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1. 发明授权

US4671179A Cartridged ammunition for gun barrel weapons 失效
标题翻译：枪支武器弹药
公开(公告)号：US4671179A
公开(公告)日：1987-06-09
申请号：US711395
申请日：1985-03-13
申请人： Reinhard Synofzik , Michael Schwenzer , Peter Wallow
发明人： Reinhard Synofzik , Michael Schwenzer , Peter Wallow
IPC分类号： F42B5/073 , F42C19/08 , F42B5/02
CPC分类号： F42B5/181 , F42B5/073 , F42C19/0826
摘要： The target-effective mass of cartridged ammunition is increased while maintaining a predetermined cartridge length.A projectile body has a projectile tail portion extending rearwardly on which a fin or wing-stabilization arrangement is mounted. This tail portion extends rearwardly towards the immediate vicinity of the propellant charge casing bottom. A projection extends rearwardly past the wing or fin-stabilization guide arrangement. This projection includes a massive portion which separates at firing from the propellant charge casing bottom. The rear portion of the projectile body is surrounded by a sheathing of combustible material forming the ignition element which sheathing extends from the cartridge case bottom up to at least the middle of the propellant charge casing and has a longitudinal extent l.sub.2. The massive projection permits, during the combustion of the propellant charge up to separation the build up of a high gas pressure, whereby in particular a loose powder propellant charge is ignited by the ignition element for a short period of time in a uniform and reproducible manner. Thus, without increasing the length of the cartridge an increase of the target-effective mass and an increase of the projectile length is achieved with an accompanying penetration capacity increase by improving the relationship of the projectile length l.sub.1 to the projectile diameter d.sub.1.
摘要翻译：弹药的目标有效质量增加，同时保持预定的药筒长度。射弹体具有向后延伸的射弹尾部，其上安装翅片或翼稳定装置。该尾部向后延伸到推进剂充电套管底部的紧邻附近。突出部向后延伸穿过机翼或翼片稳定导向装置。该突起包括在燃烧时与推进剂充电壳体底部分离的大块部分。射弹体的后部由形成点火元件的可燃材料的护套包围，护套从药筒壳底部延伸到至少推进剂充电套的中部并具有纵向延伸部分12。巨大的投影允许在推进剂的燃烧期间充电以分离高气体压力的积聚，由此特别地，以均匀和可再现的方式，点火元件点燃散装粉末推进剂电荷短时间。因此，通过改善射弹长度l1与射弹直径d1的关系，在不增加弹匣长度的情况下，实现目标有效质量的增加和射弹长度的增加。

2. 发明授权

US4619202A Multiple purpose ammunition 失效
标题翻译：多用途弹药
公开(公告)号：US4619202A
公开(公告)日：1986-10-28
申请号：US682206
申请日：1984-12-17
申请人： Rudolf Romer , Michael Schwenzer , Reinhard Synofzik
发明人： Rudolf Romer , Michael Schwenzer , Reinhard Synofzik
IPC分类号： F42B12/12 , F42B5/02 , F42B5/08 , F42B5/16
CPC分类号： F42C19/083 , F42B5/02 , F42B5/08
摘要： A multi-range ammunition unit for firing at a high angle and with preselected muzzle velocities. The ammunition unit includes at least two partial propellant charges, a first one of which is fixedly mounted to the bottom of the shell casing and the second one or ones of which are fixedly mounted to the bottom of the projectile of the ammunition unit. All partial propellant charges are coaxially arranged with respect to the shell casing. Mechanical and/or electrical ignition means are provided to first ignite the first propellant charge and then selectively sequentially ignite the second propellant charge or charges.
摘要翻译：一个多范围的弹药单元，以高角度射击，并具有预选的枪口速度。弹药单元包括至少两个部分推进剂装料，其中第一部分推进剂装料固定地安装在壳体的底部，第二个或第二部分固定地安装在弹药装置的射弹的底部。所有部分推进剂装料相对于外壳同轴布置。提供机械和/或电气点火装置以首先点燃第一推进剂装料，然后选择性地顺序地点燃第二推进剂装料或充电。

