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1. 发明申请

US20230044354A1 Cyber Threat Defense System Protecting Email Networks with Machine Learning Models using a Range of Metadata from Observed Email Communications 有权
公开(公告)号：US20230044354A1
公开(公告)日：2023-02-09
申请号：US17966708
申请日：2022-10-14
申请人： Matthew Dunn , Matthew Ferguson , Stephen Pickman
发明人： Matthew Dunn , Matthew Ferguson , Stephen Pickman
IPC分类号： H04L9/40 , G06N20/00
摘要： A cyber-threat defense system for a network including its email domain protects this network from cyber threats. Modules utilize machine learning models as well communicate with a cyber threat module. Modules analyze the wide range of metadata from the observed email communications. The cyber threat module analyzes with the machine learning models trained on a normal behavior of email activity and user activity associated with the network and in its email domain in order to determine when a deviation from the normal behavior of email activity and user activity is occurring. A mass email association detector determines a similarity between highly similar emails being i) sent from or ii) received by a collection of two or more individual users in the email domain in a substantially simultaneous time frame. Mathematical models can be used to determine similarity weighing in order to derive a similarity score between compared emails.

2. 发明授权

US08172074B2 Automated delivery of parts across diverse manufacturing stations 有权
标题翻译：在不同的加工站自动运送零件
公开(公告)号：US08172074B2
公开(公告)日：2012-05-08
申请号：US12481451
申请日：2009-06-09
申请人： Constance Jones , Edwin G. Kepler , Matthew Ferguson
发明人： Constance Jones , Edwin G. Kepler , Matthew Ferguson
IPC分类号： B65G43/10
CPC分类号： B65G37/02 , B65G43/10
摘要： A conveyor system includes a kitting conveyor subsystem arranged to transport kits to a washing station, a washing conveyor subsystem arranged to receive kits from a kitting conveyor subsystem and to transport washed kits towards an assembly station, and an assembly conveyor subsystem to receive washed kits from the washing conveyor subsystem and transport the kits to an assembly station, wherein the kits traverse the system from the kitting conveyor subsystem to the assembly station automatically without human intervention. A self-adjusting conveyor includes a table top containing a conveyor belt, legs arranged to support the table top, an adjustment fixture arranged to adjust the table top to a working height, and a controller to return the table top to a home height upon activation.
摘要翻译：输送机系统包括布置成将套件运送到洗涤站的起毛输送机子系统，布置成从起球输送机子系统接收套件并将洗涤的套件运送到组装工位的洗涤输送机子系统，以及组装输送机子系统，以从洗涤输送机子系统并将套件运输到组装站，其中套件在没有人为干预的情况下自动地将该系统从套管输送机子系统穿过组装工位。自动调节输送机包括一个包含传送带的台面，布置成支撑台面的支脚，被设置成将桌面调整到工作高度的调节夹具，以及控制器，用于在桌面启动时将桌面返回到家庭高度。

