公开(公告)号：EP0407682A2

公开(公告)日：1991-01-16

申请号：EP90101735.0

申请日：1990-01-29

申请人： THE BOEING COMPANY

发明人： Pinson, George T.

IPC分类号： B29C47/12 ,  G02B6/44

CPC分类号： B29C47/02 ,  B29C47/0014 ,  B29C47/0016 ,  B29C47/003 ,  B29C47/0033 ,  B29C47/0066 ,  B29C47/025 ,  B29C47/027 ,  B29C47/124 ,  B29C47/20 ,  G02B6/4489

摘要： Apparatus including an extruder, a die (110) having movable elements (112) defining the die opening, and die element drive solenoids for varying the dimensions of the die opening during extrusion function to yield an elongated body having a varying axial cross-section. Individual die member drive means (122) and a controller (138) are used with the apparatus to produce smoothly varying, complex cross-sectional shapes in elongated bodies such as optical fibers for various applications.

摘要翻译： 装置，包括在挤出机，是具有（110）的可动元件（112），限定了开口，并且所述元件驱动螺线管挤出功能期间改变模具开口的尺寸以产生具有变化的轴向横截面的细长体。 个别构件驱动装置（122）和控制器（138）使用具有产生在细长体平滑变化的，复杂的横截面形状的装置，包括：如用于各种应用的光纤。

公开(公告)号：EP0393237A2

公开(公告)日：1990-10-24

申请号：EP89114455.2

申请日：1989-08-04

申请人： THE BOEING COMPANY

发明人： Pinson, George T.

IPC分类号： F41G7/32 ,  F42B15/04 ,  H04B10/22

CPC分类号： G02B6/4457 ,  F41G7/32 ,  F42B15/04 ,  H04B10/25

摘要： Apparatus for optical fiber data link between tow moving bodies remote controlled vehicle/missile such as ("RCV") (12) and hereinafter launch platform (17) includes fiber-wound bobbins having opposite winding directions on each body, interconnected with unwound, reinforced fiber sections, for streaming deployment from each bobbin through tensioning devices during relative separation movement between the two bodies. Image sensors and flight control mechanisms are operatively connected through an electric/optical I/O device to the fiber on the bobbin in the RCV (12), and data analysis/display devices and controller/command units are similarly interfaced with the fiber on the bobbin associated with the helicopter (17). The bobbin housing on the helicopter uses a shaped cavity and gimbal mount to provide free-­streaming fiber deployment and pyrotechin or electro-­mechanical separation device to discharge the bobbin and attached fiber after mission completion.

摘要翻译： 遥控车辆/导弹（“RCV”）（12）和以后的发射平台（17）之间的光纤数据链路的装置包括在每个主体上具有相反卷绕方向的纤维缠绕线轴，与解开的，加强的 纤维部分，用于在两个物体之间的相对分离运动期间通过张紧装置从每个筒管流动展开。 图像传感器和飞行控制机构通过电/光I / O设备可操作地连接到RCV（12）中的线轴上的光纤，数据分析/显示设备和控制器/命令单元也类似地与光纤上的光纤 与直升机相关联的线轴（17）。 直升机上的绕线管外壳采用成形的腔体和万向架安装，以提供自由流动的纤维布置和烟火或机电分离装置，以便在任务完成后排出线轴和连接光纤。

公开(公告)号：EP0388603A1

公开(公告)日：1990-09-26

申请号：EP90101935.6

申请日：1990-01-31

申请人： THE BOEING COMPANY

发明人： Pinson, George T.

IPC分类号： G01S17/02 ,  F41G1/36 ,  G02B23/12

CPC分类号： F41G1/36 ,  G01S17/026 ,  G02B23/12

摘要： A method and apparatus for covertly viewing a target using transmission of infrared radiation through an atmosphere having given atmospheric conditions. The target is illuminated with only a selected frequency band of infrared radiation having the least effective transmittance properties of all frequencies of infrared radiation in the given atmospheric conditions. This selected frequency band of infrared radiation is reflected from the target and detected. The selected frequency band of infrared radiation may be generated by generating a broad spectrum of infrared radiation and filtering this broad spectrum to output only the selected frequency band of infrared radiation. Alternatively, a laser may be employed to output the selected frequency band of infrared radiation.

摘要翻译： 具有给定的大气条件，一种用于通过在大气观看目标隐蔽使用红外辐射的传输方法和装置。 靶与具有给定的大气条件的红外辐射的所有频率的至少有效透射特性只有红外辐射中的选定频带照明。 红外辐射的该选择的频带从目标反射和检测。 可以通过产生红外辐射的广谱和过滤该广谱只输出红外辐射的选定频带中产生红外辐射的选定频带。 可替换地，激光可以用于输出红外辐射的选定频带。

公开(公告)号：EP0337254A3

公开(公告)日：1990-05-02

申请号：EP89105896.8

申请日：1989-04-04

申请人： THE BOEING COMPANY

发明人： Pinson, George T.

