公开(公告)号：US5081931A

公开(公告)日：1992-01-21

申请号：US635826

申请日：1991-01-03

申请人： Gunter Frye ,  Klaus-Dietmar Karius ,  Heinz-Josef Kruse ,  Achim Sippel ,  Jurgen Meyer ,  Michael Primus

发明人： Gunter Frye ,  Klaus-Dietmar Karius ,  Heinz-Josef Kruse ,  Achim Sippel ,  Jurgen Meyer ,  Michael Primus

IPC分类号： F42B14/02

CPC分类号： F42B14/02

摘要： To provide a complete seal in the region of the rifling, particularly in worn-out gun barrels firing spin stabilized carrier projectiles provided with a metal guide or driving band and a thin-walled projectile connected to a projectile base and having a wall thickness less than or equal to 0.05 times the caliber of the gun barrel and to reduce the ramming deceleration and the radial pressure stresses on the projectile shell during passage through the gun barrel, a plastic ram ring is disposed on the outer surface of the projectile shell in front of the metal guide band and in a region of the shell that is not supported radially by the projectile base.

摘要翻译： 为了在膛线区域提供完整的密封，特别是在磨损的枪管中，发射设置有金属引导件或驱动带的旋转稳定的载体抛射体和连接到射弹基座的壁厚小于等于 或等于枪筒口径的0.05倍，并且在穿过枪管的过程中减少夯实减速度和射弹壳体上的径向压力应力，塑料弹簧环设置在炮弹外壳的外表面上 金属引导带并且在壳体的不被射弹基座径向支撑的区域中。

公开(公告)号：US5033388A

公开(公告)日：1991-07-23

申请号：US469590

申请日：1990-03-22

申请人： Achim Sippel ,  Heinz-Josef Kruse ,  Klaus D. Karius ,  Michael Primus

发明人： Achim Sippel ,  Heinz-Josef Kruse ,  Klaus D. Karius ,  Michael Primus

IPC分类号： F42B30/08 ,  F42B30/00

CPC分类号： F42B30/003

摘要： In projectile bases (20) for carrier projectiles which are equipped with a cavity (26) on the side facing away from the projectile tail for, for example, a parachute, it may happen that the base plate (23) is axially bent through during firing. This causes the base body (22) to be radially constricted and contact is lost between the rotating band (27) disposed on the body (22) and the gun tube, frequently resulting in a gas breakthrough. To avoid the above-mentioned radial constriction in the region of the rotating band, the projectile base (20) is provided with a base plate (23) which is curved toward the tail of the projectile. The curved configuration of the base plate (23) makes it possible to produce radial widening in the rear projectile base region during firing so as to ensure gas tightness and spin transmission from the rotating band (27) even at high gas pressures.

摘要翻译： PCT No.PCT / EP89 / 00584。 371日期1990年3月22日 102（e）1990年3月22日PCT PCT 1989年5月26日PCT公布。 公开号WO90 / 02308 1990年3月8日。在用于例如降落伞的背面背面配备有空腔（26）的载体抛射体的射弹座（20）中，可能发生基板 23）在点火期间轴向弯曲通过。 这导致基体（22）径向收缩，并且在设置在本体（22）上的旋转带（27）和枪管之间的接触损失，经常导致气体穿透。 为了避免在旋转带的区域中的上述径向收缩，射弹座（20）设置有朝向射弹尾部弯曲的基板（23）。 基板（23）的弯曲构造使得可以在烧制期间在后抛射体基部区域中产生径向加宽，从而即使在高气体压力下也确保气旋性和旋转带（27）的自旋传递。

公开(公告)号：US5297491A

公开(公告)日：1994-03-29

申请号：US947399

申请日：1992-09-21

申请人： Achim Sippel ,  Heinz-Josef Kruse ,  Gisbert Bartsch ,  Monika Wildau ,  Jurgen Meyer

发明人： Achim Sippel ,  Heinz-Josef Kruse ,  Gisbert Bartsch ,  Monika Wildau ,  Jurgen Meyer

IPC分类号： F42B5/26 ,  F42B5/28

CPC分类号： F42B5/26

摘要： A casing bottom or stub casing for a propelling charge casing whose base plate (1) has an exterior or outer surface which is curved inwardly in an annular region (7) so that the casing bottom is able to sufficiently axially expand under the high gas pressure developing during firing without requiring the use of a high strength material.