3. 发明申请

US20090035137A1 Helicopter vibration control system and rotary force generator for canceling vibrations 有权
标题翻译：直升机振动控制系统和旋转力发生器，用于消除振动
公开(公告)号：US20090035137A1
公开(公告)日：2009-02-05
申请号：US12286461
申请日：2008-09-30
申请人： Mark Jolly , Stephen Hildebrand , Russell Altieri , Matthew Ferguson , Douglas Ivers
发明人： Mark Jolly , Stephen Hildebrand , Russell Altieri , Matthew Ferguson , Douglas Ivers
IPC分类号： B64C27/32
CPC分类号： F16F15/265 , B64C27/001 , B64C2027/003 , F16F15/22 , F16F15/267
摘要： Helicopter rotating hub mounted vibration control system for a rotary wing hub having periodic vibrations while rotating at an operational rotation frequency. The vibration control system includes a housing attachable to the rotary wing hub and rotating with the hub at the operational frequency. The housing is centered about the rotary wing hub axis of rotation and has an electronics housing cavity subsystem and an adjacent rotor housing cavity subsystem. The rotor housing cavity contains a first coaxial ring motor with a first rotor and imbalance mass and a second coaxial ring motor with a second rotor and imbalance mass. The electronics housing cavity contains an electronics control system which receives sensor outputs and electrically controls and drives the first motor and the second motor such that the first imbalance mass and the second imbalance mass are driven at a vibration canceling rotation frequency greater than the operational rotation frequency wherein the helicopter rotary wing hub periodic vibrations are reduced.
摘要翻译：用于旋转翼毂的直升机旋转轮毂安装的振动控制系统，其具有以工作旋转频率旋转的周期性振动。振动控制系统包括可附接到旋转翼毂并且以工作频率与轮毂一起旋转的壳体。壳体围绕旋转翼轮毂旋转轴线居中，并且具有电子器件壳体腔子系统和相邻的转子壳体空腔子系统。转子壳体腔包含具有第一转子和不平衡质量的第一同轴环电动机和具有第二转子和不平衡质量的第二同轴环电动机。电子设备壳体腔包含电子控制系统，其接收传感器输出并电控制并驱动第一电动机和第二电动机，使得第一不平衡质量块和第二不平衡质量块以大于操作旋转频率的振动消除旋转频率被驱动其中直升机旋转翼毂周期性振动减小。

4. 发明申请

US20060083617A1 Helicopter vibration control system and rotary force generator for canceling vibrations 有权
标题翻译：直升机振动控制系统和旋转力发生器，用于消除振动
公开(公告)号：US20060083617A1
公开(公告)日：2006-04-20
申请号：US11215388
申请日：2005-08-30
申请人： Mark Jolly , Stephen Hildebrand , Russell Altieri , Matthew Ferguson , Douglas Ivers
发明人： Mark Jolly , Stephen Hildebrand , Russell Altieri , Matthew Ferguson , Douglas Ivers
IPC分类号： F04D29/26
CPC分类号： F16F15/265 , B64C27/001 , B64C2027/003 , F16F15/22 , F16F15/267
摘要： A helicopter rotating hub mounted vibration control system for a helicopter rotary wing hub having a periodic vibration while rotating at a helicopter operational rotation frequency. The helicopter rotating hub mounted vibration control system includes an annular ring rotary housing attachable to the helicopter rotary wing hub and rotating with the helicopter rotary wing hub at the helicopter operational rotation frequency. The annular ring housing is centered about the rotary wing hub axis of rotation and has an electronics housing cavity subsystem and preferably an adjacent coaxial rotor housing cavity subsystem. The rotor housing cavity subsystem contains a first coaxial frameless AC ring motor having a first rotor with a first imbalance mass and a second coaxial frameless AC ring motor having a second rotor with a second imbalance mass. The electronics housing cavity subsystem contains an electronics control system which receives sensor outputs and electrically controls and drives the first coaxial frameless AC ring motor and the second coaxial frameless AC ring motor such that the first imbalance mass and the second imbalance mass are directly driven at a vibration canceling rotation frequency greater than the helicopter operational rotation frequency wherein the helicopter rotary wing hub periodic vibration is reduced.
摘要翻译：一种直升机旋转轮毂安装的用于直升机旋转翼片的振动控制系统，其具有以直升机操作旋转频率旋转的周期性振动。直升机旋转轮毂安装的振动控制系统包括环形环旋转壳体，其可连接到直升机旋转翼毂并且以直升机操作旋转频率与直升机旋转翼毂一起旋转。环形环壳体围绕旋转翼轮毂旋转轴线居中，并且具有电子器件壳体腔子系统，并且优选地是相邻的同轴转子壳体空腔子系统。转子壳体空腔子系统包括具有第一不平衡质量的第一转子和具有第二不平衡质量的第二转子的第二同轴无框架AC环形电动机的第一同轴无框架AC环形电动机。电子设备壳体子系统包含电子控制系统，其接收传感器输出并电控制并驱动第一同轴无框架AC环形电动机和第二同轴无框架AC环形电动机，使得第一不平衡质量块和第二不平衡质量块直接在减振旋转频率大于直升机操作旋转频率，其中直升机旋翼轮毂周期性振动减小。

