公开(公告)号：US4722282A

公开(公告)日：1988-02-02

申请号：US937029

申请日：1986-11-10

申请人： Reinhard Synofzik ,  Rolf Hellwig

发明人： Reinhard Synofzik ,  Rolf Hellwig

IPC分类号： F42B23/00 ,  F42C1/14 ,  F42C15/42 ,  H01Q1/08 ,  H01Q1/12 ,  H01Q1/28 ,  F42B11/18 ,  F42B11/00

CPC分类号： F42C15/42 ,  F42C1/14 ,  H01Q1/081 ,  H01Q1/1235 ,  H01Q1/281

摘要： A payload-carrying projectile 1 includes a sensor 16 and a sensor carrier 15 disposed in a launch-resistant manner in a recess 14 in the tail section 11 of the projectile 1. After impact of the projectile, which is stabilized by extendable vanes 12, in the target area, where it may penetrate the ground as necessary, the object is to deploy the sensor from its protected position inside the projectile 1and to place it as high as possible above the surface of the ground. For this purpose, the sensor 16 is connected with a concertina bellows 15 which for its part leads into a reservoir 13a which is disposed in the projectile, and which is filled with polyurethane foam mixed with a propellant gas under high pressure. The connection of the reservoir 13 with the concertina bellows 15 is made via a valve 13c which is regulated by an electronic control element 13a containing, for instance, a timer switch. After the opening of the valve 13 c the polyurethane foam 17 enters the concertina bellows 15 and expands it, thereby expelling the sensor 16 from the recess 14. Finally, the polyurethane foam 17 hardens, so that the now extended concertina bellows 15 provides a safe support for the deployed sensor 16.

摘要翻译： PCT No.PCT / EP86 / 00043 Sec。 371日期：1986年11月10日 102（e）1986年11月10日日期PCT提交1986年1月31日PCT公布。 出版物WO86 / 05266 日期：1986年9月12日。有载荷的弹丸1包括传感器16和传感器载体15，传感器载体15以防弹的方式设置在射弹1的尾部11中的凹部14中。在射弹的撞击之后 通过在目标区域中的可延伸叶片12稳定，其中它可以根据需要穿透地面，目的是将传感器从其被保护的位置部署在射弹1内部并且将其尽可能高地放置在地面以上。 为此目的，传感器16与手风琴波纹管15连接，该波纹管15的一部分导入设置在射弹中的储存器13a，并且在高压下填充有与推进剂气体混合的聚氨酯泡沫。 储存器13与三角波箱波纹管15的连接通过阀13c制成，阀13c由包含例如定时开关的电子控制元件13a调节。 在阀13c打开之后，聚氨酯泡沫17进入三分音箱波纹管15并使其膨胀，从而将传感器16从凹槽14排出。最后，聚氨酯泡沫17硬化，使得现在伸展的三角裤波纹管15提供安全 对部署的传感器16的支持。

公开(公告)号：US4854241A

公开(公告)日：1989-08-08

申请号：US135509

申请日：1987-12-16

申请人： Reinhard Synofzik ,  Rolf Hellwig ,  Klaus D. Karius

发明人： Reinhard Synofzik ,  Rolf Hellwig ,  Klaus D. Karius

IPC分类号： F42B12/58 ,  F42B10/50 ,  F42B30/00

CPC分类号： F42B30/003

摘要： A spin stabilized carrier projectile comprising: a projectile body having a rear end; at least one submunition projectile disposed in, and ejectable from, the projectile body; and a projectile bottom disposed at, and ejectable from, the rear end of the projectile body, the projectile bottom having a side surface facing the submunition projectile and containing a recess, and a folded, expandable deceleration element for reducing the velocity and spin of the projectile bottom upon ejection from the projectile body, the deceleration element including a sheet of material fastened in the recess for producing air resistance, and the deceleration element being deployable from a folded condition to an expanded condition with the aid of rotation of the projectile bottom.

