公开(公告)号：US06418540B1

公开(公告)日：2002-07-09

申请号：US09384602

申请日：1999-08-27

Applicant: Peter Allen Dempsey ,  Daniel John Goudzwaard ,  Salvatore John Iaccarino ,  Stephen L. Kay ,  Andrew Bennett Struble ,  Davinderjit Singh Kohli

Inventor： Peter Allen Dempsey ,  Daniel John Goudzwaard ,  Salvatore John Iaccarino ,  Stephen L. Kay ,  Andrew Bennett Struble ,  Davinderjit Singh Kohli

IPC: H04L122

CPC classification number: G06F11/2028 ,  G06F11/1658 ,  G06F11/2023 ,  G06F11/2038 ,  G06F11/2041 ,  G06F11/2048 ,  G06F11/2097

Abstract: A computer system comprises an active processor and one or more spare processors. A dummy thread is created on the active processor while the active processor is running a current thread, causing the current thread to become dormant. The operating system of the active processor saves a set of internal state information for the current thread into a first memory coupled to the active processor. Each write to the first memory is duplicated in an equivalent spare memory coupled to each of the one or more spare processors. The dummy thread then activates the spare processor and de-activates the active processor.

Abstract translation: 计算机系统包括主动处理器和一个或多个备用处理器。 当活动处理器运行当前线程时，在活动处理器上创建虚拟线程，导致当前线程变为休眠状态。 主动处理器的操作系统将当前线程的一组内部状态信息保存到耦合到活动处理器的第一存储器中。 每个对第一存储器的写入被复制在耦合到一个或多个备用处理器中的每一个的等效备用存储器中。 然后，虚拟线程激活备用处理器并停用激活的处理器。

公开(公告)号：US6148247A

公开(公告)日：2000-11-14

申请号：US922584

申请日：1997-09-03

Applicant: Andrew Bennett Kaymer ,  Kelvin Maurice Cannon

Inventor： Andrew Bennett Kaymer ,  Kelvin Maurice Cannon

IPC: D05B19/08 ,  G05B19/408 ,  G05B19/4093 ,  G06F19/00

CPC classification number: G05B19/408 ,  D05B19/08 ,  G05B19/4093 ,  Y02P90/265

Abstract: A computer is operated to generate stitch data relating to an embroidery design. In the method of the invention, parameters of elements of the design are entered in the memory of the computer, said parameters being standard parameters for embroidering the design on a first type of material. First stitch data is then created in the memory of the computer for embroidering the design on the first type of material. Modified stitch data is then created in the memory of the computer for embroidering the design on a second type of material. The first stitch data or the modified stitch data, depending upon whether the design is to be embroidered onto the first type of material or onto the second type of material, is then written onto a storage medium.

Abstract translation: 操作计算机产生与刺绣设计相关的针迹数据。 在本发明的方法中，将设计元素的参数输入到计算机的存储器中，所述参数是用于在第一类材料上刺绣设计的标准参数。 然后在计算机的存储器中创建第一针迹数据，以便对第一类材料上的设计进行刺绣。 然后在计算机的存储器中创建修改的针迹数据，以便在第二种类型的材料上刺绣设计。 然后将第一针迹数据或修改后的针迹数据写入到存储介质上，这取决于是将设计绣在第一种类型的材料上还是第二种类型的材料上。

公开(公告)号：US20200255990A1

公开(公告)日：2020-08-13

申请号：US16274208

申请日：2019-02-12

Applicant: Andrew Bennett ,  Silas Hughes ,  Kristin Draper ,  David Barrett

Inventor： Andrew Bennett ,  Silas Hughes ,  Kristin Draper ,  David Barrett

IPC: D04B15/88 ,  D04B15/32

Abstract: The field of the present invention relates, in general, to apparatus and methods of knitting a material into a tubular form, where the length of such tubular form is not dictated by conventional distances between the knitting areas and the catch basins of integrated machines. In short, this invention increases the distal relationship between the needle-equipped element, which performs the knitting function, and the basin that catches the resulting tubular form of the material. The basin rotates synchronized with the rotation of the resulting tubular form. The separation facilitates the continuous production of a length of the resulting tubular form of the material. The tubular form thus can be longer than such length where, as taught in the prior art, the catch basin is fixed—as part of integrated machines—in close proximity with the element that performs the knitting. As an inventive method, the steps include (A) feeding such material into the proximity of a needle-equipped element; (B) knitting such material with such needle-equipped element to produce such resulting tubular form; (C) catching such resulting tubular form in a basin that is physically disconnected from the needle-equipped element and distanced therefrom to produce a desirably longer length of the resulting tubular form; and (D) electronically controlling such feeding step, such knitting step, and such catching step (synchronizing the catching with the rotation of resulting tubular form), whereby the rates of the feeding, knitting and catching produce such resulting tubular form that is unbuckled.

