公开(公告)号：US20030131748A1

公开(公告)日：2003-07-17

申请号：US10047410

申请日：2002-01-16

Applicant: Lockheed Martin Corporation

Inventor： Scott Van Weelden ,  Steve Ericson

IPC: F42B001/00 ,  F42C001/00

CPC classification number: F42B39/22 ,  F42B12/58

Abstract: The invention entails apparatus for mounting a payload, such as a warhead, to bulkheads carried by munitions. The apparatus comprises fore and aft bulkheads depending from the munitions, each of the bulkheads having a substantially centrally located opening; bulkhead attaching structure carried by the payload and engaging at least one of the bulkheads, and at least one fastener carried by the bulkhead attaching structure and engaging both the payload and the bulkhead attaching structure. In one embodiment, the bulkhead attaching structure is an annular ring element disposed about and secured to the aft end of said payload. The ring element includes a first annular portion of a first diameter, and a second aft portion of a second diameter, the first diameter of said first portion being smaller than the second diameter to accommodate annular portions of the aft bulkhead. In a second embodiment, the bulkhead attaching structure comprises a step element carried by the payload, which abuts the fore bulkhead. The step element may be integral with the payload or a separate discrete element. In a third embodiment, the bulkhead attaching structure comprises a vertical buttress carried by the aft bulkhead and a tension element for fastening the vertical buttress to the aft end of the payload.

Abstract translation: 本发明涉及将诸如弹头之类的有效载荷安装在弹药携带的舱壁上的装置。 该装置包括取决于弹药的前后舱壁，每个隔板具有基本上位于中心的开口; 由有效载荷承载的舱壁连接结构和与隔板中的至少一个接合，以及由舱壁连接结构承载的至少一个紧固件，并且与有效载荷和舱壁附接结构相啮合。 在一个实施例中，隔板连接结构是围绕并固定到所述有效载荷的后端的环形环元件。 环形元件包括第一直径的第一环形部分和第二直径的第二后部，所述第一部分的第一直径小于第二直径以容纳后舱壁的环形部分。 在第二实施例中，隔板连接结构包括由有效载荷承载的台阶元件，其与前隔板相邻。 步进元件可以与有效载荷或单独的离散元件成一体。 在第三实施例中，隔板附接结构包括由后舱承载的垂直支撑件和用于将垂直支撑件紧固到有效载荷的后端的张紧元件。

公开(公告)号：US20030019386A1

公开(公告)日：2003-01-30

申请号：US09938022

申请日：2001-08-23

Inventor： Richard M. Lloyd ,  Ernest C. Faccini

IPC: F42B012/22 ,  F42B012/32

CPC classification number: F42B12/32 ,  F41H11/02 ,  F42B12/205 ,  F42B12/208 ,  F42B12/58

Abstract: A kinetic energy rod warhead with aligned projectiles includes a projectile core in a hull including a plurality of individual projectiles and an explosive charge in the hull about the core. The individual projectiles are aligned when the explosive charge deploys the projectiles. The projectiles may also be aimed in a specific direction.

公开(公告)号：US6142054A

公开(公告)日：2000-11-07

申请号：US506334

申请日：2000-02-18

Applicant: Peter Ettmuller

Inventor： Peter Ettmuller

IPC: F42B12/62 ,  B65B19/34 ,  F42B12/58 ,  F42B33/02

CPC classification number: F42B12/58 ,  B65B19/34 ,  F42B33/02

Abstract: Device for filling a shell body with a plurality of sub-projectiles including a U-shaped assembly centering device coupled with a cover. A reservoir, formed between the assembly centering device and the cover, includes a slit-like shaped rectangle in cross-section. A flange is fastened in a lower area of the reservoir on the assembly centering device, and a slider for moving with respect to the reservoir includes a width corresponding to a length of the slit-like rectangle. A top portion includes a V-shaped notch extending along a longitudinal direction, and a bottom portion includes a V-shape extending along the longitudinal direction. A perforation, extending coaxially with the slider and provided in the assembly centering device, includes a first part approximately corresponding to an outline of the slider and a second part approximately corresponding to an outer periphery of a layer. A shoulder at an outlet of the perforation is provided for guiding the plurality of sub-projectiles into the shell body element, and a holding ring is fastened on the assembly centering device extending coaxially with the shoulder.

