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48 条记录 (耗时 0.028 秒)

    Stabilizing Griess reagent for explosives detection
    42.
    发明申请
    Stabilizing Griess reagent for explosives detection 审中-公开
    稳定用于爆炸物检测的Griess试剂

    公开(公告)号：US20070065944A1

    公开(公告)日：2007-03-22

    申请号：US11501375

    申请日：2006-08-08

    申请人： Peter Nunes ,  Adam Love ,  M. Carman ,  John Reynolds

    发明人： Peter Nunes ,  Adam Love ,  M. Carman ,  John Reynolds

    IPC分类号： G01N31/00

    CPC分类号： G01N31/224 ,  Y10T436/10

    摘要： The present invention provides a system wherein the Griess reagent has the ambient atmosphere removed. The present invention provides a system to treat the Griess reagent to improve storage lifetimes at room temperature or higher to over a year or more. The present invention greatly extends the useful lifetime of preparations of the Griess reagent as well as broadens the applications to field testing equipment.

    摘要翻译： 本发明提供一种其中Griess试剂除去环境气氛的系统。 本发明提供了一种治疗Griess试剂以改善室温或更高至一年或更长时间的储存寿命的系统。 本发明大大延长了Griess试剂的使用寿命，扩大了现场试验设备的应用范围。

    Spot test kit for explosives detection
    43.
    发明申请
    Spot test kit for explosives detection 审中-公开
    用于爆炸物检测的现货测试套件

    公开(公告)号：US20060216833A1

    公开(公告)日：2006-09-28

    申请号：US11159451

    申请日：2005-06-22

    申请人： Philip Pagoria ,  Richard Whipple ,  Peter Nunes ,  Joel Eckels ,  John Reynolds ,  Robin Miles ,  Marina Chiarappa-Zucca

    发明人： Philip Pagoria ,  Richard Whipple ,  Peter Nunes ,  Joel Eckels ,  John Reynolds ,  Robin Miles ,  Marina Chiarappa-Zucca

    IPC分类号： G01N33/558

    CPC分类号： G01N31/22 ,  B01L3/5023 ,  B01L3/5029 ,  B01L2200/16 ,  B01L2300/0867 ,  B01L2300/1827 ,  B01L2300/1877 ,  B01L2400/0406 ,  B01L2400/0683 ,  G01N1/02 ,  G01N33/227 ,  G01N2001/022 ,  G01N2001/028

    摘要： An explosion tester system comprising a body, a lateral flow membrane swab unit adapted to be removeably connected to the body, a first explosives detecting reagent, a first reagent holder and dispenser operatively connected to the body, the first reagent holder and dispenser containing the first explosives detecting reagent and positioned to deliver the first explosives detecting reagent to the lateral flow membrane swab unit when the lateral flow membrane swab unit is connected to the body, a second explosives detecting reagent, and a second reagent holder and dispenser operatively connected to the body, the second reagent holder and dispenser containing the second explosives detecting reagent and positioned to deliver the second explosives detecting reagent to the lateral flow membrane swab unit when the lateral flow membrane swab unit is connected to the body.

    摘要翻译： 一种爆炸测试器系统，包括主体，适于可移除地连接到主体的侧面流动的薄膜拭子单元，第一爆炸物检测试剂，可操作地连接到主体的第一试剂保持器和分配器，第一试剂保持器和分配器包含第一 爆炸物检测试剂，并且定位成当侧流膜拭子单元连接到身体时将第一炸药检测试剂输送到侧流膜拭子单元，第二爆炸物检测试剂和可操作地连接到身体的第二试剂保持器和分配器 ，所述第二试剂保持器和分配器包含所述第二炸药检测试剂，并且定位成当所述侧流膜拭子单元连接到所述主体时将所述第二炸药检测试剂输送到所述侧流膜拭子单元。

    Miniature aircraft catapult
    46.
    发明授权
    Miniature aircraft catapult 有权
    微型飞机弹射器

    公开(公告)号：US06626399B2

    公开(公告)日：2003-09-30

    申请号：US10025937

    申请日：2001-12-26

    申请人： Eric P. Young ,  John Reynolds ,  Mathew Curran ,  Joseph Wurts ,  Danny Gast

    发明人： Eric P. Young ,  John Reynolds ,  Mathew Curran ,  Joseph Wurts ,  Danny Gast

    IPC分类号： B64F106

    CPC分类号： B64F1/06 ,  A63H27/14

    摘要： A catapult for launching an aircraft is disclosed including a rail assembly having first and second ends. A support structure is provided for supporting the rail assembly above the ground at various upward angles. A container having an open end is releasably mounted on the first end of the rail assembly, the container for mounting the aircraft therein with a portion of the front end of the aircraft extending out of the open end. A device is provided for extracting the aircraft from the container and moving it from the first end to the second end of the rail assembly and release it when reaching the second end.

