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    Flight control surface actuator assembly including a free trail mechanism
    3.
    发明申请
    Flight control surface actuator assembly including a free trail mechanism 有权
    飞行控制表面执行器组件包括自由轨道机构

    公开(公告)号：US20070108343A1

    公开(公告)日：2007-05-17

    申请号：US11331755

    申请日：2006-01-13

    申请人： Paul Wingett ,  Casey Hanlon ,  Calvin Potter

    发明人： Paul Wingett ,  Casey Hanlon ,  Calvin Potter

    IPC分类号： B64C13/28

    CPC分类号： B64C13/503 ,  B64C13/28 ,  F16H25/20 ,  F16H25/2204 ,  Y10T74/19735

    摘要： A flight control surface actuator includes a mechanism that enables the actuator translation member to be selectively decoupled from the actuator rotating member. The actuator includes an actuation member, a translation member, an extension member, and a locking member. The actuation member is adapted to receive a drive force and is configured, in response to the drive force, to rotate and cause the translation member to translate. The extension member surrounds at least a portion of the translation member and is configured to be selectively coupled to, and decoupled from, the translation member. The locking member surrounds at least a portion of the extension tube and is movable between a lock position, in which the locking member couples the extension member to the translation member, and a release position, in which the locking member decouples the extension member from the translation member.

    摘要翻译： 飞行控制表面致动器包括能够使致动器平移构件与致动器旋转构件选择性地分离的机构。 致动器包括致动构件，平移构件，延伸构件和锁定构件。 致动构件适于接受驱动力，并且响应于驱动力而构造为旋转并使翻译构件平移。 延伸构件围绕平移构件的至少一部分并且被构造成选择性地联接到平移构件并与其平行。 锁定构件围绕延伸管的至少一部分，并且可在锁定位置与锁定位置之间移动，锁定构件将延伸构件与平移构件联接在一起，并且释放位置中，锁定构件将延伸构件与 翻译会员

    Electric flight control surface actuation system for aircraft flaps and slats
    4.
    发明申请
    Electric flight control surface actuation system for aircraft flaps and slats 有权

    公开(公告)号：US20060289696A1

    公开(公告)日：2006-12-28

    申请号：US11192622

    申请日：2005-07-29

    申请人： Casey Hanlon ,  Paul Wingett ,  Calvin Potter

    发明人： Casey Hanlon ,  Paul Wingett ,  Calvin Potter

    IPC分类号： B64C3/00

    CPC分类号： B64C13/503

    摘要： An aircraft flight control surface actuation system includes a plurality of electric motors-driven flap actuators, and a plurality of electric motor-driven slat actuators. The motor-driven actuators receive activation signals from flap and slat actuator controllers and is, in response to the activation signals, move the flaps and slats between stowed and a deployed positions. The flap and slat actuator controllers each include a plurality of independent actuator control channels that independently supply the activation signals to the motor-driven actuators.

    Unmanned underwater vehicle health monitoring system and method
    5.
    发明申请
    Unmanned underwater vehicle health monitoring system and method 失效
    无人机水下航行健康监测系统及方法

    公开(公告)号：US20060005758A1

    公开(公告)日：2006-01-12

    申请号：US10936954

    申请日：2004-09-08

    申请人： Calvin Potter ,  Sharon Brault ,  Paul Wingett

    发明人： Calvin Potter ,  Sharon Brault ,  Paul Wingett

    IPC分类号： B63G8/00

    CPC分类号： B63C11/42 ,  B63G2008/008 ,  G05B2223/06

    摘要： A health monitoring system for an unmanned underwater vehicle (UUV) is disposed within a submerged docking station. The health monitoring system receive signals representative of performance of the docking station equipment and uses the data to determine the health status of the docking station equipment, to generate health status data representative thereof, and transmits the health status data to a remote station. The health monitoring system also retrieves health status data from UUVs that are periodically docked in the docking station, and transmits this data to the remote station.

    摘要翻译： 一个无人驾驶水下航行器（UUV）的健康监测系统被安置在淹没式对接站内。 健康监测系统接收代表对接站设备的性能的信号，并使用数据来确定对接站设备的健康状态，生成表示其的健康状态数据，并将健康状态数据发送到远程站。 卫生监测系统还从定期停靠在坞站中的UUV检索健康状态数据，并将该数据发送到远程站。

    Valve trim adjustor for a poppet control valve
    7.
    发明授权
    Valve trim adjustor for a poppet control valve 失效
    用于提升阀控制阀的阀门调节器

    公开(公告)号：US08033525B2

    公开(公告)日：2011-10-11

    申请号：US12188811

    申请日：2008-08-08

    申请人： Paul Wingett ,  Steve Abel ,  Eric J. Ekstrom

    发明人： Paul Wingett ,  Steve Abel ,  Eric J. Ekstrom

    IPC分类号： F16K51/00

    CPC分类号： F16K1/523

    摘要： A control valve having an external valve trim adjustor is provided. The control valve comprises a valve shaft comprising a contact member extending in a direction transverse to the valve shaft, a stationary valve cap adapted to receive the valve shaft, an adjustment member coupled to the valve cap, and a stop plate coupled to the contact member and threadedly coupled to the adjustment member, the stop plate positioned at least partially between the adjustment member and the contact member and adapted to position the contact member away from the valve cap in response to manipulation of the adjustment member.

