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    Powerhead Control in a Power Injection System
    12.
    发明申请
    Powerhead Control in a Power Injection System 有权
    动力喷射系统中的动力头控制

    公开(公告)号：US20070100282A1

    公开(公告)日：2007-05-03

    申请号：US11551804

    申请日：2006-10-23

    Applicant: James Small ,  David Brooks ,  Charles Neer ,  Frank Fago ,  Gary Wagner ,  Elaine Borgemenke ,  Sean Lafferty

    Inventor： James Small ,  David Brooks ,  Charles Neer ,  Frank Fago ,  Gary Wagner ,  Elaine Borgemenke ,  Sean Lafferty

    IPC: A61M1/00 ,  G05D7/00 ,  A61B6/00 ,  G06F3/00 ,  G05D11/00 ,  G06F17/00 ,  G06F9/00

    CPC classification number: A61M5/14566 ,  A61M5/007 ,  A61M5/16827 ,  A61M2205/13 ,  A61M2205/3362 ,  A61M2205/502 ,  A61M2205/505 ,  A61M2205/583 ,  A61M2205/6018 ,  G06F19/00

    Abstract: A dual head contrast media injection system performs a patency check or test injection, determining flow rate and/or flow volume from the programmed protocol. The tubing that connects syringes to a patient shares only a short common section near to the patient. Appropriate injection steps are taken to compensate for tubing elasticity. A wireless remote control and a touch screen control are provided, improving functionality and information delivery. The display brightness is controlled based on the ambient light, and the display panel includes a double swivel permitting re-orientation. The orientation of the display may also be controlled based on, e.g., the current step, the tilt angle of the powerhead, or a manual control. Furthermore, the display is customizable to identify the type of fluid (contrast, saline, etc.) on either side of the injector, to provide matched color coding, and to provide a folder/tab analogy for retrieving injection protocol parameters.

    Abstract translation: 双头造影剂注射系统执行通畅检查或测试注射，从编程的协议确定流量和/或流量。 将注射器连接到患者的管道仅在病人附近分配一个短的共同部分。 采取适当的注射步骤来补偿管道弹性。 提供无线遥控器和触摸屏控制器，改善功能和信息传递。 基于环境光来控制显示亮度，并且显示面板包括允许重新定向的双重旋转。 还可以基于例如当前步骤，动力头的倾斜角度或手动控制来控制显示器的取向。 此外，显示器可定制以识别注射器两侧的流体类型（对比度，盐水等），以提供匹配的颜色编码，并提供用于检索注射方案参数的文件夹/片段类比。

    Mass spectrometer for entrained particles, and method for measuring masses of the particles
    14.
    发明申请
    Mass spectrometer for entrained particles, and method for measuring masses of the particles 有权

    公开(公告)号：US20050077463A1

    公开(公告)日：2005-04-14

    申请号：US10685830

    申请日：2003-10-14

    Applicant: James Small ,  Jon Leonard

    Inventor： James Small ,  Jon Leonard

    IPC: C12M1/34 ,  H01J49/00

    CPC classification number: G01N29/14 ,  G01N2291/02408 ,  G01N2291/02466 ,  G01N2291/02809

    Abstract: A particle mass spectrometer includes a supersonic flow expansion nozzle, and a source of a gas having particles entrained therein. The source is in gas-flow communication with an inlet of the expansion nozzle. The particle mass spectrometer further includes a vacuum chamber in gas-flow communication with an outlet of the expansion nozzle, wherein the vacuum chamber has a sufficient vacuum that a gas flow through the expansion nozzle is supersonic, and a microphone having an active element and an output signal responsive to a movement of the active element. The active element is disposed within the vacuum chamber and is positioned so that particles that flow from the outlet of the expansion nozzle impact upon the active element. The output signal of the active element of the microphone is a measure of the masses of the entrained particles.

    Method and system for inflight refueling of unmanned aerial vehicles
    15.
    发明申请
    Method and system for inflight refueling of unmanned aerial vehicles 有权
    无人驾驶飞行器车载加油方法与系统

    公开(公告)号：US20090045290A1

    公开(公告)日：2009-02-19

    申请号：US11891959

    申请日：2007-08-13

    Applicant: James Small ,  Frederick Davidson ,  Carlos Garcia

    Inventor： James Small ,  Frederick Davidson ,  Carlos Garcia

    IPC: B64D39/06 ,  G05D1/00

    CPC classification number: B64C39/024 ,  B64D39/00 ,  B64D39/04 ,  G05D1/104

    Abstract: A system and method for refueling unmanned aerial vehicles. The system is adapted to refuel a first unmanned aerial vehicle from a second unmanned aerial vehicle and includes an arrangement for flying the first and second vehicles to proximity within a predetermined range and for connecting an umbilical from the second vehicle to the first vehicle in flight. In the illustrative embodiment, the arrangement for connecting includes a targeting system for electromagnetically detecting a refueling receptacle on the first vehicle. The targeting system includes a first coil around a refueling receptacle on the first vehicle. A seeker is disposed at a first end of said umbilical on the second vehicle. The seeker includes three detector coils adapted to detect a magnetic signal from the first coil around the receptacle on the first vehicle. The coils are mounted such that the detector coils point in different directions. The outputs of the coils are processed to determine the direction and range to the UAV from the tanker UAV.

