FLUID DISPENSING DEVICE
    2.
    发明申请
    FLUID DISPENSING DEVICE 审中-公开
    流体分配装置

    公开(公告)号:US20160039657A1

    公开(公告)日:2016-02-11

    申请号:US14715346

    申请日:2015-05-18

    IPC分类号: B67D7/18 B67D7/74 B67D7/02

    摘要: A fluid dispensing device is provided. The fluid dispensing device includes a dispensing cylinder and a first inlet and a second inlet configured to facilitate intake of one of or more fluids into the dispensing cylinder. The first inlet is disposed within a first container on which the fluid dispensing device is mounted. The first inlet and the second inlet are configured to facilitate intake of only one fluid into the dispensing cylinder at a given point in time. The fluid dispensing device also includes a first outlet and a second outlet configured to dispense the one or more fluids. The first outlet and the second outlet are configured to dispense only one fluid out of the dispensing cylinder at a given point in time. The fluid dispensing device further includes a valve assembly fluidically coupled to the first inlet and the second inlet, and to the first outlet and the second outlet. The valve assembly is configured to control flow of the fluids within and/or out of the dispensing cylinder.

    摘要翻译: 提供流体分配装置。 流体分配装置包括分配筒,以及第一入口和第二入口,其构造成便于将一种或多种流体吸入分配筒。 第一入口设置在其中安装有流体分配装置的第一容器内。 第一入口和第二入口构造成便于在给定的时间点仅使一种流体进入分配缸。 流体分配装置还包括构造成分配一种或多种流体的第一出口和第二出口。 第一出口和第二出口构造成在给定的时间点仅将一个流体从分配缸中分配出来。 流体分配装置还包括流体耦合到第一入口和第二入口以及第一出口和第二出口的阀组件。 阀组件被配置成控制流体在分配筒内和/或出分配筒内的流动。

    Beam summing apparatus for RCS measurements of large targets
    3.
    发明授权
    Beam summing apparatus for RCS measurements of large targets 失效
    用于RCS测量大目标的光束求和装置

    公开(公告)号:US5281972A

    公开(公告)日:1994-01-25

    申请号:US949912

    申请日:1992-09-24

    申请人: Atul Jain

    发明人: Atul Jain

    IPC分类号: G01S7/41 G01S13/90 G01S13/00

    CPC分类号: G01S7/41 G01S13/9035

    摘要: Systems and methods for measuring RCS patterns of large targets in a compact target range having limited size. The present invention utilizes a compact range whose sweet spot (corresponding to the imaged area of the target) is much smaller than the target size. Inverse synthetic array radar (ISAR) images of successive sections of the target are registered to form a composite image of the whole target. The image is then Fourier transformed to generate an RCS value of the full target. This procedure is repeated for successive measurement angles, an RCS versus .theta. plot is generated corresponding to the RCS pattern of the target. The multiple images may be generated by translating the target and computing RCS plots of the target by combining the multiple images produced during translation, or generating the the multiple images by moving feeds or using multiple feeds of the ISAR system.

    摘要翻译: 用于测量具有有限尺寸的紧凑目标范围内的大目标的RCS图案的系统和方法。 本发明利用了一个紧凑的范围,其甜点(对应于目标的成像区域)远小于目标尺寸。 注册目标的连续部分的反向合成阵列雷达(ISAR)图像以形成整个目标的合成图像。 然后对图像进行傅里叶变换以产生完整目标的RCS值。 对于连续的测量角度重复该过程,产生对应于目标的RCS图案的RCS对(θ)图。 可以通过组合翻译过程中产生的多个图像来翻译目标和计算RCS图,或通过移动馈送或使用ISAR系统的多个馈送来生成多个图像来生成多个图像。

    Method and apparatus for .DELTA.K synthetic aperture radar measurement
of ocean current
    4.
    发明授权
    Method and apparatus for .DELTA.K synthetic aperture radar measurement of ocean current 失效
    用于DELTA K合成孔径雷达测量海洋电流的方法和装置

    公开(公告)号:US4509048A

    公开(公告)日:1985-04-02

    申请号:US359382

    申请日:1982-03-18

    申请人: Atul Jain

    发明人: Atul Jain

    IPC分类号: G01S13/90 G01S13/95

    CPC分类号: G01S13/9011 G01S13/955

    摘要: A synthetic aperture radar (10) is employed for .DELTA.k measurement of ocean current from a spacecraft (11) without the need for a narrow beam and long observation times. The SAR signal is compressed (12) to provide image data for different sections of the chirp bandwidth, equivalent to frequencies f.sub.1 (t.sub.a,t), f.sub.2 (t.sub.a,t) . . . f.sub.n (t.sub.a,t), and a common area for the separate image fields is selected (14). The image for the selected area at each frequency is deconvolved (16) to obtain the image signals for the different frequencies (f.sub.1, f.sub.2 . . . f.sub.n) and the same area. A product of pairs of signals is formed (18, 20), Fourier transformed (22) and squared (24). The spectrum thus obtained from different areas for the same pair of frequencies f.sub.jk, f.sub.j+n,k are added (26) to provide an improved signal to noise ratio. The shift of the peak from the center of the spectrum is measured and compared (28) to the expected shift due to the phase velocity of the Bragg scattering wave. Any difference is a measure of current velocity v.sub.c (.DELTA.k).