摘要翻译： 一种自旋稳定的载体抛射体，包括：具有后端的射弹体; 至少有一个子弹药弹放置在射弹体内并可从弹丸体中排出; 以及设置在射弹体的后端并且可从弹丸体的后端排出的射弹底部，射弹底部具有面向子弹丸的侧面并且容纳凹部，以及折叠的可扩张的减速元件，用于降低弹丸的速度和旋转 所述减速元件包括紧固在所述凹部中的用于产生空气阻力的材料片，并且所述减速元件可借助于所述抛射体底部的旋转而从折叠状态展开至膨胀状态。

公开(公告)号：US4589340A

公开(公告)日：1986-05-20

申请号：US573343

申请日：1984-01-24

申请人： Rolf Hellwig ,  Jens Seidensticker ,  Klaus D. Karius

发明人： Rolf Hellwig ,  Jens Seidensticker ,  Klaus D. Karius

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

CPC分类号： G01B5/0004 ,  F16M11/046 ,  F16M11/40 ,  F16M13/005 ,  F16M2200/047

摘要： 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.

摘要翻译： 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：US4342262A

公开(公告)日：1982-08-03

申请号：US772550

申请日：1977-02-22

申请人： Rudolf Romer ,  Rolf Hellwig ,  Dietmar Karius

发明人： Rudolf Romer ,  Rolf Hellwig ,  Dietmar Karius

IPC分类号： F42B12/58 ,  F42B13/50

CPC分类号： F42B12/58

摘要： A subcaliber missile to be launched from a barrel, in order to serve as a carrier for satellite missiles of other ejectable bodies, has an envelope divided into two half-shells of tapering configuration which are articulated to the missile bottom and are held together by a missile head and by internal partitions separating the ejectable bodies from one another. When the missile is in flight, the ejection of the head by the detonation of a charge exerts a backward reaction force upon the envelope, causing its load to move forward therein whereby the partitions are disengaged from the two half-shells and allow them to flip apart. The half-shells are provided with slots for a recessed tail-wing assembly and with back fins which, like the missile bottom, conform to the caliber of the barrel.

摘要翻译： 从桶中发射的亚纲导弹，为了作为其他可弹性体的卫星导弹的载体，具有被分成两个锥形构型的半壳，其被铰接到导弹底部并且被一个 导弹头和通过将可弹出体彼此分开的内部分隔。 当导弹处于飞行状态时，通过引爆引爆头部弹出一个反向的反作用力到外壳上，导致其载荷向前移动，从而隔板与两个半壳脱离并允许它们翻转 分开 半壳设置有用于凹陷的尾翼组件的槽，并且具有与导弹底部一致的背部翅片符合筒的口径。

公开(公告)号：US4119037A

公开(公告)日：1978-10-10

申请号：US746837

申请日：1976-12-02

申请人： Rudolf Romer ,  Rolf Hellwig ,  Dietmar Karius

发明人： Rudolf Romer ,  Rolf Hellwig ,  Dietmar Karius

IPC分类号： F42B12/62 ,  F42B13/50

CPC分类号： F42B12/62

摘要： A versatile carrier projectile for receiving and ejecting differently-sized ejectable payloads such as guided missiles and incendiary bombs is described. The payloads are disposed in successive, longitudinally spaced relation within a central cylindrical body of the projectile, with successive ones of the payloads being separated by a spacer disc. Each spacer disc carries an outwardly biased blocking rod. The outer end of each blocking rod terminates in engagement with a sawtooth-shaped groove on the inner periphery of the cylindrical body, so that the forward propulsion of the successive payloads through the cylindrical body is accomplished under a steady spring load of the blocking member on the inner wall of the cylindrical body. The front and rear portions of the cylindrical body are respectively secured to the shell head and the ignition charge container by shear pins. Other shear pins are provided to secure a drive disc to the rear portion of the ignition charge container, and a flange extending forwardly from the outer surface of the drive disc serves to normally confine the pivoted rear ends of a plurality of stabilizing wings in their retracted position until the projectile exits from the barrel of the firing weapon.

摘要翻译： 描述了用于接收和弹出不同尺寸的可弹出有效载荷（例如导弹和燃烧弹）的通用载体抛射体。 有效载荷在射弹的中心圆柱体内以连续的纵向间隔的关系设置，其中有效载荷的连续的一个由隔离盘隔开。 每个间隔盘带有向外偏置的阻挡杆。 每个阻挡杆的外端终止于圆柱体的内周上的锯齿形凹槽接合，使得连续有效载荷通过圆柱体的向前推进是在阻挡构件的稳定弹簧载荷下实现的 圆柱体的内壁。 圆柱体的前部和后部分别通过剪切销固定到壳体头部和点火充电容器上。 提供其他剪切销以将驱动盘固定到点火充电容器的后部，并且从驱动盘的外表面向前延伸的凸缘用于通常将多个稳定翼的枢转后端限制在其缩回 直到射弹从射击武器的枪管离开。