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1. 发明公开

EP3295115A1 OPTICAL WAVEGUIDE COUDE PATH FOR GIMBALED SYSTEMS 有权
公开(公告)号：EP3295115A1
公开(公告)日：2018-03-21
申请号：EP16748373
申请日：2016-07-06
申请人： RAYTHEON CO
发明人： TRAIL NICHOLAS D , HICKS JIM R , BRUNTON DANIEL W
IPC分类号： F41G7/22 , F41G7/00 , G01S7/481 , G01S17/66
CPC分类号： G01S3/786 , F41G7/008 , F41G7/2213 , F41G7/2246 , F41G7/2253 , F41G7/2293 , G01C3/08 , G01S7/4813 , G01S7/4818 , G01S17/66 , G02B6/0005 , G02B17/008
摘要： A dual-mode active and passive gimbaled optical system including a mechanism for coupling an optical signal from an off-gimbal active-mode source into the on-gimbal passive-mode optical path. One example of the system includes a passive off-gimbal detector assembly configured to image emissive electromagnetic radiation from a viewed scene, and a receiver-path optical assembly, including on-gimbal objective optics, that directs the electromagnetic radiation to the off-gimbal detector assembly. The system further includes an off-gimbal active source that generates an optical signal, a gimbal bearing assembly that supports rotation of the gimbal and includes a centrally-located output ferrule mated to an optical fiber that transports the optical signal from the active source to the output ferrule, and an on-gimbal optical coupling element that receives the optical signal from the output ferrule and couples the optical signal into the receiver optical path to direct the optical signal toward the on-gimbal objective optics.

2. 发明公开

EP2609393A4 METHOD FOR COMPENSATING FOR BORESIGHT ERROR IN MISSILES WITH COMPOSITE RADOMES AND GUIDANCE SECTION WITH BORESIGHT ERROR COMPENSATION 有权
标题翻译：方法错误在火箭中线补偿控制VERBUNDSTOFFRADOM及管理组有补偿中心线路故障
公开(公告)号：EP2609393A4
公开(公告)日：2016-10-19
申请号：EP11859441
申请日：2011-06-27
申请人： RAYTHEON CO
发明人： KESSELRING ROBERT L
IPC分类号： F41G7/22 , F42B15/01 , G01S7/40 , H01Q1/42
CPC分类号： F42B15/01 , F41G7/2213 , F41G7/2246 , F41G7/2286 , G01S7/4026 , H01Q1/28 , H01Q1/421
摘要： Embodiments of a guidance section that compensates for boresight error (BSE) caused by effects of a composite radome. The guidance section includes a BSE compensation element to add high-pass filtered noise to compensated BSE data. The guidance section also includes and a Kalman filter to generate line-of-sight rate (LOSR) BSE noise from the compensated BSE data and the added high-pass filtered noise. In some embodiments, a method for generating a revised BSE correction matrix is provided. The revised BSE correction matrix may compensate for BSE caused by effects in the composite radome and may correct for relative target velocity error.

3. 发明公开

EP2191163A4 Z-LEG SHOCK ISOLATOR 有权
标题翻译： STOSSDMPFER MITZICKZACKFÖRMIGEMBEIN
公开(公告)号：EP2191163A4
公开(公告)日：2016-09-14
申请号：EP08828213
申请日：2008-08-14
申请人： RAYTHEON CO
发明人： VO PETER H , SCHLATTER EDWARD C , LAYTON JEFFREY J
IPC分类号： F16F1/20 , F16F1/377
CPC分类号： F16F1/377
摘要： An isolator. The novel isolator includes a first mounting structure, a second mounting structure, and a structure for providing a coupling path between the first and second mounting structures, this path having a series of zigzag patterns adapted to attenuate shock and/or vibration energy. The first mounting structure is attached to the shock source, and the second mounting structure is attached to the device to be isolated. In an illustrative embodiment, the isolator provides a path having a series of ninety-degree bends and a length greater than a direct distance between the first and second mounting structures. The path length and number of bends is tuned to provide a desired attenuation level. The dimensions of the isolator may also be tuned to provide a desired resonant frequency. In a preferred embodiment, the isolator is made from metal or some other material having stable properties over time.
摘要翻译：隔离器新型隔离器包括第一安装结构，第二安装结构和用于在第一和第二安装结构之间提供耦合路径的结构，该路径具有适于衰减冲击和/或振动能量的一系列之字形图案。第一安装结构附接到冲击源，并且第二安装结构附接到待隔离的装置。在说明性实施例中，隔离器提供具有一系列九十度弯曲并且长度大于第一和第二安装结构之间的直接距离的路径。调整路径长度和弯曲数以提供所需的衰减水平。也可以调谐隔离器的尺寸以提供期望的谐振频率。在优选实施例中，隔离器由具有随时间稳定性质的金属或其它材料制成。

