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    Method and system for inflight refueling of unmanned aerial vehicles
    12.
    发明授权
    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：US08056860B2

    公开(公告)日：2011-11-15

    申请号：US12806377

    申请日：2010-08-10

    Applicant: James Small ,  Frederick Davidson ,  Carlos Garcia

    Inventor： James Small ,  Frederick Davidson ,  Carlos Garcia

    IPC: B64D39/00

    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。

    Mass spectrometer for entrained particles, and method for measuring masses of the particles
    15.
    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
    16.
    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
    17.
    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
    18.
    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。

    Magnetron anode design for short wavelength operation
    19.
    发明申请
    Magnetron anode design for short wavelength operation 有权
    磁控管阳极设计为短波长工作

    公开(公告)号：US20060097183A1

    公开(公告)日：2006-05-11

    申请号：US10982591

    申请日：2004-11-05

    Applicant: C. Baker ,  James Small

    Inventor： C. Baker ,  James Small

    IPC: G01J1/42

    CPC classification number: H01J23/02 ,  H01J25/56

    Abstract: An electromagnetic radiation source is disclosed. The electromagnetic radiation source includes an anode having a first conductor, a second conductor positioned relative to the first conductor, a plurality of pole pieces coupled to at least one of the first conductor and the second, and at least one mechanical phase reversal positioned along the first conductor or second conductor. Adjacent pole pieces are separated by a gap. The electromagnetic radiation source also includes a cathode separated from the anode by an anode-cathode space, electrical contacts for applying a dc voltage between the anode and the cathode and establishing an electric field across the anode-cathode space, and at least one magnet arranged to provide a dc magnetic field within the anode-cathode space generally normal to the electric field. Electrons emitted from the cathode are influenced by the electric and magnetic fields to follow a path through the anode-cathode space and pass in close proximity to the plurality of pole pieces, and the gaps between adjacent pole pieces provide fringing fields which interact with the electrons to produce single mode operation at a desired operating frequency.

    Abstract translation: 公开了电磁辐射源。 电磁辐射源包括具有第一导体的阳极，相对于第一导体定位的第二导体，耦合到第一导体和第二导体中的至少一个的多个极片以及沿着第一导体定位的至少一个机械相反转 第一导体或第二导体。 相邻的极片被间隙隔开。 电磁辐射源还包括通过阳极 - 阴极空间从阳极分离的阴极，用于在阳极和阴极之间施加直流电压并在阳极 - 阴极空间之间建立电场的电触点，以及布置成 以在通常垂直于电场的阳极 - 阴极空间内提供直流磁场。 从阴极发射的电子受到电场和磁场的影响，沿着通过阳极 - 阴极空间的路径并且靠近多个极片并且相邻极片之间的间隙提供与电子相互作用的边缘场 以在期望的工作频率下进行单模操作。

    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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