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公开(公告)号：US07475625B1
公开(公告)日：2009-01-13
申请号：US11366240
申请日：2006-03-02
IPC分类号： F42C17/04
摘要： A separating device is integrated in ammunition, with which a line is separated at the earliest possible time during a firing process. The separating device is composed mainly of a piston, which preferably has a sharp edge, is guided in a rigidly mounted cylinder, and, in the unloaded state, is positioned by a shear flange. The cable is preferably securely supported in a protective tube which is connected with a propellant charge primer, and in which the cable is guided as far as the tip of the propellant charge primer and is then further guided to the rear end of the projectile. In the upper area of the cylinder, the cable is guided through a bore, which preferably lies transversely to the direction of acceleration of the piston, so that when the piston moves forward, the cable is separated by the sharp edge of the piston.
摘要翻译： 分离装置集成在弹药中，在射击过程中线最早被分开。 分离装置主要由具有尖锐边缘的活塞组成，在刚性安装的气缸中被引导，并且在卸载状态下通过剪切凸缘定位。 电缆优选牢固地支撑在与推进剂充电底漆连接的保护管中，并且其中电缆被引导至推进剂充电底漆的尖端，然后进一步被引导到射弹的后端。 在气缸的上部区域中，电缆被引导通过孔，其优选地横向于活塞的加速度方向，从而当活塞向前移动时，电缆被活塞的锋利边缘分开。
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公开(公告)号：US06454205B2
公开(公告)日：2002-09-24
申请号：US09820892
申请日：2001-03-30
申请人： Torsten Niemeyer , Frank Guischard , Horst Fritsch
发明人： Torsten Niemeyer , Frank Guischard , Horst Fritsch
IPC分类号： F42B1014
CPC分类号： F42B10/20
摘要： A fin-stabilized projectile includes a projectile body having a rear portion defining a rearwardly open cavity and a stabilizing assembly which has an axially slidable fin support in the cavity. The fin support has a retracted position in which the fin support is withdrawn into the cavity and an outwardly shifted position in which the fin support projects from the projectile body. A plurality of fins are pivotally held in the fin support. Each fin has a folded state in which it is withdrawn in the fin support when the latter is in the retracted position and a deployed state in which it is unfolded and extends substantially externally of the fin support when the latter is in its outwardly shifted position. When the projectile has left the weapon barrel, the fin support is axially shifted and the fins move into the deployed state.
摘要翻译： 翅片稳定的射弹包括具有限定向后打开的空腔的后部的射弹体和在空腔中具有可轴向滑动的翅片支撑的稳定组件。 翅片支撑件具有缩回位置，在该缩回位置中，翅片支撑件被抽出到空腔中，并且翅片支撑件从射弹体突出的向外移位的位置。 多个翅片枢转地保持在翅片支撑件中。 每个翅片具有折叠状态，当折边状态处于缩回位置时，其在翅片支撑件中被撤回，并且当展开状态处于其向外移动的位置时，该展开状态展开并且基本上在翅片支撑件的外部延伸。 当抛射体离开武器枪管时，翅片支撑件轴向移动，鳍片进入展开状态。
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公开(公告)号：US20100000436A1
公开(公告)日：2010-01-07
申请号：US12523002
申请日：2008-01-07
摘要： The invention relates to a primer element, in particular for ammunition or similar, comprising at least one primer composition that has at least one sleeve acting as the housing for the primer element, at least one contact pin and a mass contact. Multiple wires, (at least two) are used, one end of said wires being connected to the contact pin and the other end of said wires to the mass contact. The multiple wires are embedded in the primer composition(s).
摘要翻译： 本发明涉及一种底漆元件，特别是用于弹药或类似物，包括至少一种底漆组合物，该底漆组合物具有至少一个用作底漆元件的壳体，至少一个接触销和大量接触的套筒。 使用多条线（至少两条），所述电线的一端连接到接触销，所述电线的另一端连接到质量接触。 多根丝线嵌入底漆组合物中。
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公开(公告)号：US06758435B2
公开(公告)日：2004-07-06
申请号：US10226241
申请日：2002-08-23
申请人： Torsten Niemeyer , Manfred Dieter Schwies , Uwe Naderhoff , Thomas Heitman , Michael Imdahl , Rudolf Rombach
发明人： Torsten Niemeyer , Manfred Dieter Schwies , Uwe Naderhoff , Thomas Heitman , Michael Imdahl , Rudolf Rombach
IPC分类号： F42B1014
CPC分类号： F42B10/14
摘要： A missile includes a missile body and a guide assembly mounted on the missile body. The guide assembly has a plurality of pivots and a plurality of vanes mounted on respective pivots for a swinging motion between a folded position of rest and a deployed flight position. The vanes are arranged for free pivotal motion during flight in response to forces acting thereon to determine the flight position. In the folded position of each vane, its center of gravity is situated at a greater distance from the longitudinal axis of the missile body than the pivotal axis of the respective vanes. Abutments limit the flight position of the vanes to a maximum angle between the length dimension of the vanes and the longitudinal axis of the missile body. The maximum angle is greater than 90°.
摘要翻译： 导弹包括导弹体和安装在导弹体上的引导组件。 引导组件具有多个枢轴和安装在相应枢轴上的多个叶片，用于在折叠的休息位置和展开的飞行位置之间的摆动运动。 叶片被布置成在飞行期间响应于作用在其上的力来自由枢转运动以确定飞行位置。 在每个叶片的折叠位置，其重心位于距导弹体的纵向轴线比相应叶片的枢转轴线更大的距离处。 基台将叶片的飞行位置限制在叶片的长度尺寸和导弹体的纵向轴线之间的最大角度。 最大角度大于90°。
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15.发明授权公开(公告)号：US06314886B1
公开(公告)日：2001-11-13
申请号：US09507728
申请日：2000-02-22
IPC分类号： F42B1014
摘要： A projectile to be fired from a weapon barrel includes a projectile body and a plurality of stabilizing wings circumferentially distributed about a rearward portion of the projectile body. A pin pivotally attaches each stabilizing wing to the projectile body for pivotal motion about a pivot axis to assume a folded state and an outwardly pivoted, deployed state. In the folded state of the stabilizing wings the center of gravity of the respective stabilizing wings is at a greater radial distance from the longitudinal axis of the projectile body than the pivot axis. A gliding body is releasably mounted on each stabilizing wing. Each gliding body has a wing-shaped extension for contacting an inner surface of the barrel in the folded state of the stabilizing wings as the projectile travels in the barrel upon firing. In the deployed state of the stabilizing wings the wing-shaped extensions are exposed, during the flight of the projectile, to an air stream causing the gliding bodies to be stripped from the stabilizing wings.
摘要翻译： 从武器炮发射的射弹包括射弹体和围绕射弹体的后部周向分布的多个稳定翼。 一个销枢转地将每个稳定翼枢转地附接到射弹体，用于围绕枢转轴线枢转运动以呈现折叠状态和向外枢转的展开状态。 在稳定翼的折叠状态下，相应的稳定翼的重心距弹射体的纵向轴线比枢转轴线更大的径向距离。 滑动体可拆卸地安装在每个稳定翼上。 每个滑动体具有翼形延伸部，用于在放射体在射出时在枪管中行进时，在稳定翼的折叠状态下接触枪管的内表面。 在稳定翼的展开状态下，翼形延伸部在弹丸飞行期间暴露于空气流中，导致滑动体从稳定翼剥离。
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