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公开(公告)号：US4616567A
公开(公告)日：1986-10-14
申请号：US747565
申请日：1985-06-20
CPC分类号： F42B12/58
摘要： A method and apparatus for covering a target area with ammunition, wherein a container, which contains active bodies W arranged on different decks 30.1, 30.2 and which is to be brought over the target area, releases the active bodies W through release openings 34 on its sides to become effective from above on respective individual flight paths against objects, for example armored vehicles, present in the target area.
摘要翻译： 一种用弹药覆盖目标区域的方法和装置，其中包含布置在不同甲板30.1,30.2上并且将被覆盖在目标区域上的活动物体W的容器通过其上的释放开口34释放活性物体W 双方将在相应的个别飞行路线上从对上述目标区域内的物体（例如装甲车辆）开始生效。
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公开(公告)号：US4555971A
公开(公告)日：1985-12-03
申请号：US398242
申请日：1982-07-14
CPC分类号： F42B12/58
摘要： In the method and apparatus for covering a target area with ammunition, a container, which contains active bodies W arranged on different decks 30.1, 30.2 and which is to be brought over the target area, releases the active bodies W through release openings 34 on its sides to become effective from above on respective individual flight paths against objects, for example armored vehicles, present in the target area.
摘要翻译： 在用弹药覆盖目标区域的方法和装置中，包含布置在不同甲板30.1,30.2上并将被覆盖在目标区域上的活动物体W的容器通过其上的释放开口34将活性物体W释放 双方将在相应的个别飞行路线上从对上述目标区域内的物体（例如装甲车辆）开始生效。
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公开(公告)号：US4177733A
公开(公告)日：1979-12-11
申请号：US834496
申请日：1977-09-19
申请人： Rudolf Romer , Manfred Moll , Christian Jaeneke
发明人： Rudolf Romer , Manfred Moll , Christian Jaeneke
CPC分类号： F42B14/064 , F42B14/02
摘要： There is described a spin stabilized projectile assembly including a projectile, a sabot, and a guide ring. The projectile is provided with a shoulder at the rear end of which abuts the sabot, the projectile and sabot being connected by the guide ring which extends around the projectile and part of the sabot. The guide ring is arranged so that after the projectile assembly has been fired and has left the barrel of the weapon the sabot and the projectile separate. The sabot has a diameter substantially equal to that of the projectile; the guide ring is secured to the sabot against relative movement in a longitudinal direction but is rotatable with respect to the sabot.
摘要翻译： 描述了一种自旋稳定的射弹组件，其包括抛射物，破坏物和引导环。 抛射体在其后端设有一个肩部，其肩部与导弹环相连，弹丸和突起通过围绕射弹和部分炮弹延伸的引导环连接。 引导环布置成使得在射弹组装已经被射出并且已经离开武器的枪管之后，将弹药和弹丸分开。 炮弹的直径与射弹的直径基本相等; 引导环固定到砧座上以防止在纵向方向上的相对运动，但是可以相对于砧座旋转。
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公开(公告)号：US4362107A
公开(公告)日：1982-12-07
申请号：US84758
申请日：1979-10-15
申请人： Rudolf Romer , Christian Jaeneke , Gunter Sikorski
发明人： Rudolf Romer , Christian Jaeneke , Gunter Sikorski
摘要： Practice projectile for target practice, which corresponds in shape and weight to a normal combat projectile, particularly to a sub-caliber combat projectile. The projectile upon impact disintegrates at preset breaking points. The projectile is unitary, but has at least one preset breaking point along its length. The projectile may be constructed as a tail-stabilized arrow-shaped projectile with a propulsive sabot extending over the preset breaking line and the preset breaking line may be positioned in the zone of the minimum firing loading.
