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公开(公告)号：US06725781B2
公开(公告)日：2004-04-27
申请号：US10394581
申请日：2003-03-24
申请人： Torsten Niemeyer , Thomas Heitmann , Rupert Reinstadler , Michael Vagedes , Frank Schötzig , Rainer Himmert
发明人： Torsten Niemeyer , Thomas Heitmann , Rupert Reinstadler , Michael Vagedes , Frank Schötzig , Rainer Himmert
IPC分类号： F42B508
CPC分类号： F42B5/181 , F42B5/02 , F42C19/0826
摘要： A cartridge, comprising a cartridge case (3), a projectile (4), a propellant charge igniter (8) extending in the direction of the longitudinal axis of cartridge (1) and arranged inside the cartridge case (3), and an electrically programmable projectile fuse arranged in the projectile (4) and connected via at least one electrical line (110) to an electrode on the cartridge base (2). The cartridge case (3) comprises at least two case sections (5, 6) with at least one separation location in the region between the front end (7) of the propellant charge igniter (8) and the projectile tail (9) for the installation of a section of the electrical line (110) between the cartridge base (2) and the projectile fuse using two rotating connector assemblies, one of which turns more easily than the other. One of the rotating connector assemblies is positioned on the propellant charge igniter and provided with a connection to the electrical line section that is oriented at an angle to the axis of rotation of the rotating connector assembly.
摘要翻译： 一种盒，包括盒壳体（3），射弹（4），沿盒（1）的纵向轴线方向延伸并布置在盒壳体（3）内的推进剂充电点火器（8） 布置在射弹（4）中并通过至少一条电线（110）连接到墨盒底座（2）上的电极的可编程弹珠熔丝。 所述盒壳体（3）包括至少两个壳体部分（5,6），所述壳体部分在所述推进剂充电点火器（8）的前端（7）和所述射弹尾部（9）之间的区域中具有至少一个分离位置，用于 使用两个旋转连接器组件在盒基座（2）和射弹保险丝之间安装电线（110）的一部分，其中之一比另一个容易转动。 旋转连接器组件中的一个定位在推进剂充电点火器上并且设置有与电线部分的连接，该电线部分以与旋转连接器组件的旋转轴线成一定角度定向。
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公开(公告)号：US06408764B1
公开(公告)日：2002-06-25
申请号：US09664069
申请日：2000-09-18
申请人： Thomas Heitmann , Torsten Niemeyer
发明人： Thomas Heitmann , Torsten Niemeyer
IPC分类号： F42B518
摘要： A case base (1; 1′) for large-caliber ammunition, in which the case jacket (2) comprises a combustible material, with the case base (1; 1′) comprising a metallic base plate (3) and a support ring (4; 4′) that projects axially beyond the surface of the base plate (3) at its edge, and an elastomer or thermoplastic obturation ring (5; 5′) that is disposed on the projectile side of the support ring (4; 4′). In order for the obturation ring (5; 5′) to be secured simply to the support ring (4; 4′) and removed again after the ammunition has been fired, the support ring (4; 4′) has, on its inner surface (6) facing the obturation ring (5; 5′), a groove-shaped undercut (7), into which the end (8) of the obturation ring (5; 5′) that faces the support ring (4; 4′) extends with a form-fit and/or positive lockup.
摘要翻译： 一种用于大口径弹药的壳体底座（1; 1'），其中所述壳体护套（2）包括可燃材料，所述壳体基部（1; 1'）包括金属基板（3）和支撑环 （4; 4'），其在其边缘处轴向突出超过所述基板（3）的表面;以及弹性体或热塑性密封环（5; 5'），其设置在所述支撑环（4; 4'）。 为了将密封环（5; 5'）简单地固定到支撑环（4; 4'）上，并且在弹药被击发之后再次被移除，支撑环（4; 4'）在其内部 面对密封环（5; 5'）的表面（6），槽形底切（7），所述密封环（5; 5'）的端部（8）面向支撑环（4; 4） '）随着形式适配和/或积极的锁定而延伸。
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3.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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公开(公告)号：US4951572A
公开(公告)日：1990-08-28
申请号：US461276
申请日：1990-01-05
申请人： Jurgen Bocker , Hans Orth , Torsten Niemeyer , Peter Tripptrap
发明人： Jurgen Bocker , Hans Orth , Torsten Niemeyer , Peter Tripptrap
IPC分类号： F42B1/02
CPC分类号： F42B1/02
摘要： A warhead for enclosing an explosive charge includes a casing for surrounding the charge. The casing has an end presenting a frontal face. A liner having a circumferential area for attachment to the end of the casing and a coefficient of thermal expansion .alpha..sub.R is fastened to the casing by way of an intermediate ring connected to the circumferential area of the liner. The intermediate ring has a portion which is brought around the frontal face of the casing and which has a pressure face which presses against the exterior of the casing. The liner has a coefficient of thermal expansion .alpha..sub.E which is at least as great as the coefficient of thermal expansion .alpha..sub.R of the intermediate ring.
