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公开(公告)号：US5463930A
公开(公告)日：1995-11-07
申请号：US241861
申请日：1994-05-12
申请人： Bernhard Bisping , Lothar Post
发明人： Bernhard Bisping , Lothar Post
摘要： A weapon for firing practice ammunition includes a barrel having a frontal length portion terminating in a muzzle; an ammunition loading chamber at a barrel end opposite the muzzle; and a plurality of first gas outlet bores provided in the frontal length portion. The first gas outlet bores are arranged in a plurality of circumferentially spaced axial rows. There is further provided a muzzle brake sleeve coaxially surrounding the frontal length portion and having a frontal end situated close to the muzzle. The muzzle brake sleeve includes a plurality of second gas outlet bores arranged in a plurality of circumferentially spaced axial rows. The first gas outlet bores are staggered with respect to the second gas outlet bores as viewed along the barrel. The frontal end of the muzzle brake sleeve is closed off by a plug.
摘要翻译： 用于射击练习弹药的武器包括具有终止于枪口的正面长度部分的枪管; 在与枪口相对的枪管端的弹药装载室; 以及设置在前长度部分中的多个第一气体出口孔。 第一气体出口孔布置成多个周向间隔开的轴向排。 还提供了一个同时围绕前长度部分并且具有位于枪口附近的前端的枪口制动套筒。 枪口制动套筒包括多个沿周向间隔开的多个轴向排列的第二气体出口孔。 第一气体出口孔相对于沿着桶观察的第二气体出口孔交错。 枪口制动套管的前端由插头封闭。
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2.发明授权Method of sealing the front of a cylindrical sleeve body of a practice cartridge 失效密封练习筒的圆筒套筒体前部的方法
公开(公告)号：US5459914A
公开(公告)日：1995-10-24
申请号：US305692
申请日：1994-09-13
申请人： Bernhard Bisping
发明人： Bernhard Bisping
CPC分类号： F42B8/04
摘要： A method of closing the forward portion or region (u) of a cylindrical sleeve body (3) of a practice cartridge (1), wherein a predetermined number of inside and outside radial folds (8, 7, respectively) are created in the forward region (4) of the sleeve body (3) in two work cycles, and wherein circular arc-shaped inside folds (8) of predetermined depth are created during the first work cycle by the application of radial pressure using correspondingly shaped profiling tools. To achieve secure closing of the sleeve body (3) through folding in a simple and cost-effective manner and without predetermined fracture points resulting in the region of the inside folds (8) during closing, the inside folds (8) are created in the forward region of the projectile body (3) during the first work cycle so that a first, central opening having a diameter of at least 2 mm remains between the inside folds (8) after completion of this work cycle. Due to this first step, tools that have a relatively large bending radius can be used for creating the inside folds, despite the high number of folds. In the subsequent second work cycle, a further radial pressing together of the inside folds (8) is effected by exerting pressure on the outside folds (7), e.g. by using a conical die.