摘要翻译： 对于目标实践的射弹，其形状和重量对应于正常的作战射弹，特别是对于低射炮作战射弹。 撞击后的弹丸在预先设定的断点处分解。 射弹是一体的，但沿其长度至少有一个预设的断点。 抛射体可以被构造为具有延伸在预设断裂线上的推进式突起的尾部稳定的箭头状射弹，并且预设的断裂线可以定位在最小燃烧负载的区域中。
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公开(公告)号：US4242960A
公开(公告)日：1981-01-06
申请号：US970182
申请日：1978-12-18
CPC分类号： F42B8/14
摘要： There is disclosed a missile which automatically disintegrates after a predetermined flight time. The missile is made up of several parts which are positively secured together by a locking means which is released at a predetermined time after the firing of the missile by the action of the air through which the missile passes during its flight. The invention may by used to advantage in both practice missiles and service missiles.
摘要翻译： 公开了一种在预定飞行时间后自动分解的导弹。 导弹由多个部件组成，这些部件通过锁定装置牢固地固定在一起，该锁定装置在导弹通过飞行中通过的空气的作用而被射击之后的预定时间被释放。 本发明可以在实践导弹和服务导弹中有利地使用。
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公开(公告)号：US4153223A
公开(公告)日：1979-05-08
申请号：US801426
申请日：1977-05-27
摘要： There is disclosed a limited range, high-speed projectile with a flat trajectory. The range is limited by controlling the air resistance of the projectile, so that the air resistance increases markedly when the projectile speed drops below a certain value.
摘要翻译： 公开了一种有限范围的，具有平坦轨迹的高速射弹。 通过控制射弹的空气阻力来限制射程，当射弹速度低于一定值时，空气阻力显着增加。
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公开(公告)号：US4577813A
公开(公告)日：1986-03-25
申请号：US153921
申请日：1980-05-05
申请人： Rudolf Romer , Manfred Moll
发明人： Rudolf Romer , Manfred Moll
CPC分类号： F42B12/14
摘要： A weapons system, especially for foot attack upon armored vehicles, has a recoilless firing tube and a discus-shaped projectile. The projectile is provided with a fork having an upper arm and a lower arm and a stabilizer connected to the fork and including a tube having a longitudinal axis and fins at the opposite end. An explosive charge is carried by a hub of the fork and a disk-shaped body is rotatable about the hub between the arms of the fork by a portion of propellant gases to stabilize the projectile along its flight toward a target.
摘要翻译： 一个武器系统，特别是对装甲车辆的脚部攻击，具有无后坐力的射击管和铁饼形弹丸。 射弹设置有具有上臂和下臂的叉，以及连接到叉的稳定器，并且包括在相对端具有纵轴和翅片的管。 爆炸装药由叉的轮毂承载，并且盘形主体可以通过推进剂气体的一部分在叉子的臂之间围绕轮毂旋转，以将射弹沿着其飞行朝向目标稳定。
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公开(公告)号：US5836540A
公开(公告)日：1998-11-17
申请号：US477121
申请日：1995-03-24
申请人： Rudolf Romer , Gerd Wollmann
发明人： Rudolf Romer , Gerd Wollmann
CPC分类号： F42B10/661 , F41G7/222
摘要： A projectile having a longitudinal axis, a sensor disposed in the substantially pointed front end of the projectile for detecting a respective target, and electronics connected to the output of the sensor for igniting a correction charge to effect a correction of the flight path of the projectile by a predetermined angle (.delta..sub.0). In order to install the apparatus for flight-path correction into the respective projectile completely and in a space-saving manner, so that, unlike in known projectiles, corresponding evaluation and signal-transmission units in the respective weapon carrier can be omitted and complicated gyroscopic systems in the projectile can be omitted, the sensor determines the angle (.delta.) between the longitudinal axis of the projectile and the line (target line) connecting the projectile and the target, and when an angle (.delta..sub.0) is reached that is identical in size/magnitude to the deviation caused by the respective correction charge, the electronics ignite this charge.
