公开(公告)号：US20100308152A1

公开(公告)日：2010-12-09

申请号：US12789607

申请日：2010-05-28

Applicant: Jens SEIDENSTICKER

Inventor： Jens SEIDENSTICKER

IPC: F42B15/01

CPC classification number: F41G7/266 ,  F41G7/305 ,  G05D1/108

Abstract: A method for correcting a trajectory of terminally guided ammunition is provided. In order to achieve a high probability of hits, in particular when firing in bursts (continuous fire, rapid single shot fire), it is provided that every individual ammunition is addressed separately. The “imprinting” is performed based on the beam rider guidance principle of terminally guided ammunition. Every individual ammunition reads only the guidance beam identified for this ammunition and can, using additional information, determine its absolute roll attitude in space in order to achieve the proper triggering of the correcting propulsion unit.

Abstract translation: 提供了一种用于校正末端引导弹药的轨迹的方法。 为了获得很高的命中率，特别是在爆发（连续射击，快速射击）射击时，规定每个单独的弹药被单独处理。 “印记”是根据终极引导弹药的梁骑手指导原则进行的。 每个单独的弹药只读取为该弹药确定的指导梁，并且可以使用附加信息确定其在太空中的绝对滚动姿态，以便正确触发校正推进单元。

公开(公告)号：US5896106A

公开(公告)日：1999-04-20

申请号：US585422

申请日：1996-01-11

Applicant: Jens Seidensticker ,  Wolfgang Kreuzer

Inventor： Jens Seidensticker ,  Wolfgang Kreuzer

IPC: F41G7/30 ,  G01S3/52 ,  G01S1/02

CPC classification number: G01S3/52 ,  F41G7/305

Abstract: In a method for determining the roll attitude of a rolling flying object having a radio receiver, in particular for guiding a ballistic flying projectile/rocket having roll compensation, the aim is to determine a line of sight between a transmitting source and the antenna and to determine the roll attitude therefrom.

Abstract translation: 在一种用于确定具有无线电接收机的滚动飞行物体的滚动姿态的方法中，特别是用于引导具有滚转补偿的弹道飞弹/火箭，目的是确定发射源和天线之间的视线，并且确定 确定辊的姿态。

公开(公告)号：US20120292432A1

公开(公告)日：2012-11-22

申请号：US13549918

申请日：2012-07-16

Applicant: Jens SEIDENSTICKER

Inventor： Jens SEIDENSTICKER

IPC: F42B15/01 ,  F42B10/00

CPC classification number: F41G7/263 ,  F41G7/266

Abstract: A method for correcting a trajectory of a projectile is provided, in that a laser beam is guide or rotated around a center of the instantaneous target course of a projectile in such a way that the projectile itself detects a divergence thereof and subsequently carries our a selfcorrection. A first laser beam is emitted over a certain region around the target course of the projectile that can at about the same time initiate a start of a timing process. A further rotating laser beam having a fixed rotational frequency Ω can be simultaneously positioned around the region. Via the second laser beam, the projectile recognizes a divergence thereof from the target course and initiates a correction based on the determined divergence, whereby a magnitude thereof is then used to effect the timed initiation of the correction. Thus, delays in the release are implemented in the projectile.

Abstract translation: 提供了一种用于校正射弹的轨迹的方法，其中激光束以射弹的瞬时目标过程的中心引导或旋转，使得射弹本身检测到其发散，并随后携带我们的自校正 。 第一激光束在射弹目标进程周围的特定区域发射，可以在大约同时启动定时过程的开始。 具有固定旋转频率ωgr的另外的旋转激光束; 可以同时定位在该地区周围。 通过第二激光束，射弹识别出与目标进程的分歧，并基于确定的发散度启动校正，由此其大小然后用于实现校正的定时启动。 因此，在弹药中实施释放的延误。

