公开(公告)号：WO2018052485A1

公开(公告)日：2018-03-22

申请号：PCT/US2017/023286

申请日：2017-03-21

Applicant: RAYTHEON COMPANY

Inventor： SZLEMKO, Emile, M. ,  LE, Huy ,  GIN, Brian, A. ,  WAHL, Ryan, P. ,  KULBACKI, Mary, L. ,  ANDERSON, Chad, V. ,  UEBERSCHAR, David, P.

IPC: F41F3/073

Abstract: An effector launching system includes an environment that has external components located within the environment. The effector launching system may include a modular controller located in the environment of an effector launching system and the external components may be located in the environment externally to the modular controller for executing an effector launching sequence. The modular controller may include a core processor module that is configured to execute a plurality of different effector launching sequences using the external components and a plurality of converting modules that each have an electro-mechanical interface and is connectable between the core processor module and one of the external components. The plurality of converting modules are configured to send and receive data with the core processor module and the plurality of external components.

Abstract translation: 效应发射系统包括具有位于环境内的外部组件的环境。 效应器发射系统可以包括位于效应器发射系统的环境中的模块化控制器，并且外部组件可以位于模块化控制器外部的环境中，用于执行效应器发射顺序。 该模块化控制器可以包括核心处理器模块，该核心处理器模块被配置为使用外部部件和多个转换模块来执行多个不同的效果器发射序列，每个转换模块具有机电接口并且可连接在核心处理器模块和 外部组件。 多个转换模块被配置为与核心处理器模块和多个外部组件发送和接收数据。

公开(公告)号：WO2012027099A1

公开(公告)日：2012-03-01

申请号：PCT/US2011/047045

申请日：2011-08-09

Applicant: LOCKHEED MARTIN CORPORATION ,  SKURDAL, Daniel, A. ,  SNEDIKER, John

Inventor： SKURDAL, Daniel, A. ,  SNEDIKER, John

IPC: F41F3/04 ,  F41F3/073

CPC classification number: F41F3/0413 ,  F41F3/073

Abstract: An apparatus is disclosed that is a self-contained gas management system (hereinafter "GMS") that accommodates individual canisters of highly energetic small munitions, but is not so limited. By decoupling the gas management system for a given munition from an adjacent munition, the risk of downing a multi-pack launcher or munition adapter is reduced. Thermal wear, overheating, restrained firing and aft closure debris can be isolated through the separation of gas management systems. In addition, the GMS allows for ease of replenishment and maintenance of a given sub-cell of a multi-pack system. The GMS works with existing munitions and canisters without the need to modify them. Each GMS is dimensioned to fit the canistered munition it receives as well as the launch system with which it is used. The illustrative GMS comprises a plenum, and a first and a second uptake structure. The plenum receives the exhaust from the canistered munition when the munition fires. The plenum is fluidically coupled to the first and second uptake structures. The uptake structures in the illustrative embodiment receive the missile exhaust from the plenum and vent the exhaust to the atmosphere. In the illustrative embodiment, the first and second uptake structures are disposed along opposite sides of the canistered munition, flanking it.

Abstract translation: 公开了一种装置，其是容纳高能量小弹药的各个罐的独立气体管理系统（以下称为“GMS”），但不限于此。 通过将给定弹药的天然气管理系统与相邻的弹药解耦，减少多包发射器或弹药适配器的风险。 通过气体管理系统的分离，可以隔离热磨损，过热，约束的点火和后盖碎片。 此外，GMS允许容易地对多包系统的给定子单元进行补充和维护。 GMS与现有的弹药和罐一起工作，无需修改它们。 每个GMS的尺寸都是为了适应它所接收的可燃弹药以及使用它的发射系统。 示例性GMS包括增压室和第一和第二吸收结构。 当弹药火灾时，全会收到了从弹药弹出的废气。 气室与第一和第二吸收结构流体耦合。 在说明性实施例中的摄取结构接收来自气室的导弹排气并将排气排放到大气中。 在说明性实施例中，第一和第二摄取结构沿着它的侧翼的相对侧布置。

