公开(公告)号：US4558918A

公开(公告)日：1985-12-17

申请号：US675790

申请日：1984-11-28

申请人： Marvin W. Shores

发明人： Marvin W. Shores

IPC分类号： H01R9/03 ,  H01R13/658

CPC分类号： H01R9/034 ,  Y10S439/927 ,  Y10T29/49208

摘要： A cable shield to connector back shell termination device includes a back shell of a multi-pin cable connector, a plurality of metallic tubes adapted to receive individually the end of a shielded cable such that substantially full circumferential conductive contact is maintained between each cable shield and a tube, and a cluster of such tubes conductively bonded together and shaped to fit the back shell for conductive bonding to the back shell. A second embodiment employs a conductive sleeve for conductive mounting on the cable shield. Ridges or fins extending generally lengthwise on the sleeve frictionally, conductively contact the metal tubes. In this manner an uninterrupted conductive surface is maintained at the connector. The connector enclosure thus provides a shield against the intrusion of electromagnetic energy in the environment in which the electrical or electronic wiring and circuits must operate.

摘要翻译： 电缆屏蔽到连接器背壳端接装置包括多针电缆连接器的后壳，多个金属管，适于独立地接收屏蔽电缆的端部，使得在每个电缆屏蔽和 管和一组这样的管导电地接合在一起并成形为适合后壳，用于导电粘合到后壳。 第二个实施例采用导电套管来导电地安装在电缆屏蔽上。 摩擦地在套筒上大致纵向延伸的脊或翅片导电地接触金属管。 以这种方式，在连接器处保持不间断的导电表面。 因此，连接器壳体提供了防止在电气或电子布线和电路必须工作的环境中的电磁能量入侵的屏蔽。

公开(公告)号：US4546621A

公开(公告)日：1985-10-15

申请号：US600069

申请日：1984-04-13

申请人： Mark L. Kline ,  Oakley G. Ross

发明人： Mark L. Kline ,  Oakley G. Ross

IPC分类号： F25B9/02 ,  G01J5/06 ,  F25B19/00

CPC分类号： G01J5/061 ,  F25B9/02

摘要： A cooled infrared detector post includes a detector post formed of a stack of wafer disks with a detector substrate wafer forming one end of the post and a cooling chamber adjacent to the detector substrate with coolant supply and return passages formed in the series of wafers with a supply passage contained to a supply port with a supply passage forming a plurality of serpentine passages at various planes within the post and a return passage including a plurality of precooling chambers with the wafer stacked in a predetermined arrangement and fused together to form a monolithic post structure.

摘要翻译： 冷却的红外检测器柱包括由堆叠的晶片盘形成的检测器柱，其具有形成柱的一端的检测器基板晶片和与检测器基板相邻的冷却室，其中形成在一系列晶片中的冷却剂供应和返回通道具有 供给通道容纳在供给口中，供给通道在柱内的各个平面上形成多个蛇形通道，以及返回通道，其包括多个预冷室，其中晶片以预定布置堆叠并熔合在一起以形成整体柱结构 。

公开(公告)号：US4545570A

公开(公告)日：1985-10-08

申请号：US686612

申请日：1984-12-24

申请人： Charles W. KaDell, Jr.

发明人： Charles W. KaDell, Jr.

IPC分类号： G01L7/04 ,  B23Q1/00

CPC分类号： G01L7/041 ,  Y10S269/902

摘要： A highly accurate rapid gimbal assembly method utilizes two fixtures for establishing the critical gimbal assembly parameters of yield and axis of intersection and an adhesive for bonding each mating surface of the gimbal assembly for holding the components of the gimbal assembly in their adjusted positions. The fixtures include an inner/outer gimbal fixture for holding the inner and outer gimbals in relative position for bonding and a gimbal/post fixture for holding the gimbal assembly in alignment on the support post for bonding. These fixtures and assembly method eliminate the need for use of shims between the mating surfaces for establishing alignment of the critical parameters.

