专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明公开

EP0022431A3 Shoulder support for fire arms 失效
标题翻译：肩负支撑火灾
公开(公告)号：EP0022431A3
公开(公告)日：1981-04-29
申请号：EP80850084
申请日：1980-06-10
申请人： Förenade Fabriksverken
发明人： Annerfalk, Karl-Erik
IPC分类号： F41F03/04 , F41C23/00 , F41C27/00
CPC分类号： F41A35/06 , F41C23/00 , F41F3/0455
摘要： A combined shoulder support-cheek support for fire arms of the type, comprising a barrel (3-5) on which the shoulder support-cheek support (6) is mounted. The shoulder support is formed so that it can be optionally adapted to right handed marksmen or left handed marksmen and it comprises a box (13) which is mounted directly on the barrel (3) and which at the upper side and lower side respectively carries a support bar (20, 21). The support bars (20, 21) are interconnected at their rear ends by means of a hinge ribbon (19) which extends through the box, and at the support bar ends which can be fold out the support bars (20, 21 ) are interconnected by means of a shoulder support ribbon (18) which extends freely through the said box and which is of such length that either of the support bars (20, 21) can be fold out to a position substantially at right angle to the box (13) whereas the opposite support bar provides a stop for such folding out

2. 发明公开

EP0226761A3 Release and alignment mechanism for jet-propelled projectiles 失效
标题翻译：喷气推进弹的释放和对准机制
公开(公告)号：EP0226761A3
公开(公告)日：1987-09-30
申请号：EP86115007
申请日：1983-07-06
申请人： BRUNSWICK CORPORATION
发明人： Baker, Alan Clark , Shiovitz, Nathan N. , Whiting, George E.
IPC分类号： F41F03/04 , F41C27/06
CPC分类号： F41F3/048 , F41C27/06 , F41F3/052
摘要： A projectile release mechanism is disclosed for facilitating launching a jet-propelled projectile in the form of a spherical spin-stabilized missile. The mechanism includes a nozzle (48) extending from the projectile (10) including fusible joint means (54) for heating by high-temperature exhaust gases expelled by the projectile to release the projectile. A projectile support includes an open-ended receptacle (28) generally coaxial with the nozzle for receiving the nozzle (48) and thereby supporting the projectile (10). Forwardly and rearwardly facing shoulders (61, 62) on the receptacle (28) engage complementary rearwardly and forwardly facing shoulders (64, 68) on the nozzle (48) for retaining the nozzle in the receptacle and permitting fore and aft sections (50, 52) of the nozzle to move out of the open ends (44, 46) of the receptacle (28) on fusing and separation of the fusible joint means (54). The forwardly facing shoulder (61) on the receptacle (28) and the rearwardly facing shoulder (64) on the nozzle (48) comprise conical sections generally concentric with the axis of the nozzle. Springs (72) are operatively associated with the nozzle (48) and are effective to maintain the shoulder portions in engagement until complete separation of the fusible joint (54), thereby accommodating any thermal expansion of the nozzle.
摘要翻译：公开了一种抛射释放机构，用于促进以球形自旋稳定导弹的形式发射喷射推进的抛射体。该机构包括从射弹（10）延伸的喷嘴（48），包括易熔接头装置（54），用于由射弹排出的高温废气加热以释放射弹。抛射体支撑件包括与喷嘴大致共轴的开放式容器（28），用于接收喷嘴（48）并由此支撑射弹（10）。容器（28）上的朝前和朝后的台肩（61,62）接合喷嘴（48）上的互补的朝后和朝前的台肩（64,68），用于将喷嘴保持在容器中并允许前后部分（50,52）当熔合接合装置（54）熔合和分离时，喷嘴（52,52）移出容器（28）的开口端（44,46）。容器（28）上的朝前的肩部（61）和喷嘴（48）上朝后的肩部（64）包括通常与喷嘴的轴线同心的锥形部分。弹簧72可操作地与喷嘴48相关联并且有效地保持肩部接合直到可熔接头54完全分离，由此适应喷嘴的任何热膨胀。

