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11. 发明授权

US5661555A Method and apparatus for determining the roll angle position of a rotating flying body 失效
标题翻译：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
IPC分类号： F41G7/30 , G01B11/26 , F41G7/00 , G01C1/00
CPC分类号： G01B11/26 , F41G7/305
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。

12. 发明授权

US4444114A Munitions round for barrel-type weapons 失效
标题翻译：炮弹型武器弹药
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
IPC分类号： F42B14/06 , F42B5/02
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。

13. 发明授权

US4119037A Carrier projectiles for ejectable payloads 失效
标题翻译：用于可卸载有效载荷的载体抛射体
公开(公告)号：US4119037A
公开(公告)日：1978-10-10
申请号：US746837
申请日：1976-12-02
申请人： Rudolf Romer , Rolf Hellwig , Dietmar Karius
发明人： Rudolf Romer , Rolf Hellwig , Dietmar Karius
IPC分类号： F42B12/62 , F42B13/50
CPC分类号： F42B12/62
摘要： A versatile carrier projectile for receiving and ejecting differently-sized ejectable payloads such as guided missiles and incendiary bombs is described. The payloads are disposed in successive, longitudinally spaced relation within a central cylindrical body of the projectile, with successive ones of the payloads being separated by a spacer disc. Each spacer disc carries an outwardly biased blocking rod. The outer end of each blocking rod terminates in engagement with a sawtooth-shaped groove on the inner periphery of the cylindrical body, so that the forward propulsion of the successive payloads through the cylindrical body is accomplished under a steady spring load of the blocking member on the inner wall of the cylindrical body. The front and rear portions of the cylindrical body are respectively secured to the shell head and the ignition charge container by shear pins. Other shear pins are provided to secure a drive disc to the rear portion of the ignition charge container, and a flange extending forwardly from the outer surface of the drive disc serves to normally confine the pivoted rear ends of a plurality of stabilizing wings in their retracted position until the projectile exits from the barrel of the firing weapon.
摘要翻译：描述了用于接收和弹出不同尺寸的可弹出有效载荷（例如导弹和燃烧弹）的通用载体抛射体。有效载荷在射弹的中心圆柱体内以连续的纵向间隔的关系设置，其中有效载荷的连续的一个由隔离盘隔开。每个间隔盘带有向外偏置的阻挡杆。每个阻挡杆的外端终止于圆柱体的内周上的锯齿形凹槽接合，使得连续有效载荷通过圆柱体的向前推进是在阻挡构件的稳定弹簧载荷下实现的圆柱体的内壁。圆柱体的前部和后部分别通过剪切销固定到壳体头部和点火充电容器上。提供其他剪切销以将驱动盘固定到点火充电容器的后部，并且从驱动盘的外表面向前延伸的凸缘用于通常将多个稳定翼的枢转后端限制在其缩回直到射弹从射击武器的枪管离开。

14. 发明授权

US4773328A Method of actuating a proximity fuze and device for implementing the method 失效
标题翻译：执行接近引信的方法和实现该方法的装置
公开(公告)号：US4773328A
公开(公告)日：1988-09-27
申请号：US16722
申请日：1986-12-22
申请人： Raimund Germershausen , Rudolf Romer , Hans-Egon Schepp
发明人： Raimund Germershausen , Rudolf Romer , Hans-Egon Schepp
IPC分类号： F42C13/00 , F42C13/04
CPC分类号： F42C13/00
摘要： A firing circuit for a projectile 10 includes a proximity fuze 11 which can be set to different target distances H1, H2. For the purpose of optimally combating different types of targets 13, 14, 15, a target sensor 17 is associated with the proximity fuze 11 so as to detect characteristic target properties and take care that proximity fuze 11 responds either at a height H1 or at a lower height H2, and causes an explosive charge 10a to detonate.
摘要翻译： PCT No.PCT / EP86 / 00098 Sec。 371日期1986年12月22日第 102（e）日期1986年12月22日PCT提交1986年2月25日PCT公布。出版物WO86 / 06470 日期：1986年11月6日。射弹10的点火电路包括可设置为不同目标距离H1，H2的邻近引信11。为了最佳地对抗不同类型的目标13,14,15，目标传感器17与邻近引信11相关联，以便检测特征目标属性并注意邻近引信11在高度H1或在较低的高度H2，并引起爆炸物体10a引爆。

15. 发明授权

US4708064A Impact projectile 失效
标题翻译：冲击射弹
公开(公告)号：US4708064A
公开(公告)日：1987-11-24
申请号：US412794
申请日：1982-08-23
申请人： Bernhard Bisping , Klaus Gersbach , Rudolf Romer
发明人： Bernhard Bisping , Klaus Gersbach , Rudolf Romer
IPC分类号： F42B12/06 , F42B11/00
CPC分类号： F42B12/06
摘要： An armor piercing breaking projectile using a stack of prepenetrating partial cores with interfitting centering bosses and respective cutting edges for piercing successive layers of armor.
摘要翻译：一个装甲穿刺的突击弹，使用一叠预先穿透的部分核心，具有相互配合的定心凸台和相应的切割刃，用于刺穿连续的铠甲层。

