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21. 发明公开

EP0730724A4 STABILIZER FOR A CANNON PROJECTILE 失效
标题翻译： STABILISATORFÜREIN KANONENGESCHOSS
公开(公告)号：EP0730724A4
公开(公告)日：1996-02-09
申请号：EP94904406
申请日：1993-11-26
申请人： US GOV SEC ARMY
发明人： GILMAN STEWART , FARINA ANTHONY
IPC分类号： F42B20060101 , F42B10/04 , F42B10/26
CPC分类号： F42B10/26 , F42B10/04
摘要： A cylindrical device (20) connected to the nose of a projectile (22) for imparting spin to the projectile fired from a non-rifled bore of a cannon. The device has at least two coaxial, adjacent, and integrally connected cylindrical segments of different diameter (32 and 34). The segment (32) having the larger diameter is positioned most rearwardly of the projectile, relative to the nose of the projectile, and the periphery of this segment has circumferentially spaced angled slots (34) for catching air moving past the projectile to spin the projectile. The segment with the smaller diameter (34) attaches the cylindrical device (20) to the aft end of the nose of the projectile (22) and directs the flow of air to and through the angled slots (38) of the segment having the larger diameter (32).
摘要翻译：一个圆柱形装置（20）连接到抛射体（22）的鼻部上，用于将旋转物从自旋炮的非线膛孔射出的射弹赋予自旋。该装置具有至少两个同轴的，相邻的并且整体连接的不同直径的圆柱段（32和34）。具有较大直径的节段（32）相对于射弹的鼻部位于射弹的最后方，并且该节段的周边具有周向间隔的成角度的狭缝（34），用于捕捉移动经过射弹的空气以旋转射弹。具有较小直径（34）的节段将圆柱形装置（20）附接到抛射物（22）的鼻部的后端，并将空气流引导到并穿过具有较大直径的节段的成角度的槽（38）直径（32）。

22. 发明公开

EP0222827A4 AMMUNITION CARTRIDGES HAVING CASINGS INCLUDING PLASTIC MATERIAL. 无效
标题翻译：与塑腿STOP端套盒弹药。
公开(公告)号：EP0222827A4
公开(公告)日：1988-02-08
申请号：EP86903050
申请日：1985-12-09
申请人： ACTION MFG COMPANY
发明人： LESHNER ERVIN , DONNARD REED E
IPC分类号： F42B20060101 , F42B5/02 , F42B5/285 , F42B5/307 , F42C20060101
CPC分类号： F42B5/02 , F42B5/307

23. 发明公开

EP0820578A4 ELECTROTHERMAL CHEMICAL CARTRIDGE 失效
标题翻译：化学电热KATEDER
公开(公告)号：EP0820578A4
公开(公告)日：2000-04-19
申请号：EP95914744
申请日：1995-03-23
申请人： MAXWELL TECHNOLOGIES INC
发明人： WILKINSON GREGORY MARK
IPC分类号： F42B20060101 , F42B5/08
CPC分类号： F42B5/08
摘要： An electrothermal chemical cartridge (10) with a fuse (18) of tapering cross section enables higher impulse energy to be imparted to a projectile (6) by means of complete controlled burning of propellant (24). A long, narrow tube (16) filled with propellant (24) has a fuse (18) on its inside surface with a cross section that tapers toward the discharge end, separated from the electrical ground of the cartridge casing by a layer of insulation sufficiently thin to be destroyed as the fuse ignites the propellant. A high-voltage electrode (26) connected at the back end (14) of the tube (16) provides for application of a pulse of sufficient current density to ohmically heat or burn the fuse in a controlled fashion from the discharge end (12) to the back end (14). Many such tubes (152) can be bundled together in a large casing (150) for wide barrel guns.

