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1. 发明授权

US4797985A Method of applying a metallic guide band to a thin-walled projectile body 失效
标题翻译：将金属引导带应用于薄壁射弹体的方法
公开(公告)号：US4797985A
公开(公告)日：1989-01-17
申请号：US927556
申请日：1986-11-06
申请人： Jurgen Prochnow , Jorg Peters , Ulrich Theis , Klaus D. Karius
发明人： Jurgen Prochnow , Jorg Peters , Ulrich Theis , Klaus D. Karius
IPC分类号： C23C4/02 , C23C4/129 , F42B14/02 , B21K21/06
CPC分类号： F42B14/02 , C23C4/02 , C23C4/129 , Y10T29/479 , Y10T29/49982
摘要： A method of applying a metallic guide band to the body of a projectile having particularly thin walls comprises making fine particles plastically deformable by heating thereof, and spraying said heated particles at high speed onto a surface section of the projectile body until a desired layer thickness of the guide band is attained. A projectile body having a circumferential guide band is produced by the method of the invention. The thin-walled projectile body has a boundary layer region on its exterior which may be roughened and/or deoxidized. The boundary layer region is formed by an intermediate layer which may be composed of molybdenum, nickel aluminide or nickel oxide and itself has a roughened boundary layer region on its exterior. This results in a particularly intimate physical bond with the particles of alloy of the guide band. The alloy is preferably of a CuZn85/15 type and has a porosity of up to 5 volume percent.
摘要翻译：将金属引导带施加到具有特别薄壁的射弹的主体的方法包括通过加热使微细颗粒塑性变形，并将所述加热的颗粒高速喷射到射弹体的表面部分上，直到所需的层厚度引导带达到。通过本发明的方法制造具有周向引导带的射弹体。薄壁射弹体在其外部具有可以被粗糙化和/或脱氧的边界层区域。边界层区域由可由钼，镍铝化物或氧化镍构成的中间层形成，其外部本身具有粗糙化的边界层区域。这导致与引导带的合金颗粒的特别亲密的物理结合。该合金优选为CuZn85 / 15型，并且具有高达5体积％的孔隙率。

2. 发明授权

US4793260A Spin-stabilized bomblet-carrying projectile 失效
标题翻译：旋转稳定的炸弹携带弹丸
公开(公告)号：US4793260A
公开(公告)日：1988-12-27
申请号：US91012
申请日：1987-08-31
申请人： Heinz J. Kruse , Karin Fey , Klaus D. Karius , Harmut Schilling
发明人： Heinz J. Kruse , Karin Fey , Klaus D. Karius , Harmut Schilling
IPC分类号： F42B12/62 , F42B13/50
CPC分类号： F42B12/62
摘要： A spin-stabilized projectile includes a casing, a plurality of bomblets accommodated in the casing, filler pieces inserted between the casing and the bomblets, and a device for ejecting the bomblets by explosive force from the projectile at a predetermined point along a trajectory thereof. The filler pieces are of steel or tungsten and are distributed in the casing such that the projectile flies stably up to the point of ejection of the bomblets.
摘要翻译：旋转稳定的射弹包括壳体，容纳在壳体中的多个炸弹，插入壳体和炸弹之间的填充片，以及用于通过爆炸力沿着其轨迹在预定点处从射弹弹出炸弹的装置。填充件是钢或钨，并且分布在壳体中，使得抛射体稳定地飞行到炸弹的喷射点。