摘要翻译： 一种闭合练习筒（1）的圆柱形套筒体（3）的前部或区域（u）的方法，其中在前进中产生预定数量的内部和外部径向折叠（8,7） （3）的区域（4），并且其中在第一工作循环期间通过使用对应形状的成形工具施加径向压力来产生预定深度的圆弧形内部折叠（8）。 为了通过简单且经济有效的方式折叠来实现套筒本体（3）的可靠闭合，并且在关闭期间没有预定的断裂点导致内折痕（8）的区域，内折痕（8）在 在第一工作循环期间射弹体（3）的向前区域，使得在完成该工作循环之后，在内部折叠（8）之间保留具有至少2mm直径的第一中心开口。 由于该第一步，尽管折叠数量很多，但是具有相对较大弯曲半径的工具可以用于创建内部折叠。 在随后的第二工作循环中，通过在外部折叠（7）上施加压力来实现内部折叠（8）进一步径向挤压在一起。 通过使用锥形模具。
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3.发明授权Fuze mechanism for projectiles, rockets, bomblets and mines having a pyrotechnic self-destruct mechanism 失效具有烟火自毁机制的射弹，火箭，炸弹和矿山的发射机制
公开(公告)号：US5375526A
公开(公告)日：1994-12-27
申请号：US190379
申请日：1994-02-02
申请人： Wolfgang Hoffmann
发明人： Wolfgang Hoffmann
IPC分类号： F42C15/184 , F42C9/16 , F42C15/22
CPC分类号： F42C15/184
摘要： A fuze mechanism (1) for projectiles, rockets, bomblets and mines which is of the type including a fuze housing (2) and a self-destruct device containing a pyrotechnic delay arrangement (10) and a firing pin (11), with the fuze housing (2) having a side opening (5) for a transversely movable detonator carrier (4) which can be moved out beyond the outer housing contour into the armed position and which contains the pyrotechnic delay arrangement (10) and a fuze detonator (7). To manufacture fuze mechanisms (1) which are simple and free of spin and whose self-destruct devices are additionally provided with a delay time that is as long as possible, the firing pin (11) for the self-destruct mechanism is pivotably fastened to the fuze housing (2) in the region of the side opening (5). Moreover, the detonator carrier (4), on its side facing the opening (5), is provided with a carrier member (12) which is in force-locking contact with the firing pin (11) and which, when the detonator carrier (4) is moved out, pivots the firing pin (11) toward the delay arrangement (10) so that the same is ignited.
摘要翻译： 一种用于弹药，火箭，炸弹和地雷的引信机构（1），包括引信罩（2）和包含烟火延迟装置（10）和撞针（11）的自毁装置，其中 具有用于横向可移动的雷管托架（4）的侧开口（5）的引信壳体（2），所述侧开口可以被移出超出外壳轮廓到布置位置并且包含烟火延迟装置（10）和引信雷管 7）。 为了制造简单且无旋转的引信机构（1），并且其自毁装置另外设置有尽可能长的延迟时间，用于自毁机构的撞针（11）可枢转地固定到 引线壳体（2）在侧开口（5）的区域中。 此外，雷管托架（4）在其面向开口（5）的一侧上设置有承载构件（12），其与击发销（11）力锁定接触，并且当雷管托架 4）被移出，将击发销（11）朝向延迟装置（10）枢转，使得其点燃。
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4.发明授权
公开(公告)号：US5295428A
公开(公告)日：1994-03-22
申请号：US6853
申请日：1993-01-22
摘要： The present invention relates to a method of disassembling large-caliber combat cartridges, particularly armor-piercing cartridges, including a combustible casing jacket that conically widens in the direction of the projectile, a casing bottom and a casing cover to which is fastened a sub-caliber projectile equipped with a propelling sabot.To be able, on the one hand, to reduce expenditures for the disassembly of such combat cartridges and, on the other hand, to reuse a major portion of the original combat cartridges for the production of corresponding training cartridges, it is proposed to separate the casing jacket as well as the casing cover starting at their outer circumference, in regions having approximately the same, predetermined diameter D1. This diameter D1 here corresponds to the maximum diameter of the component of the new cartridge to be produced later from the disassembled components. The portion of the casing jacket and of the casing cover disposed between the regions is discarded and is replaced in the production of the new cartridge by a cylindrical casing jacket component having the diameter D1.
摘要翻译： 本发明涉及一种拆卸大口径战斗弹药筒的方法，特别是穿甲弹药筒，包括在射弹方向锥形扩大的可燃外壳护套，外壳底部和外壳盖， 机芯弹射装备有推进的炮弹。 一方面，为了减少拆卸这种战斗弹药筒的开支，另一方面，为了重新使用大部分原来的战斗弹药筒来生产相应的培训弹药筒，建议将 壳体套管以及壳体盖在其外周开始，具有大致相同的预定直径的区域D1。 这里的直径D1对应于稍后从拆卸的部件产生的新的料筒的部件的最大直径。 设置在区域之间的套管套和壳体盖的部分被丢弃，并且在通过具有直径D1的圆柱形套管套件的新的料筒的生产中被替换。
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公开(公告)号：US5282423A
公开(公告)日：1994-02-01
申请号：US917383
申请日：1992-07-23
CPC分类号： F42B3/02 , F42B5/38 , Y10S102/70
摘要： A modular propellant charge (10) composed of N propellant charge modules (1; 11-16) each having a length Lo. In order to obtain an economical, durable, easily released connection between the propellant charge modules (1; 11-16), a displaceable sleeve (6; 17-22) of a length L is axially slidably arranged on the exterior of each propellant charge module (1; 11-16) with the relationship ##EQU1## applying for the length L. The displaceable sleeves are utilized to interconnect adjacent modules.
