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1. 发明授权

EP1714106B1 2-D PROJECTILE TRAJECTORY CORRECTION SYSTEM AND METHOD 有权
标题翻译： 2-D FLOOR弹道修正的系统和方法
公开(公告)号：EP1714106B1
公开(公告)日：2009-03-04
申请号：EP05810849.9
申请日：2005-01-14
申请人： Raytheon Company
发明人： GESWENDER, Chris, E. , HINSDALE, Andrew, J. , BLAHA, George, A. , DRYER, Richard
IPC分类号： F42B10/64 , B64C9/36
CPC分类号： F42B10/64
摘要： A 2-D correction system uses intermittent deployment of aerodynamic surfaces (18) to control a spin or fin stabilized projectile (10) in flight; correcting both crossrange and downrange impact errors. Intermittent surface deployment develops rotational moments, which create body lift that nudge the projectile (10) in two-dimensions to correct the projectile (10) in its ballistic trajectory. In low spin rate projectiles ("fin stabilized"), the rotational moment directly produces the body lift that moves the projectile (10). In high spin rate projectiles ("spin stabilized"), the rotational moment creates a much larger orthogonal precession that in turn produces the body lift that moves the projectile (10). The aerodynamic surfaces are suitably deployed over multiple partial roll cycles at precise on (deployed) and off (stowed) positions in the cycle to nudge the projectile (10) up or down range or left or right cross range until the desired ballistic trajectory is restored.

2. 发明授权

EP1851501B1 METHODS AND APPARATUS FOR SELECTABLE VELOCITY PROJECTILE SYSTEM 失效
标题翻译：方法和装置与可选择的速度抛射系统
公开(公告)号：EP1851501B1
公开(公告)日：2016-10-12
申请号：EP06849663.7
申请日：2006-01-10
申请人： RAYTHEON COMPANY
发明人： DRYER, Richard , CONRARDY, Neal
IPC分类号： F42B5/08 , F42B5/16
CPC分类号： F41A1/02 , F41A1/06 , F42B5/08 , F42B5/16 , F42B10/38 , F42C19/0834 , F42C19/12

3. 发明授权

EP1377792B1 PRECISION GUIDED EXTENDED RANGE ARTILLERY PROJECTILE TACTICAL BASE 有权
标题翻译：依据经调节的精确制导长途PROJEKTIL
公开(公告)号：EP1377792B1
公开(公告)日：2009-10-28
申请号：EP02757367.4
申请日：2002-08-23
申请人： RAYTHEON COMPANY
发明人： MOORE, James L. , JOHNSON, Gary H. , PETERSON, (DR.) William S. , SHAH, Rajesh H. , DRYER, Richard , QUORTRUP, Conlee O.
IPC分类号： F42B10/14
CPC分类号： F42B10/38 , F42B10/14

4. 发明授权

EP2165152B1 HYBRID SPIN/FIN STABILIZED PROJECTILE 有权
标题翻译：漩涡/ WING稳定型混合FLOOR
公开(公告)号：EP2165152B1
公开(公告)日：2014-08-06
申请号：EP08768677.0
申请日：2008-06-20
申请人： Raytheon Company
发明人： HINSDALE, Andrew J. , DRYER, Richard
IPC分类号： F42B10/00 , F42B15/01 , F42B10/54 , F42B10/26 , F42B10/14
CPC分类号： F42B10/26 , F42B10/14 , F42B10/54

5. 发明公开

EP2507580A1 LIGHTPIPE FOR SEMI-ACTIVE LASER TARGET DESIGNATION 有权
标题翻译： HOHLLICHTLEITERFÜRHALBAKTIVE LASERZIELBESTIMMUNG
公开(公告)号：EP2507580A1
公开(公告)日：2012-10-10
申请号：EP10742937.5
申请日：2010-07-28
申请人： Raytheon Company
发明人： DRYER, Richard , PRESTON, Kenneth G.
IPC分类号： F41G7/22 , G02B6/06
CPC分类号： F41G7/226 , F41G7/2293 , G02B6/06
摘要： A semi-active laser (SAL) sensing system is provided that uses a lightpipe to pass received reflected laser light from an aperture to a detector. The lightpipe facilitates further miniaturization of the SAL sensing system by taking the place of a larger lens system that would otherwise be required. For example, the use of the lightpipe in a missile or guided projectile can facilitate the placement of the SAL sensing system with other sensors in the limited available space at the front of the missile. In one embodiment, the lightpipe is formed from cladded optical fibers that are bundled together, shaped, and fused together. The core material from the optical fibers are then dissolved away, leaving the outer cladding. This remaining outer cladding remains fused together, and maintains its shape, thus forming a lightpipe that can be used in a SAL sensing system.
摘要翻译：提供半激光（SAL）感测系统，其使用光管将接收的反射的激光从孔传递到检测器。光管通过代替另外需要的更大的透镜系统来促进SAL感测系统的进一步小型化。例如，在导弹或引导射弹中使用光管可以有助于将SAL感测系统与其他传感器放置在导弹前面的有限可用空间中。在一个实施例中，光管由捆包在一起形成并熔合在一起的包层光纤形成。然后将来自光纤的芯材溶解掉，留下外包层。这种剩余的外包层保持熔合在一起，并保持其形状，从而形成可用于SAL感测系统中的光管。