摘要翻译： 具有纵向轴线的抛射体，设置在用于检测相应目标的射弹的基本上尖的前端的传感器，以及连接到传感器的输出端的电子装置，用于点燃校正电荷以实现弹丸飞行路径的校正 以预定角度（delta 0）。 为了将飞行路径校正装置完全安装在相应的抛射体中，节省空间，使得与已知的射弹不同，可以省略各个武器载体中的相应的评估和信号传输单元，并且可以使陀螺仪 射弹中的系统可以省略，传感器确定射弹的纵轴与连接射弹与目标的线（目标线）之间的角度（delta），以及达到相同角度（delta 0）时的角度 在大小/幅度上由相应的校正电荷引起的偏差，电子装置点燃这种电荷。
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9.发明授权Method and apparatus for determining the roll angle position of a rotating flying body 失效用于确定旋转飞行体的侧倾角位置的方法和装置
公开(公告)号：US5661555A
公开(公告)日：1997-08-26
申请号：US438019
申请日：1995-05-08
申请人： Rudolf Romer , Gerd Wollmann , Helmut Misoph
发明人： Rudolf Romer , Gerd Wollmann , Helmut Misoph
摘要： A method and apparatus for determining the roll angle position of a rotating flying body (2) relative to a fixed station (1) with the aid of a laser (3) light beam (4, 24) emitted by the fixed station (1) and received by the flying body (2). To determine the roll angle position of the flying body located at an arbitrary position within the guide beam (4) precisely and simply, a phase-coded laser light beam (guide beam) is produced with the aid of an optical element, particularly a holographic optical element (6). This guide beam (14) is then decoded in a receiving apparatus (8) of the flying body by means of a further holographic element (11) that is rigidly connected to the flying body (2). The further holographic element (11) is configured such that maximum brightness or intensity only occurs at the receiving detector (13) if it is located parallel to the holographic element (11) on the side of the laser (3), i.e., non-mirror-symmetric information must be impressed upon the guide beam (4).
摘要翻译： 借助于由固定站（1）发射的激光（3）光束（4,24）来确定旋转飞行体（2）相对于固定站（1）的侧倾角位置的方法和装置， 并由飞行体（2）接收。 为了精确和简单地确定位于导向梁（4）内的任意位置的飞行体的侧倾角位置，借助于光学元件特别是全息照相机产生相位编码的激光束（引导光束） 光学元件（6）。 然后，通过刚性地连接到飞行体（2）的另外的全息元件（11），将该引导光束（14）在飞行体的接收装置（8）中解码。 另外的全息元件（11）被配置为使得最大亮度或强度仅在接收检测器（13）处发生，如果它位于与激光器（3）侧面上的全息元件（11）平行的位置上， 反射镜对称信息必须印在引导梁（4）上。
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公开(公告)号：US4444114A
公开(公告)日：1984-04-24
申请号：US68865
申请日：1979-08-21
申请人： Bernhard Bisping , Rudolf Romer , Klaus Gerbach , Peter Wallow
发明人： Bernhard Bisping , Rudolf Romer , Klaus Gerbach , Peter Wallow
CPC分类号： F42B14/061 , Y10S102/703
摘要： A munitions round for a subcaliber projectile to be fired from a barrel-type weapon has a casing receiving the projectile which is at least partially surrounded by the gas-generating propellant charge. A drive body is mounted at the forward end of the projectile and has a rearward pressure-receiving surface which droops inwardly toward the projectile from an outer edge of the body which is engaged by the casing. The body is formed from a plurality of segments which form-fittingly hug the projectile and have confronting angularly spaced separating surfaces bridged by a sealing member. The forward end of the body, formed by the segments, is concave forwardly and has a leading edge which is disposed outwardly and axially ahead of the rearward inner edge of this surface which forms a pocket engaging the air upon propulsion of the projectile from the barrel to effect separation of the segments and dislodgment of the body.
摘要翻译： 用于从桶型武器发射的子弹射弹的弹药具有容纳至少部分地被气体产生推进剂装料包围的射弹的壳体。 驱动体安装在射弹的前端，并且具有向后朝向受压面的向后压力接收表面，其从与壳体接合的主体的外边缘朝向射弹向内倾斜。 主体由形成适合地拥抱射弹并且具有由密封构件桥接的面对的有角度间隔开的分隔表面的多个段形成。 由该段形成的主体的前端是向前凹入的，并且具有前缘，该前缘在该表面的向后的内边缘之后向外并且轴向地设置，该前缘形成了在将抛射体从枪管推进时与空气接合的口袋 以实现片段的分离和身体的分离。
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