公开(公告)号：US10389019B2

公开(公告)日：2019-08-20

申请号：US15382644

申请日：2016-12-17

Applicant: Andrew Bennett ,  Krzysztof Orzel

Inventor： Andrew Bennett ,  Krzysztof Orzel

IPC: G01S7/00 ,  H01Q1/42 ,  B64C1/36 ,  B64C39/02 ,  B64D47/08 ,  B64F1/36 ,  G01S13/66 ,  G01S13/87 ,  G01S13/88 ,  G05D1/00 ,  G01S13/72 ,  G01S13/86 ,  H01Q1/00 ,  H01Q1/28 ,  H01Q1/32 ,  H01Q1/34 ,  H01Q3/34 ,  H01Q21/22 ,  G01S13/02 ,  G01S13/42

Abstract: Disclosed is the networking of the radar in manners and operating utilizing methods that result in increases in the radar coverage by adding to the possible collection of locations and thus potentially increasing the data to be analyzed—ultimately increasing the accuracy of the readings.

公开(公告)号：US20170275024A1

公开(公告)日：2017-09-28

申请号：US15082498

申请日：2016-03-28

Applicant: ANDREW BENNETT

Inventor： ANDREW BENNETT

IPC: B64F1/12 ,  B64F5/00 ,  B64D5/00 ,  B60L11/18 ,  G05D1/00 ,  G05D1/10 ,  B64F1/00 ,  B64C39/02

CPC classification number: B64F1/12 ,  B60L53/00 ,  B60L2200/10 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/20 ,  B64C2201/208 ,  B64D5/00 ,  B64F1/007 ,  B64F5/30 ,  G05D1/0011 ,  G05D1/0022 ,  G05D1/101 ,  Y02T10/7072 ,  Y02T90/14

Abstract: This document describes a system and method through which unmanned aerial vehicles (UAVs) can be docked, with a device that can secure the UAVs, and information can be transmitted to and from such UAVs. The UAVs are secured through the use of magnetic fields. The system also includes a means for transmitting information between the docking system itself, the UAV(s) and/or between the docking system and a command center, which may be a notable distance from the docking system, or among the docking system, the UAV(s) and the command center.

公开(公告)号：US09194363B2

公开(公告)日：2015-11-24

申请号：US13537520

申请日：2012-06-29

Applicant: Dmytro Floriyovych Opaits ,  Seyed Gholamali Saddoughi ,  Grover Andrew Bennett, Jr. ,  Matthew Patrick Boespflug ,  Stephen Bertram Johnson ,  Peggy Lynn Baehmann ,  Anurag Gupta

Inventor： Dmytro Floriyovych Opaits ,  Seyed Gholamali Saddoughi ,  Grover Andrew Bennett, Jr. ,  Matthew Patrick Boespflug ,  Stephen Bertram Johnson ,  Peggy Lynn Baehmann ,  Anurag Gupta

IPC: F03D1/00 ,  F03D1/04 ,  F03D1/06

CPC classification number: F03D1/04 ,  F03D1/0608 ,  F05B2240/12 ,  F05B2240/33 ,  Y02E10/721 ,  Y10T29/49316

Abstract: A deployable aerodynamic component configured to be mounted to a wind turbine. The wind turbine includes at least one rotor blade. The deployable aerodynamic component configured to be positioned in front of an inner portion of the at least one rotor blade, and is structurally configured to cover a substantial portion of the inner portion of the at least one rotor blade in a wind direction during deployment of the deployable aerodynamic component and to allow the passage therethrough of an incoming wind when non-deployed. Further described is a wind turbine including the above-described deployable aerodynamic component and method for aerodynamic performance enhancement of an existing wind turbine, wherein the method includes mounting the above-described deployable aerodynamic component to a wind turbine.

