会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 1. 发明授权
    • Ammunition, especially programmable large-caliber ammunition
    • 弹药,特别是可编程的大口径弹药
    • US07475625B1
    • 2009-01-13
    • US11366240
    • 2006-03-02
    • Torsten NiemeyerJoachim KuhnleRainer HimmertWolfgang Mosig
    • Torsten NiemeyerJoachim KuhnleRainer HimmertWolfgang Mosig
    • F42C17/04
    • F42B5/08F42C19/06
    • 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.
    • 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。
    • 4. 发明授权
    • Cartridge
    • 墨盒
    • US06725781B2
    • 2004-04-27
    • US10394581
    • 2003-03-24
    • Torsten NiemeyerThomas HeitmannRupert ReinstadlerMichael VagedesFrank SchötzigRainer Himmert
    • Torsten NiemeyerThomas HeitmannRupert ReinstadlerMichael VagedesFrank SchötzigRainer Himmert
    • F42B508
    • F42B5/181F42B5/02F42C19/0826
    • 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.
    • 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。
    • 6. 发明申请
    • AMMUNITION, ESPECIALLY PROGRAMMABLE LARGE-CALIBER AMMUNITION
    • 弹药,特别是可编程的大校准弹药
    • US20080314235A1
    • 2008-12-25
    • US11366240
    • 2006-03-02
    • Torsten NiemeyerJoachim KuhnleRainer HimmertWolfgang Mosig
    • Torsten NiemeyerJoachim KuhnleRainer HimmertWolfgang Mosig
    • F42C17/04
    • F42B5/08F42C19/06
    • 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.
    • 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。
    • 7. 发明授权
    • Method and apparatus for conveying a large-calibre payload over an
operational terrain
    • 用于在操作地形上传送大口径有效载荷的方法和装置
    • US5760330A
    • 1998-06-02
    • US811687
    • 1997-03-05
    • Rainer HimmertAlfred EckelGunther ThurnerHarald Wich
    • Rainer HimmertAlfred EckelGunther ThurnerHarald Wich
    • F42B10/56F42B12/62
    • F42B12/62F42B10/56
    • A delivery apparatus (11) for full-calibre submunitions or the like payloads (12) which are coaxially stacked in its load space (19) results in a system which operates in a fault-free manner when, for ejecting the payloads (12), detachment of the load space (19) from the rocket motor (17) disposed therebehind and detachment of the ogive (14) from the opposite end of the load space (19) are each promoted by a pyrotechnic charge (28, 31), with the load space (19) being braked as a result of being positioned transversely beside the trajectory (26) of the separated motor (17) which flies further along the trajectory and past the load space in a stable configuration and with the load space (19) only then being turned by a braking parachute (23) connected to its end (22). The load space tail (18) which thereafter then faces forwardly in the direction of flight is opened by detachment of a cover (25) and the load space (19) is pulled away from the payload stack (12--12) by means of the braking parachute (23).
    • 同轴地堆叠在其负载空间(19)中的用于全口径子弹药等的有效载荷(12)的输送装置(11)产生一个以无故障的方式工作的系统,用于弹出有效载荷(12) 负载空间(19)与从装载空间(19)的相对端分离并分离的火箭发动机(17)的装载空间(19)分别由烟火装置(28,31)驱动, 其中所述负载空间(19)由于被横向地位于所述分离的马达(17)的轨迹(26)旁边而被制动,所述马达(17)沿着所述轨迹进一步飞行,并且以稳定的结构和所述载荷空间( 19)仅由连接到其端部(22)的制动降落伞(23)转动。 之后,其后面朝向飞行方向的负载空间尾部(18)通过拆卸盖(25)而打开,并且通过所述负载空间尾部(18)将负载空间(19)从有效载荷堆叠(12-12)拉出, 制动降落伞(23)。