3. 发明授权

US4589340A Sensor carrier 失效
标题翻译：传感器载体
公开(公告)号：US4589340A
公开(公告)日：1986-05-20
申请号：US573343
申请日：1984-01-24
申请人： Rolf Hellwig , Jens Seidensticker , Klaus D. Karius
发明人： Rolf Hellwig , Jens Seidensticker , Klaus D. Karius
IPC分类号： F16M11/40 , G01B5/00 , F42B23/24 , F42C19/00
CPC分类号： G01B5/0004 , F16M11/046 , F16M11/40 , F16M13/005 , F16M2200/047
摘要： The invention relates to a sensor-carrier which is transported by a useful load projectile to a predetermined target region which may be inaccessible and is set down in said region. For the purpose of avoiding damaging the sensitive sensor, the latter is, together with the sensor support, compactly mounted in a folded retracted condition in a rugged housing and is automatically projected out of the housing in an erected, extended position when the sensor-carrier is set down and the housing is opened. The sensor support consists of a plurality of rotationally symmetrical support members which are strung on a steel cable in a manner similar to a pearl necklace. The steel cable is surrounded by a sheathing and is connected via a disc to a coil spring for tensioning the steel cable. The sensor-carrier serves to position the sensor in an elevated position over the ground surface for improving its sensing and transmitting capabilities.
摘要翻译：本发明涉及一种传感器 - 载体，其通过有用的负载射弹传送到预定的目标区域，该预定目标区域可能是不可接近的并且被放置在所述区域中。为了避免损坏敏感传感器，后者与传感器支撑件一起紧凑地安装在折叠的缩回状态下在坚固的壳体中，并且当传感器载体被放下并且外壳被打开。传感器支撑件由多个旋转对称的支撑构件组成，其以类似于珍珠项链的方式串在钢缆上。钢丝绳由护套包围，并通过盘连接到用于张紧钢索的螺旋弹簧。传感器载体用于将传感器定位在地面上方的升高位置，以改善其感测和传输能力。

4. 发明授权

US5210372A Ejection device 失效
标题翻译：喷射装置
公开(公告)号：US5210372A
公开(公告)日：1993-05-11
申请号：US899843
申请日：1992-06-17
申请人： Peter Tripptrap , Karl-Heinz Vogt , Klaus D. Karius
发明人： Peter Tripptrap , Karl-Heinz Vogt , Klaus D. Karius
IPC分类号： F42B12/62
CPC分类号： F42B12/62
摘要： An arrangement for ejecting objects from a projectile, includes a hollow projectile body having a nose end with a plurality of objects disposed in a column within the projectile body. An ejection charge is disposed within the projectile body at the nose end. An ejection device including a hood enclosing a cavity is ejectably disposed within the projectile body between the ejection charge and the column. The hood has a wall with an opening facing the ejection charge so that, after ignition of the ejection charge, resulting powder gases enter into the cavity through the opening to generate a gas pressure between the hood and the adjacent object and simultaneously exert a force on an exterior portion of the wall of the hood that causes the hood and the column to be ejected from the tail end of the projectile body, whereby the hood separates from the column once the hood and column are free of the projectile due to the pressure in the cavity.
摘要翻译：用于从抛射体喷射物体的装置包括具有鼻端的中空射弹体，其具有设置在射弹体内的柱中的多个物体。喷射装置在鼻端处设置在射弹体内。包括封闭空腔的罩的喷射装置可弹射地设置在喷射装置和列之间的射弹体内。罩具有面向喷射装料的开口的壁，使得在点燃充电之后，所得到的粉末气体通过开口进入空腔，以在罩和相邻物体之间产生气体压力，同时施加力罩的壁的外部部分，其使得罩和柱从射弹体的尾端弹出，由此，一旦发动机罩和立柱由于压力而没有弹丸，则罩与柱分离空腔。

5. 发明授权

US4870905A Spin stabilized projectile 失效
标题翻译：旋转稳定的射弹
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）。