Abstract translation: 配置为安装到风力涡轮机的可部署的空气动力学部件。 风力涡轮机包括至少一个转子叶片。 所述可部署空气动力学部件被构造成定位在所述至少一个转子叶片的内部部分的前面，并且在结构上构造成在所述至少一个转子叶片的展开期间在风向方向上覆盖所述至少一个转子叶片的内部部分的大部分 可部署的空气动力学部件，并且当未部署时允许通过其中的风。 进一步描述了一种风力涡轮机，其包括上述可部署的空气动力学部件和用于现有风力涡轮机的空气动力学性能增强的方法，其中所述方法包括将上述可部署空气动力学部件安装到风力涡轮机。

公开(公告)号：US20130284273A1

公开(公告)日：2013-10-31

申请号：US13457872

申请日：2012-04-27

Applicant: Matthew Patrick Boespflug ,  Seyed Gholamali Saddoughi ,  Grover Andrew Bennett, JR. ,  Dmytro Floriyovych Opaits

Inventor： Matthew Patrick Boespflug ,  Seyed Gholamali Saddoughi ,  Grover Andrew Bennett, JR. ,  Dmytro Floriyovych Opaits

IPC: B05B1/00

CPC classification number: B64C21/08 ,  B64C21/04 ,  B64C2230/04 ,  B64C2230/06 ,  F01D5/145 ,  F03D1/0683 ,  F03D7/022 ,  F05B2240/122 ,  F05D2270/17 ,  Y02E10/721 ,  Y02E10/723 ,  Y02T50/166 ,  Y02T50/673 ,  Y10T137/0391

Abstract: A method for actively manipulating a primary fluid flow over a surface using an active flow control system including an active fluid flow device to provide lift enhancement and lift destruction. The method including the disposing of an active fluid flow device in the surface. The active fluid flow device is then operated to generate at least one of a steady blowing secondary fluid flow, a pulsed secondary fluid flow or an oscillating secondary fluid flow. While flowing the primary fluid over the surface to create a primary flow field, a secondary fluid flow is injected in an upstream direction and substantially opposed to the incoming primary fluid flow. The injecting of the secondary fluid flow in this manner provides for influencing of the primary flow field by manipulating a momentum of the secondary fluid flow to influence the incoming primary fluid flow and resultant lift.

Abstract translation: 一种用于使用包括主动流体流动装置的主动流量控制系统主动地操纵表面上的初级流体流的方法，以提供升力增强和提升破坏。 该方法包括在表面中设置活性流体流动装置。 然后使活性流体流动装置运行以产生稳定的发泡次级流体流动，脉冲的次要流体流动或振荡的次级流体流中的至少一个。 当主流体在表面上流动以产生主流场时，二次流体流在上游方向上被注入并基本上与入流的主流体流相对。 以这种方式喷射二次流体流动通过操纵次级流体流的动量来影响进入的主要流体流动和所得到的升力来提供对主流场的影响。

公开(公告)号：US20130192243A1

公开(公告)日：2013-08-01

申请号：US13362124

申请日：2012-01-31

Applicant: Matthew Patrick Boespflug ,  Seyed Gholamali Saddoughi ,  Grover Andrew Bennett, JR. ,  John Thomas Herbon

Inventor： Matthew Patrick Boespflug ,  Seyed Gholamali Saddoughi ,  Grover Andrew Bennett, JR. ,  John Thomas Herbon

IPC: F02C7/22

CPC classification number: F23C7/004 ,  F23C2900/07001 ,  F23D2212/10 ,  F23D2212/20 ,  F23D2900/00008 ,  F23R3/14 ,  F23R3/286 ,  Y02T50/675

Abstract: A fuel nozzle assembly for use with a turbine engine includes at least one fuel conduit coupled to at least one fuel source. The fuel nozzle assembly also includes at least one swirler that includes at least one wall having a porous portion. The at least one wall is coupled to the at least one fuel conduit. The porous portion is formed from a material having a porosity that facilitates fuel flow therethrough. At least one fuel flow path is thereby defined through the porous portion of the at least one wall.