    摘要翻译: 使用合成孔径雷达(10)来进行DELTA k测量来自航天器(11)的海洋电流,而不需要窄波束和长的观测时间。 SAR信号被压缩(12),为啁啾带宽的不同部分提供图像数据,相当于频率f1(ta,t),f2(ta,t)。 的。 的。 fn(ta,t),并且分离图像字段的公共区域被选择(14)。 对每个频率下的所选区域的图像进行去卷积(16),以获得不同频率(f1,f2 ... fn)和相同区域的图像信号。 形成信号对的乘积(18,20),傅里叶变换(22)和平方(24)。 对于同一对频率fjk,fj + n,k,从不同区域获得的频谱相加(26)以提供改善的信噪比。 测量峰值从光谱中心的偏移,并与布拉格散射波相位速度的预期偏移进行比较(28)。 任何差异是当前速度vc(DELTA k)的度量。

    Multibeam single frequency synthetic aperture radar processor for
imaging separate range swaths
    5.
    发明授权
    Multibeam single frequency synthetic aperture radar processor for imaging separate range swaths 失效
    Multibeam单频合成孔径雷达处理器,用于成像分离范围的条纹

    公开(公告)号:US4355311A

    公开(公告)日:1982-10-19

    申请号:US165910

    申请日:1980-07-03

    IPC分类号: G01S13/90 G01S13/00

    CPC分类号: G01S13/9005

    摘要: A single-frequency multibeam synthetic aperture radar for large swath imaging is disclosed. Each beam illuminates a separate "footprint" (i.e., range and azimuth interval). The distinct azimuth intervals for the separate beams produce a distinct Doppler frequency spectrum for each beam. After range correlation of raw data, an optical processor develops image data for the different beams by spatially separating the beams to place each beam of different Doppler frequency spectrum in a different location in the frequency plane as well as the imaging plane of the optical processor. Selection of a beam for imaging may be made in the frequency plane by adjusting the position of an aperture, or in the image plane by adjusting the position of a slit. The raw data may also be processed in digital form in an analogous manner.

    摘要翻译: 公开了一种用于大幅面成像的单频多波段合成孔径雷达。 每个光束照亮单独的“足迹”(即,范围和方位角间隔)。 单独光束的不同方位角间隔为每个光束产生不同的多普勒频谱。 在原始数据的范围相关之后,光学处理器通过空间分离光束来形成不同波束的图像数据,以将不同多普勒频谱的每个波束放置在频率平面中的不同位置以及光学处理器的成像平面。 用于成像的光束的选择可以通过调整光圈的位置或者通过调节狭缝的位置在像平面中在频率平面中进行。 原始数据也可以以类似的方式以数字形式进行处理。

    Airport surface monitoring and runway incursion warning system
    6.
    发明授权
    Airport surface monitoring and runway incursion warning system 失效
    机场地面监测和跑道侵入预警系统

    公开(公告)号:US5629691A

    公开(公告)日:1997-05-13

    申请号:US451597

    申请日:1995-05-26

    申请人: Atul Jain

    发明人: Atul Jain

    摘要: An airport runway incursion warning system for monitoring air and ground traffic at an airport. The system is optimally used with an aircraft that has an electronic tag or interrogation system that stores identification information regarding the aircraft, and an RF transponder for receiving interrogation signals and for transmitting the identification information in response thereto. A radar system comprises a plurality of radar sensor units disposed at predetermined installation sites adjacent to a runway. Each radar sensor unit typically has an interface processor and telemetry electronics for communication, although hard-wired communication paths may be used. An RF/telemetry interface is provided for communicating with the radar sensor units when the interface processor and telemetry electronics are used. The RF/telemetry interface is also used to transmit the interrogation signals to the aircraft and receive the identification information therefrom. A central processing unit is coupled to the radar sensor units for receiving and integrating radar data produced by each the radar sensor units to produce a map of the runway that identifies authorization objects and aircraft that do not constitute intrusion threats, and intruding objects that do constitute intrusion threats to the runway. The central processing unit is optionally coupled to the RF/telemetry interface for transmitting signals to and from the aircraft, and in this case, the central processing unit processes identification information received from the aircraft to integrate the identification information into to generate a displayed image. An operator display is coupled to the central processing unit for displaying the map and identification information generated thereby for use by an operator.