公开(公告)号：US4612859A

公开(公告)日：1986-09-23

申请号：US659649

申请日：1984-10-11

Applicant: Benjamin Furch ,  Jens Seidensticker

Inventor： Benjamin Furch ,  Jens Seidensticker

IPC: F42B12/16 ,  F42B12/32 ,  F42B11/22

CPC classification number: F42B12/16 ,  F42B12/32

Abstract: The invention relates to a multiple purpose warhead which is provided with a spike-forming cladding, with projectile-forming layers and with preshaped splinters, respectively splinter layers. For the simultaneous combatting of hard and semi-hard material targets as well as soft targets the impact precision, the penetration capacity and thereby the effectiveness of the multiple purpose warhead is increased relative to the multiple purpose warheads of the state of the art.The multiple purpose warhead of this invention includes within a multiple purpose warhead casing 7 at least three effective parts 1, 2, 3. This arrangement achieves optimum, however, different, target effectiveness and a separate dosable explosive charge 6.1, 6.2, 6.3 corresponding to the different target requirements by providing corresponding different claddings for each effective part. There is provided between a first effective part formed as a hollow charge 6.1 and a third effective part formed as a splinter-forming warhead 9 a projectile-forming layer 22 which forms the second effective part. There is provided within two mutually confronting conically shaped recesses 10, 11 arranged symmetrically about a longitudinal axis 12, on the one hand, an ignition arrangement 14 and, on the other hand, an inert-insert 13, whereby a common ignition of all effective parts is made possible and flaw-free detonation wave guidance is also effected not only with a spike-formation, but also with the projectile-formation thereby increasing the destructive capacity of the multiple purpose warhead.

Abstract translation: 本发明涉及一种多用途弹头，其具有尖峰形成包层，具有抛射物形成层和预分裂碎片，分别是碎片层。 为了同时打击硬质和半硬质材料目标以及软性目标，相对于现有技术的多用途弹头，冲击精度，穿透能力以及多用途弹头的有效性都有所增加。 本发明的多用途弹头包括在多用途弹头壳体7内的至少三个有效部分1,2,3。这种布置实现了目标效能最佳但不同的目标效能，以及分别对应于 通过为每个有效部分提供相应的不同的包层来满足不同的目标要求。 设置在形成为空心装料6.1的第一有效部分和形成为碎片形成弹头9的第三有效部分之间，形成第二有效部分的射弹形成层22。 在两个相互面对的锥形凹槽10,11中设置有一个围绕纵向轴线12对称设置的一个点火装置14，另一方面是一个惰性插入件13，从而使所有有效的共同点火 部件是可能的，无损探伤波引导也不仅受到尖峰形成的影响，而且还与弹丸形成有关，从而增加了多用途弹头的破坏能力。

公开(公告)号：US4589340A

公开(公告)日：1986-05-20

申请号：US573343

申请日：1984-01-24

Applicant: Rolf Hellwig ,  Jens Seidensticker ,  Klaus D. Karius

Inventor： Rolf Hellwig ,  Jens Seidensticker ,  Klaus D. Karius

IPC: F16M11/40 ,  G01B5/00 ,  F42B23/24 ,  F42C19/00

CPC classification number: G01B5/0004 ,  F16M11/046 ,  F16M11/40 ,  F16M13/005 ,  F16M2200/047

Abstract: The invention relates to a sensor-carrier which is transported by a useful load projectile to a predetermined target region which may be inaccessible and is set down in said region. For the purpose of avoiding damaging the sensitive sensor, the latter is, together with the sensor support, compactly mounted in a folded retracted condition in a rugged housing and is automatically projected out of the housing in an erected, extended position when the sensor-carrier is set down and the housing is opened. The sensor support consists of a plurality of rotationally symmetrical support members which are strung on a steel cable in a manner similar to a pearl necklace. The steel cable is surrounded by a sheathing and is connected via a disc to a coil spring for tensioning the steel cable. The sensor-carrier serves to position the sensor in an elevated position over the ground surface for improving its sensing and transmitting capabilities.

