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    • 2. 发明授权
    • Apparatus for filling shell bodies with sub-projectiles
    • 用于向炮弹填充炮弹的装置
    • US6142054A
    • 2000-11-07
    • US506334
    • 2000-02-18
    • Peter Ettmuller
    • Peter Ettmuller
    • F42B12/62B65B19/34F42B12/58F42B33/02
    • F42B12/58B65B19/34F42B33/02
    • 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.
    • 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。
    • 3. 发明授权
    • Method and apparatus for filling shell bodies with sub-projectiles
    • 使用子弹填充壳体的方法和装置
    • US6049957A
    • 2000-04-18
    • US627586
    • 1996-04-04
    • Peter Ettmuller
    • Peter Ettmuller
    • F42B12/62B65B19/34F42B12/58F42B33/02B65B35/30
    • F42B12/58B65B19/34F42B33/02
    • A method and apparatus for filling a shell body with sub-projectiles in a predefined geometric arrangement and in a very short time without creating shifting errors is provided. Prior to filling the shell body, the sub-projectiles may be combined into layers which are as thick as the length of the sub-projectiles and which extend in planes transverse to a longitudinal axis of the shell body. The sub-projectiles take up a position in the layer which corresponds to their geometric arrangement in a hollow chamber of the shell body. During the combination, the outer periphery of the layers may be shaped so that, following insertion of the layer into the hollow chamber, the sub-projectiles may be held there and fixed against relative rotation while maintaining the previously formed geometric arrangement. In accordance with a preferred embodiment, the outer periphery of the layers may assume a hexagonal shape where the axes of the cylindrical sub-projectiles are aligned with the longitudinal axis of the shell body.
    • 提供一种用于以预定的几何布置和非常短的时间填充具有子弹体的壳体的方法和装置,而不产生移位误差。 在填充壳体之前,副抛射体可以组合成与子弹体的长度一样厚的层,并且在与壳体的纵向轴线相垂直的平面中延伸。 副投射体在层中占据与壳体的中空室中的几何布置相对应的位置。 在组合期间,层的外周可以被成形为使得在将层插入中空室之后,子弹体可以保持在那里并相对于相对旋转固定,同时保持先前形成的几何布置。 根据优选实施例,层的外周可以呈六边形形状,其中圆柱形子弹体的轴线与壳体的纵向轴线对齐。
    • 4. 发明授权
    • Spin stabilized projectile with a payload
    • 旋转稳定的射弹与有效载荷
    • US5864086A
    • 1999-01-26
    • US45868
    • 1998-03-23
    • Peter Ettmuller
    • Peter Ettmuller
    • F42B12/36F42B12/58F42B12/60
    • F42B12/60F42B12/58
    • A spin-stabilized projectile containing a payload is presented. The projectile includes a projectile body with a payload chamber that may be laterally defined by a projectile casing, on top by an axial fixing device for a payload disposed in the payload chamber, and on the bottom, by a dividing wall. The projectile casing may include axial grooves on the inside, which on the contribute to the fixing of the payload and include intended break zones for freeing the payload. Below the dividing wall, an opening charge may be disposed, which includes complete radial contact and is axially spaced apart from the dividing wall by a damping device. The detonation of opening charge causes the projectile casing to immediately split open at the intended break zones to release, by centrifugal force, the payload from the payload chamber. The damping device prevents the payload from being damaged in the region of the dividing wall and prevents the release of the payload from being interrupted.
