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1. 发明授权

US4693434A Self-deploying stabilizing-vane assembly for projectile 失效
标题翻译：用于射弹的自展式稳定叶片组件
公开(公告)号：US4693434A
公开(公告)日：1987-09-15
申请号：US779228
申请日：1985-09-23
申请人： Michael Schwenzer , Armin Eskam , Walter Simon , Wilfried Becker
发明人： Michael Schwenzer , Armin Eskam , Walter Simon , Wilfried Becker
IPC分类号： F42B10/14 , F42B13/32
CPC分类号： F42B10/14 , Y10T403/11
摘要： A vane assembly for a projectile has a carrier carrying a plurality of pivots, having at the pivots respective carrier elements, and adapted to be secured to an end of the projectile. Respective vane elements are each pivotal on the pivots between an inner position lying immediately adjacent the respective carrier element and within a projection of the projectile and an outer deployed position projecting beyond the projection. Respective heat-destructible pins engaged between the vane elements and the respective carrier elements normally retain the vanes in the inner position and release the vanes for movement into the outer position when destroyed by heat. The carrier element is a rib of the carrier against which the respective vane lies when not deployed. In addition, relative to a normal longitudinal direction of travel of the projectile carrying the assembly, the vanes extend longitudinally in the direction and have relative to the direction front leading ends engaging the respective pins and rear trailing ends at the respective pivots.
摘要翻译：用于抛射体的叶片组件具有承载多个枢轴的载体，所述枢轴在枢转相应的载体元件处并且适于固定到射弹的端部。相应的叶片元件各自在位于紧邻相应的承载元件的内部位置之间并且在射弹的突出部内的突出部和突出超过突出部的外部展开位置之间的枢轴上枢转。接合在叶片元件和相应载体元件之间的相应的可热破坏的销通常将叶片保持在内部位置，并且当被热量破坏时释放叶片以移动到外部位置。载体元件是载体的肋，当未展开时，相应的叶片位于该肋上。此外，相对于承载组件的弹丸的正常的纵向运动方向，叶片沿着该方向纵向延伸并且相对于在相应枢轴处与相应销和后尾端接合的前方前端的方向。

2. 发明授权

US5433399A Device for guiding a missile 失效
标题翻译：导弹导弹装置
公开(公告)号：US5433399A
公开(公告)日：1995-07-18
申请号：US253036
申请日：1994-06-02
申请人： Wilfried Becker , Werner Grosswendt , Michael Schwenzer
发明人： Wilfried Becker , Werner Grosswendt , Michael Schwenzer
IPC分类号： F41G9/00 , F42B10/00 , F42B10/60 , F42B10/66 , F42B15/01
CPC分类号： F42B10/661
摘要： The invention relates to a device for guiding a missile (1; 30) with a missile tip (2) and a cylindrical section (3) adjoining the tip of the missile; the device is provided with at least one control block (4; 31, 32) with exhaust openings (13-15) of corresponding nozzle bodies (10-12) arranged perpendicularly in relation to the missile's surface.In order to accomplish effective guidance, particularly of high-speed missiles (1; 30), in a simple and cost-effective manner it is proposed that the control block (4; 31, 32) be constructed with a plurality of small, fast-burning rocket motors (7-9; 33-36) that are arranged radially on the missile's periphery (1; 30) and that are ignitable in a predeterminable sequence and number.
摘要翻译：本发明涉及一种引导导弹（1; 30）与导弹尖端（2）和邻接导弹尖端的圆柱形部分（3）的装置; 该装置设置有至少一个控制块（4; 31,32），其具有相对于导弹表面垂直布置的相应喷嘴体（10-12）的排气口（13-15）。为了实现特别是高速导弹（1; 30）的有效指导，以简单且具有成本效益的方式提出控制块（4; 31,32）由多个小型，快速的 - 发射火箭发动机（7-9; 33-36），其放射状地布置在导弹的周边（1; 30）上，并且以可预定的顺序和数量可点燃。

