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    • 2. 发明授权
    • Propellant charge igniter
    • 推进剂充电点火器
    • US5895881A
    • 1999-04-20
    • US904833
    • 1997-08-01
    • Stefan ThiesenManfred LubbenDieter Jungbluth
    • Stefan ThiesenManfred LubbenDieter Jungbluth
    • F42C19/08
    • F42C19/0826
    • A propellant charge igniter for cartridge ammunition, includes an ignition tube; and a transfer charge disposed within the ignition tube, wherein the ignition tube is composed of a jacket tube having defined therein a plurality of ignition openings; and a protective tube which is positioned within the jacket tube so that the outside wall of the protective tube rests flush against the inside wall of the jacket tube and covers the plurality of ignition openings, which is thin-walled and has a wall thickness ranging from 0.1 mm to 0.8 mm, which is arranged to effectively protect the transfer charge against adverse external environmental influences including humidity, and which is comprised of a material selected from the group consisting of glass, oxide ceramic material, glass ceramic material, metal or metal alloy, and plastic. This arrangement provides a reliable sealing of the transfer charge against external environmental influences over a long time period, e.g., at least 10 years, even if handled roughly.
    • 用于弹药的推进剂充电点火器包括点火管; 以及设置在所述点火管内的转移电荷,其中所述点火管由其中限定有多个点火开口的护套组成; 以及保护管,其位于护套管内,使得保护管的外壁与套管的内壁平齐地抵靠,并且覆盖多个点火开口,该点火开口是薄壁的,并且具有从 0.1mm至0.8mm,其被设置为有效地保护转印电荷免受包括湿度在内的不利外部环境影响,并且由选自玻璃,氧化物陶瓷材料,玻璃陶瓷材料,金属或金属合金的材料组成 ,和塑料。 这种安排即使大致处理,也可以在长时间内(例如至少10年)内提供转移电荷对外部环境影响的可靠密封。
    • 3. 发明授权
    • Ammunition unit
    • 弹药单位
    • US5335599A
    • 1994-08-09
    • US980197
    • 1992-11-20
    • Stefan ThiesenEckhard Rahnenfuhrer
    • Stefan ThiesenEckhard Rahnenfuhrer
    • F42B5/16F42B5/18F42B5/02
    • F42B5/181F42B5/16F42C19/0826Y10S102/70
    • A performance enhanced ammunition unit composed of a front ammunition component (1) and a rear ammunition component (2) which each include a combustible propelling charge casing (7, 12), with the rear ammunition component being filled with propelling charge powder that has been compressed into a compressed member (15). The rear ammunition component (2) has a casing bottom (13) which accommodates a bottom igniter (14) and the compressed member (15) accommodates a combustible ignition tube (16) for the propelling charge igniter (16, 17), with the combustible tube 16 being in operative engagement with the bottom igniter (14) and extending along substantially the entire axis of the bottom component. Both ammunition components (1, 2) are separated by a combustible disk (18), the front ammunition member (1) is filled in its cylindrical section (8) filled with powder rods (10) and in its section (a) ahead of the powder rods with bulk propelling charge powder (11).
    • 一个由前弹药部件(1)和后弹药部件(2)组成的性能增强的弹药单元,每个弹药部件(2)各自包括可燃推进装药套管(7,12),后弹药部件被填充有已经被 压缩成压缩构件(15)。 后弹药部件(2)具有容纳底部点火器(14)的壳体底部(13),并且压缩构件(15)容纳用于推进充电点火器(16,17)的可燃点火管(16),其中 可燃管16与底部点火器(14)操作接合并且沿着底部部件的大致整个轴线延伸。 两个弹药部件(1,2)由可燃盘(18)分开,前弹药构件(1)填充在其中装满粉棒(10)的圆柱形部分(8)中,并且在其部分(a)之前 粉末棒带散装粉末(11)。
    • 4. 发明授权
    • Process of producing a propellant charge igniter
    • 生产推进剂充电点火器的过程
    • US06302008B1
    • 2001-10-16
    • US09145547
    • 1998-09-02
    • Manfred LübbenStefan ThiesenKlaus Unterstein
    • Manfred LübbenStefan ThiesenKlaus Unterstein
    • C06C702
    • F42C19/0826
    • A process of producing a propellant charge igniter for cartridge ammunition of the type including an ignition tube with a booster charge, wherein the ignition tube is composed of a sheathing tube (4) with ignition openings (3) and a thin-walled protective tube (6) which is arranged inside the sheathing tube (4) in order to protect the booster charge, and wherein the external wall of the protective tube fits against the internal wall of the sheathing tube (4) and covers the ignition openings (3). To avoid microscopic gaps between the sheathing tube and the protective tube, which gaps influence the performance of the propellant charge igniter, a paste-like sealing agent (5) is introduced into the sheathing tube (4) before the protective tube (6) is inserted into the sheathing tube (4), and only then is the protective tube (6) inserted into the sheathing tube (4) to displace the sealing agent. Alternatively with the protective tube (6) being fully inserted, the ignition openings (3) in the sheathing tube (4) are filled with a sealing agent (5) and then the protective tube (6) as well as the sheathing tube (4) are moved axially, relative to each other.
