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公开(公告)号：US4688040A
公开(公告)日：1987-08-18
申请号：US676035
申请日：1984-11-28
CPC分类号： H01Q17/008 , F41H3/00
摘要： A radar return suppressor for use in concealing and camouflaging mobile targets such as trucks, artillery and like vehicles. One or more lengths of a support member attachable to the target and components support and position a radar signal attenuator between the target and the anticipated radar source. In one embodiment, the attenuator is a multiplicity of closely spaced flexible plastic strands having radar signal absorbing material dispersed in the strands to form a labyrinth to entrap and absorb the radar signal. In a second embodiment the labyrinth of strands is replaced by an intertwined plastic vine-like structure secured in the support member for absorbing the energy of the radar signal.
摘要翻译： 一种用于隐藏和伪装卡车，火炮和类似车辆等移动目标的雷达回波抑制器。 一个或多个长度的可附接到目标的支撑构件和部件支撑并且在目标和预期雷达源之间定位雷达信号衰减器。 在一个实施例中，衰减器是多个紧密间隔的柔性塑料股，其具有分散在股线中的雷达信号吸收材料，以形成迷宫，以捕获和吸收雷达信号。 在第二实施例中，线的迷宫被替换为固定在支撑构件中的缠绕在一起的塑料藤状结构，用于吸收雷达信号的能量。
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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
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。
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公开(公告)号：US4399962A
公开(公告)日：1983-08-23
申请号：US298128
申请日：1981-08-31
CPC分类号： F42B10/62
摘要： An articulated nose is locked in axial alignment with the longitudinal axis of a rolling projectile body. Pyrotechnic means within the nose is actuated to unlock the nose and tilt it toward the target when the error between the projectile path and the path to the target exceeds a predetermined threshold.
摘要翻译： 铰接的鼻子与滚动的射弹体的纵向轴线轴向对准。 当射弹路径和目标路径之间的误差超过预定阈值时，起动器内的烟火手段被致动以解锁鼻子并将其向目标倾斜。
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公开(公告)号：US4600218A
公开(公告)日：1986-07-15
申请号：US673697
申请日：1984-11-21
申请人： Oakley G. Ross , Mark L. Kline , Larry D. Wedertz
发明人： Oakley G. Ross , Mark L. Kline , Larry D. Wedertz
CPC分类号： F16L25/02 , Y10S285/904 , Y10S285/918
摘要： A separable electrical isolator for coupling two pieces of conductive tubing carrying high pressure cryogenic gas includes a gas-impervious dielectric spacer with a pair of opposing surfaces and a bore extending therebetween in which the pieces of tubing are sealed axially-aligned in fluid communication with an electrically-nonconductive gap between them. A pair of complementary coupling members are rigidly attached to the pieces of tubing to define outwardly-extending annular surfaces that are each sealed about the periphery of a corresponding piece in a position slightly set back from and facing an end of the piece. The coupling members are separably and nonconductively interconnected with the annular surfaces facing the spacer surfaces and O-ring seals in between to apply compressive force to the spacer and seals and thereby effect the seal.
摘要翻译： 用于联接承载高压低温气体的两片导电管的可分离电气隔离器包括具有一对相对表面的气体不可渗透的电介质间隔件和在其间延伸的孔，其中管件被轴向对准密封，与 它们之间的电绝缘间隙。 一对互补联接构件刚性地连接到管件上，以限定向外延伸的环形表面，每个环形表面围绕对应件的周边在稍微从该件的端部稍微设置的位置中密封。 联接构件与面向间隔件表面的环形表面和O形环密封件之间可分离地和不导电地互连，以将压缩力施加到间隔件和密封件，从而实现密封。
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公开(公告)号：US4581977A
公开(公告)日：1986-04-15
申请号：US490629
申请日：1983-05-02
摘要： An apparatus and method for establishing the alignment of heat seeking missiles with the longitudinal axis of a launch pod within which the missiles are contained is disclosed. A housing containing a heat source and collimating optics provides a simulated distant infrared target for the missiles. A tapered probe rigidly attachable to the housing fits securely into a central alignment socket in the launcher pod. The probe is accurately offset from the center line of the alignment socket by the housing to establish the optical axis of the simulated target parallel to the axis of the launcher pod, and in front of the stored missiles. The position of the missile within the launch pod is adjustable to maximize the target signal strength received by the missile from the simulated target to achieve missile alignment with the axis of the launcher pod.
摘要翻译： 公开了一种用于建立热寻求导弹与包含导弹的发射舱的纵向轴线对准的装置和方法。 包含热源和准直光学元件的壳体为导弹提供了一个模拟的远红外目标。 牢固地附接到壳体的锥形探针牢固地配合到发射器舱中的中心对准插座中。 探针通过外壳准确地偏离对准插座的中心线，以建立平行于发射器舱的轴线的模拟目标的光轴，并在存储的导弹前面。 发射舱内导弹的位置是可调整的，以最大限度地提高导弹从模拟目标接收到的目标信号强度，以实现与发射舱的导弹对准。
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公开(公告)号：US4412272A
公开(公告)日：1983-10-25
申请号：US297548
申请日：1981-08-31
申请人： Larry D. Wedertz , Oakley G. Ross
发明人： Larry D. Wedertz , Oakley G. Ross
CPC分类号： H05K1/189 , H05K3/284 , H05K2201/0116 , H05K2201/051 , H05K2201/10651 , H05K2203/1311 , H05K2203/1322 , H05K3/3447
摘要： A flexible printed circuit card assembly includes an insulating sheet positioned over the foil of a flexible printed circuit card and adapted to accommodate the passage of electronic component leads therethrough for soldering to the printed circuit card. A layer of protective insulating foam, having a backing thereon, is positioned over the components and the assembly is rolled into a spiral configuration with leads extending from at least one end.
