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1. 发明申请

WO2010113171A1 A MOBILE MISSILE LAUNCH SYSTEM AND METHOD THEREOF 审中-公开
标题翻译：一种移动式MISSILE发射系统及其方法
公开(公告)号：WO2010113171A1
公开(公告)日：2010-10-07
申请号：PCT/IN2010/000018
申请日：2010-01-11
申请人： DIRECTOR GENERAL, DEFENCE RESEARCH & DEVELOPMENT ORGANISATION , GURUPRASAD, Siddalingappa , KATTI, Shreedhar, Aravind , GOUD, Alasani Prasad , WAGHMARE, Vikas, Narayan , KUMAR, Sanjay , GUPTA, Atul , KHIRE, Ravindra, Sudhakar , SANTOSH, Tushar, Kant , GAUTAM, Bimal , RAM, Paras
发明人： GURUPRASAD, Siddalingappa , KATTI, Shreedhar, Aravind , GOUD, Alasani Prasad , WAGHMARE, Vikas, Narayan , KUMAR, Sanjay , GUPTA, Atul , KHIRE, Ravindra, Sudhakar , SANTOSH, Tushar, Kant , GAUTAM, Bimal , RAM, Paras
IPC分类号： F41A23/34 , F41A23/36 , F41A23/42 , F41F3/04 , F41F3/052 , F42B39/22
CPC分类号： F41A23/42 , F41A23/34 , F41A23/36 , F41F3/04 , F41F3/042 , F41F3/052 , F42B39/22
摘要： The present invention relates to launching system, more particularly relates to mobile launching system for missiles. The mobile missile launch system comprising a vehicle (14) having a chassis structure adapted to carry the launch system; a mounting frame (16) comprising predetermined truss framework mounted onto the chassis structure; plurality of sliding mechanisms mounted at rear end of the mounting frame (16); plurality of canisters (43) mounted onto said beam (22) and plurality of missiles (11) ensconced within the canisters (43); plurality of containers (42) enclosing said canisters (43) and are connected to the saddles (32, 34) for linear movement; plurality of resting units (27) abutting to rear end of the canisters (43) and are adapted to move linearly to transfer reaction forces from said missiles (11) to ground.
摘要翻译：本发明涉及发射系统，更具体地涉及用于导弹的移动发射系统。该移动导弹发射系统包括具有适于承载发射系统的底盘结构的车辆（14）; 安装框架（16），其包括安装在所述底盘结构上的预定桁架框架; 安装在安装框架（16）后端的多个滑动机构; 安装在所述梁（22）上的多个罐（43）和固定在罐（43）内的多个导弹（11）; 多个容纳所述罐（43）的容器（42）并且连接到所述鞍座（32,34）以用于线性运动; 多个静止单元（27）邻接于罐（43）的后端并且适于线性移动以将反作用力从所述导弹（11）传递到地面。

2. 发明申请

WO2010128997A3 DEFORMABLE MODULAR ARMORED COMBAT SYSTEM 审中-公开
标题翻译：可变模块化装甲系统
公开(公告)号：WO2010128997A3
公开(公告)日：2011-01-06
申请号：PCT/US2009069122
申请日：2009-12-22
申请人： HALLIDAY WACHS LLC , HALLIDAY DONALD R
发明人： HALLIDAY DONALD R
IPC分类号： F41H7/03
CPC分类号： F41H7/048 , B62D63/025 , F41A23/34 , F41A23/42 , F41H7/042 , F41H7/044
摘要： A modular, wheeled vehicle suitable for military use, includes a driver module having a width for seating one person and having length for seating a second (and optional third) person therebehind, and an engine module disposed behind the driver module containing an engine for powering the modular vehicle. The engine module has a rear surface adapted to receive a storage module. The driver module and the engine module form a central element having a pair of sides, a bottom, and a top. The central element is adapted to receive the modules on both of the central element sides. The central element has air inlet for personnel and for the engine disposed atop the central element. The bottom of the central element and troop side pods generally are V-shaped with slanted, upward extending sides. An energy attention system may be disposed between chassis and occupants to lessen negative blast acceleration affects.
摘要翻译：一种适用于军事用途的模块式轮式车辆，包括具有用于安置一个人的宽度的驾驶员模块，并且具有用于在其上安放第二（和可选择的第三）人的长度，以及设置在驾驶员模块后面的发动机模块，该发动机模块包含用于供电的发动机模块化车辆。发动机模块具有适于接收存储模块的后表面。驾驶员模块和发动机模块形成具有一对侧面，底部和顶部的中心元件。中心元件适于在两个中心元件侧接收模块。中心元件具有用于人员的空气入口和位于中心元件顶部的发动机。中央部件和部队侧荚的底部通常为V形，具有倾斜的向上延伸的侧面。能量注意系统可以设置在底盘和乘员之间，以减少负冲击加速影响。