3. 发明授权

US08528480B2 Warhead 失效
标题翻译：弹头
公开(公告)号：US08528480B2
公开(公告)日：2013-09-10
申请号：US12602460
申请日：2008-05-15
申请人： Wolfgang Seidel , Michael Schwenzer
发明人： Wolfgang Seidel , Michael Schwenzer
IPC分类号： F42B12/22
CPC分类号： F42B12/24 , F42B10/02 , F42C13/006
摘要： The invention relates to a warhead (10) for attacking particularly half-hard and/or soft targets, wherein the warhead comprises a splinter-forming casing (1) and an explosive material positioned in the casing (1). The warhead (10) further has a front plate (2) having a splinter formation, into which a distance sensor (3) is integrated. An igniter (5) for the explosive material and a stabilizing strap for adjusting perpendicular flight characteristics on the way to the target are located in the rear part of the warhead (10), wherein the initiation of the igniter (5) is determined by a property of the target to be attacked, namely, the parameter of a defined height from the target.
摘要翻译：本发明涉及一种用于攻击特别是半硬和/或软目标的弹头（10），其中弹头包括分裂成形壳体（1）和定位在壳体（1）中的爆炸材料。弹头（10）还具有一个具有分段形成的前板（2），一个距离传感器（3）被集成在其中。用于爆炸材料的点火器（5）和用于在到达目标的路上调整垂直飞行特性的稳定带位于弹头（10）的后部，其中点火器（5）的启动由要攻击的目标的属性，即从目标定义的高度的参数。

4. 发明申请

US20090151590A1 Munition or projectile for battlefield illumination 审中-公开
标题翻译：用于战场照明的弹药或射弹
公开(公告)号：US20090151590A1
公开(公告)日：2009-06-18
申请号：US12313982
申请日：2008-11-26
申请人： Ole Dau , Alfons Sackarndt , Uwe Naderhoff , Michael Schwenzer , Ralf Aumund-Kopp , Manfred Thape , Sebastian Munzner , Martin Rybol
发明人： Ole Dau , Alfons Sackarndt , Uwe Naderhoff , Michael Schwenzer , Ralf Aumund-Kopp , Manfred Thape , Sebastian Munzner , Martin Rybol
IPC分类号： F42B4/26
CPC分类号： F42B4/26 , F42B4/28 , F42B12/42 , F42B12/62
摘要： A projectile with several flare bodies, which are eccentrically housed in the body of the projectile and are ignited by at least one delay element for each flare body. The expulsion gases are conveyed from the ogive of the projectile to the delay elements through filler elements that form a channel in the center of the projectile for the expulsion gases.
摘要翻译：具有多个弹射体的弹丸，偏心地容纳在射弹的身体中，并被每个火炬体的至少一个延迟元件点燃。排出气体通过填料元件从抛射体的原子传递到延迟元件，该元件在用于排出气体的射弹的中心形成通道。

5. 发明授权

US4864932A Propellant charge module 失效
标题翻译：推进剂充电模块
公开(公告)号：US4864932A
公开(公告)日：1989-09-12
申请号：US80270
申请日：1987-07-31
申请人： Kalrheinz Reinelt , Michael Schwenzer
发明人： Kalrheinz Reinelt , Michael Schwenzer
IPC分类号： F42B3/00 , F42B5/38
CPC分类号： F42C19/085 , F42B5/38
摘要： A propellant-charge pack has an annular envelope having an outer wall extending along and centered on an axis, a pair of axially spaced end walls extending transversely inward from the axis and having inner peripheries centered on the axis, and an inner wall defining a clear axially throughgoing passage between the inner peripheries of the end walls. The envelope is generally axially symmetrical about the axis, that is it is formed as a body of revolution or of regular polygonal section, and is substantially symmetrical to a plane perpendicular to the axis midway between the end walls. A relatively easily ignited primar charge forms a part of the inner wall symmetrical of the plane and a propellant charge fills the envelope between the walls outward of the inner wall. The primar charge is of such high combustibility, compared to the diameter of the passage, that the entire primar charge, even of a stack of such packs, will be ignited before they burn through and set off the respective propellant charges.