摘要翻译： 高度精确的快速万向节组装方法利用两个固定装置来建立产量和轴线的关键万向节装配参数，以及用于粘合万向架组件的每个配合表面的粘合剂，用于将万向节组件的部件保持在调整位置。 固定装置包括用于将内部和外部万向节保持在用于粘合的相对位置的内部/外部万向节固定件，以及用于将万向架组件保持在支撑柱上对准的用于粘结的万向架/后固定装置。 这些夹具和装配方法消除了在配合表面之间使用垫片的需要，以建立关键参数的对准。

公开(公告)号：US4489638A

公开(公告)日：1984-12-25

申请号：US474994

申请日：1983-03-14

申请人： Thomas W. Bastian ,  Charles W. Schertz

发明人： Thomas W. Bastian ,  Charles W. Schertz

IPC分类号： B64D7/08 ,  F41F3/06

CPC分类号： F41F3/06 ,  B64D7/08

摘要： A missile launching system adapted for installation in a standard commercial aircraft without modification of the aircraft structure. The system comprises a plurality of frame members, linear tracks which are movable longitudinally relative to the frame members, a plurality of launch tubes for storing the missiles, an exit port for installation in an pre-established aircraft fuselage opening, and associated equipment for selectively launching the missiles from the launch tubes through the exit port. The entire system is assembled from individual components, all of which are sized to be placed on board the aircraft through a standard passenger door opening. In preparation for installing the system in a commercial aircraft, the passenger seats and related equipment conventionally installed in the interior of such an aircraft are removed. The frame members of the system are then mounted to the standard seat tracks in the floor of the aircraft. The remaining portions of the system are thereafter assembled and installed on the frame. The frame is inclined to support the launch tubes at an angle extending upward and forward so that when a missile is ejected from the launch tube, it is given a trajectory which carries it clear of the aircraft wing and empennage.

摘要翻译： 一种适合安装在标准商用飞机上而不改装飞机结构的导弹发射系统。 该系统包括多个框架构件，相对于框架构件可纵向移动的线性轨道，用于存储导弹的多个发射管，用于安装在预先建立的飞行器机身开口中的出口，以及用于选择性地设置的相关设备 通过出口将发射管的导弹发射出去。 整个系统由单个部件组装，所有这些部件的尺寸都通过标准乘客门开口放置在飞机上。 为了准备将该系统安装在商用飞机中，除去常规安装在这种飞行器内部的乘客座椅和相关设备。 然后将系统的框架构件安装到飞机地板上的标准座椅轨道上。 此后系统的其余部分组装并安装在框架上。 框架倾向于以向上和向前延伸的角度支撑发射管，使得当导弹从发射管弹出时，它被给予一个轨迹，其使飞机机翼和尾翼远离。

公开(公告)号：US4480522A

公开(公告)日：1984-11-06

申请号：US311488

申请日：1981-10-15

申请人： Edward T. Piesik

发明人： Edward T. Piesik

IPC分类号： F41F3/04

CPC分类号： F41F3/0413

摘要： Methods and apparatus are disclosed for preventing a missile's rocket exhaust gases from contacting and adversely affecting, such as by overheating, the launch rails from which a missile may be launched. Such apparatus includes orifices and pressure/flow controls in association with the rails in order to produce a cold gaseous stream directed in opposition to the exhaust gases during at least the initial phase. The stream creates a boundary plane or barrier between the rails and the exhaust gases, thereby shielding the rails from damage due to overheating.Arrangements are provided to control the time and duration of the stream so that it may be limited to the period of actual need.

摘要翻译： 公开了用于防止导弹的火箭废气接触并不利地影响（例如由于过热）发射导弹的发射轨的方法和装置。 这种设备包括与轨道相关联的孔和压力/流量控制，以便在至少初始阶段期间产生与排气相对的冷气流。 流在轨道和废气之间产生边界平面或障碍物，从而屏蔽导轨不会由于过热而损坏。 提供安排以控制流的时间和持续时间，以便将其限制在实际需要的时期。

公开(公告)号：US4470336A

公开(公告)日：1984-09-11

申请号：US405484

申请日：1982-08-05

申请人： Lynn J. Swann ,  Larry D. Wedertz

发明人： Lynn J. Swann ,  Larry D. Wedertz

IPC分类号： F41F3/04 ,  F41F3/042

CPC分类号： F41A23/42 ,  F41F3/04 ,  F41F3/042

摘要： A missile launch system includes a missile launch support structure mounted on a launch platform and including a pair of spaced apart rails having longitudinal slots formed therein, and a cooperating missile launch container having a cylindrical bore for receiving and supporting a missile for launching includes radially extending ribs spaced and oriented to engage and slide along the slots in the rails for supporting the missile launch container for launching of the missile.

