D7/00 ,  G01L5/00 ,  G01N3/00 ,  H05K1/02

CPC classification number: G01L5/0047 ,  H05K1/0268 ,  H05K1/0271 ,  H05K2201/09263 ,  H05K2201/10151

Abstract: A device for detecting strain levels imposed on a circuit board includes an apparatus mounted on the circuit board, an amplifier for detecting a change in the impedance of the apparatus and generating an output signal representing the change in the impedance of the apparatus, and a signal conditioner for receiving the output signal and setting the gain of the amplifier.

公开(公告)号：US20050089256A1

公开(公告)日：2005-04-28

申请号：US10696216

申请日：2003-10-28

Applicant: Paul Wingett ,  Todd Giles

Inventor： Paul Wingett ,  Todd Giles

IPC: F16C27/06 ,  F16C39/02 ,  F16C39/06 ,  F16C41/00

CPC classification number: F16C32/0442 ,  F16C27/066 ,  F16C39/02 ,  F16C2361/55 ,  Y10T74/2117 ,  Y10T74/2121 ,  Y10T74/2126

Abstract: An auxiliary bearing assembly for selectively engaging a shaft, preferably in an energy storage flywheel system, is configured to include a vibration damping seal, and an axial preload spring. The vibration damping seal damps out vibrations from the rotating group, following engagement of the auxiliary bearing assembly, while the rotating group is spinning down. The axial preload spring absorbs any differential thermal expansion or contraction that may occur between components.

Abstract translation: 用于选择性地接合轴的辅助轴承组件，优选地在能量存储飞轮系统中被构造成包括减振密封件和轴向预紧弹簧。 当旋转组旋转时，振动阻尼密封件在辅助轴承组件接合之后，减小旋转组的振动。 轴向预加载弹簧吸收可能在部件之间发生的任何不同的热膨胀或收缩。