    摘要翻译： 提供具有外部阀门微调调节器的控制阀。 所述控制阀包括阀轴，所述阀轴包括沿横向于所述阀轴的方向延伸的接触构件，适于容纳所述阀轴的固定阀帽，联接到所述阀盖的调节构件和联接到所述接触构件的止动板 并且螺纹地联接到所述调节构件，所述止动板至少部分地位于所述调节构件和所述接触构件之间，并且适于响应于所述调节构件的操纵而将所述接触构件定位成远离所述阀帽。

    COMPACT, ELECTROMAGNETICALLY BRAKED ACTUATOR ASSEMBLY
    8.
    发明申请
    COMPACT, ELECTROMAGNETICALLY BRAKED ACTUATOR ASSEMBLY 失效
    紧凑型，电动制动执行器总成

    公开(公告)号：US20090284089A1

    公开(公告)日：2009-11-19

    申请号：US12120938

    申请日：2008-05-15

    申请人： Paul Wingett ,  Glenn Lane ,  Cal Potter

    发明人： Paul Wingett ,  Glenn Lane ,  Cal Potter

    IPC分类号： H02K7/106

    CPC分类号： H02K7/116 ,  F16H49/001 ,  H02K7/106

    摘要： An actuator assembly includes a motor assembly, a harmonic drive gearbox, an actuator, and an electromagnet brake device. The actuator assembly is fairly compact in size and the electromagnetic brake device is a non-contact type of devices, making it less prone to wear as compared to many other brake devices.

    摘要翻译： 致动器组件包括马达组件，谐波驱动齿轮箱，致动器和电磁铁制动装置。 致动器组件的尺寸相当紧凑，并且电磁制动装置是非接触式装置，使其与许多其它制动装置相比较不容易磨损。

    Flight control surface actuation system with redundantly configured actuator assemblies
    9.
    发明申请
    Flight control surface actuation system with redundantly configured actuator assemblies 审中-公开
    具有冗余配置的执行器组件的飞行控制表面致动系统

    公开(公告)号：US20060255207A1

    公开(公告)日：2006-11-16

    申请号：US11193059

    申请日：2005-07-28

    申请人： Paul Wingett ,  Calvin Potter ,  Casey Hanlon ,  Dwayne Benson

    发明人： Paul Wingett ,  Calvin Potter ,  Casey Hanlon ,  Dwayne Benson

    IPC分类号： B64C13/00

    CPC分类号： B64C13/00 ,  B64C13/341 ,  B64C13/504 ,  B64C13/505

    摘要： A flight control surface actuator assembly includes a plurality of flight control surface actuators, and a pivot arm. Each flight control surface actuator is adapted to couple to a flight control surface, and each is further adapted to receive a drive force and is operable, upon receipt thereof, to move between at least an extended position and a retracted position. The pivot arm is rotationally coupled to, and is configured to pivot relative to, each of the flight control surface actuators, the pivot arm is also adapted to be rotationally coupled to, and configured to pivot relative to, a static airframe structure.

    摘要翻译： 飞行控制表面致动器组件包括多个飞行控制表面致动器和枢转臂。 每个飞行控制表面致动器适于联接到飞行控制表面，并且每个飞行控制表面致动器进一步适于接收驱动力，并且在其接收时可操作以在至少延伸位置和缩回位置之间移动。 枢转臂旋转地联接到每个飞行控制表面致动器并被构造成相对于每个飞行控制表面致动器枢转，枢转臂还适于旋转地联接到静止的机身结构并且被构造成相对于静止的机身结构枢转。

    Submersible vehicle object ejection system using a flywheel driven boost pump
    10.
    发明申请
    Submersible vehicle object ejection system using a flywheel driven boost pump 失效
    使用飞轮驱动的增压泵的潜水车辆物体喷射系统

    公开(公告)号：US20060249067A1

    公开(公告)日：2006-11-09

    申请号：US11122832

    申请日：2005-05-04

    申请人： Jeffrey Rayner ,  Paul Wingett ,  John Toon ,  Sharon Brault

    发明人： Jeffrey Rayner ,  Paul Wingett ,  John Toon ,  Sharon Brault

    IPC分类号： B63B1/00

    CPC分类号： B63G8/32 ,  B63G8/30 ,  B63G8/38 ,  F41F3/10

    摘要： An object ejection system uses an energy storage flywheel to drive the fluid pump that is used to pressurize the ejection tubes. The energy storage flywheel is periodically spun-up using an electric motor. The energy stored in the energy storage flywheel is used, when needed, to drive the fluid pump and supply pressurized fluid to an impulse tank. The pressurized fluid in the impulse tank is used to eject an object, such as a weapon, from one or more ejection tubes.

    摘要翻译： 物体喷射系统使用储能飞轮驱动用于对喷射管加压的流体泵。 使用电动机周期性地卷绕储能飞轮。 存储在能量存储飞轮中的能量在需要时被使用以驱动流体泵并将加压流体供应到脉冲箱。 脉冲箱中的加压流体用于从一个或多个喷射管喷射诸如武器的物体。