Abstract translation: 用于用多个子弹体填充壳体的装置，包括与盖连接的U形组件定心装置。 在组件定心装置和盖之间形成的储存器包括横截面的狭缝状矩形。 凸缘紧固在组件定心装置上的储存器的下部区域中，并且相对于储存器移动的滑块包括对应于狭缝状矩形的长度的宽度。 顶部包括沿着纵向方向延伸的V形凹口，底部包括沿着纵向延伸的V形。 与滑块同轴地设置并设置在组件定心装置中的穿孔包括大致对应于滑块的​​轮廓的第一部分和大致对应于层的外周的第二部分。 提供穿孔出口处的肩部，用于将多个子弹体引导到壳体元件中，并且保持环紧固在与肩部同轴延伸的组件定心装置上。

公开(公告)号：US5907117A

公开(公告)日：1999-05-25

申请号：US836572

申请日：1997-11-06

Applicant: Per-Olof Persson ,  Lars Paulsson ,  Stig Johnsson

Inventor： Per-Olof Persson ,  Lars Paulsson ,  Stig Johnsson

IPC: F42B10/60 ,  F42B12/58 ,  F42B12/60

CPC classification number: F42B12/58

Abstract: The present invention relates to a method and device for combating identified targets (F) using warheads (2) from a launching vehicle (1) flying over a target area, by separating from this launching vehicle (1) warheads (2) which act independently after separation, and including those targets which lie close to the flight trajectory of the launching vehicle (1) and those which lie well to the side of same flight trajectory. The invention is based on the use of that part of the kinetic energy of the launching vehicle (1) which the warhead (2) takes over from the same when it is separated in order to give the warhead (2) a looping trajectory or any other programmed flight trajectory, which carries it up to a starting height adapted to its active use, which lies considerably above the actual flight trajectory of the launching vehicle (1), and which, if so required, can carry the warhead (2) back to the geographical position where it was separated from the launching vehicle (1). The action of the warhead (2) can then follow guidelines known per se.

Abstract translation: PCT No.PCT / SE95 / 01300 Sec。 371日期：1997年11月6日 102（e）日期1997年11月6日PCT 1995年11月16日PCT公布。 出版物WO96 / 15422 PCT 日期：1996年5月23日本发明涉及一种使用从发射车辆（1）飞越目标区域的弹头（2）通过与该发射车辆（1）弹头（2）分离的来确定目标（F）的方法和装置 ），其分离后独立行动，并且包括靠近发射车辆（1）的飞行轨迹的那些目标和位于相同飞行轨迹侧的那些目标。 本发明基于使用发射车辆（1）的动能的那部分，当弹头（2）分离时，弹头（2）从其起飞从而使弹头（2）成为循环轨迹或任何 其他编程的飞行轨迹，其运载到适合其主动使用的起始高度，其大大高于发射车辆（1）的实际飞行轨迹，并且如果需要，可以将弹头（2）返回 到与发射车辆（1）分离的地理位置。 弹头（2）的作用可以遵循本身已知的指导原则。

公开(公告)号：US5191169A

公开(公告)日：1993-03-02

申请号：US812340

申请日：1991-12-23

Applicant: John B. Hu

Inventor： John B. Hu

IPC: F42B12/14 ,  F42B12/22 ,  F42B12/58

CPC classification number: F42B12/58 ,  F42B12/14 ,  F42B12/22

Abstract: A multiple module EFP warhead comprises a tubular body having a central axis with a plurality of explosively formed penetrator modules arranged tandemly within the body along the axis. Each of the modules includes a curved, dish shaped support disk having a unique forwardly convex curvature. The support disk is focused on the axis at a point behind the module. Each module has a set of circumferentially spaced apertures therethrough, each having a central aperture axis intersecting the central axis. Each aperture supports a separate ductile metal disk therein and an explosive charge behind and against the metal disk. Each of the aperture axes forms an acute angle of inclination with the central axis which is uniquely offset from the axes of the other modules so that each EFP travels along a unique forward path.

Abstract translation: 多模块EFP弹头包括具有中心轴线的管状体，所述中心轴线具有多个爆炸形成的穿透器模块，沿着轴线在身体内串联布置。 每个模块包括具有独特的向前凸曲率的弯曲的盘形支撑盘。 支撑盘聚焦在模块后面的一个轴上。 每个模块具有穿过其中的一组周向间隔开的孔，每个孔具有与中心轴线相交的中心孔径轴。 每个孔在其中支撑单独的延性金属盘，并在金属盘的后面和后面支撑爆炸物。 每个孔径轴线与中心轴线形成锐角，该倾斜角度与其他模块的轴线唯一地偏移，使得每个EFP沿独特的前进路径行进。

公开(公告)号：US4733597A

公开(公告)日：1988-03-29

申请号：US34765

申请日：1987-04-06

Applicant: Theadore E. Upham

Inventor： Theadore E. Upham

IPC: F42B12/58 ,  F41F5/02 ,  B64D1/04

CPC classification number: F42B12/58

Abstract: A sequential launching system is disclosed for sonobuoys and the like in which each of a plurality of sonobuoys is provided with a separate launch mechanism. The launch mechanism comprises a piston and piston chamber at the aft end of the sonobuoy. The cross-sectional area of the piston chamber is substantially smaller than that of the launch tube and air flow passages are provided for allowing ambient air to flow to the aft end of the sonobuoy to equalize the air pressure with that at the forward end. Air passages around the plural sonobuoys are provided by longitudinally extending, radially spaced ribs which extend from the muzzle end to the breech end of the launch tube. The ribs serve to support and guide the sonobuoys in the launch tube.