    • 一种制造用于包括具有增压剂的点火管的类型的弹药的推进剂充电点火器的过程,其中点火管由具有点火开口(3)和薄壁保护管(3)的护套管(4)组成, 6),其设置在护套管(4)的内部,以保护增压装置,并且其中保护管的外壁与护套管(4)的内壁相配合并覆盖点火开口(3)。 为了避免护套管和保护管之间的微小间隙,这些间隙影响推进剂电荷点火器的性能,在保护管(6)为保护管(6)之前,将糊状密封剂(5)引入护套管(4) 插入护套管(4)中,只有插入护套管(4)中的保护管(6)才能移动密封剂。 或者,保护管(6)被完全插入,护套管(4)中的点火开口(3)填充有密封剂(5),然后保护管(6)以及护套管(4) )相对于彼此轴向移动。
    • 5. 发明授权
    • Weapon system
    • 武器系统
    • US6067890A
    • 2000-05-30
    • US61267
    • 1998-04-17
    • Stefan ThiesenHelmut OrtmannJurgen BockerDieter Jungbluth
    • Stefan ThiesenHelmut OrtmannJurgen BockerDieter Jungbluth
    • F41G3/04F41G3/08
    • F41G3/04
    • A weapon system (1) having a weapon (2) with a weapon tube (3) and having an electronic system (4) for generating aiming signals for an aiming system (7) connected to the weapon (2). To ensure that the current weapon properties or tube properties are also considered in a simple manner for the determination of the aiming signals, the respective weapon-specific data are stored on a chip card (13) associated with the weapon (2) and are transferred via a chip card reader (11) to the corresponding electronic system (4) required for the determination of the aiming signals. During this process, the weapon-specific data are updated on the chip card at predetermined time intervals.
    • 一种具有武器(2)的武器系统(1),具有武器管(3)并具有电子系统(4),用于产生与武器(2)连接的瞄准系统(7)的瞄准信号。 为了确保目前的武器属性或管属性也以简单的方式考虑用于确定瞄准信号,相应的武器专用数据被存储在与武器(2)相关联的芯片卡(13)上并被传送 通过芯片读卡器(11)到确定瞄准信号所需的相应的电子系统(4)。 在该过程中,武器专用数据以预定的时间间隔在芯片卡上更新。
    • 6. 发明授权
    • Weapon system
    • 武器系统
    • US6085629A
    • 2000-07-11
    • US061338
    • 1998-04-17
    • Stefan ThiesenJurgen BockerHelmut OrtmannDieter Jungbluth
    • Stefan ThiesenJurgen BockerHelmut OrtmannDieter Jungbluth
    • F41G3/04F41G3/08B64D1/04
    • F42B35/00F41G3/04F41G3/08
    • A weapon system includes a weapon having a chamber; a data input device; an aiming mechanism; and an ammunition unit that can be fired with the weapon. The ammunition unit includes a data memory for storing ammunition-specific data; and a microcontroller arranged on or in the ammunition unit and being connected, when the ammunition unit is inside the chamber of weapon, to the data input device, the aiming mechanism and the data memory. The microcontroller determines aiming signals necessary to control the aiming mechanism as a function of ammunition-specific, target-specific, and weapon-specific data transmitted to the microcontroller. The microcontroller transmits the aiming signals to the aiming mechanism.
