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：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：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。