3. 发明申请

WO1998040687A1 SHELTERING APPARATUS AND METHOD OF SHELTERING SAME 审中-公开
标题翻译：剥离装置及其剥离方法
公开(公告)号：WO1998040687A1
公开(公告)日：1998-09-17
申请号：PCT/IB1997001121
申请日：1997-08-08
申请人： INTERNATIONAL DESIGN SYSTEMS COMPANY , AL-SABAH, Sabah, Naser , WUSTHOF, Peter , WIRZBERGER, Erich
发明人： INTERNATIONAL DESIGN SYSTEMS COMPANY
IPC分类号： F41F03/04
CPC分类号： F41F3/04
摘要： An apparatus (20) and methods are provided for sheltering and/or launching devices (p) such as projectiles or a tracking device. The apparatus (20) preferably includes a main body (30) having a bottom (31), a plurality of walls (32, 33, 36, 37) connecting to and extending upwardly from the bottom (31), and an inner chamber (35) defined by the inner confines of the bottom (31) and the plurality of walls (32, 33, 36, 37). An inner chamber cover (41, 43) is connected to the main body (30) for covering the inner chamber (35) of the main body (30) when in a closed position and for accessing the inner chamber (35) when in an open position. A sheltered device mount preferably is positioned in the inner chamber (35) and connected to the main body (30) for mounting a device (p) to be sheltered thereto. A sheltered device mount extender and retractor (50) is connected to the sheltered device mount for extending the sheltered device mount upwardly from the bottom (31) simultaneous with the opening of the inner chamber cover (41, 43) to thereby position the sheltered device mount downwardly toward the bottom (31) simultaneous with the closing of the inner chamber (35) cover to thereby position the sheltered device mount for sheltering.
摘要翻译：提供了用于遮蔽和/或发射诸如射弹或跟踪装置的装置（p）的装置（20）和方法。装置（20）优选地包括具有底部（31）的主体（30），连接到底部（31）并从底部（31）向上延伸的多个壁（32,33,36,37）和内部室 35）由底部（31）和多个壁（32,33,36,37）的内部限定。当处于关闭位置时，内室盖（41,43）连接到主体（30），用于在主体（30）内部覆盖主体（30）的内室（35）开仓防护装置安装件优选地定位在内室（35）中并且连接到主体（30），用于安装待遮蔽的装置（p）。防护装置安装式延伸器和牵开器（50）连接到遮蔽装置安装件，用于与内室盖（41,43）的开口同时从底部（31）向上延伸遮蔽装置安装件，从而将遮蔽装置与内室（35）盖的关闭同时向下安装到底部（31），从而定位用于遮蔽的遮蔽装置安装座。

4. 发明公开

EP0119569A3 Hand held rocket launcher 失效
标题翻译：手提式摇篮
公开(公告)号：EP0119569A3
公开(公告)日：1985-05-15
申请号：EP84102637
申请日：1984-03-10
申请人： PAINS-WESSEX LIMITED
发明人： Cutler, Peter Robert Thomas
IPC分类号： F41F03/04
CPC分类号： F41F3/077 , F41F3/04 , F41F3/042
摘要： The rocket launcher comprises a launch tube 11 mounted on a handle 14, the handle being rotatable relative to, and about the axis of, the launch tube to operate a striker 20 for firing a rocket 10 located within the launch tube. The launch tube is of hollow wall construction and permits propulsion gases discharged from the rocket upon ignition to enter the space between the walls 11a, 11 b, and flow forwardly, out of contact with the rocket, discharging from outlets at the forward end of the tube.
摘要翻译：火箭发射器包括安装在手柄14上的发射管11，手柄能够相对于发射管的轴线并且围绕发射管的轴线旋转，以操作用于点燃位于发射管内的火箭10的撞针20。发射管具有中空壁结构，并允许在点燃时从火箭排出的推进气体进入壁11a，11b之间的空间，并且向前流动，与火箭不接触，从管的前端处的出口排出。