3. 发明申请

WO1994017357A1 ANTI-AIRCRAFT TURRET DEVICE 审中-公开
标题翻译：反飞机装置
公开(公告)号：WO1994017357A1
公开(公告)日：1994-08-04
申请号：PCT/NO1994000025
申请日：1994-01-27
申请人： KVÆRNER EUREKA A.S , ASPEHAUG, Nils
发明人： KVÆRNER EUREKA A.S
IPC分类号： F41A09/45
CPC分类号： F41A23/42
摘要： In an anti-aircraft turret (2) for armoured units, especially for armoured vehicles (1), the turret (2) constitutes an independent unit and is equipped with a launching ramp (3), e.g. for rockets. The launching ramp (3) is designed as an integral part of the turret (2) and is rotatable in the vertical direction from a launching position (5), via a neutral transport position to a loading position (6) where the ramp (3) projects down through a loading hatch (9) in the unit (1) down into the turret (2). The ramp (3) is equipped with an armoured protective mantle (8), which is rotatable with the ramp (3) and which covers the ramp (3) on the top and on the sides.
摘要翻译：在用于装甲车辆的防空炮塔（2）中，特别是装甲车辆（1），炮塔（2）构成一个独立的装置，并配备有发射坡道（3），例如火箭弹发射斜坡（3）被设计为转台（2）的组成部分，并且可以在垂直方向上从发射位置（5）经由中性运输位置旋转到加载位置（6），其中斜坡（3））通过装置（1）中的装载舱（9）向下投影到炮塔（2）中。斜坡（3）装备有可以与斜面（3）一起旋转并且覆盖顶部和侧面上的坡道（3）的装甲保护罩（8）。

4. 发明申请

WO02103276A3 MULTI-PURPOSE MISSILE LAUNCHER SYSTEM FOR A MILITARY LAND VEHICLE 审中-公开
标题翻译：多用途陆地车辆多用途发射系统
公开(公告)号：WO02103276A3
公开(公告)日：2003-05-08
申请号：PCT/US0209242
申请日：2002-03-25
申请人： UNITED DEFENSE LP
发明人： BOUDREAU DAVID R , BOVEE STAN , MATTESON PHILIP , GAEDKE BRUCE , BORGWARTH DENNIS
IPC分类号： F41A23/42 , F41F3/04
CPC分类号： F41A23/42
摘要： A multi-purpose missile launcher system 10 for a military land vehicle 12 that has the capability for direct targeting both short and medium range land targets, as well launching missiles against longer-range land targets or air targets using indirect targeting. The multi-purpose missile launcher system is deployed as part of a modular weapon system that mates with a modular bed of the military land vehicle 12.
摘要翻译：一种用于军用陆地车辆12的多用途导弹发射系统10，具有直接瞄准中短程陆地目标的能力，以及使用间接瞄准对较长距离的地面目标或空中目标发射导弹。多用途导弹发射系统被部署为与军用陆地车辆12的模块化床相配合的模块化武器系统的一部分。