5. 发明授权

US07942633B2 Helicopter vibration control system and rotary force generator for canceling vibrations 有权
标题翻译：直升机振动控制系统和旋转力发生器，用于消除振动
公开(公告)号：US07942633B2
公开(公告)日：2011-05-17
申请号：US12286461
申请日：2008-09-30
申请人： Mark Jolly , Stephen Hildebrand , Russell Altieri , Matthew Ferguson , Douglas Ivers
发明人： Mark Jolly , Stephen Hildebrand , Russell Altieri , Matthew Ferguson , Douglas Ivers
IPC分类号： F01D5/26
CPC分类号： F16F15/265 , B64C27/001 , B64C2027/003 , F16F15/22 , F16F15/267
摘要： Helicopter rotating hub mounted vibration control system for a rotary wing hub having periodic vibrations while rotating at an operational rotation frequency. The vibration control system includes a housing attachable to the rotary wing hub and rotating with the hub at the operational frequency. The housing is centered about the rotary wing hub axis of rotation and has an electronics housing cavity subsystem and an adjacent rotor housing cavity subsystem. The rotor housing cavity contains a first coaxial ring motor with a first rotor and imbalance mass and a second coaxial ring motor with a second rotor and imbalance mass. The electronics housing cavity contains an electronics control system which receives sensor outputs and electrically controls and drives the first motor and the second motor such that the first imbalance mass and the second imbalance mass are driven at a vibration canceling rotation frequency greater than the operational rotation frequency wherein the helicopter rotary wing hub periodic vibrations are reduced.
摘要翻译：用于旋转翼毂的直升机旋转轮毂安装的振动控制系统，其具有以工作旋转频率旋转的周期性振动。振动控制系统包括可附接到旋转翼毂并且以工作频率与轮毂一起旋转的壳体。壳体围绕旋转翼轮毂旋转轴线居中，并且具有电子器件壳体腔子系统和相邻的转子壳体空腔子系统。转子壳体腔包含具有第一转子和不平衡质量的第一同轴环电动机和具有第二转子和不平衡质量的第二同轴环电动机。电子设备壳体腔包含电子控制系统，其接收传感器输出并电控制并驱动第一电动机和第二电动机，使得第一不平衡质量块和第二不平衡质量块以大于操作旋转频率的振动消除旋转频率被驱动其中直升机旋转翼毂周期性振动减小。

6. 发明授权

US07448854B2 Helicopter vibration control system and rotary force generator for canceling vibrations 有权
标题翻译：直升机振动控制系统和旋转力发生器，用于消除振动
公开(公告)号：US07448854B2
公开(公告)日：2008-11-11
申请号：US11215388
申请日：2005-08-30
申请人： Mark Jolly , Stephen Hildebrand , Russell Altieri , Matthew Ferguson , Douglas Ivers
发明人： Mark Jolly , Stephen Hildebrand , Russell Altieri , Matthew Ferguson , Douglas Ivers
IPC分类号： F04D29/26
CPC分类号： F16F15/265 , B64C27/001 , B64C2027/003 , F16F15/22 , F16F15/267
摘要： Helicopter rotating hub mounted vibration control system for a rotary wing hub having periodic vibrations while rotating at an operational rotation frequency. The vibration control system includes a housing attachable to the rotary wing hub and rotating with the hub at the operational frequency. The housing is centered about the rotary wing hub axis of rotation and has an electronics housing cavity subsystem and an adjacent rotor housing cavity subsystem. The rotor housing cavity contains a first coaxial ring motor with a first rotor and imbalance mass and a second coaxial ring motor with a second rotor and imbalance mass. The electronics housing cavity contains an electronics control system which receives sensor outputs and electrically controls and drives the first motor and the second motor such that the first imbalance mass and the second imbalance mass are driven at a vibration canceling rotation frequency greater than the operational rotation frequency wherein the helicopter rotary wing hub periodic vibrations are reduced.
摘要翻译：用于旋转翼毂的直升机旋转轮毂安装的振动控制系统，其具有以工作旋转频率旋转的周期性振动。振动控制系统包括可附接到旋转翼毂并且以工作频率与轮毂一起旋转的壳体。壳体围绕旋转翼轮毂旋转轴线居中，并且具有电子器件壳体腔子系统和相邻的转子壳体空腔子系统。转子壳体腔包含具有第一转子和不平衡质量的第一同轴环电动机和具有第二转子和不平衡质量的第二同轴环电动机。电子设备壳体腔包含电子控制系统，其接收传感器输出并电控制并驱动第一电动机和第二电动机，使得第一不平衡质量块和第二不平衡质量块以大于操作旋转频率的振动消除旋转频率被驱动其中直升机旋转翼毂周期性振动减小。

