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11. 发明申请

WO2022039656A1 SPRING ARRANGEMENT FOR COUNTERMEASURE MAGAZINES 审中-公开
公开(公告)号：WO2022039656A1
公开(公告)日：2022-02-24
申请号：PCT/SE2021/050805
申请日：2021-08-18
申请人： SAAB AB
发明人： SUNDBERG, Richard
IPC分类号： F41A9/61 , F41A9/00 , F41F1/00 , F41F3/04 , B64D1/00 , F41H11/02 , F42B39/00
摘要： The present invention relates to a spring arrangement (1) for use in a countermeasure magazine (4), said spring arrangement (1) comprising a plurality of elements (10, 20), wherein each one of said elements (10, 20) has a base portion (11, 21) and a plurality of spring portions (13, 23) extending from a first edge (15, 25) of said base portion (11, 21), and wherein said spring portions (13, 23) of each element (10, 20) are distributed along a length of said base portion (11, 21), and wherein said elements (10, 20) comprise mating connection means (17, 27) such that said elements (10, 20) may be connected to each other.

12. 发明申请

WO2016188869A1 DEVICE FOR LAUNCHING HAND GRENADES 审中-公开
标题翻译：启动手段的设备
公开(公告)号：WO2016188869A1
公开(公告)日：2016-12-01
申请号：PCT/EP2016/061336
申请日：2016-05-19
申请人： MYHRE, Tito Waage
发明人： ROSSI, Osvaldo Carlo
IPC分类号： F41F1/00 , F41B11/62 , F42B27/00
CPC分类号： F41F1/00 , F41B11/62 , F42B27/00
摘要： Device for launching hand bombs (10) carried by a gripping and retaining member (11) mounted on a substantially cylindrical stick (20), comprising a tubular body (30) carrying at one end an enlarged head (34), suitable for housing, respectively, said cylindrical stick (20) and said gripping member (11) with the bomb (10), and a cap (35) apt to close said enlarged head (34); a compressed air tank (36), being fixed at the other end of said tubular body (30), whose discharge can be controlled by means of a handle (41) with trigger (45) made integral with said tubular body (30).
摘要翻译：用于发射由安装在基本上圆柱形的棒（20）上的夹持和保持构件（11）承载的手炸弹（10）的装置，包括：管状体（30），其在一端承载适于外壳的扩大头部（34）所述圆柱形棒（20）和具有所述炸弹（10）的所述夹持构件（11）和容纳所述扩大头部（34）的盖子（35）; 固定在所述管状体（30）的另一端的压缩空气罐（36），其排出能够通过具有与所述管状体（30）成一体的扳机（45）的手柄（41）来控制。

13. 发明申请

WO2016160308A1 LIGHTWEIGHT COMPOSITE MORTAR TUBE 审中-公开
标题翻译：轻质复合材料MORTAR TUBE
公开(公告)号：WO2016160308A1
公开(公告)日：2016-10-06
申请号：PCT/US2016/021964
申请日：2016-03-11
申请人： PROOF RESEARCH, INC. , LINCOLN, Jason, E. , CURLISS, David, B.
发明人： LINCOLN, Jason, E. , CURLISS, David, B.
IPC分类号： F41F1/00 , F41F1/06
CPC分类号： F41F1/06 , F41A21/02
摘要： A composite barrel assembly for a gun, such as a muzzle-loading mortar for fin- stabilized projectiles. The composite construction of the barrel has a plurality of generally concentric layers built-up around a rigid supporting liner which may be fabricated from any of several metal or ceramic compositions. An inner thermal barrier coating of inorganic glass, metal refractory alloy, chromium alloy, functionally graded material or ceramic is disposed within the liner. An overwrap layer of continuous fibers embedded in a matrix surrounds the liner. The matrix is either a resin, polymer, ceramic, glass or metal. An outer shell of continuous fibers embedded in a high temperature polymer matrix surrounds the overwrap. When the liner is made from a metal-based composition, an outer thermal barrier coating may be applied in between the liner and the overwrap.
摘要翻译：用于枪的复合筒组件，例如用于翅片稳定的射弹的枪口装载砂浆。桶的复合结构具有多个大致同心的层，其围绕刚性支撑衬里构成，其可以由几种金属或陶瓷组合物中的任何一种制成。无机玻璃，金属耐火合金，铬合金，功能梯度材料或陶瓷的内部热障涂层设置在衬里内。嵌入基体中的连续纤维的外包裹层围绕衬垫。基质是树脂，聚合物，陶瓷，玻璃或金属。嵌入高温聚合物基质中的连续纤维的外壳围绕外包裹物。当衬垫由金属基组合物制成时，可以在衬垫和外包裹层之间施加外部热障涂层。