公开(公告)号：WO2009138664A3

公开(公告)日：2010-01-07

申请号：PCT/FR2009050751

申请日：2009-04-23

Applicant: DCNS ,  FALIP ALAIN

Inventor： FALIP ALAIN

IPC: F41F3/04 ,  B63G3/04 ,  F41F3/073 ,  F41F3/077

CPC classification number: F41F3/077 ,  B63B19/197 ,  B63G3/04 ,  F41F3/0413 ,  F41F3/073

Abstract: This shutter system (14) for the barrel of a missile launcher, the launcher (1) comprising at least one container (2, 3) capable of accommodating at least one missile (4, 5) and a pipe (10) for discharging the propulsion gases comprising a gas extraction barrel (11), the container being in communication with the pipe when the missile is fired and the pipe being in communication with the atmosphere (12) via the barrel equipped with the said shutter system, is characterized in that the shutter system comprises at least one panel (12, 13) and a panel retaining means (18, 19), able to move between a closed position and an open position, the retaining means comprising a means (18a) of return from the open position to the closed position and a means (18b) of dissipating the energy resulting from the opening movement and the closing movement.

Abstract translation: 该发射器（1）包括至少一个容纳至少一个导弹（4,5）和一个管（10）的容器（2,3），该容器（2,3）用于导弹发射器的枪管， 包括气体提取筒（11）的推进气体，当所述导弹被射击时，所述容器与所述管道连通，并且所述管道通过装备有所述闸门系统的筒体与大气（12）连通，其特征在于， 快门系统包括能够在关闭位置和打开位置之间移动的至少一个面板（12,13）和面板保持装置（18,19），所述保持装置包括从打开位置返回的装置（18a） 位置到关闭位置，以及消除由打开运动和关闭运动产生的能量的装置（18b）。

公开(公告)号：WO2017136650A1

公开(公告)日：2017-08-10

申请号：PCT/US2017/016394

申请日：2017-02-03

Applicant: UNITED LAUNCH ALLIANCE, LLC

Inventor： ECHELMAN, Philip, M. ,  WALTON, Edwin, W.

IPC: B64G1/00 ,  B64G1/64 ,  F41F3/04 ,  F41F3/052 ,  F41F3/073 ,  F42B15/00 ,  F42B15/36 ,  F42B15/38

CPC classification number: B64G1/645 ,  B64G1/641 ,  F16B2/14 ,  F16B7/02 ,  F16B7/0406

Abstract: A new system and apparatus for detachably joining a first component to a second component is disclosed, along with a method for detachably joining two components. Embodiments of the present invention include a tensioning apparatus and system for clamping joints. The tensioning apparatus may include a wedge block and a fastening device. The clamping joint may be a tongue and groove joint that is tightened using the tensioning apparatus.

Abstract translation: 公开了用于将第一部件可拆卸地连接到第二部件的新系统和装置，以及用于可拆卸地连接两个部件的方法。 本发明的实施例包括用于夹紧接头的张紧装置和系统。 张紧装置可以包括楔形块和紧固装置。 夹紧接头可以是使用张紧装置拧紧的舌槽接头。

公开(公告)号：WO2009108231A3

公开(公告)日：2009-09-03

申请号：PCT/US2008/084115

申请日：2008-11-20

Applicant: LOCKHEED MARTIN CORPORATION ,  SKURDAL, Daniel, A. ,  FOUTS, Timothy, R. ,  HOUSTON-MANCHESTER, Jennifer, L. ,  SNEDIKER, John

Inventor： SKURDAL, Daniel, A. ,  FOUTS, Timothy, R. ,  HOUSTON-MANCHESTER, Jennifer, L. ,  SNEDIKER, John

IPC: F41F3/073

Abstract: A launch system for use as a standalone munition launcher or as a guest launcher within a main battery host launcher.