16. 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。

17. 发明授权

US4542696A Munitions round for barrel-type weapons 失效
标题翻译：炮弹型武器弹药
公开(公告)号：US4542696A
公开(公告)日：1985-09-24
申请号：US547736
申请日：1983-11-01
申请人： Bernhard Bisping , Peter Wallow , Klaus Gersbach , Rudolf Romer
发明人： Bernhard Bisping , Peter Wallow , Klaus Gersbach , Rudolf Romer
IPC分类号： F42B14/06 , F42B5/02
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, of a uniform outer cross section substantially over its entire length, 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基本上在其整个长度上的均匀外截面的壳体，接收至少部分地被气体产生推进剂装料包围的射弹。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。

18. 发明授权

US4296685A Warhead with slave missiles disposed in a firing tube 失效
标题翻译：弹头与配置在发射管中的从属导弹
公开(公告)号：US4296685A
公开(公告)日：1981-10-27
申请号：US72434
申请日：1979-09-04
申请人： Rudolf Romer , Hans-Egon Schepp
发明人： Rudolf Romer , Hans-Egon Schepp
IPC分类号： F42B12/60 , F42B25/02
CPC分类号： F42B12/60
摘要： A plurality of warheads are disposed for ejection one behind the other, axially in a load-carrying missile with slave missiles disposed in firing tubes and parachutes connected to the warheads and causing their directional, braked descent in the target area. Proximity fuses cause the firing of the slave missiles. Each warhead consists of a firing tube which is open at both ends and in which two slave missiles are disposed with a common propellant charge between them. A parachute of each of the warheads is secured to the firing tube intermediate its length.
摘要翻译：多个弹头被布置成用于在负载导弹中轴向地弹出，其中设置在与发射管连接的击发管和降落伞中并且使其在目标区域中的方向性，制动力下降的副导弹。接近保险丝会导致从属导弹的射击。每个弹头由两个开放的发射管组成，两个导弹在其间设置有普通的推进剂电荷。每个弹头的降落伞固定在其长度之上的击发管上。

19. 发明授权

US4763577A Cartridge ammunition with at least a partially combustible propellant charge cartridge casing 失效
标题翻译：至少有一部分可燃的推进剂充电墨盒套筒的弹药弹药
公开(公告)号：US4763577A
公开(公告)日：1988-08-16
申请号：US843709
申请日：1986-03-25
申请人： Rudolf Romer , Juergen Winkelmann , Horst Sabinski
发明人： Rudolf Romer , Juergen Winkelmann , Horst Sabinski
IPC分类号： F42B5/067 , F42B5/16
CPC分类号： F42B5/181 , F42B5/067 , F42C19/0826
摘要： An improved cartridge ammunition which includes an at least partially combustible shell casing and a projectile with a fin-stabilizing tail section mounted in a neck portion of the shell casing which thereby forms a first connection between the projectile and shell casing. A second connection between the projectile and shell casing is formed by means of a support element which is form-lockingly connected to both. The shell casing has a support region axially extending forwardly inside the shell casing from its bottom. The support element being mounted on said support region and being instrumental in assuring, due to its form-locking connections, that a predetermined axial force occurs in said support of element prior to disintegration thereof, between the tail section and the support region due to gas pressure build-up in the shell casing at firing of the ammunition.
摘要翻译：一种改进的弹药，其包括至少部分可燃的壳体壳体和具有安装在壳体壳体的颈部中的翅片稳定尾部的射弹，从而形成射弹和壳体壳体之间的第一连接。射弹与壳壳之间的第二连接通过与两者形成锁定连接的支撑元件形成。壳体壳体具有从其底部在壳体壳体内向内轴向延伸的支撑区域。支撑元件安装在所述支撑区域上，并且由于其形状锁定连接而有助于确保在元件的所述支撑件在其分解之前由于气体而在尾部与支撑区域之间发生预定的轴向力发射弹药时壳体内的压力积聚。

20. 发明授权

US4671181A Anti-tank shell 失效
标题翻译：反坦克壳
公开(公告)号：US4671181A
公开(公告)日：1987-06-09
申请号：US95921
申请日：1979-11-05
申请人： Rudolf Romer , Jurgen Winkelmann , Winfried Rossmann
发明人： Rudolf Romer , Jurgen Winkelmann , Winfried Rossmann
IPC分类号： F42B12/06 , F42B14/06 , F42B11/06
CPC分类号： F42B12/06 , F42B14/061
摘要： An armor-piercing projectile has a steel jacket threadedly or otherwise positively connected with a core which has a forwardly projecting point and leaves a space to the rear of the jacket receiving an incendiary charge and a winged tail unit mechanically connected with that charge. Upon penetration of an armor plate, the tail unit is torn from the jacket and extracts the incendiary charge which then ignites and destroys the surrounding armor.
摘要翻译：穿甲弹射弹具有与外壳螺纹或以其他方式正确连接的钢护套，该芯具有向前突出的点，并且将空间留在护套的后部，并接收燃烧电荷和与该电荷机械连接的翼状尾部单元。在装甲板穿透后，尾部由夹克撕开，并提取燃烧装置，然后点燃并摧毁周围的装甲。

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