摘要翻译： 由N个推进剂充电模块（1; 11-16）组成的每个长度为Lo的模块化推进剂装药（10）。 为了在推进剂充电模块（1; 11-16）之间获得经济，耐用且容易释放的连接，长度为L的可移动套筒（6; 17-22）可轴向滑动地布置在每个推进剂装料的外部 模块（1; 11-16）具有应用长度L的关系（*化学结构*）。可移位套筒用于互连相邻的模块。
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公开(公告)号：US5267503A
公开(公告)日：1993-12-07
申请号：US929908
申请日：1992-08-17
申请人： Dieter Grabner
发明人： Dieter Grabner
CPC分类号： F41A9/10
摘要： A device for transferring ammunition from a magazine to a transfer arm of an adjustable weapon rotatable about a trunnion. The transfer arm is movable together with the weapon and tilts up to a maximum predetermined angle (.beta.') during azimuth adjustment of the weapon. Two angle compensating elements are rotatable relative to one another about a common axis in planes that are inclined by half the predetermined angle (.beta.'/2) and are operatively disposed adjacent the magazine. A planar turntable is rotatably mounted on the two angle compensating elements for rotation relative thereto about the common axis. The plane of the planar turntable is adjusted by the two angle compensating elements. An ammunition receiving and pivoting device is supported on the turntable for receiving ammunition from the magazine and pivoting the ammunition so that the ammunition can be received by the transfer arm of the weapon.
摘要翻译： 一种用于将弹药从弹匣传送到可围绕耳轴旋转的可调节武器的传送臂的装置。 传送臂可与武器一起移动，并在武器的方位调整期间倾斜至最大预定角度（β'）。 两个角度补偿元件可相对于倾斜一半预定角度（β'/ 2）的平面中的公共轴线相对于彼此旋转并且可操作地布置在与料盒相邻的位置。 平面转盘可旋转地安装在两个角度补偿元件上，用于相对于公共轴线旋转。 平面转盘的平面由两个角度补偿元件调节。 弹药接收和旋转装置支撑在转盘上，用于从杂志接收弹药并使弹药枢转，使得弹药可以被武器的传送臂接收。
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公开(公告)号：US5262921A
公开(公告)日：1993-11-16
申请号：US775979
申请日：1991-11-01
申请人： Johannes Lamers
发明人： Johannes Lamers
CPC分类号： H05K7/20254
摘要： In order to improve the cooling of one sided circuit boards for electronic power circuits in SMD configuration, the surface (14) of the circuit board (10) which is not provided with circuit components is part of the interior wall of a housing (26) through which flows a liquid coolant and which is equipped with inlet and outlet pipe connections (28, 30) for conduits through which flows a coolant. In order to remove heat, the side (14) of the circuit board (10) which is not provided with the circuit components can be directly wetted with coolant.
摘要翻译： PCT No.PCT / EP90 / 01826 Sec。 371日期1991年11月1日 102（e）1991年11月1日PCT 1990年10月31日PCT。为了改善用于SMD配置的电子电路的单面电路板的冷却，电路板（10）的表面（14） 没有设置电路部件是壳体（26）的内壁的一部分，液体冷却剂通过该内壁流动，并且配备有用于导管的入口和出口管连接（28,30），通过冷却剂流动。 为了去除热量，不设置电路部件的电路板（10）的侧面（14）可以直接用冷却剂润湿。
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公开(公告)号：US5253588A
公开(公告)日：1993-10-19
申请号：US900132
申请日：1992-06-18
申请人： Karl-Heinz Vogt , Heinz Olmscheid
发明人： Karl-Heinz Vogt , Heinz Olmscheid
CPC分类号： F42B10/54
摘要： A device is provided for reducing the rate of rotation of a spinning submunition unit having a tail end provided with a deployable braking device, from a time after the submunition unit is ejected from a spin stabilized carrier projectile until the braking device is deployed. The device includes a plurality of bands arranged to form a star-shaped symmetrical band structure for placement around the braking device. Each of the bands has a free end provided with a wind pocket.