    • 介绍了一种包含有效载荷的自旋稳定弹丸。 射弹包括具有有效载荷室的射弹体,其可以由射弹壳体侧向限定,顶部由用于有效载荷室中的有效载荷的轴向固定装置,并且在底部由分隔壁。 射弹套管可以包括在内部的轴向凹槽,这有助于有效载荷的固定,并且包括用于释放有效载荷的预期断裂带。 在分隔壁下方,可以设置开口装料,其包括完全的径向接触并且通过阻尼装置与分隔壁轴向间隔开。 开启电荷的爆炸会导致弹丸套管在预定的断裂区立即开裂,并通过离心力释放有效载荷室的载荷。 阻尼装置防止有效载荷在分隔壁的区域中被损坏并且防止有效载荷的释放被中断。
    • 5. 发明申请
    • Method for programming the shattering or projectiles and tube weapon with programming system
    • 用编程系统编程破碎或射弹和管武器的方法
    • US20050126380A1
    • 2005-06-16
    • US10785910
    • 2004-02-24
    • Peter EttmullerKlaus Munzel
    • Peter EttmullerKlaus Munzel
    • F42C17/04F42C17/00
    • F42C17/04
    • A method for programming the shattering of projectiles (G) and a weapon (12) with a programming system (14, 16, 18). The projectiles are intended to destroy a target (Z) at which they are fired along heavily curved trajectories and are detonated at shattering points near the target. The longitudinal distance (xZ) of the target from the weapon is measured and the elevation (λ) is adjusted for which a known muzzle velocity (v0(0)) and a longitudinal distance of the shattering point at a predetermined optimal height (y*) are taken into consideration. The actual muzzle velocity (v0(eff)) is determined and a calculation for the programming is carried out in which the actual muzzle velocity is taken into account and the optimal height of the shattering point is held constant. The corresponding programming is transmitted to the projectiles. The weapon has an associated programming system for correspondingly programming the projectiles. The programming system has v0-measuring means (14) for determining the actual muzzle velocity, and computer means (16) for calculating the programming of the projectiles, as well as transmitting means for transmitting the programming to the projectiles.
    • 一种用于编程弹丸(G)和武器(12)与编程系统(14,16,18)进行编程的方法。 射弹旨在摧毁一个目标(Z),在这些目标(Z)下,它们沿着弯曲的轨迹被射击,并在目标附近的爆炸点被引爆。 测量来自武器的目标的纵向距离(xLZ),并且调整已知枪口速度(v 0> 0(0))的仰角(λ) 并且考虑到在预定的最佳高度(y *)处的破碎点的纵向距离。 确定实际的枪口速度(v <0>(eff)),并且执行用于编程的计算,其中考虑实际的枪口速度,并且破碎点的最佳高度保持恒定 。 相应的编程被传送到射弹。 该武器具有相关的编程系统,用于对射弹进行相应的编程。 编程系统具有用于确定实际枪口速度的测量装置(14),以及用于计算射弹编程的计算机装置(16),以及用于将编程传送到 射弹。
    • 6. 发明授权
    • Spin-stabilized projectile with payload
    • 自旋稳定的有弹性的射弹
    • US5817969A
    • 1998-10-06
    • US647324
    • 1996-05-09
    • Peter Ettmuller
    • Peter Ettmuller
    • F42B12/36F42B12/58F42B12/60
    • F42B12/60F42B12/58
    • A spin-stabilized projectile containing a payload is presented. The projectile includes a projectile body with a payload chamber that may be laterally defined by a projectile casing, on top by an axial fixing device for a payload disposed in the payload chamber, and on the bottom, by a dividing wall. The projectile casing may include axial grooves on the inside, which on the contribute to the fixing of the payload and include intended break zones for freeing the payload. Below the dividing wall, an opening charge may be disposed, which includes complete radial contact and is axially spaced apart from the dividing wall by a damping device. The detonation of opening charge causes the projectile casing to immediately split open at the intended break zones to release, by centrifugal force, the payload from the payload chamber. The damping device prevents the payload from being damaged in the region of the dividing wall and prevents the release of the payload from being interrupted.
    • 介绍了一种包含有效载荷的自旋稳定弹丸。 射弹包括具有有效载荷室的射弹体,其可以由射弹壳体侧向限定,顶部由用于有效载荷室中的负载的轴向固定装置,并且在底部上由分隔壁。 射弹套管可以包括在内部的轴向凹槽,这有助于有效载荷的固定,并且包括用于释放有效载荷的预期断裂带。 在分隔壁下方,可以设置开口装料,其包括完全的径向接触并且通过阻尼装置与分隔壁轴向间隔开。 开启电荷的爆炸会导致弹丸套管在预定的断裂区立即开裂,并通过离心力释放有效载荷室的载荷。 阻尼装置防止有效载荷在分隔壁的区域中被损坏并且防止有效载荷的释放被中断。