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    • 3. 发明授权
    • Spin stabilized projectile assembly
    • 旋转稳定的射弹组件
    • US4177733A
    • 1979-12-11
    • US834496
    • 1977-09-19
    • Rudolf RomerManfred MollChristian Jaeneke
    • Rudolf RomerManfred MollChristian Jaeneke
    • F42B14/02F42B14/06F42B13/02
    • F42B14/064F42B14/02
    • There is described a spin stabilized projectile assembly including a projectile, a sabot, and a guide ring. The projectile is provided with a shoulder at the rear end of which abuts the sabot, the projectile and sabot being connected by the guide ring which extends around the projectile and part of the sabot. The guide ring is arranged so that after the projectile assembly has been fired and has left the barrel of the weapon the sabot and the projectile separate. The sabot has a diameter substantially equal to that of the projectile; the guide ring is secured to the sabot against relative movement in a longitudinal direction but is rotatable with respect to the sabot.
    • 描述了一种自旋稳定的射弹组件,其包括抛射物,破坏物和引导环。 抛射体在其后端设有一个肩部,其肩部与导弹环相连,弹丸和突起通过围绕射弹和部分炮弹延伸的引导环连接。 引导环布置成使得在射弹组装已经被射出并且已经离开武器的枪管之后,将弹药和弹丸分开。 炮弹的直径与射弹的直径基本相等; 引导环固定到砧座上以防止在纵向方向上的相对运动,但是可以相对于砧座旋转。
    • 4. 发明授权
    • Subcaliber projectile with pivotally separable drive cage
    • 具有可旋转分离的驱动器笼的Subcaliber射弹
    • US4850279A
    • 1989-07-25
    • US84534
    • 1987-08-12
    • Reinhart FuchsHans W. LutherPeter WallowJuergen BoeckerWalter SimonRudolf RomerKlaus GersbachBernahrd BispingKarl W. Bethmann
    • Reinhart FuchsHans W. LutherPeter WallowJuergen BoeckerWalter SimonRudolf RomerKlaus GersbachBernahrd BispingKarl W. Bethmann
    • F42B12/06F42B14/06
    • F42B12/06F42B14/061F42B14/062
    • A subcaliber projectile has a small-diameter projectile body extending along and centered on an axis, having a radially outwardly directed outer surface, and adapted to move in a predetermined axial back-to-front direction, and a sabot formed of a plurality of similar segments annularly surrounding at least a portion of the body, the segments forming an inner surface generally on the outer surface of the body and having an extreme front end and an extreme rear end. This projectile is formed on one of these surfaces at the extreme rear end of the sabot with a radially projecting ridge of generally semicircular shape having a center of curvature. The other of the surfaces is formed at the extreme rear end of each segment of the sabot with a radially open recess complementary to and receiving the ridge. In addition the segments are pivotal about the center of curvature without the ridge leaving the recess from a position with the respective inner surface lying on the outer projectile-body surface and a position with the inner surface projecting at an angle away therefrom.
    • 亚型射弹具有沿着轴线延伸并居中的小直径射弹体,具有径向向外指向的外表面,并且适于在预定的轴向前后方向上移动,并且由多个相似的形状 所述片段环绕所述主体的至少一部分环绕,所述片段通常在所述主体的外表面上形成内表面,并且具有极端的前端和极端的后端。 该抛射体形成在砧座的最后端的这些表面中的一个上,具有具有曲率中心的大致半圆形的径向突出的脊。 另一个表面形成在砧板的每个部分的最后端,并具有与脊部互补并且接收脊部的径向开口的凹部。 此外,段围绕曲率中心枢转,而没有脊从相应的内表面位于外弹体体表面上的位置离开凹槽,并且内表面以与其远离的角度突出的位置。
    • 9. 发明授权
    • Discus-shaped projectile
    • 铁饼型射弹
    • US4577813A
    • 1986-03-25
    • US153921
    • 1980-05-05
    • Rudolf RomerManfred Moll
    • Rudolf RomerManfred Moll
    • F42B12/14F42B13/24
    • F42B12/14
    • A weapons system, especially for foot attack upon armored vehicles, has a recoilless firing tube and a discus-shaped projectile. The projectile is provided with a fork having an upper arm and a lower arm and a stabilizer connected to the fork and including a tube having a longitudinal axis and fins at the opposite end. An explosive charge is carried by a hub of the fork and a disk-shaped body is rotatable about the hub between the arms of the fork by a portion of propellant gases to stabilize the projectile along its flight toward a target.
    • 一个武器系统,特别是对装甲车辆的脚部攻击,具有无后坐力的射击管和铁饼形弹丸。 射弹设置有具有上臂和下臂的叉,以及连接到叉的稳定器,并且包括在相对端具有纵轴和翅片的管。 爆炸装药由叉的轮毂承载,并且盘形主体可以通过推进剂气体的一部分在叉子的臂之间围绕轮毂旋转,以将射弹沿着其飞行朝向目标稳定。
    • 10. 发明授权
    • Projectile having an apparatus for flight-path correction
    • 具有飞行路径校正装置的弹丸
    • US5836540A
    • 1998-11-17
    • US477121
    • 1995-03-24
    • Rudolf RomerGerd Wollmann
    • Rudolf RomerGerd Wollmann
    • F41G7/22F41G7/00
    • F42B10/661F41G7/222
    • A projectile having a longitudinal axis, a sensor disposed in the substantially pointed front end of the projectile for detecting a respective target, and electronics connected to the output of the sensor for igniting a correction charge to effect a correction of the flight path of the projectile by a predetermined angle (.delta..sub.0). In order to install the apparatus for flight-path correction into the respective projectile completely and in a space-saving manner, so that, unlike in known projectiles, corresponding evaluation and signal-transmission units in the respective weapon carrier can be omitted and complicated gyroscopic systems in the projectile can be omitted, the sensor determines the angle (.delta.) between the longitudinal axis of the projectile and the line (target line) connecting the projectile and the target, and when an angle (.delta..sub.0) is reached that is identical in size/magnitude to the deviation caused by the respective correction charge, the electronics ignite this charge.
    • 具有纵向轴线的抛射体,设置在用于检测相应目标的射弹的基本上尖的前端的传感器,以及连接到传感器的输出端的电子装置,用于点燃校正电荷以实现弹丸飞行路径的校正 以预定角度(delta 0)。 为了将飞行路径校正装置完全安装在相应的抛射体中,节省空间,使得与已知的射弹不同,可以省略各个武器载体中的相应的评估和信号传输单元,并且可以使陀螺仪 射弹中的系统可以省略,传感器确定射弹的纵轴与连接射弹与目标的线(目标线)之间的角度(delta),以及达到相同角度(delta 0)时的角度 在大小/幅度上由相应的校正电荷引起的偏差,电子装置点燃这种电荷。