专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

81. 发明授权

US5123610A Retrofit digital electronics unit for a tube-launched missile 失效
标题翻译：改造数字电子单元，用于管道发射的MISSILE
公开(公告)号：US5123610A
公开(公告)日：1992-06-23
申请号：US384229
申请日：1989-07-21
申请人： Richard W. Oaks
发明人： Richard W. Oaks
IPC分类号： B64C13/18 , B64G1/24 , F41G7/30 , F41G7/32 , F42B15/04 , G05D1/10 , G05D1/12
CPC分类号： F41G7/301 , F41G7/32 , G05D1/107
摘要： A retrofit digital electronics unit replaces the analog electronics unit of a tube-launched optically-tracked wire-guided missile. The retrofit digital electronics unit is smaller in size permitting the warhead of the missile to be enlarged. Additionally, the retrofit digital electronics unit is more susceptible to modification through simple changes in software.

82. 发明授权

US5111524A Signal transmitting steering cable including optical fiber with fluorescent dye 失效
标题翻译：信号发射转向电缆，其中包括具有荧光染料的光纤
公开(公告)号：US5111524A
公开(公告)日：1992-05-05
申请号：US736643
申请日：1991-07-26
申请人： Bernd Schunk , Reinfried Stolllewerk , Gerhard Hubricht , Jorg Peters
发明人： Bernd Schunk , Reinfried Stolllewerk , Gerhard Hubricht , Jorg Peters
IPC分类号： F42B15/04 , F41G7/32 , G02B6/00 , G02B6/44
CPC分类号： F41G7/32
摘要： A signal transmitting steering cable (4, 40, 40') for remotely-controlled flying bodies (1) which, once the flying body (1) has been launched, can be located and disposed of easily. For this purpose the surface layer (44, 46) of the steering cable (4) includes a material which is fluorescent when illuminated with light of a predetermined wavelength range. Preferably, a dye whose emission spectrum lies approximately between 530 and 690 nm is employed as the fluorescent material.
摘要翻译：用于远程控制的飞行体（1）的信号传递转向电缆（4,40,40'），一旦飞行体（1）被启动，可以容易地定位和处理。为此，转向电缆（4）的表面层（44,46）包括当用预定波长范围的光照射时是荧光的材料。优选使用其发射光谱位于530和690nm之间的染料作为荧光材料。

83. 发明授权

US5102064A Missile guidance systems 失效
标题翻译：导弹引导系统
公开(公告)号：US5102064A
公开(公告)日：1992-04-07
申请号：US89139
申请日：1970-11-12
申请人： Martin A. K. Daly
发明人： Martin A. K. Daly
IPC分类号： F41G7/30 , F41G7/32
CPC分类号： F41G7/303 , F41G7/32
摘要： A guidance system for controlling the flight of a guided missile onto a target, comprising an optical sight and a tracker mounted with their optical axes approximately in alignment in a common housing which is pivotable for aiming the sight at a target. The housing also carries a missile firing button and a manually-operable joystick for generating primary direction control signals for controlling the missile. The tracker produces automatically secondary control signals representative of the displacement of the missile in flight from the axis of the tracker. Transmitter means is provided in a separate housing for transmitting both primary and secondary control signals simultaneously to a receiver in the missile so that the flight of the missile is controlled by the combined primary and secondary signals.
摘要翻译：一种用于控制导弹飞行到目标上的引导系统，其包括光学瞄准器和跟踪器，该瞄准器和跟踪器将其光轴大致对准在共同的壳体中，所述公共壳体可枢转以将视线瞄准目标。外壳还具有导弹发射按钮和手动操作的操纵杆，用于产生用于控制导弹的主方向控制信号。跟踪器自动产生代表飞行中的导弹从跟踪器的轴的位移的二次控制信号。发射器装置设置在单独的壳体中，用于同时向导弹中的接收器发送主控制信号和辅助控制信号，使得导弹的飞行由组合的主信号和次信号控制。