摘要翻译： 提供一种装置，用于从子弹药单元从旋转稳定的载体抛射体喷射直到制动装置展开之后的时间，降低具有设置有可展开制动装置的尾端的旋转子弹药单元的旋转速度。 该装置包括布置成形成用于放置在制动装置周围的星形对称带结构的多个带。 每个乐队都有一个带有风口的自由端。
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公开(公告)号：US5239927A
公开(公告)日：1993-08-31
申请号：US899870
申请日：1992-06-17
申请人： Gunter Frye , Karl-Heinz Vogt , Volker Bartels
发明人： Gunter Frye , Karl-Heinz Vogt , Volker Bartels
摘要： A deceleration device for a submunition unit includes a cartridge releasably attached to the submunition unit. A releasable package including at least one pocket is disposed in the cartridge and is connected to the cartridge by a packaging line. An auxiliary parachute and a rotation parachute are disposed in the cartridge, with at least the rotation parachute being accommodated in the at least one pocket of the releasable package and the auxiliary parachute being disposed in a pocket separate from the at least one pocket. The auxiliary parachute is connected to the cartridge and the rotation parachute is connected to the submunition unit. A deployment mechanism causes the auxiliary parachute to be deployed in advance of the rotation parachute after the cartridge is released from the submunition unit and the rotation parachute to be deployed after the cartridge is decelerated by the auxiliary parachute for decelerating the submunition unit.
摘要翻译： 用于子弹药单元的减速装置包括可释放地附接到子弹药单元的盒。 包括至少一个口袋的可释放包装被设置在盒中并且通过包装线与盒连接。 辅助降落伞和旋转降落伞设置在盒中，至少旋转降落伞容纳在可释放包装的至少一个袋中，并且辅助降落伞设置在与所述至少一个袋分离的口袋中。 辅助降落伞连接到墨盒，旋转降落伞连接到子弹药单元。 一个展开机构使辅助降落伞在旋转降落伞之前被放置在弹药盒从子弹药单元释放之后，并且在弹药筒被辅助降落伞减速以使子弹药单元减速之后被部署。
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公开(公告)号：US5183962A
公开(公告)日：1993-02-02
申请号：US884141
申请日：1992-05-18
申请人： Klaus D. Karius , Armin Eskam , Karl-Heinz Vogt
发明人： Klaus D. Karius , Armin Eskam , Karl-Heinz Vogt
CPC分类号： F42C19/04 , F42B30/003
摘要： A submunition unit for a spin stabilized carrier projectile (1), with the submunition unit including an antenna disposed at the nose of its casing (7), and with the antenna (5) being covered by a protective cover (6). The casing (7) and the protective cover (6) are provided with respective axially overlapping collars (8, 9) which are each provided with respective opposed circumferential grooves (14, 15) to form an annular recess to accommodate an elastic securing ring (16). The securing ring, which is normally positioned within the innermost of the circumferential grooves, expands under the influence of centrifugal forces to connect the casing and protective cover together in a form-locking manner.
摘要翻译： 一种用于自旋稳定的载体射弹（1）的子弹药单元，子弹药单元包括设置在其壳体（7）的鼻部处的天线，并且天线（5）被保护盖（6）覆盖。 壳体（7）和保护盖（6）设置有相应的轴向重叠的轴环（8,9），每个轴环重叠的轴环（8,9）分别设置有相应的相对的周向槽（14,15），以形成环形凹部以容纳弹性固定环（ 16）。 通常位于圆周槽的最内侧的固定环在离心力的影响下膨胀，从而将壳体和保护罩以形状锁定的方式连接在一起。
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