Abstract translation: 与涡轮发动机一起使用的燃料喷嘴组件包括联接到至少一个燃料源的至少一个燃料管道。 燃料喷嘴组件还包括至少一个旋流器，其包括具有多孔部分的至少一个壁。 所述至少一个壁联接到所述至少一个燃料导管。 多孔部分由具有促进燃料流过其中的孔隙率的材料形成。 由此至少一个燃料流动路径通过至少一个壁的多孔部分被限定。

公开(公告)号：US20120193483A1

公开(公告)日：2012-08-02

申请号：US13016691

申请日：2011-01-28

Applicant: Katherine Anne Essenhigh ,  Fengfeng Tao ,  Grover Andrew Bennett ,  Matthew Boespflug ,  Robert C. Murray ,  Seyed Gholami Saddoughi

Inventor： Katherine Anne Essenhigh ,  Fengfeng Tao ,  Grover Andrew Bennett ,  Matthew Boespflug ,  Robert C. Murray ,  Seyed Gholami Saddoughi

IPC: B64C21/10 ,  B64C21/00

CPC classification number: B64C23/005 ,  Y02T50/166

Abstract: Systems, apparatus, and program product and methods for controlling boundary layer flow across an aerodynamic structure which can produce separate regions of flow structures at different strengths by means of dielectric-barrier-discharge (DBD) type plasmas, are provided. An example of such apparatus provides plasma regions that are capable of being individually controlled by voltage and/or frequency, and modulated for the purposes of flow control. The apparatus includes an electrode assembly fitted with electrodes on either side of a dielectric such that different electrode geometries and arrangements create isolated regions of plasmas which results in separate regions of flow structures. These regions may be further controlled and modulated by the use of electronic-switching to produce irregularly shaped flow structures and strengths including those having a primarily vertical component.

Abstract translation: 提供了用于控制跨越空气动力学结构的边界层流动的系统，装置和程序产品和方法，其可以通过介电阻挡放电（DBD）型等离子体产生不同强度的流动结构的分离区域。 这种装置的一个实例提供能够被电压和/或频率单独控制的等离子体区域，并且为了流量控制的目的进行调制。 该装置包括在电介质的任一侧上装配有电极的电极组件，使得不同的电极几何形状和布置产生等离子体的隔离区域，这导致分离的流动结构区域。 可以通过使用电子切换来进一步控制和调制这些区域，以产生不规则形状的流动结构和强度，包括具有主要垂直分量的流动结构和强度。

公开(公告)号：US08195257B2

公开(公告)日：2012-06-05

申请号：US12526121

申请日：2008-02-06

Applicant: Anthony Pallone ,  Thierry Gartner ,  Gregory Girard ,  Eric Proteau ,  John Howard ,  Andrew Bennett ,  Keith Smith ,  James E. Thompson

Inventor： Anthony Pallone ,  Thierry Gartner ,  Gregory Girard ,  Eric Proteau ,  John Howard ,  Andrew Bennett ,  Keith Smith ,  James E. Thompson

IPC: H04M1/00

CPC classification number: H01Q1/246

Abstract: The invention relates to a case assembly for antenna amplifying system, an antenna amplifying system and a mast antenna incorporating such a system. According to the invention, the case assembly for antenna amplifying system having a general shape elongated along a longitudinal axis (34) comprises a control module (16) and two amplifying modules (9a, 9b) aligned therewith along the longitudinal axis (34), the control module (16) and both amplifying modules (9a, 9b) each comprising two longitudinal lateral walls (11a, 11b, 11c, 12a, 12b, 12c), an upper surface (36a, 36b, 36c) and a lower surface (37a, 37b, 37c) and having a small thickness.

Abstract translation: 本发明涉及用于天线放大系统的壳体组件，天线放大系统和结合了这种系统的桅杆天线。 根据本发明，具有沿着纵向轴线（34）伸长的总体形状的天线放大系统的壳体组件包括控制模块（16）和沿着纵向轴线（34）与其对准的两个放大模块（9a，9b） 控制模块（16）和两个放大模块（9a，9b），每个放大模块包括两个纵向侧壁（11a，11b，11c，12a，12b，12c），上表面（36a，36b，36c）和下表面 37a，37b，37c）并且具有小的厚度。