专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

21. 发明授权

US07185575B1 Weapon mounting and remote position recognition system 失效
标题翻译：武器安装和远程位置识别系统
公开(公告)号：US07185575B1
公开(公告)日：2007-03-06
申请号：US11251532
申请日：2005-10-04
申请人： Ronald F. Collier , John T. Dillon
发明人： Ronald F. Collier , John T. Dillon
IPC分类号： F41F3/04
CPC分类号： F41F3/04 , F41A23/24
摘要： A system for remote tracking of a tactical missile assembly orientation during targeting and leading to launch from a platform, including a weapon station frame rotatably attached to the platform and a command launch unit attached to the weapon station frame. A launch tube assembly is pivotably attached thereon, including a launch tube in which a tactical missile is positioned prior to launch. The launch tube is replaceable with a like-configured launch tube and tactical missile. A launch tube position recognition unit is disposed proximal of the launch tube and adjacent of the weapon station frame. The position recognition unit includes a tracking and encoder device enclosed by a protective encoder member rotatably attachable between the launch tube and weapon station frame. The tracking and encoder device identifies launch tube positions and remotely relays position coordinates to the command launch unit during targeting of the missile leading to missile launch.
摘要翻译：一种在瞄准期间远程跟踪战术导弹组件方向并导致从平台发射的系统，包括可旋转地附接到平台的武器站框架和附接到武器站框架的命令发射单元。发射管组件可枢转地附接在其上，包括发射管，其中在发射之前定位战术导弹。发射管可以用类似配置的发射管和战术导弹替换。发射管位置识别单元设置在发射管的近侧并且与武器站框架相邻。位置识别单元包括跟踪和编码器装置，该跟踪和编码器装置由可旋转地附接在发射管和武器站框架之间的保护编码器构件包围。跟踪和编码器设备识别发射管位置，并且在瞄准导弹导弹发射的目标期间，将命令发射单元的位置坐标远程中继。

22. 发明授权

US06926579B2 Toy rocket launch pad with directional safety valve 有权
公开(公告)号：US06926579B2
公开(公告)日：2005-08-09
申请号：US10915748
申请日：2004-08-11
申请人： Mark Rappaport
发明人： Mark Rappaport
IPC分类号： F41B11/00 , F41B11/24 , F41F3/04 , A63H27/26
CPC分类号： F41B11/89 , F41B11/66 , F41F3/04
摘要： Disclosed herein is an apparatus and method for launching a toy rocket that includes rotating a launch tube about an axis that is parallel with a connecting tube, which is rotatably connected to the launch tube; extending the launch tube in a perpendicular direction; progressively closing a safety valve by rotating the launch tube toward a vertical position, relative to a launch pad assembly; loading the toy rocket onto a distal end of the extended launch tube; and rapidly compressing a bellows in communication with the launch tube.

23. 发明授权

US06318229B1 System for boosting velocity of a rocket 失效
标题翻译：用于提高火箭速度的系统
公开(公告)号：US06318229B1
公开(公告)日：2001-11-20
申请号：US09450838
申请日：1999-11-22
申请人： Joel P. Nevels , Margaret H. Nevels
发明人： Joel P. Nevels , Margaret H. Nevels
IPC分类号： F41F304
CPC分类号： F41F3/04
摘要： A system for boosting the velocity of a rocket utilizing a container having a bottom and a side wall portion extending outwardly from the bottom. The side portion terminates in a peripheral edge and forms a chamber. A platform is supported in the chamber and is movable from a first position to a second position adjacent the peripheral edge of the side wall portion of the container. Exhaust gases are conducted to the chamber such that movement of the platform within the container supporting the rocket takes place.
摘要翻译：一种利用具有从底部向外延伸的底部和侧壁部分的容器来提高火箭速度的系统。侧部终止于周边边缘并形成一个室。平台被支撑在腔室中并且可以从第一位置移动到与容器的侧壁部分的周边边缘相邻的第二位置。废气被引导到室，使得平台在支撑火箭的容器内的运动发生。

24. 发明授权

US06227117B1 Retaining device, especially for the rear igniter of a missile 失效
标题翻译：保持装置，特别适用于导弹的后方点火器
公开(公告)号：US06227117B1
公开(公告)日：2001-05-08
申请号：US09170279
申请日：1998-10-13
申请人： Guy Peltier , Paul Goillot , André Gouthiere , Gérard Koenig
发明人： Guy Peltier , Paul Goillot , André Gouthiere , Gérard Koenig
IPC分类号： F42B400
CPC分类号： F41F3/04 , F41A17/00
摘要： A device for retaining an element ejected by a pyrotechnic device when it is fired comprises at least one metal cap placed behind the nozzle of the device and designed to receive the ejected element, the cap being held in position by curved rigid links. The kinetic energy of the captured element carries along the cap and the captured element and the motion of the assembly is braked by the deformation of the rigid links. Application especially to the retaining of the rear igniter of a missile.
摘要翻译：用于保持由烟火装置喷射的元件在被烧毁时的装置包括设置在装置的喷嘴后面的至少一个金属帽，并被设计成容纳所弹出的元件，帽通过弯曲的刚性连杆保持就位。捕获的元件的动能沿着盖和捕获的元件携带，并且组件的运动被刚性连杆的变形制动。特别适用于保留导弹后方点火器。

