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    • 7. 发明申请
    • Braking device for a trajectory-correctable spin-stabilized artillery projectile
    • 用于轨迹可修正的自旋稳定炮弹的制动装置
    • US20050258308A1
    • 2005-11-24
    • US10527306
    • 2003-09-10
    • Klaus BarKarl Kautzsch
    • Klaus BarKarl Kautzsch
    • B64C9/32F42B10/50
    • F42B10/50
    • In order to move a textile braking element (16) which is in the form of an annular disk and which is deployed radially under the effect of centrifugal force rapidly into a contour which is stable in respect of shape and which is always properly defined even under afflux flow conditions, a cloth (33) which is cut in the form of a circular ring is provided by virtue of radially extending tucks or darts, with a reduced outside periphery (32) in such a way that the opening movement is thereby limited to the shape of a flat obtuse-angled hollow truncated cone which, by means of reinforcing bands (34) which are sewn on along generatrices of the frustoconical surface, is pivotably mounted to the holding ring (15) at the inside periphery (31) while along the outside periphery (32), it is provided with a peripherally extending accumulation of mass (29) for increasing the centrifugal deployment forces; wherein in the front end region of the stowage space (14), the ring (15) is axially fitted into the contour of the fuse (12), in such a way as to temporarily slip relative to the projectile spin.
    • 为了移动呈环形盘形式的纺织品制动元件(16),其在离心力的作用下径向展开成一个轮廓,该轮廓在形状方面是稳定的,并且即使在 通过径向延伸的折叠或飞镖,通过减小的外周(32)提供以圆环形式切割的布(33),使得打开运动被限制为 通过沿着截头圆锥形表面的母线缝合的加强带(34)的扁平钝角中空圆锥体的形状在内周边(31)可枢转地安装到保持环(15),同时 沿着外周(32),设置有用于增加离心展开力的周向延伸的质量堆积(29); 其特征在于,在所述装载空间(14)的前端区域中,所述环(15)以相对于所述弹丸旋转临时滑动的方式轴向地配合到所述保险丝(12)的轮廓中。
    • 8. 发明申请
    • Programmable artillery fuse
    • 可编程火炮保险丝
    • US20050211085A1
    • 2005-09-29
    • US10522053
    • 2003-08-02
    • Karl KautzschVolker KochJohann PannhorstRolf Kaden
    • Karl KautzschVolker KochJohann PannhorstRolf Kaden
    • F42C17/04F42C17/00
    • F42C17/04
    • In an artillery fuse (12), particularly having a braking fuse function, in the course of the loading procedure of the howitzer for firing ammunition equipped with such a fuse (12), a quantity of data significantly larger than the typical fuse-setting information may be supplied parallel in time to the typical inductive fuse-setting procedure, particularly initialization information for satellite navigation to be performed on board after firing the ammunition, if the fuse (12) is equipped according to the present invention in the region of its cap (11), which is shaped like a hollow truncated cone, with at least one infrared-radiation-sensitive data interface (13), which works together bidirectionally with a coupling element (16). Preferably, a transceiver is positioned on the fuse (12) for bidirectional data communication, while a ring (15), which may be pulled over its tip (14), is equipped with at least three receivers distributed around the ring circumference as the coupling elements (16).