14. 发明申请

WO2013180579A1 LINE DELIVERY APPARATUS 审中-公开
公开(公告)号：WO2013180579A1
公开(公告)日：2013-12-05
申请号：PCT/NZ2013/000090
申请日：2013-05-30
申请人： LINE LAUNCHER HOLDINGS LIMITED
发明人： HIGHAM, Anthony John , SCHOLZ, Kurt Laurence
IPC分类号： B63C9/26 , F41F1/00 , F42B12/68 , F41B1/00 , F41B11/00
CPC分类号： F42B12/68 , B63C9/26 , F41B11/62 , F41B11/723
摘要： A line launcher (110) capable of firing a projectile (117) and an attached line (125) up to about 70 metres. It has a barrel (113) large enough for a resilient projectile attached to a line. It has a pre-charge chamber capable of storing a pressurised gas from a pressurised gas cartridge. A trigger mechanism vents the gases in this pre-charge chamber into the barrel to expel the projectile and line. Gas from the pressurised gas cartridge (e.g. a CO 2 bulb) is released slowly enough to pressurise the pre-charge chamber but without the cartridge freezing as might occur if the gas was discharged directly from the cartridge into the barrel to directly propel the projectile.
摘要翻译：能够射击射弹（117）和直到约70米的连接线（125）的线发射器（110）。它具有足够大的桶（113），用于连接到线上的弹性弹丸。它具有能够存储来自加压气体盒的加压气体的预充电室。触发机构将该预充气室内的气体排入筒体以排出射弹和管线。来自加压气体筒（例如CO 2球泡）的气体被缓慢释放以对预充气室加压，但是如果气体直接从筒排出到筒中以直接推进射弹，则可能会发生冷冻。

15. 发明申请

WO2006124392A3 PAINTBALL SYSTEM 审中-公开
标题翻译：彩绘系统
公开(公告)号：WO2006124392A3
公开(公告)日：2009-04-30
申请号：PCT/US2006017857
申请日：2006-05-09
申请人： HALL DAVID L
发明人： HALL DAVID L
IPC分类号： F41B11/00 , F41F1/00
CPC分类号： F41B11/57 , F41B11/50 , F41B11/73
摘要： A paintball system may include a marker and delivery system configured to deliver paintballs to the marker. The delivery system may include a conduit and a gas supply. The gas supply may be configured to provide gas flow to the conduit, which may propel paintballs in the conduit to the marker. The gas supply may be configured to dynamically alter the gas flow to the conduit. The delivery system may include a first seal sized and configured to form a seal with at least one of the paintballs in the conduit.
摘要翻译：彩弹系统可以包括被配置成将彩弹弹送到标记的标记和输送系统。输送系统可以包括导管和气体供应。气体供应可以被配置为向导管提供气流，这可以将导管中的彩弹球推进到标记。气体供应可以被配置为动态地改变到管道的气流。输送系统可以包括尺寸和构造成与导管中的至少一个彩弹球形成密封的第一密封件。

16. 发明申请

WO2004099551B1 METHOD AND APPARATUS FOR PENETRATING SUBSURFACE FORMATIONS 审中-公开
标题翻译：用于沉积表面形态的方法和装置
公开(公告)号：WO2004099551B1
公开(公告)日：2005-09-29
申请号：PCT/US2004013295
申请日：2004-04-29
申请人： NACKERUD ALAN L
发明人： NACKERUD ALAN L
IPC分类号： E21B43/116 , E21B43/118 , F41A1/10 , F41F1/00
CPC分类号： F41A1/10 , E21B43/116 , E21B43/118 , F41F1/00
摘要： A method and apparatus (9, 53) for driving at least one explosive driven projectile (11, 58) into an open hole (H) or well bore (B) of a subterranean formation for the purpose of stimulating productive formation. The apparatus is capable of pivoting within the open hole or well bore for desired firing at an angle and is also capable of deep penetration into a subterranean formation. The apparatus may also be conveyed by a tubing (51) in horizontal drilling applications.
摘要翻译：用于将至少一个爆炸性驱动的射弹（11,58）驱动到地下地层的开孔（H）或井眼（B）中以便刺激生产性地层的方法和装置（9,53）。该装置能够在露天孔或井眼内以一定角度进行所需的发射，并且还能够深入到地层中。该装置还可以在水平钻井应用中由管道（51）传送。

