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    • 31. 发明授权
    • Armor car-mounted mortar
    • 装甲车载砂浆
    • US4489639A
    • 1984-12-25
    • US385006
    • 1982-06-03
    • Gert WinklerWilfried BeckerErich ZielinskiHerbert Lipp
    • Gert WinklerWilfried BeckerErich ZielinskiHerbert Lipp
    • F41A9/16F41A9/21F41A23/34F41F1/06
    • F41A9/21F41A23/34F41A9/16
    • A muzzle loading mortar constructed for mounting on a protected enclosure, for example, an armored vehicle. The mortar includes a mortar tube having an open end for receiving and discharging a projectile, and mounting means, including a tube cradle connected with a recoil-return means, are provided for mounting the tube on the enclosure. The recoil-return means includes a hydraulic member which cooperates with a spring for reducing the forces introduced into the enclosure during development of a shot from the mortar. A loading means is mounted for relative movement between the open end of the tube and the protected enclosure for muzzle loading the open end of the tube with a projectile. The loading means can be operated from within the protected enclosure to load a projectile into the mortar tube.
    • 用于安装在受保护的外壳上的枪口装载砂浆,例如装甲车辆。 砂浆包括具有用于接收和排出抛射体的开口端的砂浆管,并且提供包括与反冲返回装置连接的管支架的安装装置,用于将管安装在外壳上。 反冲返回装置包括液压元件,该液压元件与弹簧相配合,用于在从研钵中发射的过程中减少引入外壳的力。 安装装载装置用于在管的开口端和受保护的外壳之间的相对运动,用于枪口用射弹装载管的开口端。 装载装置可以在受保护的外壳内操作,以将射弹装入砂浆管。
    • 35. 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。
    • 40. 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。