5. 发明公开

EP0090184A3 Practice rocket 失效
标题翻译：实践摇滚
公开(公告)号：EP0090184A3
公开(公告)日：1983-11-30
申请号：EP83101908
申请日：1983-02-26
申请人： HÜLS TROISDORF AKTIENGESELLSCHAFT
发明人： Mathey, Christoph
IPC分类号： F42B15/32 , F42B13/16 , F42B09/20 , F42B13/20 , F41F03/04
CPC分类号： F42B8/24 , F41F3/048 , F42B14/061
摘要： Übungsrakete zum Abschuß aus einem Original-Wer ferrohr für den scharfen Schuß, bei welcher der äußere Durchmesser kleiner als derjenige der Originalrakete für den scharfen Schuß ist und die Übungsrakete zur Führung im Werferrohr mit - in Längsrichtung betrachtet - im Ab stand voneinander angeordneten, beim Abschuß an der Werferrohrwandung entlang gleitenden Distanzelementen versehen ist.

6. 发明公开

EP0223082A3 Release and alignment mechanism for jet-propelled projectiles 失效
公开(公告)号：EP0223082A3
公开(公告)日：1987-09-16
申请号：EP86114479
申请日：1983-07-06
申请人： BRUNSWICK CORPORATION
发明人： Baker, Alan Clark , Shiovitz, Nathan N. , Whiting, George E.
IPC分类号： F41F03/04 , F41C27/06
CPC分类号： F41F3/048 , F41C27/06 , F41F3/052
摘要： A projectile release mechanism is disclosed for facilitating launching a jet-propelled projectile in the form of a spherical spin-stabilized missile. The mechanism includes a nozzle extending from the projectile, including fusible joint means for heating by high-temperature exhaust gases expelled by the projectile to release the projectile. A projectile support includes an open-ended receptacle generally coaxial with the nozzle for receiving the nozzle and thereby supporting the projectile. Forwardly and rearwardly facing shoulders on the support engage complementary rearwardly and forwardly facing shoulders on the nozzle for retaining the nozzle in the receptacle and permitting fore and aft sections of the nozzle to move out of the open ends of the receptacle on fusing and separation of the fusible joint means. The forwardly facing shoulder on the support means and the rearwardly facing shoulder on the nozzle comprise conical sections generally concentric with the axis of the nozzle. Springs are operatively associated with the nozzle and are effective to maintain the shoulder portions in engagement until complete separation of the fusible joint, thereby accommodating any thermal expansion of the nozzle.

7. 发明公开

EP0022756A3 Muzzle cover for fire tube arms 失效
标题翻译：用于火管的MUZZLE盖子
公开(公告)号：EP0022756A3
公开(公告)日：1981-05-06
申请号：EP80850085
申请日：1980-06-10
申请人： Förenade Fabriksverken
发明人： Annerfalk, Karl-Erik
IPC分类号： F41C21/14 , F41F03/04
CPC分类号： F41F3/077 , F41A35/04 , F41F3/042
摘要： A muzzle cover for fire arms of the type having a barrel (5) through which a shell or a similar projectile is intended to be launched. The muzzle cover is made of an elastic material and comprises a collar (12) which carries a flexible diaphragm (13) and which is adapted to be pushed over the muzzle of the barrel (5). The diaphragm (13) is bowed concavely inwards and is integral with the collar (12) over a recess (15) which is bowed convexly outwards and has a reduced thickness of material as compared with the diaphragm (13). The recess (15) provides a kerf for removing the diaphragm (13) when the pressure in the barrel (5) has increased to a predetermined level when the shell or similar projectile is launched. The collar (12) is slightly conical so that the muzzle cover can be forced onto the barrel, and the collar (12) has a successively reduced thickness in the direction rearwardly.

