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公开(公告)号：US06910658B1
公开(公告)日：2005-06-28
申请号：US07456817
申请日：1989-12-08
申请人： David Hart , Robert L. Cooke
发明人： David Hart , Robert L. Cooke
CPC分类号： G01S7/4818 , F41G7/2246 , F41G7/2293 , F41G7/32 , F42B19/10 , G01S17/66 , G01S17/88
摘要： An anti-torpedo torpedo having laser homing head, the torpedo being launched from a parent vessel or platform which itself houses the expensive to replace, the bulky, or the high power consuming parts of the laser, said parts being optically connected to an optical projector in the homing head in the torpedo itself and to any parts of the laser not housed in the parent vessel.
摘要翻译： 具有激光归位头的反鱼雷鱼雷，鱼雷是从家用船只或平台发射的，该船只或平台本身容纳更换的昂贵的物体，笨重的或大功率的激光器部件，所述部件被光学连接到光学投影仪 在鱼雷本身的归位头部以及不在母船上的激光的任何部分。
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公开(公告)号：US5493627A
公开(公告)日：1996-02-20
申请号：US809038
申请日：1991-12-16
CPC分类号： F41G7/32 , F42B15/04 , G02B6/4457 , F41G2700/005 , Y10S425/007
摘要： A waveguide pack for transmission of information that includes a length of a dielectric waveguide wound into a free-standing coil with an inner diameter of less than three inches and coated with a binder suited to maintaining the waveguide in the coil, and a method for preparing the pack.
摘要翻译： 一种用于传输信息的波导组件，其包括缠绕在内径小于3英寸的独立线圈中的电介质波导的长度，并涂覆有适于将波导保持在线圈中的粘合剂，以及一种制备方法 包裹。
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公开(公告)号：US5125590A
公开(公告)日：1992-06-30
申请号：US640755
申请日：1991-01-14
申请人： George W. LeCompte
发明人： George W. LeCompte
CPC分类号： G02B6/4457 , B65H75/14 , B65H2701/5136 , B65H2701/51522 , B65H2701/51528
摘要： A hollow winding bobbin base (18) is constructed of a material having a relatively low thermal coefficient of expansion (e.g., quartz) and has a pair of flanges (32) slidably located on the ends. A metal tube (24) is received within the base (18) and has annular springs (40) on its ends urging the flanges (32) toward each other. An elastomer baselayer (30) is fitted onto the outer surface of the base (18).
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公开(公告)号：US5104057A
公开(公告)日：1992-04-14
申请号：US686081
申请日：1991-04-16
CPC分类号： B65H49/02 , B65H49/08 , F42B15/04 , B65H2701/32
摘要： A missile data link filament (12) dispenser (10) is located within an enclosure (20) having a single eyelet opening (26) through which the filament feeds on launch. A quantity of a damping gas having an effective density of at least about two times that of air (28) is provided within the enclosure (20). The gas serves to damp the helical motion of the filament by absorbing its rotational energy, to inhibit ballooning of the filament (12) as it is paid out from the dispenser (10).
摘要翻译： 导弹数据连接灯丝（12）分配器（10）位于具有单个孔眼开口（26）的外壳（20）内，灯丝在发射时通过该孔口开口供应。 在外壳（20）内设有一定数量的有效密度至少大约为空气（28）密度的两倍的阻尼气体。 气体用于通过吸收其旋转能量来阻尼细丝的螺旋运动，以防止细丝（12）从分配器（10）中支出时膨胀。
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公开(公告)号：US5062586A
公开(公告)日：1991-11-05
申请号：US524495
申请日：1990-05-17
摘要： Apparatus (10) for acquiring and tracking a missile (M), and guiding it to a target (T). Beacons (18, 19) are carried on the missile to provide an indication of its location in a field of view. One beacon (18) is a xenon beacon which emits energy in a short wave-length portion of the light spectrum. The other beacon (19) is a thermal source which emits infrared radiation in a longer wave-length portion of the spectrum. A sight unit (20) includes both a xenon beacon detector and a forward looking infrared receiver (FLIR). The FLIR provides two independent channels (A, B) of video. An electrical signal developed within the sight unit is separately processed on both of the channels. One channel is used to develop a video display for an operator for target acquisition and tracking. The other channel is used for missile tracking and clutter and countermeasure (CM) rejection. A tracking unit (40) processes the signal to determine missile location relative to the target; and, if corrections to the missile freight path are necessary, a missile control unit (56) transmits them to the missile over wires (W). If two or more objects (M, D1, D2) are located in the field of view, a module (88) of the tracking unit undertakes a "segmentation" process to differentiate and characterize the objects to determine which object is the missile and which is not.
