公开(公告)号：US5183962A

公开(公告)日：1993-02-02

申请号：US884141

申请日：1992-05-18

申请人： Klaus D. Karius ,  Armin Eskam ,  Karl-Heinz Vogt

发明人： Klaus D. Karius ,  Armin Eskam ,  Karl-Heinz Vogt

IPC分类号： F42B30/00 ,  F42C19/04

CPC分类号： F42C19/04 ,  F42B30/003

摘要： A submunition unit for a spin stabilized carrier projectile (1), with the submunition unit including an antenna disposed at the nose of its casing (7), and with the antenna (5) being covered by a protective cover (6). The casing (7) and the protective cover (6) are provided with respective axially overlapping collars (8, 9) which are each provided with respective opposed circumferential grooves (14, 15) to form an annular recess to accommodate an elastic securing ring (16). The securing ring, which is normally positioned within the innermost of the circumferential grooves, expands under the influence of centrifugal forces to connect the casing and protective cover together in a form-locking manner.

摘要翻译： 一种用于自旋稳定的载体射弹（1）的子弹药单元，子弹药单元包括设置在其壳体（7）的鼻部处的天线，并且天线（5）被保护盖（6）覆盖。 壳体（7）和保护盖（6）设置有相应的轴向重叠的轴环（8,9），每个轴环重叠的轴环（8,9）分别设置有相应的相对的周向槽（14,15），以形成环形凹部以容纳弹性固定环（ 16）。 通常位于圆周槽的最内侧的固定环在离心力的影响下膨胀，从而将壳体和保护罩以形状锁定的方式连接在一起。

公开(公告)号：US5210372A

公开(公告)日：1993-05-11

申请号：US899843

申请日：1992-06-17

申请人： Peter Tripptrap ,  Karl-Heinz Vogt ,  Klaus D. Karius

发明人： Peter Tripptrap ,  Karl-Heinz Vogt ,  Klaus D. Karius

IPC分类号： F42B12/62

CPC分类号： F42B12/62

摘要： An arrangement for ejecting objects from a projectile, includes a hollow projectile body having a nose end with a plurality of objects disposed in a column within the projectile body. An ejection charge is disposed within the projectile body at the nose end. An ejection device including a hood enclosing a cavity is ejectably disposed within the projectile body between the ejection charge and the column. The hood has a wall with an opening facing the ejection charge so that, after ignition of the ejection charge, resulting powder gases enter into the cavity through the opening to generate a gas pressure between the hood and the adjacent object and simultaneously exert a force on an exterior portion of the wall of the hood that causes the hood and the column to be ejected from the tail end of the projectile body, whereby the hood separates from the column once the hood and column are free of the projectile due to the pressure in the cavity.

摘要翻译： 用于从抛射体喷射物体的装置包括具有鼻端的中空射弹体，其具有设置在射弹体内的柱中的多个物体。 喷射装置在鼻端处设置在射弹体内。 包括封闭空腔的罩的喷射装置可弹射地设置在喷射装置和列之间的射弹体内。 罩具有面向喷射装料的开口的壁，使得在点燃充电之后，所得到的粉末气体通过开口进入空腔，以在罩和相邻物体之间产生气体压力，同时施加力 罩的壁的外部部分，其使得罩和柱从射弹体的尾端弹出，由此，一旦发动机罩和立柱由于压力而没有弹丸，则罩与柱分离 空腔。

公开(公告)号：US5233126A

公开(公告)日：1993-08-03

申请号：US898531

申请日：1992-06-15

申请人： Karl-Heinz Vogt ,  Heinz Olmscheid ,  Klaus-Dietmar Karius

发明人： Karl-Heinz Vogt ,  Heinz Olmscheid ,  Klaus-Dietmar Karius

IPC分类号： F42B10/50

CPC分类号： F42B10/50

摘要： A deceleration device for a submunition unit ejectable from a spin stabilized carrier projectile includes a deployable deceleration element. The deceleration element is packaged in textile package including an essentially circular disc, at least three straps connected and arranged radially to the disc, with each strap having a free end and provided with a loop and a closing line received through the loops for pulling the loops together to close the package about the deceleration element. An activation line is connected to the closing line and held by the textile package for releasing the closing line for allowing the package to open for deployment of the deceleration element after the activation line is released from the package by being stretched in a controlled manner.

摘要翻译： 用于从自旋稳定的载体抛射体喷射的子弹药单元的减速装置包括可展开的减速元件。 减速元件包装在纺织品包装中，包括基本上圆形的盘，至少三个带子连接并径向设置在盘上，每个带子具有自由端，并且设置有环和通过环接收的闭合线，用于拉环 一起关闭减速元件的包装。 活动线连接到关闭线并由纺织品包装件保持，用于释放闭合线，以通过以受控的方式拉伸活化线从包装中释放之后允许包装部件打开以展开减速元件。

公开(公告)号：US5237925A

公开(公告)日：1993-08-24

申请号：US897053

申请日：1992-06-11

申请人： Karl-Heinz Vogt ,  Heinz Olmscheid

发明人： Karl-Heinz Vogt ,  Heinz Olmscheid

IPC分类号： F42B10/50

CPC分类号： F42B10/50

摘要： A deceleration element is provided for attachment to a tail end of a submunition unit for deployment when the submunition unit is ejected from a spin stabilized carrier projectile for reducing velocity and spin of the submunition unit. The deceleration element includes two approximately circular, air-tight, planar textile fabric layers of essentially the same size having a diameter exceeding the diameter of the submunition unit and circumferentially sewn together to form an inflatable interior between the two fabric layers. The fabric layer disposed closest to the tail end of the submunition unit is clamped by fasteners to the tail end of the submunition unit and has a front side facing the tail end of the submunition unit for encountering air when the deceleration unit is deployed. At least four air capture pockets are disposed at the front side of the one fabric layer and are distributed at regular intervals in a circumferential direction. At least one air inlet opening is provided in the one fabric layer leading to the inflatable interior between the two fabric layers and is disposed in the region of at least one of the air pockets.