84. 发明授权

US5042743A Apparatus and method for multiple target engagement 失效
标题翻译：用于多目标接合的装置和方法
公开(公告)号：US5042743A
公开(公告)日：1991-08-27
申请号：US482152
申请日：1990-02-20
申请人： Edwin R. Carney
发明人： Edwin R. Carney
IPC分类号： F41G7/22 , F41G7/30 , F41G7/32
CPC分类号： F41G7/2233 , F41G7/2206 , F41G7/2253 , F41G7/2293 , F41G7/303 , F41G7/308 , F41G7/32
摘要： Apparatus (10) for simultaneously engaging a multiplicity of selected targets (V1-V7) to launch one or more missiles (T) at each target and acquire, track, and guide each missile to its respective target. A field of view (FOV) is scanned to detect one or more targets therewithin. A target selection system (34) is used to designate various of the targets at which to launch missiles. A plurality of missiles are then launched, and directed to each selected target. A plurality of sensors (58) detect radiation from each missile as it travels toward its respective target. An acquisition and tracking system (74) is used to track each missile and its target. The system includes a processor (80) for determining the position of each missile relative to its respective target, and a control module (82) responsive to the processor for generating and transmitting guidance signals to each missile to guide it to its target.
摘要翻译：用于同时接合多个选定目标（V1-V7）以在每个目标处发射一个或多个导弹（T）并且获取，跟踪和引导每个导弹到其相应目标的装置（10）。扫描视场（FOV）以检测其中的一个或多个目标。目标选择系统（34）用于指定发射导弹的各种目标。然后启动多个导弹，并引导到每个所选择的目标。多个传感器（58）检测来自每个导弹的辐射，当它朝向其相应目标行进时。采集跟踪系统（74）用于跟踪每个导弹及其目标。该系统包括用于确定每个导弹相对于其相应目标的位置的处理器（80）以及响应于处理器的控制模块（82），用于产生并向每个导弹发射引导信号以将其引导到其目标。

85. 发明授权

US4860968A Communication link between moving bodies 失效
标题翻译：移动体之间的通信连接
公开(公告)号：US4860968A
公开(公告)日：1989-08-29
申请号：US182025
申请日：1988-04-15
申请人： George T. Pinson
发明人： George T. Pinson
IPC分类号： F41G7/32 , F42B15/04 , G02B6/00 , G02B6/44 , H04B3/60 , H04B10/00 , H04B10/12 , H04B10/13 , H04B10/135 , H04B10/14 , H04B10/22
CPC分类号： G02B6/4457 , F41G7/32 , F42B15/04 , H04B10/25
摘要： Apparatus for optical fiber data link between two moving bodies remote controlled vehicle/missile such as ("RCV") and hereinafter launch platform 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 a electric/optical I/O device to the fiber on the bobbin in the RCV, and data analysis/display devices and controller/command units are similarly interfaced with the fiber on the bobbin associated with the helicopter. 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.

86. 发明授权

US4770370A Optical fiber guided tube-launched projectile system 失效
标题翻译：光纤导管射出射弹系统
公开(公告)号：US4770370A
公开(公告)日：1988-09-13
申请号：US32448
申请日：1987-03-31
申请人： George T. Pinson
发明人： George T. Pinson
IPC分类号： F41G7/32 , F42B15/04
CPC分类号： F42B15/04 , F41G7/32 , B65H2701/32
摘要： An optical fiber guided projectile for firing from a generally tubular launcher comprising a tubular casing, an extended length of optical fiber disposed in the casing for continuous streaming from the trailing end thereof, a portion of the fiber extending from the casing for operative connection to a controller, an axial groove in the casing surface for removably receiving a part of the extending fiber, tape securing the fiber part in the groove with force sufficient to withstand axial launch forces but insufficient to resist imposed radial forces, and a communication device providing two-way communication over the fiber. A controller is also provided in two-way communication with the projectile for receiving and processing target data from the projectile and for transmitting guidance data, including operator manual guidance, to the projectile.
摘要翻译：一种用于从通常管状的发射器发射的光纤引导射弹，其包括管状壳体，设置在壳体中的延伸长度的光纤，用于从其后端连续流动，从壳体延伸的一部分光纤，用于操作连接到控制器，壳体表面中的用于可移除地接收一部分延伸纤维的轴向槽，用于足够承受轴向发射力但不足以抵抗所施加的径向力的力将光纤部分固定在槽中的带;以及提供二维轮廓的通信装置，通过光纤进行通信。还提供一个控制器与射弹进行双向通信，用于从射弹接收和处理目标数据，并向导弹发送包括操作员手册指导的指导数据。