25. 发明授权

US5924648A System for upending/reclining launch vehicles 失效
标题翻译：运载火箭/升降系统
公开(公告)号：US5924648A
公开(公告)日：1999-07-20
申请号：US943454
申请日：1997-10-03
申请人： James William Ellinthorpe
发明人： James William Ellinthorpe
IPC分类号： B64G1/00 , B64G5/00 , F41A23/42 , F41F3/04 , B64F1/04 , F41A9/00
CPC分类号： B64G5/00 , F41A23/42 , F41F3/04 , B64G1/002
摘要： An improved system is disclosed for upending/reclining an extraterrestrial vehicle. In one embodiment, first and second trunnion supports may be positioned on opposing sides of a u-shaped opening provided at the rearward end of a mobile support platform. A launch vehicle may be pivotably supported via trunnions received by the first and second trunnion supports for pivotal movement between a reclined position on top of the support platform to an upended position. In the upended position a launch vehicle will extend through the u-shaped opening. A bridge assembly may be selectively interconnected to the launch vehicle to facilitate handling, transport and storage therewith.
摘要翻译：公开了一种改进的系统，用于升级/斜倚地外车辆。在一个实施例中，第一和第二耳轴支撑件可以定位在设置在移动支撑平台的后端处的u形开口的相对侧上。运载火箭可以通过由第一和第二耳轴支撑件接收的耳轴枢转地支撑，用于在支撑平台的顶部上的倾斜位置到支撑平台之间的枢转运动。在最后的位置，运载火箭将延伸穿过U型开口。桥式组件可以选择性地互连到运载火车，以便于其处理，运输和存储。

26. 发明授权

US5845875A Modular launch pad system 失效
标题翻译：模块化发射台系统
公开(公告)号：US5845875A
公开(公告)日：1998-12-08
申请号：US627565
申请日：1996-04-04
申请人： Gary G. Deel
发明人： Gary G. Deel
IPC分类号： B64F1/04 , B64G5/00 , F41F3/04 , B64F1/14
CPC分类号： F41F3/04 , B64F1/04 , B64G5/00 , F41F3/0413
摘要： A modular launch pad for a launch vehicle which comprises a frame and a plurality of building units separably connected to the frame by means of connectors. The building unit comprise a concrete slab and a peripheral frame made of U-shaped channel sections connected to one another to form a frame, wherein the legs of the U are directed inwardly to engage the major surfaces of the slab. At least one of the legs of the channel sections is partially embedded in the slab so that the outer surfaces of the legs lie flush with the portion of the major surface extending between the legs. A plurality of longitudinally and transversely extending reinforcement bars are embedded in the concrete slab and a plurality of connecting means are secured to the slab. The pad has a launch vehicle mount for supporting a launch vehicle and defines exhaust gas channels in flow communication with an exhaust gas opening in the mount. Deflectors serve to channel launch exhaust gases of the launch vehicle into the channels away from the vehicle.
摘要翻译：一种用于运载火箭的模块化发射台，其包括通过连接器可分离地连接到所述框架的框架和多个建筑物单元。建筑单元包括混凝土板和由彼此连接以形成框架的U形通道部分制成的周边框架，其中U的脚向内指向以接合板坯的主表面。通道部分的腿部中的至少一个部分地嵌入板坯中，使得腿部的外表面与在腿部之间延伸的主表面的部分齐平。多个纵向和横向延伸的加强筋嵌入在混凝土板中，多个连接装置固定在板坯上。垫具有用于支撑运载火箭的运载火箭架，并且限定与安装件中的废气开口流动连通的排气通道。导向器用于将运载火箭的废气引导到远离车辆的通道中。