5. 发明申请

WO99017989A1 SYSTEM FOR UPENDING/RECLINING LAUNCH VEHICLES 审中-公开
标题翻译：装备/拆卸启动车辆的系统
公开(公告)号：WO99017989A1
公开(公告)日：1999-04-15
申请号：PCT/US1998/015899
申请日：1998-07-27
IPC分类号： B64G1/00 , B64G5/00 , F41A23/42 , F41F3/04
CPC分类号： B64G5/00 , B64G1/002 , F41A23/42 , F41F3/04
摘要： An improved system is disclosed for upending/reclining a launch vehicle (60). In one embodiment, first and second trunnion supports (20a, 20b) may be positioned on opposing sides of a u-shaped opening (14) provided at the rearward end (16) of a mobile support platform (10). A launch vehicle (60) may be pivotally supported via trunnions received by the first and second trunnion supports (20a, 20b) for pivotal movement between a reclined position on top of the support platform to an upended position. In the upended position the launch vehicle (60) will extend through the u-shaped opening (14). A bridge assembly (40) may be selectively interconnected to the launch vehicle (60) to facilitate handling, transport and storage therewith.
摘要翻译：公开了一种用于升高/倾斜运载火箭（60）的改进的系统。在一个实施例中，第一和第二耳轴支撑件（20a，20b）可以定位在设置在移动支撑平台（10）的后端（16）处的u形开口（14）的相对侧上。运载火箭（60）可以通过由第一和第二耳轴支撑件（20a，20b）接收的耳轴枢转地支撑，以便在支撑平台的顶部上的倾斜位置到支撑平台之间枢转运动。运载火箭（60）在朝向的位置延伸穿过U形开口（14）。桥组件（40）可以选择性地互连到运载火箭（60），以便于其处理，运输和存储。

6. 发明申请

WO2019083395A2 САМОХОДНАЯ ОГНЕВАЯ УСТАНОВКА 审中-公开
公开(公告)号：WO2019083395A2
公开(公告)日：2019-05-02
申请号：PCT/RU2017/000973
申请日：2017-12-26
申请人： АКЦИОНЕРНОЕ ОБЩЕСТВО "КОНЦЕРН ВОЗДУШНО-КОСМИЧЕСКОЙ ОБОРОНЫ "АЛМАЗ - АНТЕЙ" , АКЦИОНЕРНОЕ ОБЩЕСТВО "УЛЬЯНОВСКИЙ МЕХАНИЧЕСКИЙ ЗАВОД"
发明人： САВИНОВ, Андрей Леонидович , БАСАЛОВ, Станислав Алексеевич , ЛАПИН, Вячеслав Викторович , ВОРОНЦОВ, Владимир Алексеевич , КУЗНЕЦОВ, Вячеслав Петрович , ГОРНОСТАЕВ, Владимир Михайлович , БЕЛЫЙ, Юрий Иванович , ФЁДОРОВ, Станислав Владимирович , МОНИН АЛЕКСАНДР ЕВГЕНЬЕВИЧ , ВАСИЛЬЕВ, Анатолий Фёдорович , ЛАРИОНОВ, Юрий Петрович , ШАРОВ, Владимир Сергеевич , МАКЕЕВ, Анатолий Васильевич
CPC分类号： F41A23/42 , F41G7/224 , F41H11/02
摘要： Полезная модель относится к области военной техники и может быть использована в составе зенитных ракетных комплексов средней дальности в качестве основного боевого средства. Самоходная огневая установка содержит расположенные на самоходном шасси пусковое устройство с комплектом зенитных управляемых ракет, электрогидравлический следящий привод, радиолокационную станцию, цифровую вычислительную систему, систему телекодовой связи, оптико-электронную систему с приводом наведения, блок пассивный. Полезная модель обеспечивает своевременное выключение передатчика РЛС и обзор пространства оптическим объективом оптико- электронной системы по «спирали» при обнаружении цели в пассивном режиме в режиме внешнего целеуказания. Техническим результатом является обеспечение скрытности самоходной огневой установки (СОУ) при целеуказании от внешнего командного пункта (КП).