公开(公告)号：WO2008010180A3

公开(公告)日：2008-03-06

申请号：PCT/IB2007052827

申请日：2007-07-16

Applicant: SPACEGO TECHNOLOGIES PROPRIETA ,  LEUSCHNER ANDRIES HERMANN

Inventor： LEUSCHNER ANDRIES HERMANN

IPC: F41F3/073 ,  F41B6/00

CPC classification number: F41B6/003 ,  F41A1/02 ,  F41B6/00 ,  F41F3/073

Abstract: This invention relates to launching of a flight vehicle, such as a rocket, an aircraft and the like, from a generally upwardly directed subterranean launch shaft of at least 300 m length, preferably of a length of 500 m or more. Preferably, the launch shaft is an amortized mine shaft. Launching is by means of one of, or a combination of, several possible propulsion systems. For each system, at least some components are external of the flight vehicle and associated with or mounted in the launch shaft. One kind of propulsion system may use expansion of gas in the launch shaft behind the flight vehicle. Other propulsion systems use electromagnetism or Lorentz-type actuators, such as a coil gun or gauss gun, a linear induction motor or linear synchronous motor, or a rail gun. The launch shaft mounts guiding means for guiding the flight vehicle along the launch shaft.

Abstract translation: 本发明涉及从大体向上的长度至少为300m，优选长度为500m或更长的地下发射轴发射飞行器，例如火箭，飞机等。 优选地，发射井是分期安排的矿井。 发射是通过几种可能的推进系统之一或其组合。 对于每个系统，至少一些部件在飞行器外部并且与发射井相关联或安装在发射井中。 一种推进系统可以使用飞行器后面的发射轴中的气体膨胀。 其他推进系统使用电磁或Lorentz型执行器，如线圈枪或高斯枪，线性感应电机或线性同步电机，或轨道枪。 发射轴安装用于沿着发射轴引导飞行器的引导装置。

公开(公告)号：WO2023287743A1

公开(公告)日：2023-01-19

申请号：PCT/US2022/036760

申请日：2022-07-12

Applicant: BLKBOX LLC

Inventor： CRYE, Caleb

IPC: F41G3/04 ,  F41F3/073 ,  F41G9/00 ,  F41G3/14 ,  F41G7/00 ,  F41G7/34 ,  F42B10/64 ,  G01S19/18 ,  G01S19/41

Abstract: A method of executing a mission for at least one mobile munition assembly in a mission environment is provided, the at least one mobile munition assembly having a container that encloses one or more launchers configured to receive and launch a munition. One or more electronic devices in communicatively coupling with one another in the mission environment form a secure network. A status of a situational awareness (SA) corresponding to each of the one or more electronic devices in the mission environment is transmitted. An input of parameters of the mission for the at least one mobile munition assembly is enabled, the parameters having one or more predefined rules associated therewith and configured to be applied to the parameters based on at least the status of the situational awareness (SA). An authorization or a denial of the mission for the at least one mobile munition assembly is requested.

公开(公告)号：WO2019106106A1

公开(公告)日：2019-06-06

申请号：PCT/EP2018/083048

申请日：2018-11-29

Applicant: NAVAL GROUP

Inventor： RASPIC, Pierre ,  PAUMIER, Philippe

IPC: F41A9/22 ,  F41A9/39 ,  F41F3/073 ,  F41F3/08

CPC classification number: F41F3/073 ,  F41A9/22 ,  F41A9/39 ,  F41F3/08

Abstract: Dispositif modulaire de lutte anti-sous-marine sur bâtiment de surface Le dispositif modulaire de lutte anti-sous-marine pour bâtiment de surface, comprend : - un premier sous-système (16) de stockage de munitions (18) comportant une sortie (28) pour lesdites munitions (18), - un deuxième sous-système (20) de tir desdites munitions (18) comportant une entrée (50) pour lesdites munitions (18), et - un troisième sous-système (22) de manutention adapté pour transférer les munitions (18) à l'écart du premier sous-système (16), Le troisième sous-système (22) comporte au moins un composant commun à au moins un des premier (16) et deuxième sous-systèmes (20).

