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    • 2. 发明授权
    • High-explosive projectile
    • 高爆弹药
    • US5009167A
    • 1991-04-23
    • US296150
    • 1989-01-12
    • Achim SippelHeinz-Josef KruseWilfried Becker
    • Achim SippelHeinz-Josef KruseWilfried Becker
    • F42B10/44F42B12/22F42B14/02
    • F42B14/02F42B12/22
    • A high-explosive projectile including a projectile body having a forward region and a tail region which transitions to a base, with an explosive charge disposed within the body and detonated by a suitable fuse, and a driving band disposed on the outer circumferential surface of the projectile body in the tail region, wherein the wall thickness of the tail region of the projectile body is substantially the same as the wall thickness of the forward region of the projectile body; the tail region of the projectile body has a cylindrical shape up to its transition to the base and forms a circumferential edge at the transition; and the rearward, gas pressure receiving side of the driving band is disposed adjacent the circumferential edge.
    • 一种高爆炸弹体,包括具有向前区域和尾部区域的射弹体,其过渡到基部,爆炸装置设置在主体内并由合适的保险丝引爆;以及驱动带,其布置在 射弹体尾部区域的射出体,射弹体的尾部区域的壁厚与射弹体的前方区域的壁厚基本相同; 射弹体的尾部区域具有直到其过渡到基部的圆柱形形状并且在转变处形成圆周边缘; 并且驱动带的向后的气体压力接收侧设置成与周向边缘相邻。
    • 4. 发明授权
    • Fin stabilized projectile
    • 鳍稳定射弹
    • US5261629A
    • 1993-11-16
    • US861416
    • 1992-04-02
    • Wilfried BeckerGerhard GlotzJosef OsthuesHans-Peter OpitzHeinz-Josef KruseJutta PetersHelmut Peller
    • Wilfried BeckerGerhard GlotzJosef OsthuesHans-Peter OpitzHeinz-Josef KruseJutta PetersHelmut Peller
    • F42B15/01F42B10/66
    • F42B15/01F42B10/661
    • A fin stabilized ballistic projectile comprises a projectile body having a plurality of stabilizing fins and an ejectable projectile tip detachably attached to the front of the projectile body. An ejection mechanism is operatively disposed for ejecting the projectile tip. A sensor is disposed in the projectile tip for scanning a target area. A warhead is disposed at the front of the projectile body behind the projectile tip and includes a curved fragmentation plate for discharging fragments at a target, with the fragmentation plate being openly exposed when the projectile tip is ejected, and an explosive charge disposed behind the fragmentation plate. A control unit is connected to the sensor for receiving the target signals and having outputs coupled to the ejection mechanism and the explosive charge, the control unit producing controls signals in dependence of the target signals for causing the ejection mechanism to eject the projectile tip and for subsequently detonating the explosive charge thereby causing the fragmentation plate to break up into fragments and discharging the fragments at high acceleration within an angle of revolution determined by the degree of curvature of the fragmentation plate.
    • 翅片稳定的弹道射弹包括具有多个稳定翅片的弹丸体和可拆卸地附接到射弹体前部的可弹出射弹末端。 可操作地设置弹出机构以弹出射弹尖端。 传感器设置在射弹尖端,用于扫描目标区域。 弹头位于射弹尖端后方的射弹体的前方,并包括一个用于在目标上排放碎屑的弯曲分裂板,当射弹尖端被弹出时,碎片板被露出露面,并在碎片后面放置爆炸物 盘子。 控制单元连接到传感器,用于接收目标信号并且具有耦合到弹出机构和爆炸装药的输出,所述控制单元根据目标信号产生控制信号,以使喷射机构弹出射弹尖端并且 随后引爆炸药,从而使破碎板分裂成碎片,并以高加速度在由分片板的曲率度确定的旋转角度内排出碎片。
    • 6. 发明授权
    • Weapon system with a carrier vehicle and a preferably vehicle dependent mortar
    • 具有载体车辆和优选车辆依赖砂浆的武器系统
    • US08534180B2
    • 2013-09-17
    • US13089040
    • 2011-04-18
    • Wilfried BeckerWolfgang BoerHans-Ulrich DesgrangesHans Moser
    • Wilfried BeckerWolfgang BoerHans-Ulrich DesgrangesHans Moser
    • F41F1/06
    • F42B30/12F41H7/02
    • A weapon system includes a carrier vehicle and a vehicle dependent mortar, wherein the carrier vehicle has a crew space and a weaponry space to house the mortar, and the mortar is charged in an index position with mortar grenades, with several sheddable propellant modules on the tail shaft thereof. The weapon system avoids manual loading of the mortar with mortar grenades because an automatic loader is arranged in a weapon space separated from the crew space by a separating wall. The loader transports the mortar grenade from a magazine in the weapon space into the index position of the barrel of the mortar and axially inserts it into the mouth of the barrel, and an automatic shedding device is arranged in the weapon space to automatically remove unnecessary propellant modules from the mortar grenade after fixing target parameters and before insertion of the mortar grenade into the barrel.