7. 发明申请

WO2006091240A3 INFANTRY COMBAT WEAPONS SYSTEM 审中-公开
标题翻译：无限制武器系统
公开(公告)号：WO2006091240A3
公开(公告)日：2007-02-01
申请号：PCT/US2005035535
申请日：2005-09-30
申请人： CHAMPION EDWIN J
发明人： CHAMPION EDWIN J
IPC分类号： F41G9/00
CPC分类号： F41A23/42 , F41A3/38 , F41A3/54 , F41A5/14 , F41A5/18 , F41A5/34 , F41A19/14 , F41A21/12 , F41A21/36 , F41A21/48 , F41A25/12 , F42B12/62 , F42B12/64
摘要： There is presented a system for infantry combat that combines weapons, transportation, and logistical approaches to deploy a highly mobile and agile infantry-based army to effectively operate in open-field or urban warfare environments against threats ranging from individual militants to heavy armor and aircraft. Among components of the infantry combat weapons system are a large-caliber recoil-mitigated battle rifle; an automatic grenade launcher and grenade system; a personal carrier transport to convey and deploy ammunition, equipment and weapons; an improved tactical missile capable of defeating new-generation armored vehicles and aircraft; an integrated targeting and reconnaissance drone; and a jet-assisted rotary wing air vehicle.
摘要翻译：提出了一种步兵作战系统，结合了武器，运输和后勤方法，部署高度流动和敏捷的步兵部队，以有效地在野外或城市战争环境中进行作战，以应对个人武装分子到重型装甲和飞机的威胁。步兵作战武器系统的组成部分是大口径反冲式步枪; 自动榴弹发射器和手榴弹系统; 传送和部署弹药，设备和武器的个人运输工具; 一种能够击败新一代装甲车和飞机的改进的战术导弹; 综合瞄准和侦察无人机; 和喷气辅助旋翼飞行器。

8. 发明申请

WO2005001372A3 MULTIPLE TUBE PNEUMATIC LAUNCHER 审中-公开
标题翻译：多管气动推杆
公开(公告)号：WO2005001372A3
公开(公告)日：2005-08-11
申请号：PCT/US2004009427
申请日：2004-03-29
申请人： AAI CORP , MILLER STEPHEN W , FOX STEVEN J , FEILD DAVID M , BAUERNSCHUB RICHARD A , METTEE JUSTIN A
发明人： MILLER STEPHEN W , FOX STEVEN J , FEILD DAVID M , BAUERNSCHUB RICHARD A , METTEE JUSTIN A
IPC分类号： F41F20060101 , F41F3/042
CPC分类号： F41A23/42 , F41B11/00 , F41B11/62 , F41F3/042
摘要： A launcher includes a plurality of launch tubes (110) for stowing and launching a plurality of air vehicles. A central air manifold (310) is operatively connected to an air storage tank (150); a first launch tube air manifold (320) is operatively connected to a first group of the launch tubes (110) and operatively connected to the central air manifold (310). The first launch air manifold (320) has a separate port corresponding to each launch tube (110) of the first group of launch tubes. A release valve mechanism (360) is removably mounted in one of the ports (355) of the first launch tube air manifold (320), the release valve mechanism (360) controlling the passage of launch air between the first launch tube air manifold (320) and the launch tube corresponding to the port (355) in which the release valve mechanism (360) is mounted. A plug (350) is removably mounted in each of the ports (355) not occupied by the release valve mechanism (360).
摘要翻译：发射器包括多个用于收起和发射多个空中飞行器的发射管（110）。中央空气歧管（310）可操作地连接到空气存储罐（150）; 第一发射管空气歧管（320）可操作地连接到第一组发射管（110）并可操作地连接到中央空气歧管（310）。第一发射空气歧管（320）具有对应于第一组发射管的每个发射管（110）的单独端口。释放阀机构（360）可移除地安装在第一发射管空气歧管（320）的一个端口（355）中，释放阀机构（360）控制发射空气在第一发射管空气歧管（ 320）和对应于其中安装有释放阀机构（360）的端口（355）的发射管。插塞（350）可移除地安装在不被释放阀机构（360）占据的每个端口（355）中。