17. 发明申请

WO03031296A3 METHOD AND APPARATUS FOR THE RECOVERY OF BODIES TOWED FROM MOVING VEHICLES 审中-公开
标题翻译：从移动车辆回收车体的方法和设备
公开(公告)号：WO03031296A3
公开(公告)日：2003-10-16
申请号：PCT/US0232501
申请日：2002-10-10
申请人： BAE SYSTEMS INFORMATION
发明人： CARLSON MARK A , JORDAN JAMES J , RUSSOTTI JOHN
IPC分类号： B64D3/02 , F41J2/00 , F41J9/10 , G01S7/02 , H01Q1/30 , F41F1/00
CPC分类号： F41J2/00 , B64D3/02 , F41J9/10 , G01S7/021 , H01Q1/30
摘要： Recovery of a towed body, in one embodiment in the form of a decoy which is initially stowed in a receptacle or canister and which is allowed to pay out behind an aircraft on a towing cable wrapped around a spindle, is accomplished by snaring or lassoing a portion of the towing cable and by dragging it to a further spindle which is driven so as to cause the lasso and a portion of the towing cable to wind up around the driven spindle. When a sufficient amount of the cable is wound around the driven spindle, the cable end secured to the canister is severed to allow all of the rest of the towing cable to be wound up. In one embodiment, a telescoping saddle or docking cradle is provided which extends from the canister to receive the retracted towed body so that it may be secured to the moving vehicle from whence it can be recovered, refurbished, and redeployed.
摘要翻译：在一个实施例中，被拖曳的物体以最初装载在容器或罐中并且被允许在围绕心轴缠绕的牵引缆线上的飞机后面放出的诱饵形式的回收，通过捕捉或套住牵引缆线的一部分并且通过拖拽到另一主轴上，该主轴被驱动以便使套索和一部分牵引缆线围绕从动主轴缠绕。当足够数量的电缆缠绕在从动主轴上时，固定到罐上的电缆端被切断，以允许所有其余的牵引电缆被卷起。在一个实施例中，提供伸缩鞍座或对接摇架，其从罐延伸以接收缩回的拖曳主体，使得其可被固定到移动车辆，从其可被回收，翻新和重新部署。

18. 发明申请

WO02046682A1 ROCKET LAUNCHER SYSTEM AND METHOD FOR CONTROLLING A ROCKET LAUNCHER SYSTEM 审中-公开
标题翻译： ROCKET LAUNCHER系统及其控制方法
公开(公告)号：WO02046682A1
公开(公告)日：2002-06-13
申请号：PCT/SE2001/002709
申请日：2001-12-07
IPC分类号： B63G1/00 , F41A9/10 , F41A21/20 , F41F3/04 , F42B15/00 , F41F1/00
CPC分类号： F41A23/20 , F41A9/10 , F41A21/20 , F41F3/04 , F42B15/00
摘要： The present invention relates to a rocket launcher system and a method for controlling a rocket launcher system. The rocket launcher system (1) is placed below deck (100) on a ship to improve the ship's stealth capability and comprises a launcher (11, 15), a charger (12, 15) and a magazine (13) containing one or more different types of rocket missiles (3). The method for controlling the rocket launcher system (1) comprises transferring of an operating signal (6), comprising preparation data, to the rocket launcher system from one or more operators (2; 21, 22, 23, 24, 25). The preparation data is transferred to a rocket missile (3) and charge (12) is caused to fetch the rocket missile form a magazine (13) and charge a launcher (11). A hatch (101) in the ship's deck (100) is opened, and the launcher is caused to sight the rocket missile (3) at a target area (4).
摘要翻译：本发明涉及一种火箭发射系统和一种控制火箭发射系统的方法。火箭发射器系统（1）被放置在船上的甲板（100）下方以提高船舶的隐身能力，并且包括发射器（11,15），充电器（12,15）和包含一个或多个不同类型的火箭弹（3）。用于控制火箭发射器系统（1）的方法包括从一个或多个操作者（2; 21,22,23,24,25）将包括准备数据的操作信号（6）传送到火箭发射器系统。准备数据被转移到火箭弹（3），并且（12）由一个杂志（13）取出火箭导弹，并向发射器（11）充电。打开船甲板（100）的舱口（101），使发射器在目标区域（4）上看到火箭弹（3）。