    摘要翻译： 公开了一种用于发射飞行器的弹射器，其包括具有第一端和第二端的导轨组件。 提供了一种支撑结构，用于以各种向上的角度将轨道组件支撑在地面上方。 具有开口端的容器可释放地安装在轨道组件的第一端上，用于将飞机安装在其中的容器具有飞行器前端的一部分延伸出开口端。 提供一种用于从容器中提取飞行器并将其从轨道组件的第一端移动到第二端并且在到达第二端时将其释放的装置。

    Parachute assembly for a miniature aircraft
    47.
    发明授权
    Parachute assembly for a miniature aircraft 失效
    降落伞装配的微型飞机

    公开(公告)号：US06565041B1

    公开(公告)日：2003-05-20

    申请号：US10028956

    申请日：2001-12-27

    申请人： Eric P. Young ,  John Reynolds ,  Mathew Curran ,  Danny Gast ,  Joseph Wurts

    发明人： Eric P. Young ,  John Reynolds ,  Mathew Curran ,  Danny Gast ,  Joseph Wurts

    IPC分类号： B64D1780

    CPC分类号： B64D17/40 ,  B64C39/024 ,  B64C39/028 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/165 ,  B64C2201/185 ,  B64D17/54 ,  B64D17/76 ,  B64D17/80

    摘要： A parachute system for a miniature aircraft having a storable parachute mounted on an upper surface of the aircraft. The system includes a canopy having a stored condition and an expanded condition. A plurality of suspension lines have first ends connected to the periphery of the canopy and second ends connected to an elastic member. First and second risers are connected by their first ends to the upper surface of the aircraft between the front end and center of gravity on either side of the longitudinal axis and by their second ends to the elastic member. A restraint system releasably restrains the parachute in the stored condition on the top surface of the aircraft; and a release system coupled to the restraint system releases the parachute upon command such that aerodynamic forces will cause the parachute to open.

    摘要翻译： 用于具有安装在飞行器的上表面上的可存放降落伞的微型飞机的降落伞系统。 该系统包括具有存储条件和扩展状态的遮篷。 多个悬挂线具有连接到顶盖的周边的第一端和连接到弹性构件的第二端。 第一和第二立管通过其第一端连接到飞行器的上表面，在纵轴的任一侧上的前端和重心之间，并且通过其第二端连接到弹性构件。 约束系统可释放地将降落伞限制在飞机顶表面上的储存状态; 并且联接到约束系统的释放系统根据命令释放降落伞，使得空气动力将使降落伞打开。

    Playload dispensing system
    48.
    发明授权
    Playload dispensing system 失效
    播放点胶系统

    公开(公告)号：US06460445B1

    公开(公告)日：2002-10-08

    申请号：US10038424

    申请日：2002-01-07

    申请人： Eric P. Young ,  John Reynolds ,  Brian Hershberger

    发明人： Eric P. Young ,  John Reynolds ,  Brian Hershberger

    IPC分类号： B64D104

    CPC分类号： B64D1/06

    摘要： A payload dispensing system for an aircraft is disclosed that includes a housing mounted to the aircraft. A hollow shaft is mounted to the housing having an open first end and a closed off second end with a hole therethrough. The payload includes an aperture having a first end on an external surface thereof and a second end in the interior therein. A wire cable releasably secures the payload to the housing such that the hollow shaft extends into the aperture of the payload. A compression spring is mounted at least partially within the hollow shaft, having a first end in contact with the second end of the hollow shaft and a second end in contact with the second end of the aperture within the payload, the spring having a compressed position when the hollow shaft is within the aperture in the payload and asserts a force tending to separate the payload from the aircraft. A cable cutter is used to cut the cable to release the payload from the housing, such that the spring forces the payload away from the aircraft and the hollow shaft guides the payload during separation.

    摘要翻译： 公开了一种用于飞机的有效载荷分配系统，其包括安装到飞行器的壳体。 空心轴安装到壳体上，其具有敞开的第一端和封闭的第二端，其中穿过孔。 有效载荷包括其外表面上具有第一端并且其内部具有第二端的孔。 线缆可释放地将有效载荷固定到壳体，使得空心轴延伸到有效载荷的孔中。 压缩弹簧至少部分地安装在中空轴内，其具有与中空轴的第二端接触的第一端和与有效载荷内的孔的第二端接触的第二端，弹簧具有压缩位置 当空心轴在有效载荷内的孔内时，并且确定趋向于将有效载荷与飞行器分开的力。 电缆切割器用于切割电缆以从壳体释放有效载荷，使得弹簧迫使有效载荷远离飞行器，空心轴在分离期间引导有效载荷。