    Abstract translation: 一种用于加油无人机的系统和方法。 该系统适用于将第一无人驾驶飞行器从第二无人驾驶飞行器加油并且包括用于使第一和第二车辆在预定范围内飞行接近的装置，并用于将脐带与第二车辆连接至飞行中的第一车辆。 在说明性实施例中，连接装置包括用于电磁检测第一车辆上的加油容器的瞄准系统。 瞄准系统包括围绕第一车辆上的加油容器的第一线圈。 在第二车辆上的所述脐带的第一端设置探测器。 探测器包括三个检测器线圈，其适于在第一车辆上的容器周围检测来自第一线圈的磁信号。 线圈被安装成使得检测器线圈指向不同的方向。 处理线圈的输出以确定来自油罐无人机的UAV的方向和范围。

    MULTI-LAYERED TEXTILE STRUCTURES FOR FLAME RESISTANT MATTRESSES
    16.
    发明申请
    MULTI-LAYERED TEXTILE STRUCTURES FOR FLAME RESISTANT MATTRESSES 有权
    多层耐火材料的纺织结构

    公开(公告)号：US20080045110A1

    公开(公告)日：2008-02-21

    申请号：US11870804

    申请日：2007-10-11

    Applicant: James Small ,  John Walton

    Inventor： James Small ,  John Walton

    IPC: B32B5/26 ,  B32B37/14

    CPC classification number: B32B5/26 ,  A47C31/001 ,  Y10S428/92 ,  Y10S428/921 ,  Y10T442/2631 ,  Y10T442/659 ,  Y10T442/696

    Abstract: Mattress panels and mattresses (including mattress foundations) that satisfy the rigorous requirements of new and promulgated state and federal regulations regarding flammability of mattresses, such as Technical Bulletin 603 of the State of California department of Consumer Affairs (TB-603) and U.S. Consumer Product Safety Commission Standard for Flammability of Mattresses and Mattress/Foundation Sets (16 CFR 1633), are provided. A mattress includes one or more panels of material assembled as a non-quilted, non-perforated, multi-layered structure, wherein the mattress maintains flame and heat resistant integrity when impinged with a gas flame in accordance with the testing protocol set forth in Technical Bulletin 603 of the State of California department of Consumer Affairs (TB-603) and/or in accordance with the testing protocol set forth in U.S. Consumer Product Safety Commission Standard for Flammability of Mattresses and Mattress/Foundation Sets (16 CFR 1633).

    Abstract translation: 满足新颁布的州和联邦关于床垫可燃性的规定的严格要求的床垫和床垫（包括床垫基础），例如加利福尼亚州消费者事务部（TB-603）的技术公报603和美国消费品 提供了床垫和床垫/基础套件的可燃性安全委员会标准（16 CFR 1633）。 床垫包括一个或多个材料面板，其被组装成非绗缝的，非穿孔的多层结构，其中当根据技术上所述的测试方案撞击气体火焰时，床垫保持火焰和耐热完整性 加利福尼亚州消费者事务部（TB-603）和/或根据美国消费品安全委员会床垫和床垫/基础套件易燃性标准（16 CFR 1633）中规定的测试方案的公告603。

    Multi-layered textile structures for flame resistant mattresses
    17.
    发明申请
    Multi-layered textile structures for flame resistant mattresses 审中-公开
    用于阻燃床垫的多层纺织结构

    公开(公告)号：US20070141938A1

    公开(公告)日：2007-06-21

    申请号：US11639883

    申请日：2006-12-15

    Applicant: James Small ,  John Walton

    Inventor： James Small ,  John Walton

    IPC: B32B5/26

    CPC classification number: A47C31/001 ,  B32B5/26 ,  B32B7/12 ,  B32B2250/20 ,  B32B2262/0253 ,  B32B2262/0276 ,  B32B2262/067 ,  B32B2307/3065 ,  B32B2479/00 ,  B32B2601/00 ,  Y10T442/3472 ,  Y10T442/3528 ,  Y10T442/3976

    Abstract: Mattress panels and mattresses (including mattress foundations) that satisfy the rigorous requirements of new and promulgated state and federal regulations regarding flammability of mattresses, such as Technical Bulletin 603 of the State of California department of Consumer Affairs (TB-603) and U.S. Consumer Product Safety Commission Standard for Flammability of Mattresses and Mattress/Foundation Sets (16 CFR 1633), are provided. A mattress includes one or more panels of material assembled as a non-quilted, non-perforated, multi-layered structure, wherein the mattress maintains flame and heat resistant integrity when impinged with a gas flame in accordance with the testing protocol set forth in Technical Bulletin 603 of the State of California department of Consumer Affairs (TB-603) and/or in accordance with the testing protocol set forth in U.S. Consumer Product Safety Commission Standard for Flammability of Mattresses and Mattress/Foundation Sets (16 CFR 1633).