7. 发明申请

US20050114053A1 Magnetostrictive wavelet method for measuring pulse propagation time 审中-公开
标题翻译：用于测量脉冲传播时间的磁致伸缩小波方法
公开(公告)号：US20050114053A1
公开(公告)日：2005-05-26
申请号：US10965085
申请日：2004-10-14
申请人： Steve Southward , Mark Jolly , Matthew Ferguson , Leslie Fowler
发明人： Steve Southward , Mark Jolly , Matthew Ferguson , Leslie Fowler
IPC分类号： G01B7/02 , G01D5/48 , G01R29/02 , G01S13/28 , G04F10/00 , G06F19/00
CPC分类号： G01B7/023 , G01D5/485 , G01R29/02 , G04F10/00
摘要： A magnetostrictive sensor system and a method of measuring a magnetostrictive sensor pulse is provided. The measurement system and method includes providing a digital buffer circuit connected with an analog to digital converter to an analog waveform detector for receiving a magnetostrictive pulse waveform from a magnetostrictive waveguide. A template waveform is provided, and a returned magnetostrictive pulse waveform is recieved into the digital buffer circuit. The received pulse waveform is compared with the template waveform to determine an arrival time of the returned magnetostrictive pulse waveform. Providing the template waveform includes providing a synthesized return waveform generated to simulate a characteristic magnetostrictive return pulse waveform of the magnetostrictive system. The magnetostrictive sensor system includes a magnetostrictive waveguide, an analog waveform detector for receiving a magnetostrictive pulse waveform from the magnetostrictive waveguide, a comparing correlating processor with a template waveform for comparing the received magnetostrictive pulse waveform with the template waveform to determine an arrival time of the returned magnetostrictive pulse waveform.
摘要翻译：提供了一种磁致伸缩传感器系统和一种测量磁致伸缩传感器脉冲的方法。测量系统和方法包括提供与模数转换器连接的数字缓冲电路到模拟波形检测器，用于从磁致伸缩波导接收磁致伸缩脉冲波形。提供了一个模板波形，并将一个返回的磁致伸缩脉冲波形接收到数字缓冲电路中。将接收到的脉冲波形与模板波形进行比较，以确定返回的磁致伸缩脉冲波形的到达时间。提供模板波形包括提供生成的用于模拟磁致伸缩系统的特征磁致伸缩返回脉冲波形的合成返回波形。磁致伸缩传感器系统包括磁致伸缩波导，用于从磁致伸缩波导接收磁致伸缩脉冲波形的模拟波形检测器，用于将接收的磁致伸缩脉冲波形与模板波形进行比较的模板波形的比较相关处理器，以确定返回磁致伸缩脉冲波形。