摘要翻译： 用于推进式充电套管的壳体底部或短管壳体，其底板（1）具有在环形区域（7）内向内弯曲的外表面或外表面，使得壳体底部能够在高气压下充分轴向膨胀 在焙烧期间显影而不需要使用高强度材料。

公开(公告)号：US5204494A

公开(公告)日：1993-04-20

申请号：US683959

申请日：1991-04-12

申请人： Jurgen Meyer ,  Achim Sippel ,  Heinz-Josef Kruse ,  Siegfried Kessler ,  Horst Kantner ,  Ulrich Theis

发明人： Jurgen Meyer ,  Achim Sippel ,  Heinz-Josef Kruse ,  Siegfried Kessler ,  Horst Kantner ,  Ulrich Theis

IPC分类号： F42B14/06

CPC分类号： F42B14/061 ,  F42B14/062

摘要： A subcaliber projectile including a segmented discardable propelling cage sabot which encloses at least a portion of the projectile body and has a common form-locking zone for the transfer of acceleration forces from the propelling cage to the projectile body. The form-locking zone has mating annular grooves and counter grooves on the exterior surface of the projectile body and on the interior surface of the propelling cage, and is subdivided into several form-locking zone regions in which the annular grooves have a different groove spacing that is adapted to the locally occurring shear stresses. These measures enhance simplification of the manufacturing process and result in an improvement of the release of the propelling cage sabot from the projectile body and in an increase in the target impact velocity of the projectile body.

摘要翻译： 一个亚型射弹，包括一个分段的可抛弃的推进式笼式破坏物，其包围至少一部分射弹体，并具有用于将加速力从推进笼转移到射弹体的共同形状锁定区。 形状锁定区域在射弹体的外表面和推进笼的内表面上具有配合的环形槽和相对槽，并且被细分成多个形状锁定区域，其中环形槽具有不同的槽间距 这适应于局部发生的剪切应力。 这些措施增强了制造过程的简化，并且导致推进式笼式破坏物从射弹体的释放以及射弹体的目标冲击速度的增加。

公开(公告)号：US5289777A

公开(公告)日：1994-03-01

申请号：US25400

申请日：1993-02-26

申请人： Achim Sippel ,  Heinz-Josef Kruse ,  Walter Klumpp ,  Jurgen Bocker ,  Jurgen Meyer ,  Michael Geis ,  Rolf Holl

发明人： Achim Sippel ,  Heinz-Josef Kruse ,  Walter Klumpp ,  Jurgen Bocker ,  Jurgen Meyer ,  Michael Geis ,  Rolf Holl

IPC分类号： F42B14/06

CPC分类号： F42B14/061

摘要： A subcaliber kinetic energy projectile (1) including a penetrator (2) and a segmented sabot (3) which is provided with a front support (4) and with a second support (5) that is disposed at an axial distance behind the first support, with the second support (5) including a rotationally symmetrical air pocket (6) that faces the first support (4) and the first support (4) is provided with air passage openings (43, 44, 45).In the sabot, the relationship of L/D.gtoreq.1.2 exists between the length L of the penetrator tip (8) ahead of the first support (4) and the caliber D. The relationship x.gtoreq.0.45 * .iota. further applies between the distances x and .iota., with x being the distance between the trailing edge (10) of the sabot and the base surface (11) of the air pocket (6) in the second support (5) and .iota. being the distance between the trailing edge (10) of the sabot (3) and the leading edge (12) of the sabot at the surface of the penetrator (2). Finally, the first support (4) is composed of at least three laterally extending web-like components (40-42) whose shape and dimensions are such that they form and have the effect of three separate air pockets.

摘要翻译： 一种包括穿透器（2）和分段式破坏物（3）的亚规模动能射弹（1），其设置有前支撑件（4）和第二支撑件（5），所述第二支撑件设置在所述第一支撑件后面的轴向距离处 第二支撑件（5）包括面向第一支撑件（4）的旋转对称的气穴（6），并且第一支撑件（4）设置有空气通道开口（43,44,45）。在支架中， L / D> = 1.2之间的关系存在于第一支撑件（4）之前的穿透尖端（8）的长度L与口径D之间。关系x> = 0.45 *（iota）还应用于距离x 和（iota），其中x是在第二支撑件（5）中的破坏件的后缘（10）和气囊（6）的基部表面（11）之间的距离，并且（iota） 砧座（3）的后缘（10）和砧座的前缘（12）在穿透器（2）的表面。 最后，第一支撑件（4）由至少三个横向延伸的网状部件（40-42）组成，其形状和尺寸使得它们形成并具有三个独立气囊的作用。