摘要翻译： 导弹发射系统包括安装在发射平台上的导弹发射支撑结构，并且包括一对具有形成在其中的纵向槽的间隔开的轨道，以及具有用于接收和支撑用于发射的导弹的圆柱形孔的配合导弹发射容器包括径向延伸 肋条间隔开并定向成沿轨道中的狭槽接合和滑动，用于支撑用于发射导弹的导弹发射容器。

公开(公告)号：US4456862A

公开(公告)日：1984-06-26

申请号：US421539

申请日：1982-09-22

申请人： William R. Yueh

发明人： William R. Yueh

IPC分类号： F41G7/22 ,  G05D1/12 ,  G05B13/00

CPC分类号： F41G7/22 ,  G05D1/12

摘要： A method for augmenting a noise-adaptive predictive proportional navigation terminal guidance scheme. In a second order configuration with noise adaptive varying gain parameters calculated as a function of time-to-go, this system implements an optimal control law to augment proportional navigation with a missile acceleration feedback term and a navigation ratio to account for first order autopilot time lag. This configuration results in nearly optimal miss distance behavior, with sensitivity to unmodeled errors being substantially less than that in modern guidance systems. The system is particularly useful for high altitude, minimally maneuvering targets.

摘要翻译： 一种用于增强噪声自适应预测比例导航终端指导方案的方法。 在具有作为随时间的函数计算的噪声自适应变化增益参数的二阶配置中，该系统实施最佳控制规则以通过导弹加速度反馈项和导航比来增加比例导航，以考虑一阶自动驾驶时间 落后。 这种配置导致几乎最佳的错过距离行为，对未建模误差的敏感性远远小于现代引导系统中的错误距离行为。 该系统对于高空，最低限度的机动目标特别有用。

公开(公告)号：US4431150A

公开(公告)日：1984-02-14

申请号：US371044

申请日：1982-04-23

申请人： Edwin H. Epperson, Jr.

发明人： Edwin H. Epperson, Jr.

IPC分类号： F41G7/22 ,  F41G7/30 ,  F42B15/01 ,  F41G7/00

CPC分类号： F42B15/01 ,  F41G7/222 ,  F41G7/305

摘要： A projectile body has a gyro mounted therein including a rotor and a mechanism for supporting the rotor for rotation about a spin axis initially coincident with the longitudinal axis of the projectile body and pivotable away from the longitudinal axis of the projectile body. The rotor is initially locked to the projectile body so that it is spun with the projectile body during launch. Thereafter, the rotor is unlocked and the projectile body is de-spun to a relatively slow rate of rotation while transferring angular momentum to the free spinning rotor which continues to rotate at a high rate relative to the projectile body. Rotationally phased steering commands, which are generated from on-board homing sensor signals or up-link data signals received from a remote error sensor, are applied to a linear actuator within the projectile body. The actuator pivots the spin axis of the rotor away from the longitudinal axis of the projectile body. The resulting precession torque of the spinning rotor induces a change in the angle of attack between the projectile body axis and the actual velocity vector of the projectile thereby inducing midcourse trajectory shaping.