    • 在具有制动保险丝功能的火炮保险丝(12)中,在装备有这样的保险丝(12)的用于点火弹药的榴弹炮的装载过程中,显着大于典型的熔断器设置信息的数据量 可以及时提供与典型的感应熔断器设置程序并行提供的(特别是用于在发射弹药之后在船上进行卫星导航的初始化信息),如果根据本发明在其盖的区域中配备了熔丝 (11),其形状类似于中空截头圆锥​​体,具有至少一个与耦合元件(16)双向工作的红外辐射敏感数据接口(13)。 优选地,收发器位于保险丝(12)上用于双向数据通信,而可以被拉过其尖端(14)的环(15)配备有围绕环圆周分布的至少三个接收器,作为耦合 元素(16)。
    • 9. 发明授权
    • Process for the target-related correction of a ballistic trajectory
    • 弹道轨迹的目标相关校正过程
    • US06467721B1
    • 2002-10-22
    • US09716089
    • 2000-11-17
    • Karl KautzschJurgen LeiningerJurgen WittmannAlbrecht Reindler
    • Karl KautzschJurgen LeiningerJurgen WittmannAlbrecht Reindler
    • F41G730
    • F41G7/346
    • In order to perceptibly reduce the inevitable trajectory scatter or spread of ballistically fired projectiles in the target area without the technological expenditure involved in automatic target-seeking control, and in order thereby substantially to improve the level of target hit accuracy, the minimum trajectory path is laid through the previously ascertained target position, having regard to the error budget of the weapon and the external influencing parameters to be expected so that all real trajectories up to the maximum trajectory of that overall error budget are behind the target position. The descent of the projectile into the target area is then shortened from the real trajectory to the minimum trajectory, that is to say towards the target position. For that purpose, attainment of the optimum initialisation point, which is dependent on the theoretical remaining flight time, for the aerodynamic braking device on the projectile is determined on the real trajectory by a procedure whereby the real trajectory is continuously measured by means of satellite navigation, and the approach to the point of intersection with the triggering curve, that is to say the sequence of optimum initialisation points for the array of real trajectories, is established in dependence on interference, from which a transitional trajectory is adjusted to match the minimum trajectory through the target position.
    • 为了明确地减少弹道射弹在目标区域的不可避免的轨迹散射或扩散,而无需涉及自动寻靶控制的技术支出,为了大幅度提高目标命中精度水平,最小轨迹路径为 考虑到武器的误差预算和预期的外部影响参数,使得所有真实轨迹直到该总体误差预算的最大轨迹落在目标位置之后,才能确定目标位置。 然后将射弹进入目标区域的下降从实际轨迹缩短到最小轨迹,即朝向目标位置。 为此目的,通过一个程序确定飞弹上空气动力学制动装置的理论剩余飞行时间的最佳初始化点达到实际轨迹,实际轨迹通过卫星导航连续测量 以及与触发曲线相交点的方法,也就是说,实际轨迹阵列的最佳初始化点的序列依赖于干扰而被确定,从该干扰调整过渡轨迹以匹配最小轨迹 通过目标位置。
    • 10. 发明授权
    • Braking device for a trajectory-correctable spin-stabilized artillery projectile
    • 用于轨迹可修正的自旋稳定炮弹的制动装置
    • US07347147B2
    • 2008-03-25
    • US10527306
    • 2003-09-10
    • Klaus BärKarl Kautzsch
    • Klaus BärKarl Kautzsch
    • F42B10/50F42B10/14
    • F42B10/50
    • In order to move a textile braking element (16) which is in the form of an annular disk and which is deployed radially under the effect of centrifugal force rapidly into a contour which is stable in respect of shape and which is always properly defined even under afflux flow conditions, a cloth (33) which is cut in the form of a circular ring is provided by virtue of radially extending tucks or darts, with a reduced outside periphery (32) in such a way that the opening movement is thereby limited to the shape of a flat obtuse-angled hollow truncated cone which, by means of reinforcing bands (34) which are sewn on along generatrices of the frustoconical surface, is pivotably mounted to the holding ring (15) at the inside periphery (31) while along the outside periphery (32), it is provided with a peripherally extending accumulation of mass (29) for increasing the centrifugal deployment forces; wherein in the front end region of the stowage space (14), the ring (15) is axially fitted into the contour of the fuse (12), in such a way as to temporarily slip relative to the projectile spin.
    • 为了移动呈环形盘形式的纺织品制动元件(16),其在离心力的作用下径向展开成一个轮廓,该轮廓在形状方面是稳定的,并且即使在 通过径向延伸的折叠或飞镖,通过减小的外周(32)提供以圆环形式切割的布(33),使得打开运动被限制为 通过沿着截头圆锥形表面的母线缝合的加强带(34)的扁平钝角中空圆锥体的形状在内周边(31)可枢转地安装到保持环(15),同时 沿着外周(32),设置有用于增加离心展开力的周向延伸的质量堆积(29); 其特征在于,在所述装载空间(14)的前端区域中,所述环(15)以相对于所述弹丸旋转临时滑动的方式轴向地配合到所述保险丝(12)的轮廓中。