摘要翻译： 当亚弹药单元从自旋稳定的载体抛射体喷出以减少子弹药单元的速度和旋转时，提供减速元件用于附接到用于展开的子弹药单元的尾端。 减速元件包括两个基本上相同尺寸的大致圆形的气密的平面织物层，其直径超过子弹药单元的直径并且周向地缝合在一起以在两个织物层之间形成可充气的内部。 最靠近子弹药单元尾端布置的织物层通过紧固件夹紧到子弹药单元的尾端，并且具有面向子弹药单元的尾端的前侧，用于当减速单元展开时遇到空气。 至少四个空气捕获袋设置在一个织物层的前侧，并且沿周向以规则的间隔分布。 至少一个空气入口开口设置在一个织物层中，导致两个织物层之间的可充气内部，并且设置在至少一个气穴的区域中。

公开(公告)号：US5199669A

公开(公告)日：1993-04-06

申请号：US922230

申请日：1992-07-31

申请人： Karl-Heinz Vogt ,  Heinz Olmscheid

发明人： Karl-Heinz Vogt ,  Heinz Olmscheid

IPC分类号： B64D17/14

CPC分类号： B64D17/14

摘要： A rotary parachute includes a canopy having an apex and comprised of triangular, sewn-together fabric segments each having a base edge along an outer circumference of the canopy, a tip opposite the base edge and longitudinal edges on either side of said tip with seams connecting together the adjacent longitudinal edges of adjacent segments and rotation slits existing in regions of the respective seams. The tip of each segment is offset laterally from the apex of the canopy to form an apex opening in the canopy having a shape of a regular polygon and the base edges are offset from one another so that each segment has a circumferentially projecting tip.

摘要翻译： 旋转降落伞包括具有顶点的顶盖，其包括三角形缝合的织物片段，每个织物片段沿着顶盖的外圆周具有基部边缘，与基部边缘相对的尖端以及在所述尖端的任一侧上的纵向边缘， 将相邻段的相邻纵向边缘和存在于各个接缝的区域中的旋转狭缝组合在一起。 每个段的尖端从顶盖的顶点横向偏移，以在冠层中形成具有正多边形形状的顶点开口，并且基部边缘彼此偏移，使得每个段具有周向突出的尖端。

公开(公告)号：US5253588A

公开(公告)日：1993-10-19

申请号：US900132

申请日：1992-06-18

申请人： Karl-Heinz Vogt ,  Heinz Olmscheid

发明人： Karl-Heinz Vogt ,  Heinz Olmscheid

IPC分类号： F42B10/54 ,  F42B10/14

CPC分类号： F42B10/54

摘要： A device is provided for reducing the rate of rotation of a spinning submunition unit having a tail end provided with a deployable braking device, from a time after the submunition unit is ejected from a spin stabilized carrier projectile until the braking device is deployed. The device includes a plurality of bands arranged to form a star-shaped symmetrical band structure for placement around the braking device. Each of the bands has a free end provided with a wind pocket.

摘要翻译： 提供一种装置，用于从子弹药单元从旋转稳定的载体抛射体喷射直到制动装置展开之后的时间，降低具有设置有可展开制动装置的尾端的旋转子弹药单元的旋转速度。 该装置包括布置成形成用于放置在制动装置周围的星形对称带结构的多个带。 每个乐队都有一个带有风口的自由端。

公开(公告)号：US5239927A

公开(公告)日：1993-08-31

申请号：US899870

申请日：1992-06-17

申请人： Gunter Frye ,  Karl-Heinz Vogt ,  Volker Bartels

发明人： Gunter Frye ,  Karl-Heinz Vogt ,  Volker Bartels

IPC分类号： F42B10/48 ,  F42B10/56

CPC分类号： F42B10/56 ,  F42B10/48

摘要： A deceleration device for a submunition unit includes a cartridge releasably attached to the submunition unit. A releasable package including at least one pocket is disposed in the cartridge and is connected to the cartridge by a packaging line. An auxiliary parachute and a rotation parachute are disposed in the cartridge, with at least the rotation parachute being accommodated in the at least one pocket of the releasable package and the auxiliary parachute being disposed in a pocket separate from the at least one pocket. The auxiliary parachute is connected to the cartridge and the rotation parachute is connected to the submunition unit. A deployment mechanism causes the auxiliary parachute to be deployed in advance of the rotation parachute after the cartridge is released from the submunition unit and the rotation parachute to be deployed after the cartridge is decelerated by the auxiliary parachute for decelerating the submunition unit.

摘要翻译： 用于子弹药单元的减速装置包括可释放地附接到子弹药单元的盒。 包括至少一个口袋的可释放包装被设置在盒中并且通过包装线与盒连接。 辅助降落伞和旋转降落伞设置在盒中，至少旋转降落伞容纳在可释放包装的至少一个袋中，并且辅助降落伞设置在与所述至少一个袋分离的口袋中。 辅助降落伞连接到墨盒，旋转降落伞连接到子弹药单元。 一个展开机构使辅助降落伞在旋转降落伞之前被放置在弹药盒从子弹药单元释放之后，并且在弹药筒被辅助降落伞减速以使子弹药单元减速之后被部署。