    • 武器系统包括载体车辆和车辆依赖砂浆,其中运载工具具有船员空间和用于容纳迫击炮的武器空间,并且将砂浆以灰浆手榴弹装载在索引位置,并在其上安装若干可喷洒的推进剂模块 尾轴。 武器系统避免用砂浆手榴弹手动装载砂浆,因为将自动装载机布置在与船员空间分离的武器空间中。 装载机将迫击炮手榴弹从武器空间的杂志运送到砂浆桶的索引位置,并将其轴向插入枪管的口中,并在武器空间内设置自动卸载装置,以自动移除不必要的推进剂 在固定目标参数后,将砂浆手榴弹插入枪管之前,从迫击炮手榴弹模块。
    • 7. 发明授权
    • Missile having a pivotal warhead
    • 导弹有一个关键的弹头
    • US5631442A
    • 1997-05-20
    • US641642
    • 1996-05-01
    • Wilfried BeckerDirk KilfittWerner Grosswendt
    • Wilfried BeckerDirk KilfittWerner Grosswendt
    • F42B12/14F42B12/20
    • F42B12/204F42B12/14
    • A missile includes a warhead accommodated in an inner space at a front portion of the missile; a ball joint being in alignment with the longitudinal missile axis and pivotally supporting the warhead; and an aiming device for placing the warhead into a desired pivotal orientation. The aiming device includes a plurality of inflatable vessels arranged axially adjacent the warhead in a distribution about the missile axis. Each vessel has a first end oriented toward the warhead and a second end oriented away therefrom. The vessels are supported at their second end by a disk situated in the inner space of the missile. A gas generator is coupled to each vessel for charging the vessel with a gas to place the vessel into its inflated state. In the inflated state each vessel exerts a torque on the warhead about the ball joint by an engagement between the first end of the respective vessel and the warhead. Further, an electronic control system is accommodated in the inner space of the vessel. The electronic control system is connected to each gas generator for actuating a selected gas generator to place the warhead into a desired inclined orientation relative to the missile axis.
    • 导弹包括容纳在导弹前部内空间的弹头; 球形接头与纵向导弹轴线对齐并枢转地支撑弹头; 以及用于将弹头置于期望的枢转方向的瞄准装置。 瞄准装置包括在围绕导弹轴线的分布中沿轴向邻近弹头布置的多个可充气容器。 每个船舶具有朝向弹头的朝向的第一端和朝向其的第二端。 船只在其第二端由位于导弹内部空间的盘支撑。 气体发生器联接到每个容器,用于用气体对容器充电以将容器置于其充气状态。 在充气状态下,每个船舶通过相应船舶的第一端和弹头之间的接合,在弹头上围绕球窝接头施加扭矩。 此外,电子控制系统容纳在容器的内部空间中。 电子控制系统连接到每个气体发生器,用于致动选定的气体发生器,以将弹头相对于导弹轴置于期望的倾斜方位。
    • 9. 发明授权
    • Self-deploying stabilizing-vane assembly for projectile
    • 用于射弹的自展式稳定叶片组件
    • US4693434A
    • 1987-09-15
    • US779228
    • 1985-09-23
    • Michael SchwenzerArmin EskamWalter SimonWilfried Becker
    • Michael SchwenzerArmin EskamWalter SimonWilfried Becker
    • F42B10/14F42B13/32
    • F42B10/14Y10T403/11
    • A vane assembly for a projectile has a carrier carrying a plurality of pivots, having at the pivots respective carrier elements, and adapted to be secured to an end of the projectile. Respective vane elements are each pivotal on the pivots between an inner position lying immediately adjacent the respective carrier element and within a projection of the projectile and an outer deployed position projecting beyond the projection. Respective heat-destructible pins engaged between the vane elements and the respective carrier elements normally retain the vanes in the inner position and release the vanes for movement into the outer position when destroyed by heat. The carrier element is a rib of the carrier against which the respective vane lies when not deployed. In addition, relative to a normal longitudinal direction of travel of the projectile carrying the assembly, the vanes extend longitudinally in the direction and have relative to the direction front leading ends engaging the respective pins and rear trailing ends at the respective pivots.
    • 用于抛射体的叶片组件具有承载多个枢轴的载体,所述枢轴在枢转相应的载体元件处并且适于固定到射弹的端部。 相应的叶片元件各自在位于紧邻相应的承载元件的内部位置之间并且在射弹的突出部内的突出部和突出超过突出部的外部展开位置之间的枢轴上枢转。 接合在叶片元件和相应载体元件之间的相应的可热破坏的销通常将叶片保持在内部位置,并且当被热量破坏时释放叶片以移动到外部位置。 载体元件是载体的肋,当未展开时,相应的叶片位于该肋上。 此外,相对于承载组件的弹丸的正常的纵向运动方向,叶片沿着该方向纵向延伸并且相对于在相应枢轴处与相应销和后尾端接合的前方前端的方向。