8. 发明授权

US09259492B2 Tuned multifunctional magnetic nanoparticles for biomedicine 有权
标题翻译：调谐用于生物医学的多功能磁性纳米颗粒
公开(公告)号：US09259492B2
公开(公告)日：2016-02-16
申请号：US13805763
申请日：2011-06-20
申请人： Kannan M. Krishnan , R. Matthew Ferguson , Amit Praful Khandhar
发明人： Kannan M. Krishnan , R. Matthew Ferguson , Amit Praful Khandhar
IPC分类号： A61K49/18 , A61K41/00 , A61K9/14 , C12Q1/02
CPC分类号： A61K49/1824 , A61K9/14 , A61K41/0052 , A61K49/1854 , A61K49/186 , C12Q1/02 , Y10T428/2982 , Y10T428/2998
摘要： Magnetic nanoparticles and related devices and methods are described. Compositions and methods can include magnetic nanoparticles having a narrow size distribution for use in diagnostics and therapeutics.
摘要翻译：描述了磁性纳米颗粒及其相关的装置和方法。组合物和方法可以包括具有窄尺寸分布的磁性纳米颗粒用于诊断和治疗。

9. 发明申请

US20130149539A1 TUNED MULTIFUNCTIONAL MAGNETIC NANOPARTICLES FOR BIOMEDICINE 有权
标题翻译：调谐多功能磁性纳米颗粒生物素
公开(公告)号：US20130149539A1
公开(公告)日：2013-06-13
申请号：US13805763
申请日：2011-06-20
申请人： Kannan M. Krishnan , R. Matthew Ferguson , Amit Praful Khandhar
发明人： Kannan M. Krishnan , R. Matthew Ferguson , Amit Praful Khandhar
IPC分类号： A61K49/18 , C12Q1/02 , A61K9/14
CPC分类号： A61K49/1824 , A61K9/14 , A61K41/0052 , A61K49/1854 , A61K49/186 , C12Q1/02 , Y10T428/2982 , Y10T428/2998
摘要： Magnetic nanoparticles and related devices and methods are described. Compositions and methods can include magnetic nanoparticles having a narrow size distribution for use in diagnostics and therapeutics.
摘要翻译：描述了磁性纳米颗粒及其相关的装置和方法。组合物和方法可以包括具有窄尺寸分布的磁性纳米颗粒用于诊断和治疗。

10. 发明申请

US20100307888A1 AUTOMATED DELIVERY OF PARTS ACROSS DIVERSE MANUFACTURING STATIONS 有权
标题翻译：自动化交付多个生产制造站的零件
公开(公告)号：US20100307888A1
公开(公告)日：2010-12-09
申请号：US12481451
申请日：2009-06-09
申请人： Constance H. Jones , Edwin G. Kepler , Matthew Ferguson
发明人： Constance H. Jones , Edwin G. Kepler , Matthew Ferguson
IPC分类号： B65G49/02 , B65G43/10
CPC分类号： B65G37/02 , B65G43/10
摘要： A conveyor system includes a kitting conveyor subsystem arranged to transport kits to a washing station, a washing conveyor subsystem arranged to receive kits from a kitting conveyor subsystem and to transport washed kits towards an assembly station, and an assembly conveyor subsystem to receive washed kits from the washing conveyor subsystem and transport the kits to an assembly station, wherein the kits traverse the system from the kitting conveyor subsystem to the assembly station automatically without human intervention. A self-adjusting conveyor includes a table top containing a conveyor belt, legs arranged to support the table top, an adjustment fixture arranged to adjust the table top to a working height, and a controller to return the table top to a home height upon activation.
摘要翻译：输送机系统包括布置成将套件运送到洗涤站的起毛输送机子系统，布置成从起球输送机子系统接收套件并将洗涤的套件运送到组装工位的洗涤输送机子系统，以及组装输送机子系统，以从洗涤输送机子系统并将套件运输到组装站，其中套件在没有人为干预的情况下自动地将该系统从套管输送机子系统穿过组装工位。自动调节输送机包括一个包含传送带的台面，布置成支撑台面的支脚，被设置成将桌面调整到工作高度的调节夹具，以及控制器，用于在桌面启动时将桌面返回到家庭高度。

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