摘要翻译： 柔性印刷电路卡组件包括位于柔性印刷电路卡的箔上的绝缘片，并适于容纳电子元件引线通过其中以焊接到印刷电路卡。 一层保护性绝缘泡沫，其上具有背衬，位于部件上方，并且组件被卷成具有从至少一端延伸的引线的螺旋形构造。
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公开(公告)号：US4411398A
公开(公告)日：1983-10-25
申请号：US255413
申请日：1981-04-20
CPC分类号： F42B10/146
摘要： A simple, retractable, self-erecting wing for a low speed missile having a fabric wing cover affixed to a leading edge structure that is the only erected structural member in the wing operative position. The wing cover forms a pocket that contains air. The leading edge structure is hinged and folds, along with the wing cover, into a compact slotted space adjacent the outer wall of a missile body. In the folded position the leading edge structure forms a cover for the slot and the cover coincides with the outer shape of the missile body. A large fabric wing can be completely stored within the missile body for minimum drag during any high speed portion of the missile flight, the wing being released to the operative position by a simple mechanism.
摘要翻译： 一种用于低速导弹的简单的，可伸缩的自立式机翼，其具有固定到作为机翼操作位置中唯一竖立的结构构件的前缘结构的织物翼罩。 机翼盖形成一个包含空气的口袋。 前缘结构与翼盖一起铰接并折叠成与导弹体外壁相邻的紧凑的狭槽空间。 在折叠位置，前缘结构形成用于槽的盖，并且盖与导弹体的外形重合。 在导弹飞行的任何高速部分期间，可以将大型织物翼片完全储存在导弹体内，以达到最小的阻力，机翼通过简单的机构释放到操作位置。
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公开(公告)号：US5442991A
公开(公告)日：1995-08-22
申请号：US558077
申请日：1983-12-05
CPC分类号： F41A9/36
摘要： A device for use in a rapid-fire weapons system wherein a gun is movable in both elevation and azimuth. The device is designed to have a high round storage capacity and transfers rounds across the azimuth axis, thus allowing the gun to move in azimuth with respect to the magazine. The storage, or accumulation, feature of the device allows rounds to be fed to the gun before the magazine has been driven to the demand rate.The device also provides a closed loop round carrier system which allows for the return of expended round casings to the magazine.
摘要翻译： 一种用于快速发射武器系统的装置，其中枪可以在高程和方位角上移动。 该设备被设计为具有高的圆形存储容量并且在方位角轴上传送轮，从而允许枪相对于刀库移动方位角。 设备的存储或累积功能允许在刀库被驱动到需求速率之前将回合送入枪。 该装置还提供一个闭环圆形载体系统，其允许将消耗的圆形壳体返回到料盒。
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公开(公告)号：US5365826A
公开(公告)日：1994-11-22
申请号：US6281
申请日：1993-01-19
申请人： Larry D. Wedertz
发明人： Larry D. Wedertz
IPC分类号： F41A9/45
CPC分类号： F41A9/45
摘要： A rotary breech mechanism (10) is provided for loading large caliber guns. The mechanism comprises a rotary transfer member (12) which is cylindrical and mounted in the gun barrel (16) near the breech end (18). A hole (14) through the rotary transfer member (12) is aligned either with an ammunition magazine tube (48) for loading or with the gun barrel (16) for firing of a projectile (20). Once the projectile (20) has been fired, the rotary transfer member (12) is rotated to accept the next projectile, no matter what position the gun is in. The azimuthal orientation of the barrel (16) does not affect the operation of the loading mechanism.
摘要翻译： 提供用于装载大口径枪的旋转后膛机构（10）。 该机构包括旋转传递构件（12），该旋转传递构件（12）是圆柱形的并且安装在靠近枪口（18）的枪管（16）内。 通过旋转传递构件（12）的孔（14）与用于装载的弹药盒管（48）或用于射弹（20）的枪管（16）对准。 一旦抛射体（20）被点燃，旋转传递构件（12）旋转以接受下一个射弹，无论枪的位置如何。枪管（16）的方位取向不影响 装载机制。
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公开(公告)号：US4667899A
公开(公告)日：1987-05-26
申请号：US676034
申请日：1984-11-28
申请人： Larry D. Wedertz
发明人： Larry D. Wedertz
CPC分类号： F42B10/14
摘要： A self-erecting wing structure for increased missile performance and maneuverability without significant sacrifice of payload space includes a wing pivotally attached to an air frame in a retracted position in which the wing is both rotated about its spanwise axis relative to an erected position and pivoted forward alongside the air frame. Rotational components enable passing air to swing the wing to the erected position when it is released from the retracted position during flight. A secondary wing surface is included that automatically deploys to increase wing area.
摘要翻译： 用于增加导弹性能和机动性而没有有效空间的显着牺牲的自立式翼结构包括在缩回位置中枢转地附接到空气框架的翼，其中翼相对于竖立位置围绕其翼展方向轴线旋转并且向前枢转 与空气框架一起。 旋转部件使飞行中的空气能够在飞行期间从缩回位置释放时使机翼摆动到竖立位置。 包括二次翼面，自动部署以增加机翼面积。
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