    • 武器系统包括具有腔室的武器; 数据输入装置; 瞄准机制; 以及可以用武器射击的弹药单位。 弹药单元包括用于存储特定于弹药的数据的数据存储器; 布置在弹药单元上或其上的微控制器,当弹药单元在武器室内时,连接到数据输入装置,瞄准机构和数据存储器。 微控制器确定控制瞄准机构所需的瞄准信号,作为特定于弹药的目标特定数据和武器特定数据传输到微控制器的功能。 微控制器将瞄准信号发送到瞄准机构。
    • 7. 发明授权
    • Method for aiming the weapon of a weapon system and weapon system for
implementing the method
    • 瞄准武器系统武器和武器系统实施该方法的方法
    • US6038955A
    • 2000-03-21
    • US61322
    • 1998-04-17
    • Stefan ThiesenDieter JungbluthJurgen Bocker
    • Stefan ThiesenDieter JungbluthJurgen Bocker
    • F41G3/14F41G1/00
    • F41G3/142
    • A method for aiming the weapon (4) of a weapon system (1) with an aiming system (5) and a heat imaging device (6) while considering external influences acting on the projectiles to be fired into a target region (3). In order to accomplish that influences acting on the projectiles (2) during their flight into the target region (3) are considered in a simple manner for the aiming of the weapon (4), the amount of lateral deviation (13) of the point of impact (11) of the projectile from a predetermined point of aim (12) of the weapon (4)is determined by measuring or tracking the tracer (10) of the projectile (2) by the heat imaging device (6). The amount of lateral deviation (13) thus determined is then compensated for in the subsequent firing by a corresponding lateral aiming correction of the weapon (4). A weapon system (1) for implementing the method is likewise disclosed.
    • 一种用于在考虑作用于待射击的射弹的目标区域(3)的外部影响的同时瞄准武器系统(1)的武器(4)的瞄准系统(5)和热成像装置(6)的方法。 为了完成在飞行进入目标区域(3)期间作用于射弹(2)的影响,以武器(4)瞄准的简单方式被考虑,点的横向偏差(13) 通过由热成像装置(6)测量或跟踪射弹(2)的示踪器(10)来确定来自武器(4)的预定瞄准点(12)的射弹的撞击(11)。 然后通过相应的武器(4)的侧向瞄准校正在随后的射击中补偿由此确定的横向偏差(13)的量。 同样公开了用于实现该方法的武器系统(1)。
    • 10. 发明授权
    • Weapon
    • 武器
    • US5149907A
    • 1992-09-22
    • US755061
    • 1991-09-05
    • Stefan Thiesen
    • Stefan Thiesen
    • F41A1/02F41A1/04
    • F41A1/04F41A1/02
    • A weapon including a barrel (2), with a charge chamber (5) and an arrangement for delaying a drop in the maximum gas pressure in the barrel after firing of a charge in the chamber, with the arrangement for delaying a drop in the maximum gas pressure injecting an additional quantity of a liquid propellant (13, 13') into the charge chamber (5). To effect the injection of the liquid propellant (13, 13') into the chamber (5), primarily with a view toward short loading times, openings (10, 10', 18, 18') are provided in the barrel wall portion (9) defining the chamber (5), and these openings are connected by valves (12, 12') with containers (14, 14') containing the liquid propellant (13, 13'). The valves may be directly responsive to the maximum pressure in the chamber (5) to directly inject a measure or quantity of the liquid propellant into the charge chamber or prior to firing of a charge in the charge chamber (5) may supply the measured quantity of additional liquid propellant to a further tubular container (16, 16') connected at both ends to the charge chamber (5). In this latter case, the liquid propellant is injected via a piston (19, 19') disposed in the tubular container (16, 16') and responsive to gas pressure, and in particular gas pressure gradients in the charge chamber (5).
    • 一种武器,包括具有充电室(5)的桶(2)和用于在燃烧室中的电荷之后延迟桶中的最大气体压力的装置的装置,用于延迟最大值的下降 气体压力将额外量的液体推进剂(13,13')注入到充电室(5)中。 为了使液体推进剂(13,13')注入到腔室(5)中,主要以缩短加载时间的方式,在筒壁部分(10,10',18,18')中设置开口 9)限定腔室(5),并且这些开口通过阀(12,12')与容纳液体推进剂(13,13')的容器(14,14')连接。 阀可以直接响应于腔室(5)中的最大压力,以直接将液体推进剂的量或数量注入到充气室中,或者在充电室(5)中的燃料点燃之前,可以将测量量 的另外的液体推进剂连接到两端连接到充电室(5)的另一管状容器(16,16')上。 在后一种情况下,液体推进剂通过设置在管状容器(16,16')中的活塞(19,19')注入,并响应气体压力,特别是充电室(5)中的气体压力梯度。