3. 发明授权

US4619201A Graduated-density packed propellant charge 失效
标题翻译：刻度密度包装推进剂充电
公开(公告)号：US4619201A
公开(公告)日：1986-10-28
申请号：US648798
申请日：1984-09-07
申请人： Rudolf Romer , Michael Schwenzer , Reinhard Synofzik
发明人： Rudolf Romer , Michael Schwenzer , Reinhard Synofzik
IPC分类号： F42B5/16 , F42B33/02 , C06D5/06
CPC分类号： F42B5/16 , F42B33/025
摘要： A charge formed of a mass of packed propellant is generally centered on an axis and is of radially generally uniformly and radially outwardly increasing density. This charge has a predetermined size and shape and is made by first filling particulate propellant into a chamber centered on an axis and defined by side walls extending at least generally parallel to the axis. This chamber is radially somewhat larger than the predetermined size and shape for the charge. At least some of the side walls are then displaced radially inward to reduce the volume of the chamber until the reduced chamber generally has the size and shape for the charge. The weight of the particulate propellant filled into the chamber is equal to the desired weight for the charge. The tail of a projectile is positioned in the chamber before filling the particulate propellant into the chamber. The projectile downwardly closes the chamber and can be raised after the mass is packed to push it up out of the chamber.
摘要翻译：由大量的包装推进剂形成的电荷通常以轴线为中心，并且径向地大致均匀且径向向外增加密度。该装料具有预定的尺寸和形状，并且通过首先将颗粒状推进剂填充到以轴线为中心并由至少大致平行于轴线延伸的侧壁限定的室中来制造。该室径向地稍大于用于充电的预定尺寸和形状。至少一些侧壁然后径向向内移动以减小腔室的体积，直到减压腔通常具有用于电荷的尺寸和形状。填充到室中的颗粒状推进剂的重量等于电荷的期望重量。在将颗粒状推进剂装入室之前，将射弹的尾部定位在腔室中。抛射体向下关闭室，并且可以在物料被包装之后将其推出室外。

4. 发明授权

US4722282A Payload-carrying projectile 失效
标题翻译：有载载弹体
公开(公告)号：US4722282A
公开(公告)日：1988-02-02
申请号：US937029
申请日：1986-11-10
申请人： Reinhard Synofzik , Rolf Hellwig
发明人： Reinhard Synofzik , Rolf Hellwig
IPC分类号： F42B23/00 , F42C1/14 , F42C15/42 , H01Q1/08 , H01Q1/12 , H01Q1/28 , F42B11/18 , F42B11/00
CPC分类号： F42C15/42 , F42C1/14 , H01Q1/081 , H01Q1/1235 , H01Q1/281
摘要： A payload-carrying projectile 1 includes a sensor 16 and a sensor carrier 15 disposed in a launch-resistant manner in a recess 14 in the tail section 11 of the projectile 1. After impact of the projectile, which is stabilized by extendable vanes 12, in the target area, where it may penetrate the ground as necessary, the object is to deploy the sensor from its protected position inside the projectile 1and to place it as high as possible above the surface of the ground. For this purpose, the sensor 16 is connected with a concertina bellows 15 which for its part leads into a reservoir 13a which is disposed in the projectile, and which is filled with polyurethane foam mixed with a propellant gas under high pressure. The connection of the reservoir 13 with the concertina bellows 15 is made via a valve 13c which is regulated by an electronic control element 13a containing, for instance, a timer switch. After the opening of the valve 13 c the polyurethane foam 17 enters the concertina bellows 15 and expands it, thereby expelling the sensor 16 from the recess 14. Finally, the polyurethane foam 17 hardens, so that the now extended concertina bellows 15 provides a safe support for the deployed sensor 16.
摘要翻译： PCT No.PCT / EP86 / 00043 Sec。 371日期：1986年11月10日 102（e）1986年11月10日日期PCT提交1986年1月31日PCT公布。出版物WO86 / 05266 日期：1986年9月12日。有载荷的弹丸1包括传感器16和传感器载体15，传感器载体15以防弹的方式设置在射弹1的尾部11中的凹部14中。在射弹的撞击之后通过在目标区域中的可延伸叶片12稳定，其中它可以根据需要穿透地面，目的是将传感器从其被保护的位置部署在射弹1内部并且将其尽可能高地放置在地面以上。为此目的，传感器16与手风琴波纹管15连接，该波纹管15的一部分导入设置在射弹中的储存器13a，并且在高压下填充有与推进剂气体混合的聚氨酯泡沫。储存器13与三角波箱波纹管15的连接通过阀13c制成，阀13c由包含例如定时开关的电子控制元件13a调节。在阀13c打开之后，聚氨酯泡沫17进入三分音箱波纹管15并使其膨胀，从而将传感器16从凹槽14排出。最后，聚氨酯泡沫17硬化，使得现在伸展的三角裤波纹管15提供安全对部署的传感器16的支持。

5. 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。

6. 发明授权

US4860660A Projectile 失效
标题翻译：射弹
公开(公告)号：US4860660A
公开(公告)日：1989-08-29
申请号：US135510
申请日：1987-12-16
申请人： Reinhard Synofzik , Karl-Friedrich Doherr , Dieter Munscher , Christos Saliaris
发明人： Reinhard Synofzik , Karl-Friedrich Doherr , Dieter Munscher , Christos Saliaris
IPC分类号： F42B10/50 , F42B10/54
CPC分类号： F42B10/54 , F42B10/50
摘要： A projectile comprising a projectile body having a rear end; and a deceleration element composed of a sheet of material at the rear end, the deceleration element having an edge region and being deployable from a folded condition to an expanded condition with the aid of rotation of the projectile, the deceleration element, when in the expanded condition, having the general form of a disk with a periphery defined by the edge region and being effective for decelerating the projectile, and wherein the deceleration element is constructed such that the edge region has a higher mass density than the remainder thereof.
摘要翻译：一种抛射体，包括具有后端的射弹体; 以及减速元件，其在后端由一片材料组成，所述减速元件具有边缘区域，并且借助于所述弹丸的旋转，所述减速元件在膨胀时能够从折叠状态展开到膨胀状态具有由所述边缘区域限定的具有周边的盘的一般形式，并且对于使所述抛射体减速有效的状态，并且其中所述减速元件被构造成使得所述边缘区域具有比其余部分更高的质量密度。