IPC分类号： F41G7/32 ,  H04B10/22 ,  F42B15/04

CPC分类号： G02B6/4457 ,  F41G7/32 ,  F42B15/04 ,  H04B10/25

摘要： Apparatus for optical fiber data link between tow moving bodies remote controlled vehicle/missile such as ("RCV") (12) and hereinafter launch platform (17) includes fiber-wound bobbins having opposite winding directions on each body, interconnected with unwound, reinforced fiber sections, for streaming deployment from each bobbin through tensioning devices during relative separation movement between the two bodies. Image sensors and flight control mechanisms are operatively connected through an electric/optical I/O device to the fiber on the bobbin in the RCV (12), and data analysis/display devices and controller/command units are similarly interfaced with the fiber on the bobbin associated with the helicopter (17). The bobbin housing on the helicopter uses a shaped cavity and gimbal mount to provide free-­streaming fiber deployment and pyrotechin or electro-­mechanical separation device to discharge the bobbin and attached fiber after mission completion.

公开(公告)号：EP0284668A2

公开(公告)日：1988-10-05

申请号：EP87118968.4

申请日：1987-12-21

申请人： THE BOEING COMPANY

发明人： Pinson, George T.

IPC分类号： B65H55/04 ,  B65H54/10 ,  B65H54/02

CPC分类号： B65H54/10 ,  B65H55/04

摘要： A method comprising alternately winding in one direction around the bobbin (34) compact (30) and crossover (52) layers. Each compact layer extends axially of the bobbin from a start end (36) proximate one end (38) of the bobbin to a finish end (40) proximate the other end (42) of the bobbin and includes a plurality of fiber turns (44) in virtual axial contact with each other which define generally parallel grooves (46) in the surface of the compact layer. The turn defining the start and finish ends of each compact layer is aligned with a respective start and finish set-back groove in the surface of the immediately preceding compact layer axially spaced from the respective start and finish ends of the preceding compact layer. Each crossover layer extends axially of the bobbin from the finish end of the preceding compact layer to proximate the start end of the preceding compact layer and includes one or more turns of fiber axially spaced from each other and dis­posed at an angle to the turns and grooves of the preceding compact layer.

摘要翻译： 一种方法包括在一个方向上围绕所述线轴（34）压实体（30）和交叉（52）层交替卷绕。 每个致密层从绕线筒的一端（38）的起始端（36）延伸到靠近线轴的另一端（42）的精加工端（40），并且包括多个纤维圈（44） ）彼此虚拟的轴向接触，其在紧凑层的表面中限定大致平行的凹槽（46）。 定义每个致密层的开始和结束端的转弯与紧邻前一致密层的表面中的相应的起始和后退的凹槽对准，该凹槽与前述致密层的相应的起始和终点轴向间隔开。 每个交叉层从线轴的轴向延伸从前一致密层的端部到接近前一致密层的起始端，并且包括彼此轴向间隔开并且与匝和凹槽成角度设置的一匝或多匝 的前述紧凑层。

公开(公告)号：EP0405051A2

公开(公告)日：1991-01-02

申请号：EP90101511.5

申请日：1990-01-25

申请人： THE BOEING COMPANY

发明人： Pinson, George T.

IPC分类号： G02B17/06

CPC分类号： H04N5/2253 ,  G01J3/2823 ,  G02B7/10 ,  G02B17/0694 ,  H04N5/2251 ,  H04N5/2259 ,  H04N5/30

摘要： A multispectral band imaging and detecting device for use with a catoptric (10,18) zoom optical device having a focal plane (21). A plurality of electromagnetic radiation detectors are provided that are sensitive to one or more portions of the electromagnetic spectrum. An optical bench has the plurality of electromagnetic radiation detectors disposed thereon. A torque motor or the like is operatively connected to move the optical bench relative to the focal plane to move a selected one of the detectors into coincidence with the focal plane.

摘要翻译： 一种用于与具有焦平面（21）的折射（10,18）变焦光学装置一起使用的多光谱带成像和检测装置。 提供对电磁光谱的一个或多个部分敏感的多个电磁辐射检测器。 光学工作台具有设置在其上的多个电磁辐射检测器。 扭矩电动机等可操作地连接以相对于焦平面移动光学台，以将所选择的一个检测器与焦平面移动成一致。

公开(公告)号：EP0393237A3

公开(公告)日：1991-01-02

申请号：EP89114455.2

申请日：1989-08-04

申请人： THE BOEING COMPANY

发明人： Pinson, George T.