摘要翻译： 抛射体具有安装在其中的陀螺仪，其包括转子和用于支撑转子的机构，所述旋转器围绕最初与射弹体的纵向轴线重合并且可远离射弹体的纵向轴线枢转的旋转轴旋转。 转子最初被锁定在射弹体上，使其在发射过程中与射弹体旋转。 此后，将转子解锁，并将射弹体旋转到相对较慢的旋转速度，同时将角动量传递到相对于射弹体以高速率继续旋转的自由旋转转子。 通过从远程误差传感器接收的车载归位传感器信号或上行链路数据信号产生的旋转相位转向命令被施加到射弹体内的线性致动器。 执行器使转子的旋转轴远离射弹体的纵向轴线。 旋转转子的进动转矩引起弹丸体轴线与射弹的实际速度矢量之间的迎角变化，从而引起中线轨迹整形。

公开(公告)号：US4429611A

公开(公告)日：1984-02-07

申请号：US344097

申请日：1982-01-29

申请人： Delbert J. Oldham ,  John A. Karish

发明人： Delbert J. Oldham ,  John A. Karish

IPC分类号： F42B17/00 ,  F41F3/06 ,  F41F3/04

CPC分类号： F41F3/06

摘要： An airborne missile launcher for air launching of man-portable, tube-launched missiles includes a central support frame with attachment means for detachable attachment to an aircraft or other launching platform, with a central frame member having a launch tube saddle support assembly at each side of the frame member with quick detachable clamp means and an alignment guide for quickly positioning and securing launch tubes into position with auto connecting means for automatically connecting the electronics control system and coolant gas to the launch tube assembly upon clamping the assembly into position. An aerodynamic shell encloses the support structure and includes a quick release cover for providing access to the tube clamp assemblies for loading and unloading launch tubes.

摘要翻译： 用于空中发射便携式管导弹的空中导弹发射器包括具有用于可拆卸地附接到飞行器或其它发射台的附接装置的中央支撑框架，中央框架构件在每一侧具有发射管鞍座支撑组件 的框架构件具有快速可拆卸的夹紧装置和对准引导件，用于通过自动连接装置快速地将发射管定位和固定到位，用于在将组件固定就位时自动连接电子控制系统和冷却剂气体到发射管组件。 空气动力学外壳包围支撑结构，并且包括快速释放盖，用于提供对用于装载和卸载发射管的管夹组件的通路。

公开(公告)号：US4426617A

公开(公告)日：1984-01-17

申请号：US388821

申请日：1982-06-16

申请人： Lester L. Forrester

发明人： Lester L. Forrester

IPC分类号： G01R19/165 ,  G01R27/02 ,  G01R19/14

CPC分类号： G01R19/16576

摘要： An audible test device which provides a tone when a resistance being measured is less than a selected value, the selected value being variable to a few milli-ohms. A first or second source of voltage is applied to a constant current source. The constant current generated is divided between two paths, one path including test leads holding the resistance being measured therebetween, the other path through a voltage adjusting device. The output from the voltage adjusting device is applied to one input of a voltage comparator, the voltage appearing across the resistance under test being applied to the other input of the voltage comparator. The output of the comparator is applied to a voltage controlled oscillator (VCO), the output of the VCO being applied to a piezoelectric device and to a speaker operable only when the second voltage source is utilized, thereby generating an audible tone. To set the threshold below which the audible tone will be generated, test leads are placed across a known resistance value equal to the threshold desired and the voltage adjusting device is adjusted until a tone is heard. This occurs only when the output of the voltage adjusting device exceeds the voltage across the resistance under test, the output of the comparator causing the VCO to generate an output. Thereafter, when the test leads are placed across a circuit path or resistance under test having a resistance value below the set desired value, a tone will be emitted.

摘要翻译： 当测量的电阻小于所选值时提供音调的可听测试装置，所选择的值可变为几毫欧。 将第一或第二电压源施加到恒定电流源。 产生的恒定电流在两条路径之间分开，一条路径包括保持其间测量电阻的测试线，另一条通过电压调节装置的路径。 电压调节装置的输出被施加到电压比较器的一个输入端，被测电阻上出现的电压被施加到电压比较器的另一个输入端。 比较器的输出被施加到压控振荡器（VCO），VCO的输出被施加到压电器件和仅在使用第二电压源时可操作的扬声器，从而产生可听见的音调。 要设置低于此阈值的阈值，测试线将跨过已知的等于所需阈值的电阻值，并调整电压调节装置直到听到声音。 这仅在电压调节装置的输出超过被测电阻两端的电压时，才产生VCO的比较器的输出。 此后，当测试引线横跨电路路径或电阻值低于设定的所需值的电阻测试时，会发出一个音调。