7. 发明授权

US4856432A Spin stabilized carrier projectile including at least two submunition projectiles 失效
标题翻译：旋转稳定的载体射弹，包括至少两个子弹药弹
公开(公告)号：US4856432A
公开(公告)日：1989-08-15
申请号：US135508
申请日：1987-12-16
申请人： Reinhard Synofzik
发明人： Reinhard Synofzik
IPC分类号： F42B10/14 , F42B10/50 , F42B12/58 , F42B12/62
CPC分类号： F42B10/50 , F42B12/62
摘要： A spin stabilized carrier projectile having a longitudinal axis comprising: a projectile body; and at least two submunition bodies disposed in, and ejectable from, the projectile body, the submunition bodies being spaced along the axis, each submunition body having a folded, expandable deceleration means for reducing the velocity and spin of the submunition body upon ejection from the projectile body, the deceleration means including a sheet of material for producing air resistance, and the deceleration means having different dimensions for respectively different submunition bodies so that each respective submunition body is decelerated less than the submunition body disposed behind the respective submunition body.
摘要翻译：具有纵向轴线的自旋稳定的载体抛射体包括：射弹体; 以及至少两个子弹药体，其被布置在弹丸体内并且可从弹丸体中排出，所述子弹药体沿着轴线间隔开，每个子弹药体具有折叠的可扩张减速装置，用于在从弹药体弹出时缩小子弹药体的速度和旋转速度所述减速装置包括用于产生空气阻力的材料片，所述减速装置具有分别不同的子弹药体的不同尺寸，使得每个子弹药体比设置在相应的子弹药体后面的子弹药体减速。

8. 发明授权

US4805532A Deploying arrangement for an on-board targeting device of a bomblet 失效
标题翻译：部署针对小型机的目标设备的安排
公开(公告)号：US4805532A
公开(公告)日：1989-02-21
申请号：US141376
申请日：1988-01-07
申请人： Reinhard Synofzik , Manfred Busch
发明人： Reinhard Synofzik , Manfred Busch
IPC分类号： F42B25/00 , F42B10/54 , F42B30/00 , F42C19/00 , H01Q1/12 , H01Q1/28 , H01Q15/16 , F42B25/20 , F42C13/02
CPC分类号： F42B30/006 , H01Q1/1235 , H01Q1/28 , H01Q15/161
摘要： A bomblet has a casing and a targeting device provided with a reflector swingably secured to the casing. The reflector has a position of rest in which it is situated within a cross-sectional outline of the casing and a working position in which it is in a deployed state externally of the casing. A first guide arm is articulated to the reflector to provide for a relative pivotal motion about a first pivotal axis, and to the casing to provide for a relative pivotal motion about a second pivotal axis. A second guide arm is articulated to the reflector to provide for a relative pivotal motion about a third pivotal axis, and to the casing to provide for a relative pivotal motion about a fourth pivotal axis. All the pivotal axes are parallel to and spaced from one another and are perpendicular to the central longitudinal axis of the bomblet. The guide arms guide the reflector in a swinging motion from the position of rest into the working position. The reflector has a center of gravity located, in the position of rest, offset from the longitudinal axis in a direction of the swinging motion, whereby, upon rotary motion of the bomblet, the reflector is moved by centrifugal forces from the position of rest into the working position. Further, a locking engagement is provided for immobilizing the reflector in the working position.
摘要翻译：炸弹具有壳体和设置有可摆动地固定到壳体的反射器的瞄准装置。反射器具有静止位置，其位于壳体的横截面轮廓内以及处于壳体外部的展开状态的工作位置。第一引导臂铰接到反射器以提供关于第一枢转轴线的相对枢转运动，并且提供到壳体以提供围绕第二枢转轴线的相对枢转运动。第二引导臂铰接到反射器以提供关于第三枢转轴线的相对枢转运动，并且连接到壳体以提供围绕第四枢转轴线的相对枢转运动。所有的枢转轴线彼此平行并且彼此间隔开并且垂直于炸弹的中心纵向轴线。引导臂将反射器从静止位置的摆动运动引导到工作位置。反射器具有重心的位置，其位置在摆动运动的方向上从纵向轴线偏移，由此，在炸弹的旋转运动时，反射器通过离心力从静止位置移动到工作岗位。此外，提供锁定接合以将反射器固定在工作位置。

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