摘要翻译： 用于封装爆炸物的弹头包括用于围绕电荷的壳体。 外壳具有呈现正面的端部。 具有用于附接到壳体的端部的圆周区域和热膨胀系数αR的衬套通过连接到衬套的圆周区域的中间环固定到壳体。 中间环具有围绕壳体的前表面的部分，并且具有压靠壳体外部的压力面。 衬里的热膨胀系数αE至少与中间环的热膨胀系数αR一样大。
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公开(公告)号：US08037825B2
公开(公告)日：2011-10-18
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：US20080314235A1
公开(公告)日：2008-12-25
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：US08336458B2
公开(公告)日：2012-12-25
申请号：US12495912
申请日：2009-07-01
CPC分类号： F42C19/06 , Y10T29/49002
摘要： A projectile in which the metallic base body itself is used as a ground wire and only the signal line is passed through the inside of the base body so that it is insulated by a suitable bore of the base body. The signal line is insulated from the ground wire by a coating of an electrically insulating material applied to the base body, before the signal line is introduced into the bore. The two ends of the signal line are provided with connecting contacts, which preferably can be screwed at least partially into the base body and are mounted in such a way that they are insulated from the base body. To allow contacting of the ground wire, which is formed by the base body itself, the front end and the rear end of the base body are provided with coating-free blind bores.
摘要翻译： 使用金属基体本身作为接地线的射弹，只有信号线通过基体的内部，使其通过基体的合适的孔绝缘。 在信号线被引入孔内之前，信号线通过施加到基体的电绝缘材料的涂层与接地线绝缘。 信号线的两端设置有连接触点，其优选地可以至少部分地拧入基体中并且以使得它们与基体绝缘的方式安装。 为了允许由基体本身形成的接地线与基体的前端和后端的接触设置有无涂层的盲孔。
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公开(公告)号：US08297189B2
公开(公告)日：2012-10-30
申请号：US12619543
申请日：2009-11-16
申请人： Wolfgang Hoffmann , Wolfgang Scherge , Mathias Lengnick , Holger Brase , Stefan Kell , Torsten Niemeyer
发明人： Wolfgang Hoffmann , Wolfgang Scherge , Mathias Lengnick , Holger Brase , Stefan Kell , Torsten Niemeyer
IPC分类号： F42B99/00
CPC分类号： F42C19/02 , F42B12/207
摘要： The invention relates to so-called fuze damping in projectiles, in particular, those provided with a built-in firing delay. Thus, a projectile (1) is provided having a rear part (1a) and a fuze (2), wherein at least one damping element (7) is inserted between a fuze base (5) and the projectile (1) and/or between a fuze shoulder (6) and a possible threaded ring (4), or similar attachment element. The damping element (7) is in the form of a disc, ring or pot, and is composed of a material with a lower acoustic impedance than the material of the projectile (1).
摘要翻译： 本发明涉及射弹中的所谓引信阻尼，特别涉及具有内置点火延迟的引信阻尼。 因此，提供具有后部（1a）和引信（2）的射弹（1），其中至少一个阻尼元件（7）插入在引信基座（5）和射弹（1）之间和/或 在引信肩部（6）和可能的螺纹环（4）之间，或类似的附接元件。 阻尼元件（7）呈盘形，环形或罐状，并且由具有比射弹（1）的材料低的声阻抗的材料组成。
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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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