19. 发明申请

WO01086224A1 ATTACK AIRCRAFT 审中-公开
标题翻译：攻击飞机
公开(公告)号：WO01086224A1
公开(公告)日：2001-11-15
申请号：PCT/AU2001/000511
申请日：2001-05-04
IPC分类号： F41F1/00 , B64D1/04 , B64D7/00 , B64D7/04 , B64D7/08 , F41A1/00 , F42B5/03
CPC分类号： B64D7/08 , B64D1/04 , B64D7/04 , F42B5/035
摘要： Aircraft (10) carries at least two clusters of barrel assemblies. At least one cluster is oriented normal to the longitudinal axis of aircraft (10) and at least one other cluster is oriented parallel to the longitudinal axis of aircraft (10). Each cluster comprises a plurality of barrel assemblies, with each barrel having a plurality of axially disposed projectiles therein. Each projectile is associated with a discrete, sequentially activated propellant charge for propelling it through the muzzle of the barrel. Various methods of deploying a multiplicity of projectiles onto a target from aircraft (10) are also described and claimed. The projectiles deployment might occur at any time whils aircraft (10) is approaching the target, overflying the target, or departing from the target. The projectiles may include smoke canisters, high explosive canisters, flares, electronic and thermal countermeasures, mines, grenades or cameras.
摘要翻译：飞机（10）携带至少两组筒组件。至少一个群集平行于飞机（10）的纵向轴线定向，并且至少一个其他群集平行于飞行器（10）的纵向轴线定向。每个簇包括多个筒组件，每个筒在其中具有多个轴向设置的抛射体。每个抛射体与不连续的，依次激活的推进剂装药相关联，以将其推进通过枪管的枪口。还描述和要求保护从飞机（10）将多个弹体部署到目标上的各种方法。飞机部署可能随时飞行（10）接近目标，飞越目标，或离开目标。射弹可能包括烟筒，高爆炸罐，火炬，电子和热对策，矿山，手榴弹或照相机。

20. 发明申请

WO99029567A1 WATER RESCUE DEVICE 审中-公开
标题翻译：水回收装置
公开(公告)号：WO99029567A1
公开(公告)日：1999-06-17
申请号：PCT/US1998/026036
申请日：1998-12-08
IPC分类号： B63C9/26 , F41B7/00 , F41F1/00
CPC分类号： F41B7/003 , B63C9/26
摘要： A water rescue device (10) is provided which includes a spring loaded firearm (12). The firearm (12) includes a barrel (20), a shoulder stock (22) and trigger (24). Situated within the barrel is a spring (40). An aerodynamic floatation device (14) is adapted to be releasably secured to one end of the spring (40). A supply of safety line (16) has one end secured to the spring loaded firearm (12) and a second end secured to the floatation device (14). The spring (40) is adapted to be releasably locked in an extended position so that when the trigger (24) is depressed, the restoring forces of the spring (40) cause the floatation device (14) to be propelled into the air carrying the supply line (16) therewith.
摘要翻译：提供了一种水救援装置（10），其包括弹簧加载的枪支（12）。火器（12）包括枪管（20），肩架（22）和扳机（24）。在桶内是弹簧（40）。空气动力学漂浮装置（14）适于可释放地固定到弹簧（40）的一端。安全线（16）的供应具有固定到弹簧加载的枪支（12）的一端和固定到浮动装置（14）的第二端。弹簧（40）适于可释放地锁定在延伸位置，使得当触发器（24）被压下时，弹簧（40）的恢复力使得浮动装置（14）被推入到承载供应管线（16）。

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