公开(公告)号：US5063855A

公开(公告)日：1991-11-12

申请号：US600414

申请日：1990-10-16

申请人： Rainer Diel ,  Achim Sippel ,  Jurgen Meyer ,  Heinz-Josef Kruse

发明人： Rainer Diel ,  Achim Sippel ,  Jurgen Meyer ,  Heinz-Josef Kruse

IPC分类号： F42B14/06

CPC分类号： F42B14/061 ,  F42B14/062

摘要： A projectile arrangement including a subcaliber projectile body and a segmented, discardable propelling cage sabot provided with a common form locking zone for the transmission of the acceleration forces. To reduce the notch effect on the projectile body, and thus the danger of breakage, due to the conventional thread grooves in the form locking zone, particularly in long, slender penetrators made of a breakage susceptible tungsten heavy metal, a novel form locking connection for the inner form locking region between the propelling cage and the projectile body is provided. This novel form locking connection is characterized in that in the region of the form locking zone beneath the exterior gas pressure receiving surface of the sabot, only the exterior surface of the projectile body is provided with preferably annular microgrooves and the surrounding inner surface of the sabot is smooth. The microgrooves are produced preferably by non-cutting shaping such as, for example, rolling or pressing in, and are configured as arcuate recesses having a relatively flat groove bottom and pointed lands between adjacent recesses. When the projectile arrangement is fired, the microgrooves of the relatively hard projectile body press themselves into the previously smooth interior surface of the relatively soft sabot, and thus produce a corresponding form locking connection only at the moment of firing.

摘要翻译： 一种抛射体装置，包括一个亚型射弹体和一个分段的，可抛弃的推进式笼式破碎机，其具有用于传递加速力的通用形式锁定区域。 由于常规的形式锁定区域的螺纹沟槽，特别是在由易破坏的钨重金属构成的长而细长的穿透器中，为了减小抛射体的切口效应，并因此导致断裂的危险，新颖的形式锁定连接 提供了推进笼和射弹体之间的内部形式锁定区域。 这种新颖的形式锁定连接的特征在于，在形状锁定区域的下方的外部气体压力接收表面的区域内，只有射弹体的外表面设置有优选的环形微槽和其周围的内表面 顺利 微槽优选地通过非切割成形例如轧制或压制而制成，并且被构造成具有相对平坦的凹槽底部和相邻凹部之间的尖锐平台的弓形凹部。 当抛射体布置被发射时，相对较硬的抛射体的微槽将其自身压入相对柔软的破坏物的先前光滑的内表面中，因此仅在烧制时产生相应的形状锁定连接。

公开(公告)号：US4870905A

公开(公告)日：1989-10-03

申请号：US213606

申请日：1988-06-30

申请人： Achim Sippel ,  Heinz-Josef Kruse ,  Klaus D. Karius

发明人： Achim Sippel ,  Heinz-Josef Kruse ,  Klaus D. Karius

IPC分类号： F42B14/02

CPC分类号： F42B14/02

摘要： A spin stabilized projectiles (1) having a rotating band (3) arranged on the shell body (2), with such rotating band being provided with grooves (35, 36, 37) to receive rotating band material sheared off toward the rear during passage of the projectile (1) through a gun barrel (4) so that the transfer of spin is effected with the aid of annular rotating band zones (31, 32, 33, 34) which form spin transfer ring. The diameter (38) of at least one spin transfer ring (31, 34), preferably the rearmost ring, is larger than the diameter (45) of the rifling grooves (42) in the gun barrel (4). Due to the high radial pressure on the shell body in the region of the rotating band, great radial deformations may occur, particularly in thin-walled shell bodies. The consequences are untightness of the rotating band and too much stress on the projectile. To overcome these drawbacks of prior art rotating bands, the diameter (39) of at least one of the remaining spin transfer rings (32, 33) is smaller than the diameter of the rifling grooves (45) but larger than the caliber (44) of the gun barrel (4).

摘要翻译： PCT No.PCT / EP87 / 00662 Sec。 371日期：1988年6月30日 102（e）日期1988年6月30日PCT提交1987年11月3日PCT公布。 第WO88 / 05899号公报 日期：1988年8月11日。具有设置在壳体（2）上的旋转带（3）的旋转稳定化弹丸（1），其旋转带设有槽（35,36,37），以接收旋转带材料 在抛射体（1）穿过枪管（4）的过程中，向后方剪切，从而借助于形成自旋转移环的环形旋转带区（31,32,33,34）实现自旋转移 。 至少一个自旋转移环（31,34）（优选最后面的环）的直径（38）大于枪筒（4）中的膛线槽（42）的直径（45）。 由于壳体在旋转带的区域内的高的径向压力，可能会发生大的径向变形，特别是在薄壁壳体中。 后果是旋转带的不紧密性和对弹丸的应力太大。 为了克服现有技术旋转带的这些缺点，剩余的自旋转移环（32,33）中的至少一个的直径（39）小于膛线槽（45）的直径，但比口径（44）大， 的枪管（4）。