公开(公告)号：WO2017021135A1

公开(公告)日：2017-02-09

申请号：PCT/EP2016/067132

申请日：2016-07-19

Applicant: THYSSENKRUPP MARINE SYSTEMS GMBH ,  THYSSENKRUPP AG

Inventor： JUNGE, Matthias ,  KLOTH, Oliver ,  FEUERHERDT, Tobias ,  KÖHN, Michael

IPC: F41F3/08 ,  F41F3/052 ,  B63G8/32 ,  F41F3/073 ,  F41F3/10 ,  F42B39/22 ,  F41F3/00 ,  F41A9/42

CPC classification number: F41F3/08 ,  F41A9/42 ,  F41F3/00 ,  F41F3/052 ,  F41F3/073 ,  F41F3/10 ,  F42B39/22

Abstract: Die Erfindung betrifft eine Waffenkupplung zum Einsatz in einem Waffenrohr. Die Waffenkupplung weist einen Ladebock (10), ein Gehäuse (20) und wenigstens eine am Gehäuse angeordnete Fixiervorrichtung (50) auf, wobei die Fixiervorrichtung zur Fixierung einer Waffe ausgebildet ist. Die Waffenkupplung weist ferner eine Längsrichtung auf.

Abstract translation: 本发明涉及一种连接臂用于在武器枪管使用。 连结臂具有设置在所述壳体（50），其中，所述固定装置用于固定一个枪上形成的防滑（10），壳体（20）和至少一个固定设备。 武器离合器还具有纵向方向。

公开(公告)号：WO2010036418A3

公开(公告)日：2010-06-10

申请号：PCT/US2009046359

申请日：2009-06-05

Applicant: RAYTHEON CO ,  PATTERSON WILLIAM N ,  DUPONT JAMES H ,  LOEHR RICHARD D ,  KIM HENRI Y ,  HALL GARRETT L ,  COOK JAMES M

Inventor： PATTERSON WILLIAM N ,  DUPONT JAMES H ,  LOEHR RICHARD D ,  KIM HENRI Y ,  HALL GARRETT L ,  COOK JAMES M

IPC: F41H11/02 ,  F41F3/073 ,  F41H5/007 ,  F42B10/66 ,  F42B15/01 ,  F42B15/10

CPC classification number: F41H11/02 ,  F41F3/073 ,  F42B10/661 ,  F42B15/01 ,  F42B15/10

Abstract: A method of defeating an incoming missile (120), such as a rocket propelled grenade, includes soft launching an interceptor missile (10), and then using pitch over motors of the interceptor missile to alter course of the missile to a desired interception direction. By launching at a relatively slow speed, such as a speed less than or equal to 40 m/sec (130 ft/sec), the interceptor missile may reach the desired interception direction within 250 milliseconds of launch. The interceptor missile may be able to cover substantially all interception directions over a hemisphere or greater extent around a launch location. For example, the interceptor missile may be launched vertically from a ground vehicle, and be capable of altering course to any above-ground trajectory within 250 milliseconds.

Abstract translation: 一种击败诸如火箭推进式榴弹的输入导弹（120）的方法包括软式发射拦截导弹（10），然后使用拦截导弹的发动机上的俯仰来改变导弹的航向至期望的拦截方向。 通过以相对较低的速度启动，例如小于或等于40米/秒（130英尺/秒）的速度，拦截导弹可以在发射250毫秒内达到期望的拦截方向。 拦截导弹可能能够覆盖围绕发射位置的半球或更大范围内的基本上所有拦截方向。 例如，拦截导弹可以从地面车辆垂直发射，并且能够在250毫秒内改变航向到任何地面轨迹。