6. 发明公开

EP1851501A2 METHODS AND APPARATUS FOR SELECTABLE VELOCITY PROJECTILE SYSTEM 失效
标题翻译：方法和装置与可选择的速度抛射系统
公开(公告)号：EP1851501A2
公开(公告)日：2007-11-07
申请号：EP06849663.7
申请日：2006-01-10
申请人： RAYTHEON COMPANY
发明人： DRYER, Richard , CONRARDY, Neal
IPC分类号： F42B7/00
CPC分类号： F41A1/02 , F41A1/06 , F42B5/08 , F42B5/16 , F42B10/38 , F42C19/0834 , F42C19/12
摘要： Methods and apparatus according to various aspects of the present invention comprise a propelling system for propelling projectiles with variable velocity, In one embodiment, a cartridge comprises a cartridge case, the propelling system, and the projectile attached to the cartridge case.

7. 发明授权

EP2507580B1 LIGHTPIPE FOR SEMI-ACTIVE LASER TARGET DESIGNATION 有权
公开(公告)号：EP2507580B1
公开(公告)日：2018-09-05
申请号：EP10742937.5
申请日：2010-07-28
申请人： Raytheon Company
发明人： DRYER, Richard , PRESTON, Kenneth G.
IPC分类号： F41G7/22 , G02B6/06
CPC分类号： F41G7/226 , F41G7/2293 , G02B6/06
摘要： A semi-active laser (SAL) sensing system is provided that uses a lightpipe to pass received reflected laser light from an aperture to a detector. The lightpipe facilitates further miniaturization of the SAL sensing system by taking the place of a larger lens system that would otherwise be required. For example, the use of the lightpipe in a missile or guided projectile can facilitate the placement of the SAL sensing system with other sensors in the limited available space at the front of the missile. In one embodiment, the lightpipe is formed from cladded optical fibers that are bundled together, shaped, and fused together. The core material from the optical fibers are then dissolved away, leaving the outer cladding. This remaining outer cladding remains fused together, and maintains its shape, thus forming a lightpipe that can be used in a SAL sensing system.

8. 发明公开

EP1924817A2 TELESCOPED PROJECTILE 有权
标题翻译： MESH下滑FLOOR
公开(公告)号：EP1924817A2
公开(公告)日：2008-05-28
申请号：EP06849815.3
申请日：2006-08-08
申请人： Raytheon Company
发明人： DRYER, Richard
IPC分类号： F41B6/00 , F42B6/00 , F42B10/00 , F42B10/02 , F42B10/66
CPC分类号： F41B6/00 , F42B6/006 , F42B10/00 , F42B10/02 , F42B10/663
摘要： A projectile (10) reconfigures in flight from a launch configuration, in which the center of gravity is aft of the center of pressure, to a flight configuration, in which the center of gravity is forward of the center of pressure. The projectile includes a forward portion (12) and an aft portion (14), and the reconfiguration involves movement of at least part of one of the portions relative to the other portion. The projectile may have an overall substantially conical shape when in the launch configuration. The forward portion may include a substantially conical nose (20), and a cylindrical central body (22) attached to the nose. In the launch configuration, at least part of the central body may be located within a hollow (26) in a base (24) of the aft portion. The base may be slidable relative to the central body.

9. 发明公开

EP1714106A1 2-D PROJECTILE TRAJECTORY CORRECTION SYSTEM AND METHOD 有权
标题翻译： 2-D FLOOR弹道修正的系统和方法
公开(公告)号：EP1714106A1
公开(公告)日：2006-10-25
申请号：EP05810849.9
申请日：2005-01-14
申请人： Raytheon Company
发明人： GESWENDER, Chris, E. , HINSDALE, Andrew, J. , BLAHA, George, A. , DRYER, Richard
IPC分类号： F42B10/64 , B64C9/36
CPC分类号： F42B10/64
摘要： A 2-D correction system uses intermittent deployment of aerodynamic surfaces (18) to control a spin or fin stabilized projectile (10) in flight; correcting both crossrange and downrange impact errors. Intermittent surface deployment develops rotational moments, which create body lift that nudge the projectile (10) in two-dimensions to correct the projectile (10) in its ballistic trajectory. In low spin rate projectiles ('fin stabilized'), the rotational moment directly produces the body lift that moves the projectile (10). In high spin rate projectiles ('spin stabilized'), the rotational moment creates a much larger orthogonal precession that in turn produces the body lift that moves the projectile (10). The aerodynamic surfaces are suitably deployed over multiple partial roll cycles at precise on (deployed) and off (stowed) positions in the cycle to nudge the projectile (10) up or down range or left or right cross range until the desired ballistic trajectory is restored.

10. 发明授权

EP2596317B1 PROJECTILE MODIFICATION METHOD 有权
标题翻译：方法变革弹
公开(公告)号：EP2596317B1
公开(公告)日：2016-05-25
申请号：EP11714189.5
申请日：2011-03-31
申请人： Raytheon Company
发明人： DRYER, Richard , GESWENDER, Chris E.
IPC分类号： F42B10/06 , F42B10/04 , F42B10/16 , F42B10/14
CPC分类号： F42B10/16

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