6. 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。

7. 发明授权

US07150228B2 Gas pressure switch 有权
标题翻译：气压开关
公开(公告)号：US07150228B2
公开(公告)日：2006-12-19
申请号：US10829278
申请日：2004-04-22
申请人： Wolfgang Scherge , Michael Schwenzer , Werner Koch
发明人： Wolfgang Scherge , Michael Schwenzer , Werner Koch
IPC分类号： F42C15/40
CPC分类号： F42C19/06 , F42B3/006 , F42C15/30 , H01H35/24
摘要： A gas pressure switch is provided for an ignition and safety system for ammunition. The switch includes a housing; a piston actuator within the housing, the piston actuator being displaceable from an idle position to a contacting position by propellant gases of the ammunition during use; at least two contact pins that are attached immovably to the housing; a contacting device operatively associated with the piston actuator and located on a first side of the piston actuator, the first side being opposite a second side on which the propellant gases act during use, the contacting device connecting electrically to the contact pins when the piston actuator is in the contacting position; and a locking pin which holds the piston actuator in the idle position until a predetermined gas pressure is reached and which shears off when the predetermined gas pressure is reached, so that the piston actuator can be displaced into the contacting position.
摘要翻译：为燃料点火和安全系统提供气体压力开关。该开关包括壳体; 所述活塞致动器在所述壳体内，所述活塞致动器在使用期间由所述弹药的推进剂气体从空闲位置移动到接触位置; 至少两个不可移动地连接到壳体的接触销; 接触装置，其与所述活塞致动器可操作地相关联并且位于所述活塞致动器的第一侧上，所述第一侧与所述推进剂气体在使用期间作用的第二侧相对，所述接触装置在所述活塞致动器处于联系状态; 以及锁定销，其将活塞致动器保持在空转位置，直到达到预定的气体压力并且在达到预定的气体压力时剪切，使得活塞致动器可以移动到接触位置。

8. 发明授权

US07118065B1 Lateral thrust control 失效
标题翻译：横向推力控制
公开(公告)号：US07118065B1
公开(公告)日：2006-10-10
申请号：US10990970
申请日：2004-11-18
申请人： Thomas Heitmann , Michael Schwenzer
发明人： Thomas Heitmann , Michael Schwenzer
IPC分类号： F42B15/01
CPC分类号： F42B10/66 , F42B10/661
摘要： A lateral thrust control is provided for influencing the flight trajectory of a projectile. The control has a main control unit; a central, axially extending main recess in the main control unit; a plurality of thruster recesses in the main control unit for accepting correction thrusters; an ignition element for one of the correction thrusters disposed in each of the thruster recesses; and at least one tubular conductor support of an electrically insulating material arranged inside the main recess of main control unit. At least some of the electrical conductors are in the form of conductive tracks fixedly arranged on the at least one tubular conductor support such that a particular contact element for a particular ignition element contacts the conductive track assigned to the particular contact element.
摘要翻译：提供横向推力控制来影响射弹的飞行轨迹。控制器有一个主控单元; 主控制单元中的中心轴向延伸的主凹槽; 主控制单元中的多个推进器凹槽，用于接收校正推进器; 用于设置在每个推进器凹部中的校正推进器之一的点火元件; 以及布置在主控制单元的主凹部内部的电绝缘材料的至少一个管状导体支撑件。至少一些电导体是固定地布置在至少一个管状导体支撑件上的导电轨迹的形式，使得用于特定点火元件的特定接触元件接触分配给特定接触元件的导电轨道。

9. 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。

10. 发明申请

US20140076191A1 SPIN-STABILIZED PROJECTILE 审中-公开
标题翻译：旋转稳定的项目
公开(公告)号：US20140076191A1
公开(公告)日：2014-03-20
申请号：US13560529
申请日：2012-07-27
申请人： Georg Abeln , Michael Schwenzer
发明人： Georg Abeln , Michael Schwenzer
IPC分类号： F42B14/02 , F42B10/26
CPC分类号： F42B14/02 , F42B10/26
摘要： A spin-stabilized projectile with a guide band which is composed of at least two annular sub-guide bands that lie axially one behind the other is provided. An object of the invention is to ensure a durability of the connection between the multi-part guide band and the corresponding projectile body of the projectile even when high centrifugal forces act on the guide band, such as those centrifugal forces that occur in artillery projectiles. To achieve this, each of the sub-guide bands lies in a separate groove of the projectile.
摘要翻译：提供了一种具有引导带的自旋稳定的抛射体，该引导带由至少两个沿轴向一个在另一个之上的环形副引导带组成。本发明的目的是确保即使当高的离心力作用于引导带上时，例如在炮弹中发生的那些离心力，也能确保多部分引导带与射弹的相应射弹体之间的连接的耐久性。为了达到这个目的，每个分导带位于抛射体的独立凹槽中。

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