公开(公告)号：US5272983A

公开(公告)日：1993-12-28

申请号：US947397

申请日：1992-09-21

申请人： Achim Sippel ,  Heinz-Josef Kruse ,  Gisbert Bartsch ,  Egon Gampe ,  Wilfried Becker

发明人： Achim Sippel ,  Heinz-Josef Kruse ,  Gisbert Bartsch ,  Egon Gampe ,  Wilfried Becker

IPC分类号： F42B5/36 ,  F42B5/26

CPC分类号： F42B5/181 ,  F42B5/36

摘要： A casing bottom for a propelling charge including a circular ring shaped (annular) base plate (1) which accommodates a centrally arranged primer sleeve (7) in a form-locking manner. In order to be able to unload ammunition, particularly two-part ammunition including sub-caliber projectiles, the rear surface of the primer sleeve is provided with a recess for form-fittingly receiving an extractor. Preferably the recess is of a size which can be accommodated on a sub-caliber projectile.

摘要翻译： 用于推进装药的壳体底部，包括圆形环形（环形）底板（1），其以成形锁定的方式容纳中心布置的底漆套筒（7）。 为了能够卸载弹药，特别是包括次级射弹的两部分弹药，底漆套筒的后表面设置有用于成形接合提取器的凹部。 优选地，凹部具有能够容纳在子口径射弹上的尺寸。

公开(公告)号：US5009167A

公开(公告)日：1991-04-23

申请号：US296150

申请日：1989-01-12

申请人： Achim Sippel ,  Heinz-Josef Kruse ,  Wilfried Becker

发明人： Achim Sippel ,  Heinz-Josef Kruse ,  Wilfried Becker

IPC分类号： F42B10/44 ,  F42B12/22 ,  F42B14/02

CPC分类号： F42B14/02 ,  F42B12/22

摘要： A high-explosive projectile including a projectile body having a forward region and a tail region which transitions to a base, with an explosive charge disposed within the body and detonated by a suitable fuse, and a driving band disposed on the outer circumferential surface of the projectile body in the tail region, wherein the wall thickness of the tail region of the projectile body is substantially the same as the wall thickness of the forward region of the projectile body; the tail region of the projectile body has a cylindrical shape up to its transition to the base and forms a circumferential edge at the transition; and the rearward, gas pressure receiving side of the driving band is disposed adjacent the circumferential edge.

摘要翻译： 一种高爆炸弹体，包括具有向前区域和尾部区域的射弹体，其过渡到基部，爆炸装置设置在主体内并由合适的保险丝引爆;以及驱动带，其布置在 射弹体尾部区域的射出体，射弹体的尾部区域的壁厚与射弹体的前方区域的壁厚基本相同; 射弹体的尾部区域具有直到其过渡到基部的圆柱形形状并且在转变处形成圆周边缘; 并且驱动带的向后的气体压力接收侧设置成与周向边缘相邻。

公开(公告)号：US4884508A

公开(公告)日：1989-12-05

申请号：US247623

申请日：1988-09-22

申请人： Heinz-Josef Kruse ,  Klaus D. Karius ,  Achim Sippel

发明人： Heinz-Josef Kruse ,  Klaus D. Karius ,  Achim Sippel

IPC分类号： F42B14/02

CPC分类号： F42B14/02

摘要： The present invention relates to a spin-stabilized carrier projectile having a projectile base which is connected with a projectile body for carrying sub-ammunition projectiles, and a driving band arrangement connected respectively about the projectile base and about the projectile body for engaging the rifling of the gun barrel to impart spin respectively to the projectile base and the projectile body. The driving band arrangement includes a first partial driving band connected coaxially about the projectile base and a second partial driving band connected coaxially about the projectile body. This driving band arrangement reduces the spin forces transferred by the joint between the projectile base and the projectile body, thereby reducing the required joint strength. This in turn reduces the required ejection charge used to separate the projectile body and projectile base for release of sub-ammunition bodies contained in the carrier projectile.

摘要翻译： 本发明涉及一种具有射弹座的自旋稳定载体抛射体，该射弹基座与用于承载弹药弹丸的射弹体连接，以及分别围绕射弹基座和射弹体连接的驱动带装置， 枪筒分别给予弹射基座和射弹体。 驱动带装置包括与射弹座同轴地连接的第一部分驱动带和与射弹体同轴地连接的第二部分驱动带。 该驱动带布置减少了弹丸基体与射弹体之间的接合传递的旋转力，从而降低了所需的接合强度。 这反过来又减少了用于分离射弹体和射弹基座的弹药费用，用于释放运载火箭弹中所含的次弹体。