24. 发明公开

EP0131573A4 RAM AIR COMBUSTION STEERING SYSTEM FOR A GUIDED MISSILE. 失效
标题翻译：与冲压发动机的转向装置灼伤火箭。
公开(公告)号：EP0131573A4
公开(公告)日：1987-01-22
申请号：EP83901443
申请日：1983-01-20
申请人： FORD AEROSPACE & COMMUNICATION
发明人： MORENUS RICHARD C , FRAZER ALSON C
IPC分类号： F02K7/18 , F02K9/00 , F02K9/80 , F02K9/95 , F41G7/00 , F42B20060101 , F42B10/66 , H04K1/02
CPC分类号： F42B10/663
摘要： An open-ended diffusion chamber (16) and an adjacent combustion chamber (18) located in the nose (12) of a projectile (10) to receive ram air that ignites a solid fuel material (20) within the combustion chamber (18). A pair of oppositely disposed lateral steering ports (22, 24) are provided aft of the combustion chamber (18) and are interconnected therewith via a diverting valve (28) that is controllable to selectively divert the escaping combustion gases from the combustion chamber (18) to one or both of the steering ports (22, 24) to thereby change or maintain the trajectory course of the projectile (10) after firing.

25. 发明申请

US20050192472A1 System and method for treatment of hazardous materials, e.g., unexploded chemical warfare ordinance 审中-公开
标题翻译：用于处理有害物质的系统和方法，例如未爆炸的化学战法
公开(公告)号：US20050192472A1
公开(公告)日：2005-09-01
申请号：US10821020
申请日：2004-04-07
申请人： Jay Quimby , Richard Johnson , Alan Edwards , McRea Willmert , John Donovan
发明人： Jay Quimby , Richard Johnson , Alan Edwards , McRea Willmert , John Donovan
IPC分类号： A62D3/40 , A62D3/00 , B01D53/34 , F42B20060101
CPC分类号： F42B33/067
摘要： Systems and methods for treating hazardous materials are disclosed. One exemplary implementation provides a system for rendering chemical weapons materiel less hazardous. This system includes a detonation chamber, an expansion chamber, and an emission treater adapted to treat gas from detonation of the chemical weapons materiel. The emission treater yields a substantially dry residual waste stream and a treated gas suitable for venting to atmosphere. The emission treater may treat the gas with an alkaline powder that interacts with the gas, producing the residual waste stream.
摘要翻译：公开了用于处理危险材料的系统和方法。一个示例性的实施方式提供了一种使化学武器装备危险性较低的系统。该系统包括一个爆炸室，一个膨胀室和一个排放处理器，适用于处理爆炸化学武器物质的气体。排放处理器产生基本干燥的残留废物流和适合于排放到大气中的经处理的气体。排放处理器可以用与气体相互作用的碱性粉末处理气体，产生残余废物流。

26. 发明授权

US4829903A Ammunition device 失效
标题翻译：弹药装置
公开(公告)号：US4829903A
公开(公告)日：1989-05-16
申请号：US127149
申请日：1987-12-01
申请人： Jan Axinger , Bernt-Olov Bergman , Ingemar Johansson , Tomas Lonnermo , Lars Paulsson , Per-Olof Persson
发明人： Jan Axinger , Bernt-Olov Bergman , Ingemar Johansson , Tomas Lonnermo , Lars Paulsson , Per-Olof Persson
IPC分类号： F42B20060101 , F42B10/14 , F42B10/16 , F42B10/48 , F42B10/54 , F42B12/56
CPC分类号： F42B10/16 , F42B10/54
摘要： A device for reducing the rotational speed of an ammunition unit, for instance a submunition unit, and at the same time imparting to the ammunition unit a lateral speed includes a body arranged to be swung out from the ammunition unit and be released in a specific outswung position. The body preferably consists of a band which is wrapped about the outer peripheral surface of the ammunition unit. One end of the band is fixed to the ammunition unit in such a way that the band is released in a specific outswung position.

27. 发明授权

US4211378A Steering arrangement for projectiles of the missile kind, and projectiles fitted with this arrangement 失效
标题翻译：导弹类抛射物的指导安排和配备这种安排的射弹
公开(公告)号：US4211378A
公开(公告)日：1980-07-08
申请号：US894209
申请日：1978-04-06
申请人： Roger Crepin
发明人： Roger Crepin
IPC分类号： F42B10/66 , B64C15/00 , F02K20060101 , F02K9/00 , F41G20060101 , F41G7/00 , F42B20060101 , F42B10/62 , F42B15/01 , F42B15/18
CPC分类号： F42B10/663
摘要： A steering arrangement for missile type projectiles. A source of steering propulsion which is accommodated in the vicinity of the center of gravity of the missile comprises two gas generators which are positioned symmetrically on either side of the center of gravity a system being provided to switch or divert the gases to the exterior of the missile in at least two directions which are transverse to the projectile and to its axis.The arrangement according to the invention considerably improves the reliability and effectiveness with which the projectile is steered.
摘要翻译：导弹型射弹的导向装置。容纳在导弹重心附近的转向推进源包括两个气体发生器，其对称地位于重心的任一侧，该系统被设置成将气体切换或转移到在至少两个方向的导弹，横向于射弹和其轴线。根据本发明的装置显着提高了抛射体的可靠性和有效性。