9. 发明申请

WO2010128997A2 DEFORMABLE MODULAR ARMORED COMBAT SYSTEM 审中-公开
标题翻译：可变模块化装甲系统
公开(公告)号：WO2010128997A2
公开(公告)日：2010-11-11
申请号：PCT/US2009/069122
申请日：2009-12-22
申请人： HALLIDAY WACHS, LLC , HALLIDAY, Donald, R.
发明人： HALLIDAY, Donald, R.
IPC分类号： B60K5/00
CPC分类号： F41H7/048 , B62D63/025 , F41A23/34 , F41A23/42 , F41H7/042 , F41H7/044
摘要： A modular, wheeled vehicle suitable for military use, includes a driver module having a width for seating one person and having length for seating a second (and optional third) person therebehind, and an engine module disposed behind the driver module containing an engine for powering the modular vehicle. The engine module has a rear surface adapted to receive a storage module. The driver module and the engine module form a central element having a pair of sides, a bottom, and a top. The central element is adapted to receive the modules on both of the central element sides. The central element has air inlet for personnel and for the engine disposed atop the central element. The bottom of the central element and troop side pods generally are V-shaped with slanted, upward extending sides. An energy attention system may be disposed between chassis and occupants to lessen negative blast acceleration affects.
摘要翻译：一种适用于军事用途的模块式轮式车辆，包括具有用于安置一个人的宽度的驾驶员模块，并且具有用于在其上安放第二（和可选择的第三）人的长度，以及设置在驾驶员模块后面的发动机模块，该发动机模块包含用于供电的发动机模块化车辆。发动机模块具有适于接收存储模块的后表面。驾驶员模块和发动机模块形成具有一对侧面，底部和顶部的中心元件。中心元件适于在两个中心元件侧接收模块。中心元件具有用于人员的空气入口和位于中心元件顶部的发动机。中央部件和部队侧荚的底部通常为V形，具有倾斜的向上延伸的侧面。能量注意系统可以设置在底盘和乘员之间，以减少负冲击加速影响。

10. 发明申请

WO2006091240A2 INFANTRY COMBAT WEAPONS SYSTEM 审中-公开
标题翻译：无限制武器系统
公开(公告)号：WO2006091240A2
公开(公告)日：2006-08-31
申请号：PCT/US2005/035535
申请日：2005-09-30
申请人： CHAMPION, Edwin, J.
发明人： CHAMPION, Edwin, J.
IPC分类号： F41G3/26
CPC分类号： F41A23/42 , F41A3/38 , F41A3/54 , F41A5/14 , F41A5/18 , F41A5/34 , F41A19/14 , F41A21/12 , F41A21/36 , F41A21/48 , F41A25/12 , F42B12/62 , F42B12/64
摘要： There is presented a system for infantry combat that combines weapons, transportation, and logistical approaches to deploy a highly mobile and agile infantry-based army to effectively operate in open-field or urban warfare environments against threats ranging from individual militants to heavy armor and aircraft. Among components of the infantry combat weapons system are a large-caliber recoil-mitigated battle rifle; an automatic grenade launcher and grenade system; a personal carrier transport to convey and deploy ammunition, equipment and weapons; an improved tactical missile capable of defeating new-generation armored vehicles and aircraft; an integrated targeting and reconnaissance drone; and a jet-assisted rotary wing air vehicle.
摘要翻译：提出了一种步兵作战系统，结合了武器，运输和后勤方法，部署高度流动和敏捷的步兵部队，以有效地在野外或城市战争环境中开展行动，以应对个人武装分子到重型装甲和飞机的威胁。步兵作战武器系统的组成部分是大口径反冲式步枪; 自动榴弹发射器和手榴弹系统; 传送和部署弹药，设备和武器的个人运输工具; 一种能够击败新一代装甲车和飞机的改进的战术导弹; 综合瞄准和侦察无人机; 和喷气辅助旋翼飞行器。

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