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1. 发明公开

EP2038602A2 TWO-AXIS TRAJECTORY CONTROL SYSTEM 审中-公开
标题翻译：双轴轨迹控制系统
公开(公告)号：EP2038602A2
公开(公告)日：2009-03-25
申请号：EP07873817.6
申请日：2007-07-06
申请人： Lockheed Martin Corporation
发明人： BANKS, Johnny, E.
IPC分类号： F42B10/00 , F42B15/01 , B64C27/00 , B64C5/04 , B64C5/12 , B64C39/12
CPC分类号： F42B15/01 , F42B10/64
摘要： A trajectory control system includes a first control mechanism having a pair of outputs operably associated with a first pair of control surfaces, the first control mechanism operable to articulate the first pair of control surfaces in unison and a second control mechanism having a pair of outputs operably associated with a second pair of control surfaces, the second control mechanism operable to articulate the second pair of control surfaces in unison. The second control mechanism is nested in the first control mechanism such that the pair of outputs of the first control mechanism is substantially coplanar with the pair of outputs of the second control mechanism.
摘要翻译：轨迹控制系统包括第一控制机构，该第一控制机构具有与第一对控制表面可操作地关联的一对输出，第一控制机构可操作以一致地铰接第一对控制表面，以及第二控制机构具有可操作地一对输出与第二对控制表面相关联，第二控制机构可操作以一致地铰接第二对控制表面。第二控制机构嵌套在第一控制机构中，使得第一控制机构的一对输出基本上与第二控制机构的一对输出共面。

2. 发明公开

EP2115382A2 APPARATUS AND METHOD FOR SELECTIVELY AFFECTING A LAUNCH TRAJECTORY OF A PROJECTILE 审中-公开
标题翻译：装置和方法的用于启动列车弹丸选择性地操纵
公开(公告)号：EP2115382A2
公开(公告)日：2009-11-11
申请号：EP08795795.7
申请日：2008-02-15
申请人： Lockheed Martin Corporation
发明人： PATEL, Umang, R. , SCHROEDER, Wayne, K. , BANKS, Johnny, E.
IPC分类号： F42B5/067
CPC分类号： F42B5/067 , F41F3/042 , F41F3/052 , F41F3/077 , F42B5/073
摘要： An apparatus for selectively affecting a launch trajectory of a projectile from a canister includes means for selectively positioning the projectile with respect to the canister and a sabot operably associated with the projectile and the means for selectively positioning the projectile. A projectile launch system includes a canister, a projectile disposed in the canister, and means for selectively positioning the projectile with respect to the canister. A method for affecting a launch trajectory of a projectile includes providing a canister and a projectile disposed in the canister and adjusting a position of the projectile with respect to the canister.

3. 发明公开

EP2044384A2 DEVICE FOR PENETRATING AND EXPLODING A TARGET 审中-公开
标题翻译：设备技术渗透测试上的目标
公开(公告)号：EP2044384A2
公开(公告)日：2009-04-08
申请号：EP07873856.4
申请日：2007-07-20
申请人： Lockheed Martin Corporation
发明人： SCHROEDER, Wayne, K. , BANKS, Johnny, E.
IPC分类号： F42B12/00
CPC分类号： F42B12/06 , F42B12/08 , F42B12/44
摘要： A lethality device includes a penetrator structure configured to penetrate a target and an incendiary material disposed near the penetrator structure. The incendiary material self-ignites and is injected into the target after penetration of the target. A projectile includes a penetrator structure configured to penetrate a target, an incendiary material disposed near the penetrator structure, and one or components other than the penetrator structure and the incendiary material disposed aft of the penetrator structure. Loads from the one or more components are transferred to the penetrator structure upon impact with the target. The incendiary material self-ignites and is injected into the target after penetration of the target. A method for defeating a target containing an ignitable material includes broaching or puncturing an outer skin of the target, self-igniting an incendiary material, injecting the ignited incendiary material into the target, and igniting a material disposed within the target.

4. 发明公开

EP1543289A1 A PENETRATOR AND METHOD FOR USING SAME 审中-公开
标题翻译：穿甲弹和这样的弹丸的用途
公开(公告)号：EP1543289A1
公开(公告)日：2005-06-22
申请号：EP03759375.3
申请日：2003-09-17
申请人： Lockheed Martin Corporation
发明人： HUNN, David, L. , BANKS, Johnny, E. , COWAN, Carlton, B.
IPC分类号： F42B10/02 , F42B10/08 , F42B12/06 , F42B12/64
CPC分类号： F42B12/06 , F42B10/02 , F42B10/08 , F42B12/64
摘要： A penetrator (100) includes a fore body (120) having a center of aerodynamic pressure (122) forward of a center of gravity (120) and a stabilizing portion (104) removably attached to the fore body such that, when attached to the fore body, a center of gravity for the penetrator is forward of a center of aerodynamic pressure for the penetrator. A method of using a penetrator includes propelling the penetrator toward a first target, penetrating the first target with a fore body of the penetrator, and detaching a stabilizing portion of the penetrator from the fore body. The method further includes impacting the second target with the fore body.

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