IPC分类号： F41G7/32 ,  F42B15/04 ,  H04B10/22

CPC分类号： G02B6/4457 ,  F41G7/32 ,  F42B15/04 ,  H04B10/25

摘要： Apparatus for optical fiber data link between tow moving bodies remote controlled vehicle/missile such as ("RCV") (12) and hereinafter launch platform (17) includes fiber-wound bobbins having opposite winding directions on each body, interconnected with unwound, reinforced fiber sections, for streaming deployment from each bobbin through tensioning devices during relative separation movement between the two bodies. Image sensors and flight control mechanisms are operatively connected through an electric/optical I/O device to the fiber on the bobbin in the RCV (12), and data analysis/display devices and controller/command units are similarly interfaced with the fiber on the bobbin associated with the helicopter (17). The bobbin housing on the helicopter uses a shaped cavity and gimbal mount to provide free-­streaming fiber deployment and pyrotechin or electro-­mechanical separation device to discharge the bobbin and attached fiber after mission completion.

摘要翻译： 遥控车辆/导弹（“RCV”）（12）和以后的发射平台（17）之间的光纤数据链路的装置包括在每个主体上具有相反卷绕方向的纤维缠绕线轴，与解开的，加强的 纤维部分，用于在两个物体之间的相对分离运动期间通过张紧装置从每个筒管流动展开。 图像传感器和飞行控制机构通过电/光I / O设备可操作地连接到RCV（12）中的线轴上的光纤，数据分析/显示设备和控制器/命令单元也类似地与光纤上的光纤 与直升机相关联的线轴（17）。 直升机上的绕线管外壳采用成形的腔体和万向架安装，以提供自由流动的纤维布置和烟火或机电分离装置，以便在任务完成后排出线轴和连接光纤。

公开(公告)号：EP0402564A1

公开(公告)日：1990-12-19

申请号：EP90101731.9

申请日：1990-01-29

申请人： THE BOEING COMPANY

发明人： Pinson, George T.

IPC分类号： F41G7/22

CPC分类号： G02B6/06 ,  F42B15/01 ,  G02B23/16

摘要： A missile seeker head comprises a telescope mounted on a gimbal apparatus in a forward end of a projectile, pivotal in the gimbal sufficient to search a field of regard of up to 60°, and a camera mounted further back in the projectile, connected to the telescope by a coherent fiber optic bundle.

摘要翻译： 导弹头头包括安装在弹头前端的万向架装置上的望远镜，其在万向架中枢枢转，足以搜索高达60°的视场，以及安装在后方的射弹的相机，连接到 望远镜由一个相干光纤束组成。

公开(公告)号：EP0359985A2

公开(公告)日：1990-03-28

申请号：EP89114931.2

申请日：1989-08-11

申请人： THE BOEING COMPANY

发明人： Pinson, George T.

IPC分类号： G02B6/44 ,  H01B11/22

CPC分类号： G02B6/4415 ,  F41G7/32 ,  G02B6/4416 ,  H01B7/182 ,  H01B11/22

摘要： Apparatus for interconnecting a missile/RCV launch device with a remote control station includes composite cable having glass fibers for transmitting optical signals and electrical conductors embedded in a coating layer that is reinforced with fibers, for transmitting electric power. The apparatus also includes electrical and optical connectors at the cable end portions wherein the reinforcing fibers are grouped with the glass fiber at termination.

摘要翻译： 用于将导弹/ RCV发射装置与远程控制站相互连接的装置包括具有用于传输光信号的玻璃纤维和嵌入在用光纤增强的涂层中的电导体的复合电缆，用于传输电力。 该设备还包括电缆端部处的电连接器和光学连接器，其中在端接时增强纤维与玻璃纤维分组。

公开(公告)号：EP0294514A3

公开(公告)日：1989-04-05

申请号：EP87117502.2

申请日：1987-11-26

申请人： THE BOEING COMPANY

发明人： Pinson, George T.

IPC分类号： H02K7/02

CPC分类号： H02J15/00 ,  H02J3/30 ,  H02K7/025 ,  Y02E60/16 ,  Y10T74/2117

摘要： A variable inertia energy storage system for storing large amounts of mechanical energy for an extended period of time on land or on a mobile vehicle includes a fly wheel having a rotating hub with spoke appendages each having an associate mass the center of which can be controllably changed with respect to the hub axis of rotation. The energy storage system also includes motor/­generator elements for providing rotation forces to input mechanical energy to the flywheel or for generating electrical power for use on demand by a subsystem or the like.