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    • 4. 发明授权
    • Sealing ring and propellant charge cartridge
    • 密封圈和推进剂充电盒
    • US08833227B2
    • 2014-09-16
    • US13539669
    • 2012-07-02
    • Axel PfersmannFritz SchlenkManfred HechtlAlfred Eckel
    • Axel PfersmannFritz SchlenkManfred HechtlAlfred Eckel
    • F41A3/74F41A3/76F42B5/18
    • F41A3/74F41A3/76
    • A sealing ring obturates a propellant charge cartridge of an automatic firearm for caseless ammunition, in particular against an end face of a firearm element, in particular for a breech or a projectile cartridge. The sealing ring contains a sealing surface that can be brought into contact with the end face. The sealing surface contains a first region around an annular opening of the sealing ring and a second region around the first region. The second region is set back relative to a tangential surface to the first region. In addition, a propellant charge cartridge for an automatic firearm for caseless ammunition, has at least one of the sealing rings. The propellant charge cartridge preferably contains one or multiple, in particular two, propellant charge chambers, which are provided with a sealing ring on each of the breech side and the projectile cartridge side.
    • 密封环堵塞用于无弹药弹药的自动火器的推进剂充电筒,特别是针对枪支元件的端面,特别是用于后膛弹药或弹药筒。 该密封环包含能够与端面接触的密封面。 密封表面包含围绕密封环的环形开口的第一区域和围绕第一区域的第二区域。 第二区域相对于第一区域的切向表面回退。 此外,用于无弹药弹药的自动枪支的推进剂充电盒具有至少一个密封环。 推进剂充气筒优选地包含一个或多个,特别是两个推进剂装料室,其在后膛侧和弹丸筒侧的每个上设置有密封环。
    • 5. 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)。
    • 7. 发明申请
    • PROPELLANT CHARGE
    • US20110072996A1
    • 2011-03-31
    • US12959612
    • 2010-12-03
    • Axel PfersmannAlfred Eckel
    • Axel PfersmannAlfred Eckel
    • F42B5/38F42C19/08
    • F42B5/38
    • A propellant charge for use for ammunition, in which the propellant charge is separate from the projectile, has a propellant charge substance which can be initiated by a fuse. In order to solve the problem of providing a propellant charge for use in a two-part munition, which on the one hand can be produced easily and at low cost and on the other hand does not present any risk of damage when mechanically loaded before use, it is proposed that a propellant charge casing be provided which surrounds the propellant charge substance, with the propellant charge casing being in the form of a plastic part which is composed of a non-combustible, temperature-stable plastic material.
    • 用于弹药的推进剂费用,其中推进剂费用与射弹分开,具有可由保险丝启动的推进剂充电物质。 为了解决在两部分弹药中提供推进剂费用的问题,一方面可以容易地和低成本地制造,另一方面在使用前机械加载时不会有损坏的危险 建议提供围绕推进剂充电物质的推进剂充电壳体,其中推进剂充电壳体为由不可燃的温度稳定的塑料材料构成的塑料部件的形式。
    • 8. 发明授权
    • Braking fabric fastened to the base of a carrier projectile containing
articles of submunition
    • 制动织物紧固在载有弹药的基座上,其中包含子弹药物
    • US5033384A
    • 1991-07-23
    • US493470
    • 1990-03-14
    • Alfred EckelGunther Thurner
    • Alfred EckelGunther Thurner
    • F42B10/56
    • F42B10/56
    • A braking fabric or canvas which is fastened to the base of a carrier projectile which contains articles of submunition, through the intermediary of a fastening device, wherein the canvas is spread apart or unfolded after the separation of the base from the carrier projectile and is provided for the retardation and change in the trajectory of the base relative to the articles of submunition. The braking fabric is connected by a central surface section thereof with at least one plate element forming the fastening device. This connection between the at least one plate element and the braking fabric is preferably effectuated through an adhesive connection. Naturally, it is also possible to select a different type in effecting the connection; for example, such as a riveting connection, a combined adhesive and riveting connection, or any other suitable type of connection.
    • 一种制动织物或帆布,其紧固到载体抛射体的基部,该载体抛射体通过紧固装置的中间而包含子弹药的制品,其中在将基部与载体抛射体分离之后,帆布被展开或展开,并且被提供 对于基地相对于子弹药物的轨迹的延迟和变化。 制动织物通过其中心表面部分连接有形成紧固装置的至少一个板状元件。 优选地,通过粘合剂连接来实现至少一个板元件和制动织物之间的这种连接。 当然,也可以选择不同的类型来实现连接; 例如铆接连接,组合粘合剂和铆接连接,或任何其它合适类型的连接。
    • 9. 发明授权
    • Propellant charge
    • 推进剂费
    • US08161882B2
    • 2012-04-24
    • US12959612
    • 2010-12-03
    • Axel PfersmannAlfred Eckel
    • Axel PfersmannAlfred Eckel
    • F42B5/30F42B5/38
    • F42B5/38
    • A propellant charge for use for ammunition, in which the propellant charge is separate from the projectile, has a propellant charge substance which can be initiated by a fuse. In order to solve the problem of providing a propellant charge for use in a two-part munition, which on the one hand can be produced easily and at low cost and on the other hand does not present any risk of damage when mechanically loaded before use, it is proposed that a propellant charge casing be provided which surrounds the propellant charge substance, with the propellant charge casing being in the form of a plastic part which is composed of a non-combustible, temperature-stable plastic material.
    • 用于弹药的推进剂费用,其中推进剂费用与射弹分开,具有可由保险丝启动的推进剂充电物质。 为了解决在两部分弹药中提供推进剂费用的问题,一方面可以容易地和低成本地制造,另一方面在使用前机械加载时不会有损坏的危险 建议提供围绕推进剂充电物质的推进剂充电壳体,其中推进剂充电壳体为由不可燃的温度稳定的塑料材料构成的塑料部件的形式。