87. 发明授权

US4705237A Launcher for an optically guided, wire-controlled missile with improved electronic circuitry 失效
标题翻译：具有改进电子电路的光导导线控制导弹发射器
公开(公告)号：US4705237A
公开(公告)日：1987-11-10
申请号：US919666
申请日：1986-10-16
申请人： Emil Goldfeld , Shlomo Harush , Yuri Takserman , Shmuel Weiler
发明人： Emil Goldfeld , Shlomo Harush , Yuri Takserman , Shmuel Weiler
IPC分类号： F41G7/32
CPC分类号： F41G7/32
摘要： Launcher for a tube-launched, optically guided wire controlled missile. Inhe electronic circuitry that forms part of a feedback servomechanism there are provided pitch and yaw channels with time variable gains having different transfer functions. Optionally there are further provided at least two different generators of signals for gravity bias with automatic means for selecting between them in accordance with the physical characteristics of the missile.
摘要翻译：发射器，用于管式发射的光导导线控制导弹。在构成反馈伺服机构的一部分的电子电路中，提供了具有不同传递函数的时间可变增益的俯仰和偏航通道。可选地，还提供至少两个用于重力偏置的不同的信号发生器，其具有根据导弹的物理特性在其间进行选择的自动装置。

88. 发明授权

US4274353A Acoustic imaging system for wire guided torpedo 失效
标题翻译：导线鱼雷声成像系统
公开(公告)号：US4274353A
公开(公告)日：1981-06-23
申请号：US694025
申请日：1967-12-22
申请人： Rene N. Foss , Sidney Levine
发明人： Rene N. Foss , Sidney Levine
IPC分类号： F41G7/22 , F41G7/32 , F42B19/10 , G10K11/00 , G10K11/26 , F41G7/02
CPC分类号： F41G7/228 , F41G7/32 , G10K11/008 , G10K11/26 , F41G2700/005
摘要： An acoustic imaging system for a wire guided torpedo having an array of tsducers arranged in the nose of a torpedo to receive acoustic signals. A spherical acoustic lens focuses the signals on the array of transducers. The outputs of the transducers are amplified, integrated, detected and passed to a set of gates which are sampled sequentially, and the outputs of the gates are passed by a wire to the launching vehicle.
摘要翻译：一种用于导线鱼雷的声学成像系统，其具有布置在鱼雷鼻中的传感器阵列以接收声信号。球面声透镜将信号聚焦在换能器阵列上。换能器的输出被放大，积分，检测并传递到一组顺序采样的栅极，并且栅极的输出通过导线传递到发射车辆。

89. 发明授权

US3266423A Ground controlled rocket missiles 失效
标题翻译：地面控制火箭弹
公开(公告)号：US3266423A
公开(公告)日：1966-08-16
申请号：US20365662
申请日：1962-06-19
申请人： FAIREY ENG
发明人： CHARLES SIMPSON JAMES
IPC分类号： B65H49/02 , F41G7/32 , F42B15/04 , H02G11/02
CPC分类号： H02G11/02 , B65H49/02 , F41G7/32 , F42B15/04

90. 发明授权

US3163711A Cable-controlled flying objects and cables therefor 失效
标题翻译：电缆控制的飞行物体和电缆
公开(公告)号：US3163711A
公开(公告)日：1964-12-29
申请号：US83483659
申请日：1959-08-19
申请人： LUDWIG BOLKOW
发明人： WERNER SCHINDLER
IPC分类号： F41G7/32 , F42B15/04 , H01B7/04
CPC分类号： H01B7/043 , F41G7/32 , F42B15/04

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式