    Abstract translation: 满足新颁布的州和联邦关于床垫可燃性的规定的严格要求的床垫和床垫（包括床垫基础），例如加利福尼亚州消费者事务部（TB-603）的技术公报603和美国消费品 提供了床垫和床垫/基础套件的可燃性安全委员会标准（16 CFR 1633）。 床垫包括一个或多个材料面板，其被组装成非绗缝的，非穿孔的多层结构，其中当根据技术上所述的测试方案撞击气体火焰时，床垫保持火焰和耐热完整性 加利福尼亚州消费者事务部（TB-603）和/或根据美国消费品安全委员会床垫和床垫/基础套件易燃性标准（16 CFR 1633）中规定的测试方案的公告603。

    Powerhead of a Power Injection System
    18.
    发明申请
    Powerhead of a Power Injection System 有权
    动力注射系统的动力头

    公开(公告)号：US20070106153A1

    公开(公告)日：2007-05-10

    申请号：US11551792

    申请日：2006-10-23

    Applicant: Charles Neer ,  Jonathan Gibbs ,  John Bruce ,  Robert Ziemba ,  David Brooks ,  James Small ,  Gary Wagner

    Inventor： Charles Neer ,  Jonathan Gibbs ,  John Bruce ,  Robert Ziemba ,  David Brooks ,  James Small ,  Gary Wagner

    IPC: A61M5/00

    CPC classification number: A61M5/007 ,  A61B6/548 ,  A61M5/14546 ,  A61M5/14566 ,  A61M5/16827 ,  A61M5/1785 ,  A61M2205/3306 ,  A61M2205/3317 ,  A61M2205/3389 ,  A61M2205/502 ,  A61M2205/52 ,  A61M2205/587 ,  A61M2205/6054 ,  A61M2205/6063

    Abstract: A contrast media injection system includes detects the absolute position of the syringe ram using a non-contact sensor. A series of magnets and Hall-Effect sensors may be used or an opto-reflective system. Illuminated knobs that are connected to the drive mechanism for the syringe ram rotate with the drive and provide visual feedback on operation through the illumination. Analog Hall-Effect sensors are used to determine the presence or absence of magnets that identify the type of faceplate being used. The faceplates include control electronics, connected to the powerhead through connectors, which may be interchangeably used by the two faceplates. The faceplate electronics include detectors for automatically detecting the capacity of pre-filled syringes. Additional features include using historical data to provide optimum pressure limit values during an injection protocol, a removable memory device for storing and transferring information such as injection protocols and injector statistics, and password protection of such protocols.

    Abstract translation: 造影剂注射系统包括使用非接触传感器检测注射器柱塞的绝对位置。 可以使用一系列磁体和霍尔效应传感器或光反射系统。 连接到注射器柱塞的驱动机构的照明旋钮随驱动器旋转，并通过照明提供对操作的视觉反馈。 使用模拟霍尔效应传感器来确定是否存在识别所使用面板类型的磁体。 面板包括通过连接器连接到动力头的控制电子装置，其可由两个面板互换使用。 面板电子设备包括用于自动检测预填充注射器容量的检测器。 附加功能包括使用历史数据在注射协议期间提供最佳压力极限值，用于存储和传送诸如注射协议和注射器统计信息的可移除存储器装置以及这些协议的密码保护。

    ROTATING FLYING WING AIRCRAFT AND CONTROL SYSTEM
    20.
    发明申请
    ROTATING FLYING WING AIRCRAFT AND CONTROL SYSTEM 有权
    旋转飞行器飞行器和控制系统

    公开(公告)号：US20060011778A1

    公开(公告)日：2006-01-19

    申请号：US10891588

    申请日：2004-07-15

    Applicant: James Small ,  Donald Lacey ,  Lloyd Kinsey ,  Mark Zepeda

    Inventor： James Small ,  Donald Lacey ,  Lloyd Kinsey ,  Mark Zepeda

    IPC: B64C15/00

    CPC classification number: B64C39/00

    Abstract: A rotating wing aircraft has a rotating fuselage and wings. The aircraft is configured to rotate with the air passing over the wings because of the rotation providing the lift needed to keep the aircraft aloft. The wings have rudders coupled to them, such as at the tips of the wings, to provide force for laterally moving the aircraft. The aircraft may be able to remain airborne by hovering for a long period of time, on the order of days. Power for the aircraft may be provided by a central diesel electric generator, which provides power for electric motors that turn propellers that are on the wings. The aircraft may be used for any of a variety of applications, such as for surveillance, communications, or as a radar platform.

    Abstract translation: 旋翼机具有旋转的机身和机翼。 飞机被配置为随着空气通过机翼而旋转，因为旋转提供了使飞机保持高空所需的升力。 机翼具有与它们相连的方向舵，例如在翼的顶端，以提供用于横向移动飞行器的力。 飞机可以通过在几天的时间内长时间徘徊而保持机载。 飞机的动力可以由中央柴油发电机提供，该发电机为转动在机翼上的螺旋桨的电动机提供动力。 该飞机可用于任何各种应用，例如用于监视，通信或作为雷达平台。

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