摘要翻译： 用于获取和跟踪导弹（M）并将其引导到目标（T）的装置（10）。 信标（18,19）在导弹上运载，以便在视野中提供其位置的指示。 一个信标（18）是在光谱的短波长部分中发射能量的氙信标。 另一个信标（19）是在光谱的较长波长部分发射红外辐射的热源。 视觉单元（20）包括氙信标检测器和前视红外接收器（FLIR）。 FLIR提供两个独立的视频通道（A，B）。 在两个通道上分别处理在瞄准单元内形成的电信号。 一个通道用于开发用于操作者的视频显示器以进行目标采集和跟踪。 另一个通道用于导弹跟踪和杂波和对策（CM）的拒绝。 跟踪单元（40）处理信号以确定相对于目标的导弹位置; 并且如果需要对导弹运输路径进行修正，则导弹控制单元（56）将它们传输到导线（W）上。 如果两个或多个对象（M，D1，D2）位于视场中，跟踪单元的模块（88）进行“分割”过程以区分和表征对象以确定哪个对象是导弹，以及哪个 不是。
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公开(公告)号：US5042390A
公开(公告)日：1991-08-27
申请号：US423311
申请日：1989-10-18
申请人： Daniel K. Schotter
发明人： Daniel K. Schotter
CPC分类号： F41F3/055
摘要： Guided missiles (10) which trail control umbilicals such as optical fibers (20) are launched from an array (16) of launch tubes (14) that point in the same direction. A swing arm (40) extends over the face of the array (16) to capture and move the umbilicals (20) of previously launched missiles (10) away from the portion of the array (16) from which the next missile (10) will be launched, to avoid interference between the launched missile (10) and the exisiting umbilicals (20). As each missile (10) is launched, the swing arm (40) recycles to capture the umbilical (20) of the newly launched missile (10).
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公开(公告)号：US5031997A
公开(公告)日：1991-07-16
申请号：US500449
申请日：1990-03-28
CPC分类号： G02B6/4457
摘要： An optical fiber (18) payout system for a missile (10) which is to be hot-launched from a tube (12) reinforces that part of the fiber to be exposed to propulsion gases by juxtaposing with one or more wires (24) and encasing within a thermally protective sheath (22) forming a so-called leader (20). The leader (20) extends outwardly of the missile aft end (16) and is releasably secured within a rail assembly (32) by a flexible strip (46) having a line of perforations (48) extending along its longitudinal axis. The outer end portion of the leader (20) is secured to an anchor block (52). On launch, the leader (20) tears loose from the flexible strip (46), the restraining action of which prevents optical fiber predispensing.
摘要翻译： 用于从管（12）热发射的用于导弹（10）的光纤（18）支付系统通过与一根或多根电线（24）和并置而将该部分纤维加强以暴露于推进气体中， 封装在形成所谓的引导件（20）的热保护套（22）内。 引导件（20）延伸到导弹后端部（16）的外侧，并且通过具有沿其纵向轴线延伸的穿孔线（48）的柔性条带（46）可释放地固定在轨道组件（32）内。 引导件（20）的外端部分固定到锚块（52）上。 在发射时，领导者（20）从柔性条（46）撕裂，其抑制作用阻止了光纤预先分配。
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公开(公告)号：US5029765A
公开(公告)日：1991-07-09
申请号：US440968
申请日：1989-11-22
申请人： Raymond P. Gastreich
发明人： Raymond P. Gastreich
CPC分类号： B65H54/2812 , B65H54/70 , G02B6/4457 , B65H2701/32
摘要： A pair of grippers or clampers (34) are arranged at opposite ends of a drum (14) that is to be provided with a wound optical fiber (12) pack. When a winding layer is being finished and a new layer is about to be started a clamper (34) is actuated to engage the last few windings and hold them in place while the new winding is initiated.