Abstract translation: 公开了一种用于声波器等的顺序发射系统，其中多个声波发生器中的每一个设置有单独的发射机构。 发射机构包括位于声纳鸟尾端的活塞和活塞室。 活塞室的横截面面积大大小于发射管的横截面面积，并且设置空气流动通道以允许环境空气流到声波探测器的后端，以将空气压力与前端的压力相等。 多个声波周围的空气通道由从枪口端延伸到发射管的后膛端的纵向延伸的径向隔开的肋提供。 肋骨用于支撑和引导发射管中的声波。

公开(公告)号：US4648321A

公开(公告)日：1987-03-10

申请号：US720204

申请日：1985-04-04

Applicant: Kenneth P. Lusk

Inventor： Kenneth P. Lusk

IPC: F42B12/58 ,  F42B15/36 ,  F42B13/32 ,  F42B15/02

CPC classification number: F42B12/58 ,  F42B15/36

Abstract: A missile separation system for fixedly attaching a rocket motor section a payload section has cofunctioning attaching and retarding means integrated to retain plural sections of a missile system in mated relationship until a predetermined point in the missile flight path.

Abstract translation: 用于固定地附接火箭发动机部分和有效载荷部分的导弹分离系统具有集成的联接和延迟装置，其将导弹系统的多个部分保持在配合关系中直到导弹飞行路径中的预定点。

公开(公告)号：US4616567A

公开(公告)日：1986-10-14

申请号：US747565

申请日：1985-06-20

Applicant: Rudolf Romer ,  Karl W. Bethmann ,  Christian Jaeneke ,  Manfred Moll

Inventor： Rudolf Romer ,  Karl W. Bethmann ,  Christian Jaeneke ,  Manfred Moll

IPC: F42B12/58 ,  F42B25/16 ,  F41F5/02 ,  F42B25/06

CPC classification number: F42B12/58

Abstract: A method and apparatus for covering a target area with ammunition, wherein a container, which contains active bodies W arranged on different decks 30.1, 30.2 and which is to be brought over the target area, releases the active bodies W through release openings 34 on its sides to become effective from above on respective individual flight paths against objects, for example armored vehicles, present in the target area.

Abstract translation: 一种用弹药覆盖目标区域的方法和装置，其中包含布置在不同甲板30.1,30.2上并且将被覆盖在目标区域上的活动物体W的容器通过其上的释放开口34释放活性物体W 双方将在相应的个别飞行路线上从对上述目标区域内的物体（例如装甲车辆）开始生效。

公开(公告)号：US4557198A

公开(公告)日：1985-12-10

申请号：US468596

申请日：1983-02-22

Applicant: Dennis J. Hickey

Inventor： Dennis J. Hickey

IPC: F42B12/58 ,  F42B39/20 ,  F42B41/00

CPC classification number: F42B39/20 ,  F42B12/58

Abstract: A carrier shell for secondary projectiles having a shell casing, a plurality of secondary projectiles within the casing, an explosive dispersal charge for dispersing the projectiles and a safety device having a body closing a venting aperature in the casing. A first mechanical connection secures the body to the casing and yields on detonation of the charge before firing to vent any explosion before firing without dispersing the projectiles. A second mechanical connection is moved in response to firing to a condition preventing venting.

Abstract translation: 一种用于二次射弹的载体壳，其具有外壳，壳体内的多个二次射弹，用于分散射弹的爆炸分散装置和具有封闭壳体中的通气孔的主体的安全装置。 第一个机械连接将本体固定在外壳上，并在起火前产生爆炸物的电荷，以便在射出之前排放任何爆炸物，而不会分散射弹。 第二机械连接响应于点火而移动到防止排气的状态。

公开(公告)号：US4480552A

公开(公告)日：1984-11-06

申请号：US422398

申请日：1982-09-24

Applicant: Alfred Eckel ,  Manfred Kastenhuber ,  Erich Bock

Inventor： Alfred Eckel ,  Manfred Kastenhuber ,  Erich Bock

IPC: F42B12/58 ,  F42B25/16 ,  F42B13/50

CPC classification number: F42B12/58

Abstract: Clustered ammunition which is ejectable from canisters for the combating of ground targets, which includes a central body which is encompassed by the ammunition with a member for clustering the ammunition. The clustered ammunition is retained by a clamping band and is fixed in position through the intermediary of formed-fitted components.

Abstract translation: 集群弹药可从罐中喷出以打击地面目标，其中包括弹药所包围的中心体与用于聚集弹药的部件。 集束弹药由夹紧带保持，并通过成形配件的中间件固定在适当的位置。