6. 发明授权

US4854241A Spin stabilized carrier projectile 失效
标题翻译：旋转稳定的载体抛射体
公开(公告)号：US4854241A
公开(公告)日：1989-08-08
申请号：US135509
申请日：1987-12-16
申请人： Reinhard Synofzik , Rolf Hellwig , Klaus D. Karius
发明人： Reinhard Synofzik , Rolf Hellwig , Klaus D. Karius
IPC分类号： F42B12/58 , F42B10/50 , F42B30/00
CPC分类号： F42B30/003
摘要： A spin stabilized carrier projectile comprising: a projectile body having a rear end; at least one submunition projectile disposed in, and ejectable from, the projectile body; and a projectile bottom disposed at, and ejectable from, the rear end of the projectile body, the projectile bottom having a side surface facing the submunition projectile and containing a recess, and a folded, expandable deceleration element for reducing the velocity and spin of the projectile bottom upon ejection from the projectile body, the deceleration element including a sheet of material fastened in the recess for producing air resistance, and the deceleration element being deployable from a folded condition to an expanded condition with the aid of rotation of the projectile bottom.
摘要翻译：一种自旋稳定的载体抛射体，包括：具有后端的射弹体; 至少有一个子弹药弹放置在射弹体内并可从弹丸体中排出; 以及设置在射弹体的后端并且可从弹丸体的后端排出的射弹底部，射弹底部具有面向子弹丸的侧面并且容纳凹部，以及折叠的可扩张的减速元件，用于降低弹丸的速度和旋转所述减速元件包括紧固在所述凹部中的用于产生空气阻力的材料片，并且所述减速元件可借助于所述抛射体底部的旋转而从折叠状态展开至膨胀状态。

7. 发明授权

US5183962A Submunition for a spin stabilized carrier projectile 失效
标题翻译：用于旋转稳定运载器项目的分支
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
IPC分类号： F42B30/00 , F42C19/04
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。

8. 发明授权

US4803929A Projectile having a rotating band disposed on the projectile body 失效
标题翻译：抛射体具有设置在射弹体上的旋转带
公开(公告)号：US4803929A
公开(公告)日：1989-02-14
申请号：US92688
申请日：1987-09-03
申请人： Heinz-Josef Kruse , Klaus D. Karius
发明人： Heinz-Josef Kruse , Klaus D. Karius
IPC分类号： F42B14/02 , F42B31/00
CPC分类号： F42B14/02
摘要： A projectile for firing from a gun barrel which comprises a projectile body having a radial and longitudinal directions; a rotating band disposed on the projectile body and having at least one material receiving groove to accommodate rotating band material sheared off during passage of the projectile through the gun barrel, and at least one pressure relief groove located in a region of the rotating band where the projectile body is subjected to maximum stress in the radial direction.
摘要翻译：一种用于从枪管射出的射弹，其包括具有径向和纵向方向的射弹体; 设置在射弹体上并具有至少一个材料容纳槽的旋转带，以容纳在弹丸穿过枪筒期间剪切的旋转带材料，以及位于旋转带的区域中的至少一个压力释放槽，射弹体在径向方向受到最大应力。

9. 发明授权

US5561262A Spin-stabilized carrier projectile 失效
标题翻译：旋转稳定的载体抛射体
公开(公告)号：US5561262A
公开(公告)日：1996-10-01
申请号：US516618
申请日：1995-08-18
申请人： Volker Bartels , Klaus D. Karius
发明人： Volker Bartels , Klaus D. Karius
IPC分类号： F42B12/58
CPC分类号： F42B12/58
摘要： A projectile assembly includes a spin-stabilized carrier projectile having a carrier casing and a base at one end of the casing; and a sub-ammunition assembly composed of a plurality of sub-ammunition components stacked to form a column. One of the components is an end component adjoining the base. A component surface of the end component is oriented towards and is in engagement with the base surface. At least two of the components are sub-ammunition projectiles. An arrangement maintains a frictional lock between the base surface and the component surface of the end component. According to the arrangement a portion of the base surface and a portion of the component surface of the end component have high coefficients of friction.
摘要翻译：射弹组件包括具有载体壳体的旋转稳定的载体抛射体和在壳体的一端的基部; 以及由堆叠形成柱的多个子弹部件组成的子弹组件。其中一个部件是与基座相邻的端部部件。端部部件的部件表面被定向朝向并与基部表面接合。至少有两个部件是次弹药弹。一种布置在基部表面和端部部件的部件表面之间保持摩擦锁定。根据该布置，底部表面的一部分和端部部件的部件表面的一部分具有高摩擦系数。

10. 发明授权

US5033388A Projectile base for carrier projectiles 失效
标题翻译：运载火箭射弹基地
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。

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