Abstract translation: 本发明涉及一种传感器 - 载体，其通过有用的负载射弹传送到预定的目标区域，该预定目标区域可能是不可接近的并且被放置在所述区域中。 为了避免损坏敏感传感器，后者与传感器支撑件一起紧凑地安装在折叠的缩回状态下在坚固的壳体中，并且当传感器载体 被放下并且外壳被打开。 传感器支撑件由多个旋转对称的支撑构件组成，其以类似于珍珠项链的方式串在钢缆上。 钢丝绳由护套包围，并通过盘连接到用于张紧钢索的螺旋弹簧。 传感器载体用于将传感器定位在地面上方的升高位置，以改善其感测和传输能力。

公开(公告)号：US4557437A

公开(公告)日：1985-12-10

申请号：US405417

申请日：1982-08-05

Applicant: Jens Seidensticker ,  Werner Grosswendt

Inventor： Jens Seidensticker ,  Werner Grosswendt

IPC: F41G7/20 ,  F41G7/34 ,  F42C13/06 ,  F41G7/00

CPC classification number: F42C13/06 ,  F41G7/20 ,  F41G7/34

Abstract: A process for controlling the flight attitude of a flying body and/or the activation of a useful live load on a flying body and the arrangement for carrying out the process. At least one receiving-emitting-unit for emitting and receiving energy in the form of ultra soundwaves is first emitted in bundled form from the unit and then reflected from the region immediately adjoining the flying body, for example, the ground surface, and received by the unit, whereupon the soundwaves are converted into electrical signals. By means of time lapse measurements of the emitted and reflected soundwaves there can, for example, be measured the distance of the flying body from the ground. If the flying body deviates from a predetermined flight path, control surfaces for correcting the flight path are adjusted by control means. Moreover, by means of the receiving-emitting-unit and via the control means a useful live load can be activated.

Abstract translation: 用于控制飞行体的飞行姿态和/或激活飞行体上有用的活载的过程和用于执行该过程的装置。 用于发射和接收超声波形式的能量的至少一个接收发射单元首先从该单元以捆绑形式发射，然后从紧邻飞行体（例如地面）的区域反射，并由 该单元，因此声波被转换成电信号。 通过发射和反射的声波的时间流逝测量，可以例如测量飞行体与地面的距离。 如果飞行体偏离预定的飞行路径，则通过控制装置调整用于校正飞行路径的控制面。 此外，通过接收发射单元并且经由控制装置，可以激活有用的有功负载。

公开(公告)号：US08558151B2

公开(公告)日：2013-10-15

申请号：US13549918

申请日：2012-07-16

Applicant: Jens Seidensticker

Inventor： Jens Seidensticker

IPC: F41G7/24 ,  F42B15/01 ,  F41G7/00 ,  F41G7/30 ,  F42B15/00

CPC classification number: F41G7/263 ,  F41G7/266

Abstract: A method for correcting a trajectory of a projectile is provided, in that a laser beam is guide or rotated around a center of the instantaneous target course of a projectile in such a way that the projectile itself detects a divergence thereof and subsequently carries our a selfcorrection. A first laser beam is emitted over a certain region around the target course of the projectile that can at about the same time initiate a start of a timing process. A further rotating laser beam having a fixed rotational frequency Ω can be simultaneously positioned around the region. Via the second laser beam, the projectile recognizes a divergence thereof from the target course and initiates a correction based on the determined divergence, whereby a magnitude thereof is then used to effect the timed initiation of the correction. Thus, delays in the release are implemented in the projectile.

Abstract translation: 提供了一种用于校正射弹的轨迹的方法，其中激光束围绕射弹的瞬时目标过程的中心引导或旋转，使得射弹本身检测到其发散，并随后携带我们的自校正 。 第一激光束在射弹目标进程周围的特定区域发射，可以在大约同时启动定时过程的开始。 具有固定旋转频率Ω的另一旋转激光束可以同时位于该区域周围。 通过第二激光束，射弹识别出与目标进程的分歧，并基于确定的发散度启动校正，由此其大小然后用于实现校正的定时启动。 因此，在弹药中实施释放的延误。