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公开(公告)号：US5022607A
公开(公告)日：1991-06-11
申请号：US273310
申请日：1988-11-18
申请人： Daniel K. Schotter
发明人： Daniel K. Schotter
CPC分类号： G02B6/4478 , F41G7/32 , F42B15/04
摘要： A fiberoptic leader connected between a missile and a launch tube is paid out upon missile launch with a controlled degree of bend in the fiberoptic filament, and is furthermore protected from blast effects in the launch. The fiberoptic filament is stiffened within a leader comprised of a TEFLON sleeve insulating the fiberoptic filament. A protective sheathing of high tensile strength longitudinally wires are disposed about and encase the TEFLON sleeve, and in turn are encased within an outer sleeve. The stiffened leader is led along the longitudinal length of a C-shaped channel attached to the side of the missile. The channel is disposed upon a longitudinal portion of the missile. The stiffened leader is laid against and under one of the channel arms from the aft end of the missile, where the fiberoptic leader is fed out during launch, to a forward end of the missile and channel. The leader is then led across the width of the channel to the opposing arm of the C-shaped channel. The stiffened leader is then led partly aft along the opposing arm of the channel and then out to an open longitudinal slot defining the ends of the C-shaped channel. That end of the stiffened leader is coupled to a fixed point within the launch tube from which point optical communications are provided to the missile during flight. As the missile is launched, the bend propagates down the channel tearing the stiffened leader from a longitudinally perforated tape which secures the leader into and under one of the arms of the channel.
摘要翻译： 导弹与发射管之间连接的光纤导管在导弹发射时得到光纤灯丝受到控制的弯曲程度，并在发射时进一步受到爆炸的影响。 光纤丝在由TEFLON套筒组成的导线内加固，绝缘纤维光纤丝。 高抗拉强度纵向丝线的保护套围绕TEFLON套筒设置并包裹在外套筒内。 加强的导弹沿着附着在导弹一侧的C形通道的纵向长度引导。 通道设置在导弹的纵向部分上。 加强的领导人被放置在导弹的后端的一个通道臂下面，导弹的后端，光纤引导者在发射时被送出到导弹和通道的前端。 然后，领导者穿过通道的宽度到C形通道的相对臂。 然后，加强的引导件沿着通道的相对臂部分地向前引导，然后出口到限定C形通道的端部的敞开的纵向狭槽。 加强的引导件的该端部连接到发射管内的固定点，在飞行期间将光通信从该点提供给导弹。 当导弹发射时，弯道向下传播，从纵向穿孔的带撕开加强的引导件，该导带将引导件固定在通道的一个臂之中和之下。
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公开(公告)号：US4907763A
公开(公告)日：1990-03-13
申请号：US195621
申请日：1988-05-17
申请人： George T. Pinson
发明人： George T. Pinson
CPC分类号： F41G7/32 , B65H49/02 , F42B15/04 , G02B6/4457 , B65H2701/32
摘要： An optical fiber-guided projectile launch system for firing from a generally tubular launcher comprising a projectile having 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. An alternative embodiment uses an un-grooved projectile casing with a tube launcher having a preformed fiber relief-groove in the inner peripheral surface and a discarding sabot having a tab member receivable in the relief. For both embodiments, a controller is 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, and an adaptor is provided for guiding fiber streaming axially from a wound bobbin in 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发射系统，其包括具有管状壳体的射弹，设置在壳体中的延伸长度的光纤，用于从其后端连续流动，光纤的一部分从 壳体，用于与控制器的操作性连接，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，将纤维部分固定在槽中的力，足以承受轴向发射力但不足以抵抗施加的径向力;以及 通过光纤提供双向通信的通信设备。 替代实施例使用具有在内周表面中具有预成型纤维释放槽的管发射器的未开槽的抛射体套管和具有可接收在浮雕中的突片构件的废弃物。 对于两个实施例，控制器被提供为与射弹双向通信，用于从射弹接收和处理目标数据，并且将包括操作员手动引导的引导数据传送到射弹，并且提供适配器用于沿轴向引导纤维流 从射弹中的绕线筒。
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