    摘要翻译: 机场跑道入侵预警系统,用于监控机场的空中和地面交通。 该系统与具有存储关于飞行器的识别信息的电子标签或询问系统的飞行器最佳地使用,以及用于接收询问信号的RF应答器以及响应于其发送识别信息。 雷达系统包括设置在与跑道相邻的预定安装地点的多个雷达传感器单元。 尽管可以使用硬连线的通信路径,但每个雷达传感器单元通常具有用于通信的接口处理器和遥测电子装置。 当使用接口处理器和遥测电子设备时,提供RF /遥测接口用于与雷达传感器单元通信。 RF /遥测接口还用于将询问信号发送到飞机并从其接收识别信息。 中央处理单元耦合到雷达传感器单元,用于接收和整合由每个雷达传感器单元产生的雷达数据,以产生跑道的地图,其识别不构成入侵威胁的授权对象和飞机,以及构成的入侵物体 对跑道的入侵威胁。 中央处理单元可选地耦合到RF /遥测接口,用于向飞机发送信号,并且在这种情况下,中央处理单元处理从飞机接收的识别信息以将识别信息集成以生成显示的图像。 操作者显示器耦合到中央处理单元,用于显示由此产生的地图和识别信息供操作者使用。

    Bistatic angle-cued radar system and processing method
    7.
    发明授权
    Bistatic angle-cued radar system and processing method 失效
    双向角度雷达系统及其处理方法

    公开(公告)号:US5608407A

    公开(公告)日:1997-03-04

    申请号:US423076

    申请日:1995-04-17

    IPC分类号: G01S13/00 G01S13/48 G01S13/46

    CPC分类号: G01S13/003 G01S13/48

    摘要: A radar system and method employing a radar with an electronically scanned antenna array for estimating range and range rate to a target using angle cueing only. The radar transmits radar pulses at the target and searches the projection of the line-of-sight to the target on the ground for ground-bounce returns associated with each transmitted pulse. A processor coupled to the radar and processes the ground-bounce returns to determine an angle corresponding to the maximum reflected multipath ground-bounce return when the antenna array scans the ground. The angle data derived from processing the multipath ground-bounce returns permits computation of the range to and range rate of the target.

    摘要翻译: 一种使用具有电子扫描天线阵列的雷达的雷达系统和方法,用于仅使用角度提示来估计到目标的范围和距离率。 雷达在目标处发射雷达脉冲,并将视线的投影搜索到地面上的目标,以与每个发射的脉冲相关的地面反弹返回。 处理器耦合到雷达并处理地面反弹返回以确定当天线阵列扫描地面时对应于最大反射多径地面反弹返回的角度。 从处理多路径反跳返回得到的角度数据允许计算目标的范围和范围速率。

    System for relative motion detection between wave transmitter-receiver
and irregular reflecting surface
    8.
    发明授权
    System for relative motion detection between wave transmitter-receiver and irregular reflecting surface 失效
    波发射机 - 接收机和不规则反射面之间的相对运动检测系统

    公开(公告)号:US4210399A

    公开(公告)日:1980-07-01

    申请号:US879046

    申请日:1978-02-21

    申请人: Atul Jain

    发明人: Atul Jain

    IPC分类号: G01P3/36 G01P3/80

    CPC分类号: G01P3/36 G01P3/806

    摘要: Apparatus for detecting relative motion between a rough reflecting surface and a wave transmitting and receiving system in a plane parallel or perpendicular to the reflecting surface comprised of a transmitter (radar, laser, acoustic, and the like), a receiver having the same or different aperture as the transmitter, and means for detecting the finest interference fringes in the reflected wave pattern. Each fringe detected represents relative motion through a distance, S, that is a function of the maximum dimension, D, of the transmitting aperture. By counting fringes, total relative motion is determined, and by counting fringes for a unit of time, the rate of that motion is determined. For a small transmitting aperture, the distance, S, between fringes is directly related to kD in the parallel plane and to kD/tan .theta., in the normal plane, where .theta. is the angle between a reference axis normal to the reflecting surface and the axis of the receiving aperture, and k is a calibration constant equal to unity when the transmitting and receiving apertures are at the same distance, H, from the reflecting surface. For a large aperture, S.perspectiveto..lambda.H/kD in the parallel plane and S.perspectiveto..lambda.H/kD tan .theta. in the normal plane. In either plane, for the condition of k.perspectiveto.1, the spacing S.perspectiveto..lambda.H/D and S.perspectiveto..lambda.H/D tan .theta. can be measured with a linear scan array so that with .lambda., D and .theta. known, the distance H can be determined.

    摘要翻译: 用于检测平行或垂直于由发射器(雷达,激光,声学等)组成的反射表面的平面中的粗糙反射表面和波发射和接收系统之间的相对运动的装置,具有相同或不同的接收器 孔径作为发射器,以及用于检测反射波图案中最好的干涉条纹的装置。 每个检测到的边缘表示通过距离S的相对运动,S是发射孔径的最大尺寸D的函数。 通过计算边缘,确定总相对运动,并且通过对一个单位时间的边缘计数,确定该运动的速率。 对于小的发射孔径,条纹之间的距离S与平行平面中的kD直线相关,并且在正常平面中与kD /tanθ直接相关,其中θ是垂直于反射表面的参考轴与 并且k是当发射和接收孔径距反射表面相同距离H时的校准常数等于1。 对于大孔径,平行平面中的S&persp&lambda H / kD和正常平面中的S&persp&lambda H / kDtanθ。 在任一平面中,对于k&persp&1的条件,可以用线性扫描阵列测量间距S&persp&lambda H / D和S&persp&lambda H / Dtanθ,以便利用λ,D和θ知道距离H 可以确定。