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    • 1. 发明授权
    • Device for guiding a missile
    • 导弹导弹装置
    • US5433399A
    • 1995-07-18
    • US253036
    • 1994-06-02
    • Wilfried BeckerWerner GrosswendtMichael Schwenzer
    • Wilfried BeckerWerner GrosswendtMichael Schwenzer
    • F41G9/00F42B10/00F42B10/60F42B10/66F42B15/01
    • F42B10/661
    • The invention relates to a device for guiding a missile (1; 30) with a missile tip (2) and a cylindrical section (3) adjoining the tip of the missile; the device is provided with at least one control block (4; 31, 32) with exhaust openings (13-15) of corresponding nozzle bodies (10-12) arranged perpendicularly in relation to the missile's surface.In order to accomplish effective guidance, particularly of high-speed missiles (1; 30), in a simple and cost-effective manner it is proposed that the control block (4; 31, 32) be constructed with a plurality of small, fast-burning rocket motors (7-9; 33-36) that are arranged radially on the missile's periphery (1; 30) and that are ignitable in a predeterminable sequence and number.
    • 本发明涉及一种引导导弹(1; 30)与导弹尖端(2)和邻接导弹尖端的圆柱形部分(3)的装置; 该装置设置有至少一个控制块(4; 31,32),其具有相对于导弹表面垂直布置的相应喷嘴体(10-12)的排气口(13-15)。 为了实现特别是高速导弹(1; 30)的有效指导,以简单且具有成本效益的方式提出控制块(4; 31,32)由多个小型,快速的 - 发射火箭发动机(7-9; 33-36),其放射状地布置在导弹的周边(1; 30)上,并且以可预定的顺序和数量可点燃。
    • 2. 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。
    • 3. 发明授权
    • Projectile designed for recoilless and virtually noiseless firing
    • 射弹设计用于无后坐力和几乎无噪声的射击
    • US4244293A
    • 1981-01-13
    • US807315
    • 1977-06-09
    • Werner GrosswendtManfred MollWilfried Becker
    • Werner GrosswendtManfred MollWilfried Becker
    • F41A1/10F41F3/02
    • F41A1/10
    • A projectile to be fired from a tubular or rail-shaped launcher has a warhead integral with a rearwardly extending tube of smaller diameter which contains a propulsive charge inserted between the warhead and a sabot carrying a frangible inertial mass. The rear end of the tube has a constricted opening which, upon detonation of the charge, retains the rearwardly moving sabot while giving passage to the disintegrating mass as the projectile is propelled forwardly. The propulsion gases evolving within the tube are temporarily retained by one or more heat-destructible plugs in the sabot and/or in the tube which melt, burn or char to allow the delayed escape of the gases whereby an in-flight thrust is imparted to the projectile.
    • 从管状或轨​​道式发射器发射的射弹具有与直径较小的向后延伸的管一体的弹头,其包含插入在弹头和携带易碎惯性质量的炮弹之间的推进炸药。 管的后端具有收缩开口,当开始爆炸时,当弹丸向前推进时,该开口保持向后移动的破坏物,同时通向碎裂物质。 在管内释放的推进气体由一个或多个可破坏的塞子临时保持在膛体和/或管中,其熔化,燃烧或炭化以允许气体的延迟逸出,从而将飞行中的推力施加到 射弹。
    • 4. 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。
    • 5. 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。
    • 8. 发明授权
    • Tank mortar
    • 坦克砂浆
    • US4198897A
    • 1980-04-22
    • US939227
    • 1978-09-05
    • Herbert LippWilfried Becker
    • Herbert LippWilfried Becker
    • F41A9/27F41F1/06F41F9/06
    • F41F1/06F41A9/27
    • A tank mortar having a magazine receiving a plurality of fin-stabilized projectiles which can be selectively aligned with the barrel. The barrel is movable relative to the magazine to enable sealing engagement of the barrel with the selected magazine chamber. The weapon frame which rotatably receives the magazine has an upper portion in which the bottom of the barrel is axially shiftable, e.g. by a bayonet arrangement, and a lower portion which sealingly engages the bottom of the munition chamber which is aligned with the barrel includes the firing element which triggers the displacement of the projective from the round chamber through the barrel. The base of the weapon frame is also provided with a ball received in a socket which is shiftable to traverse the weapon.
    • 一种罐式砂浆,其具有容纳可以选择性地与筒对准的多个翅片稳定的射弹的盒。 枪管相对于刀库可移动,以使枪管与所选刀库腔密封接合。 可旋转地接收盒子的武器框架具有上部,其中筒的底部可轴向移动,例如, 通过卡口布置,以及密封地接合与枪筒对准的弹药室的底部的下部包括触发元件,其触发投射物从圆形腔通过枪管的位移。 武器框架的底部还设置有容纳在插座中的球,其可移动以横穿武器。