公开(公告)号：US20070074625A1

公开(公告)日：2007-04-05

申请号：US11436327

申请日：2006-05-18

Applicant: Jens Seidensticker ,  Dietrich Stauffacher

Inventor： Jens Seidensticker ,  Dietrich Stauffacher

IPC: F42C17/00

CPC classification number: F42C17/04 ,  F42C11/065

Abstract: To avoid mechanical and thermodynamic wear of a programming system, a microwave transmitter, preferably operating in the GHz range, is integrated in the system, while at the same time the advantages of measurement of the muzzle velocity and of a current compensated fuse setting are preserved. The microwave transmitter transmits the current fuse setting, for example, as determined by a fire control computer, to the ammunition, e.g., a projectile. A direct measurement of the actual muzzle velocity itself can be dispensed with, since the real muzzle velocity is determined by the current flight velocity information of the projectile, i.e., it is extrapolated back from this. On the basis of this current projectile velocity, the ignition time, which was preset with the ignition time of the projectile using a standard muzzle velocity, is corrected and used as the current fuse set time.

Abstract translation: 为了避免编程系统的机械和热力学磨损，优选在GHz范围内工作的微波发射器被集成在系统中，同时保持测量枪口速度和电流补偿保险丝设置的优点被保留 。 微波发射器将例如由消防控制计算机确定的当前保险丝设置传送到弹药，例如射弹。 实际的枪口速度本身的直接测量可以省掉，因为实际的枪口速度是由射弹的当前飞行速度信息决定的，也就是从外推。 根据当前的射弹速度，使用标准炮口速度预测的射弹点火时间的点火时间被校正并用作当前的保险丝设定时间。

公开(公告)号：US4584943A

公开(公告)日：1986-04-29

申请号：US628751

申请日：1984-07-09

Applicant: Norbert Vavra ,  Jens Seidensticker

Inventor： Norbert Vavra ,  Jens Seidensticker

IPC: F42B10/56 ,  F42B12/10 ,  F42B30/00 ,  F42C13/00 ,  F42C19/06 ,  F42C13/04

CPC classification number: F42B12/10 ,  F42B10/56 ,  F42B30/006 ,  F42C13/006 ,  F42C19/06

Abstract: Missile head to be released in an airplane cargo drop or from a flying body. The missile head has a target-sensor having a transmitter, a receiver, an antenna and an explosive charge ignitable by a target location signal. In order not to interfere with the function of the explosive charge, it is best that the antenna be located in front of the target-sensor with respect to the flight direction, while the target-sensor is located behind the explosive charge with respect to the flight direction. The connection between the antenna and the target-sensor is provided by a wave carrier filled with explosives.

Abstract translation: 导弹头在飞机货物下降或从飞行的身体释放。 导弹头具有目标传感器，其具有发射器，接收器，天线和由目标位置信号可点燃的炸药。 为了不干扰爆炸物的功能，天线最好相对于飞行方向位于目标传感器的前方，而目标传感器位于爆炸物的后面。 飞行方向。 天线和目标传感器之间的连接由装有爆炸物的波浪载体提供。

公开(公告)号：US08288698B2

公开(公告)日：2012-10-16

申请号：US12789607

申请日：2010-05-28

Applicant: Jens Seidensticker

Inventor： Jens Seidensticker

IPC: F41G7/24 ,  F41G7/30 ,  F41G7/00

CPC classification number: F41G7/266 ,  F41G7/305 ,  G05D1/108

Abstract: A method for correcting a trajectory of terminally guided ammunition is provided. In order to achieve a high probability of hits, in particular when firing in bursts (continuous fire, rapid single shot fire), it is provided that every individual ammunition is addressed separately. The “imprinting” is performed based on the beam rider guidance principle of terminally guided ammunition. Every individual ammunition reads only the guidance beam identified for this ammunition and can, using additional information, determine its absolute roll attitude in space in order to achieve the proper triggering of the correcting propulsion unit.

Abstract translation: 提供了一种用于校正末端引导弹药的轨迹的方法。 为了获得很高的命中率，特别是在爆发（连续射击，快速射击）射击时，规定每个单独的弹药被单独处理。 基于终端引导弹药的梁骑手指导原则执行印记。 每个单独的弹药只读取为该弹药确定的指导梁，并且可以使用附加信息确定其在太空中的绝对滚动姿态，以便正确触发校正推进单元。