专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

11. 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。

12. 发明授权

US4702167A Propellant-charge module 失效
标题翻译：推进剂充电模块
公开(公告)号：US4702167A
公开(公告)日：1987-10-27
申请号：US858209
申请日：1986-06-06
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 primer 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 primer charge is of such high combustibility, compared to the diameter of the passage, that the entire primer charge, even of a stack of such packs, will be ignited before they burn through and set off the respective propellant charges.
摘要翻译： PCT No.PCT / EP85 / 00433 Sec。 371日期：1986年6月6日 102（e）日期1986年6月6日PCT提交1985年8月24日PCT公布。公开号WO86 / 01584 日期：1986年3月13日。推进剂 - 充电组件具有环形外壳，其具有沿轴线延伸并居中的外壁，一对轴向间隔开的端壁，其从轴线横向向内延伸并具有以轴线为中心的内周边，以及在所述端壁的内周面之间限定清楚的轴向穿过通道的内壁。外壳通常围绕轴线轴对称，即其形成为旋转体或正多边形截面，并且基本上对称于垂直于端壁之间的轴线的平面。相对容易点燃的引物电荷形成对称于该平面的内壁的一部分，并且推进剂电荷填充内壁外侧的封套。与通道的直径相比，底漆装料具有如此高的可燃性，即使是这样的包装的堆叠，整个底漆装料将在它们燃烧之前被点燃并且排出相应的推进剂装料。

13. 发明申请

US20100192797A1 WARHEAD 失效
标题翻译：弹头
公开(公告)号：US20100192797A1
公开(公告)日：2010-08-05
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： F42B12/24 , F42B10/02 , F42C13/00
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。

14. 发明申请

US20050188877A1 Gas pressure switch 有权
标题翻译：气压开关
公开(公告)号：US20050188877A1
公开(公告)日：2005-09-01
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： F42C15/20 , F42B3/00 , F42B3/12 , F42C15/30 , F42C19/06 , H01H35/24 , F42C15/40 , F41F5/00
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。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。

15. 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。

16. 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。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式