8. 发明公开

EP0022430A3 Expendable type weapon system 无效
标题翻译：支付型武器系统
公开(公告)号：EP0022430A3
公开(公告)日：1981-05-06
申请号：EP80850083
申请日：1980-06-10
申请人： Förenade Fabriksverken
发明人： Annerfalk, Karl-Erik
IPC分类号： F41F03/04 , F41F15/00 , F41C17/08
CPC分类号： F41A19/29 , F41A17/46 , F41F3/0455
摘要： A weapon system of the expendable type comprising both an ammunition part (1) having a barrel (3), ammunition and a fuze means (10, 11), and a weapon part (2) having a firing mechanism (12) and a sighting mechanism (13). The weapon part (2) is designed for being connected to a connection means (9) of the ammunition part (1) and to be locked (41) in such connected position. The firing mechanism (12) of the weapon part (2) comprises several coacting catches (27, 37; 39,41; 39, 42; 29,32) for preventing any type of shooting by misadventure.

9. 发明申请

WO2003033348A3 LAUNCHER PLATFORM 审中-公开
公开(公告)号：WO2003033348A3
公开(公告)日：2003-04-24
申请号：PCT/US2002/031722
申请日：2002-10-04
申请人： RAYTHEON COMPANY , GENERAL DYNAMICS ARMAMENT AND TECHNICAL PRODUCTS, INC.
发明人： SMITH, Joseph, P. , COOLIDGE, John, K. , TURNER, Stanley, G.
IPC分类号： F41F03/04
摘要： A launcher platform including a support structure and a number of rails mounted on the support structure for supporting missiles thereon, each adjacent rail elevated above the other rails to accommodate additional missiles and different type missiles while maintaining low center of gravity.

10. 发明申请

WO1996013694A1 MISSILE LAUNCHING AND STEERING SYSTEM 审中-公开
标题翻译：发射和转向系统
公开(公告)号：WO1996013694A1
公开(公告)日：1996-05-09
申请号：PCT/FR1995001423
申请日：1995-10-27
申请人： THOMSON-CSF , LE BUREAU DE CONSTRUCTIONS MECANIQUES "e;FAKEL"e; , ARKHANGELSKY, Ivan, Ivanovitch , BOLOTOV, Eugène, Gueorguevitch , PHILIPPOV, Vladimir, Sergueevitch , MIZROKHI, Vladimir, Yakovlevitch , SVETLOV, Vladimir, Grigorievitch , STANEVSKY, Gregory, Andreevitch , KHITENKOV, Serge, Grigorievitch , GAIDOUKEVITCH, Victor, Leonidovitch , CHMIKOV, Eugène, Afanassievitch
发明人： THOMSON-CSF , LE BUREAU DE CONSTRUCTIONS MECANIQUES "e;FAKEL"e;
IPC分类号： F41F03/04
CPC分类号： F42B10/663 , F41F3/04 , F41F3/077 , F42B10/66
摘要： A launching system, particularly a missile launching and steering system, whereby angle-launched missiles may be modernised by converting them into controlled missiles for circular defence, and ejection of the passive mass on the launch pad is prevented. For this purpose, the launching system includes a driven launching means (10) for the aerodynamic control surfaces (2) and a steering means comprising at least one gas generator (4) and nozzles (5) joined thereto. The steering means consists of an annular body (3) rigidly connected to the rear portion of the missile body. The inner surface of the annular body is tapered and covered with a thermal insulating material to form a gas ducting (7) with a profile in line with that of the sustainer motor nozzle (6) of the missile.
摘要翻译：发射系统，特别是导弹发射和转向系统，其中角度发射的导弹可以通过将它们转换成用于圆形防御的受控导弹而被现代化，并且防止发射台上的被动质量块的弹出。为此，发射系统包括用于空气动力学控制表面（2）的驱动发射装置（10）和包括至少一个气体发生器（4）和与其连接的喷嘴（5）的转向装置。转向装置由刚性地连接到导弹体的后部的环形体（3）组成。环形体的内表面是锥形的并被绝热材料覆盖以形成具有与导弹的维持器电动机喷嘴（6）的轮廓一致的轮廓的气体管道（7）。

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