27. 发明授权

US4916999A Offshore launching system 失效
标题翻译：离岸发射系统
公开(公告)号：US4916999A
公开(公告)日：1990-04-17
申请号：US263625
申请日：1988-10-27
申请人： C. R. Palmer , Robert A. Keller , Daniel F. McNease
发明人： C. R. Palmer , Robert A. Keller , Daniel F. McNease
IPC分类号： F41F3/04
CPC分类号： F41F3/04
摘要： A jack-up type of offshore oil-drilling platform is adapted for rocket launching, wherein the rocket is assembled on a mobile launch pad in a protected on-shore facility then loaded onto the floating jack-up barge for transport to a launch site miles offshore. The barge is jacked up to create a stable, sea-bottom supported structure; a particular feature is the used of a movable cantilever structure on which the rocket and its supporting pad are loaded while in the on-shore facility, then this structure is moved to a central location on the barge, the barge is floated, and the floating barge is towed to the launch site. At the launch site the structure is moved back to a cantilevered position for launch. In this manner the exhaust gasses from the rocket motors can be directed harmlessly into the sea.
摘要翻译：一种自升式海上石油钻井平台适用于火箭发射，其中火箭组装在受保护的岸上设施的移动发射台上，然后装载到浮动自升式驳船上，以运送到发射场数英里离岸驳船被打倒，形成一个稳定的海底支撑结构; 特别的特征是在岸上设施中使用了可移动的悬臂结构，火箭及其支撑垫在其上装载，然后将该结构移动到驳船上的中心位置，驳船浮起，浮动驳船被拖到发射场。在发射场地，结构被移回悬臂位置进行发射。以这种方式，来自火箭发动机的废气可以无害地引导到海中。

28. 发明授权

US4470336A Armored missile launch/shipping container 失效
标题翻译：装甲导弹发射/运输集装箱
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。

29. 发明授权

US4431349A Ice-filled structure and tunnelling method for the egress and launching of deep-based missiles 失效
标题翻译：用于深基导弹出口和发射的冰盖结构和隧道掘进方法
公开(公告)号：US4431349A
公开(公告)日：1984-02-14
申请号：US368125
申请日：1982-04-14
申请人： David L. Coursen
发明人： David L. Coursen
IPC分类号： E02D29/00 , E21D1/14 , F41F3/04 , E21D5/12
CPC分类号： F41F3/04 , E02D29/00 , E21D1/14
摘要： Missiles located in the deeper (hard rock) portion of a shaft or tunnel are protected from damage during a nuclear attack by a mass of ice, preferably trumpet-shaped, located in the outermost portion (e.g., 600-900 meters). When missile egress is required, an ice-supported passageway is bored through the ice, preferably by melting. The trumpet shape assures a straight path for missile egress even if the shaft or tunnel should become transversely displaced by a cratering explosion against the surface.
摘要翻译：位于轴或隧道的较深（硬岩）部分的导弹在核攻击期间被保护，以免受位于最外部分（例如600-900米）的大量冰，优选小号形状的导弹。当导弹需要出口，冰支撑的通道穿过冰，优选通过熔化而钻孔。喇叭形状确保导弹出口的直线路径，即使轴或隧道应该通过对表面的火山口爆炸而横向移位。

30. 发明授权

US4063485A Decoy launcher system 失效
标题翻译：诱饵发射系统
公开(公告)号：US4063485A
公开(公告)日：1977-12-20
申请号：US603498
申请日：1966-12-21
申请人： William M. Carter , Robert W. Klauschie , George H. Schillreff
发明人： William M. Carter , Robert W. Klauschie , George H. Schillreff
IPC分类号： F41F3/04 , F41H11/02 , F41F3/00
CPC分类号： F41H11/02 , F41F3/04
摘要： The disclosure broadly relates to a launcher system for providing a protective cover against homing devices operating upon infrared, sound navigation and ranging, and/or microwave-reflected energy. The launcher system is illustrated in one embodiment as a nine round portable system wherein the decoy rounds are selectively fired manually by nine pushbuttons located in the control box. The decoy rounds each contain an electric squib which simultaneously ignites both a lift charge and a time fuse. The lift charge propels the round from the launcher in a ballistic trajectory and the time fuse ignites a burst charge which disperses the payload at the optimum altitude for the type of round being used. Other embodiments of the system illustrate a ten round system which may also be utilized in multiples thereof, with the control therefor being located within the control section of a ship or the like and activated through an intervalometer. The rounds for each of the embodiments are connected to receptacles positioned intermediate the launch tubes. The squib plug, wires, and shielding braid all fly with the rounds when fired.
摘要翻译：本发明广泛地涉及一种用于提供针对在红外线，声音导航和测距和/或微波反射能量上操作的归巢装置的保护盖的发射器系统。发射器系统在一个实施例中示出为九轮便携式系统，其中通过位于控制箱中的九个按钮来选择性地发射诱饵轮。诱饵轮每个都包含一个电子爆管，同时点燃电梯充电和时间保险丝。提升装置以弹道轨迹推动发射器的一轮，并且时间保险丝点燃突发电荷，将有效载荷分散在所使用的类型的最佳高度。该系统的其他实施例示出了也可以以其倍数使用的十轮系统，其控制位于船等的控制部分内并通过间隔计激活。每个实施例的轮连接到位于发射管之间的插座。点火塞，电线和屏蔽编织物在发射时都与飞轮一起飞行。

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