28. 发明授权

US3850387A Deflection device for rocket motor propelled projectiles 失效
标题翻译：用于摇臂电机螺旋桨的偏转装置
公开(公告)号：US3850387A
公开(公告)日：1974-11-26
申请号：US37966173
申请日：1973-07-16
申请人： BOFORS AB
发明人： BJORNSON B , STRADALEN Y
IPC分类号： F42B10/66 , F42B20060101 , F42C20060101 , F42B13/30
CPC分类号： F42B10/665
摘要： A rocket propelled projectile is provided with a deflection device for temporarily deflecting the direction of flow of a gas jet issuing from the nozzle of the rocket motor. The deflection device comprises a flow deflecting member which is pivotally attached to the rocket motor and which extends to an active position wherein the flow deflecting member overlies a portion of the exhaust area of the nozzle. The deflecting member is temporarily retained in its active position by a locking pin which is positioned within the nozzle in the path of flow of the gas jet. The locking pin is eroded by the gas jet to release the flow deflecting member after a period of time, to permit the flow deflecting member to pivot to an inactive position wherein the flow deflecting member no longer overlies the exhaust area of the nozzle.
摘要翻译：火箭推进射弹设置有用于暂时偏转从火箭发动机的喷嘴发出的气体射流的流动方向的偏转装置。偏转装置包括流动偏转构件，其可枢转地附接到火箭发动机并且延伸到活动位置，其中流动偏转构件覆盖在喷嘴的排气区域的一部分上。偏转构件通过在气体射流的流动路径中位于喷嘴内的锁定销暂时保持在其主动位置。锁定销被气体喷射器侵蚀以在一段时间之后释放流动偏转构件，以允许流动偏转构件枢转到非活动位置，其中流动偏转构件不再覆盖喷嘴的排气区域。

29. 发明专利

JP4268635B2 System and method for handling hazardous materials, such as unexploded chemical military weapons 有权
公开(公告)号：JP4268635B2
公开(公告)日：2009-05-27
申请号：JP2006514296
申请日：2004-05-05
申请人：シーエイチ2エムヒルインコーポレイテッド
发明人：ジェイエムクィンビー , リチャードエイジョンソン
IPC分类号： A62D3/40 , F42B33/06 , A62D3/00 , B01D53/34 , F42B20060101
CPC分类号： F42B33/067

30. 发明专利

JP2552924B2 失效
公开(公告)号：JP2552924B2
公开(公告)日：1996-11-13
申请号：JP50868989
申请日：1989-08-14
申请人： NIKO PIROTEHINIIKU HANSU YURUGEN DEIIDERITSUHISU KG
发明人： RYUTSUBERUSU UIRURI
IPC分类号： F42B20060101 , F42C20060101 , F42C1/00 , F42C1/04 , F42C15/00 , F42C15/24
摘要： PCT No. PCT/DE89/00533 Sec. 371 Date Apr. 13, 1990 Sec. 102(e) Date Apr. 13, 1990 PCT Filed Aug. 14, 1989 PCT Pub. No. WO90/02309 PCT Pub. Date Mar. 8, 1990.The invention relates to an impact fuse (2) having fore-bore safety for a projectile (1), comprising a percussion needle (3) stationary on the fuse and an impact body (4) containing a percussion cap (5) and supported slidingly in the direction of flight, as well as a race for a blocking ball (23) between the impact body and the inner wall of the projectile casing. Which, upon premature impact on an obstacle, is jammed in its race (22) between a shoulder (18, 19, 20) on the inner wall of the casing and a ramp (17) of a groove (14, 15, 16) on the impact body (4), thereby preventing detonation. In order to allow for adjustment of predefined distances for the fore-bore safety, the invention proposes giving the race (22) for the blocking ball (23) a stepped design so that the blocking ball (23) can be jammed at several places within the fuse (2) between shoulders (18, 19, 20) and ramps (17) of different grooves (14, 15, 16).

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