4. 发明公开

EP2917683A4 ROCKET PROPELLED PAYLOAD WITH DIVERT CONTROL SYSTEM WITHIN NOSE CONE 有权转让
标题翻译： RAKETENGETRIEBENE NUTZLAST MIT ABWEICHUNGSSTEUERSYSTEM IN DER NASENHAUBE
公开(公告)号：EP2917683A4
公开(公告)日：2016-07-27
申请号：EP13853167
申请日：2013-09-03
申请人： RAYTHEON CO
发明人： FACCIANO ANDREW B , ALKEMA MICHAEL S , MOORE ROBERT T
IPC分类号： F42B15/01
CPC分类号： F42B10/663
摘要： A rocket is provided and includes booster stages at a rear of the nose cone, the booster stages being configured for propelling the nose cone in a propulsion direction and a divert control system housed entirely in the nose cone for controlling an orientation of the propulsion direction.
摘要翻译：提供火箭并且包括在鼻锥后部的增压器级，增压级构造成用于沿推进方向推进鼻锥，而转向控制系统完全容纳在鼻锥中，用于控制推进方向的取向。

5. 发明公开

EP2984596A4 INVERSE-CONTOUR MACHINING TO ELIMINATE RESIDUAL STRESS DISTORTION 有权转让
标题翻译：逆向黑龙江泽西尔艾美岛EINER RESTSPANNUNGSVERZERRUNG
公开(公告)号：EP2984596A4
公开(公告)日：2016-07-13
申请号：EP14783260
申请日：2014-02-11
申请人： RAYTHEON CO
发明人： SIMON ROBERT T , GREGORY KRIS E , HORSTMAN THOMAS
IPC分类号： G06F19/00 , B23C3/00 , B23Q15/22 , G05B19/401 , G05B19/404 , G05B19/4097
CPC分类号： G05B19/4097 , B23C3/00 , B23C2250/00 , G05B19/404 , G05B2219/37308 , G05B2219/37576 , G05B2219/45145 , G05B2219/49184
摘要： A method for manufacturing a part to compensate for residual stress distortion is disclosed. The method can include obtaining a first part based on a nominal part. The first part can be distorted from the nominal part by residual stress. The method can also include determining a variation of the first part from the nominal part. The method can further include determining an offset of the variation relative to the nominal part to compensate for the variation. Additionally, the method can include making a second part using the offset of the variation, wherein residual stress distorts the second part within tolerance of the nominal part.
摘要翻译：公开了一种用于制造补偿残余应力变形的零件的方法。该方法可以包括基于标称部分获得第一部分。第一部分可以通过残余应力从标称部分扭曲。该方法还可以包括从标称部分确定第一部分的变化。该方法还可以包括确定变化相对于标称部分的偏移量以补偿变化。此外，该方法可以包括使用变化的偏移来制造第二部分，其中残余应力使第二部分在标称部分的公差内扭曲。

6. 发明公开

EP2598832A4 PROJECTILE THAT INCLUDES A GIMBAL STOP 有权
标题翻译： PROJEKTIL MIT EINEM KARDANANSCHLAG
公开(公告)号：EP2598832A4
公开(公告)日：2016-06-29
申请号：EP11829698
申请日：2011-05-27
申请人： RAYTHEON CO
发明人： DALE ERIK T , EGBERT RYAN A
IPC分类号： F41G7/22 , F42B15/01 , F42B15/08
CPC分类号： F42B15/08 , F41G7/2213 , F41G7/2253 , F41G7/2293 , F42B15/01

7. 发明公开

EP2912721A4 MULTI-BANDPASS, DUAL-POLARIZATION RADOME WITH COMPRESSED GRID 有权
标题翻译：多普勒超声波多普勒麻醉剂KOMPRIMIERTEM GITTER
公开(公告)号：EP2912721A4
公开(公告)日：2016-05-25
申请号：EP13849916
申请日：2013-08-15
申请人： RAYTHEON CO
发明人： JORDAN JARED W , CANNON BENJAMIN L
IPC分类号： H01Q1/42 , H01Q5/00 , H01Q15/00
CPC分类号： H01Q1/425 , H01Q5/00 , H01Q15/0026 , H01Q15/0086
摘要： A radome is provided and includes a dielectric wall and one or more inductive metallic grids embedded in and/or disposed on the dielectric wall. Each of the one or more grids includes compressed grid arms and is tuned to permit bandpass transmission at upper and lower frequencies.
摘要翻译：提供了一个天线罩，其包括电介质壁和一个或多个嵌入电介质壁和/或设置在电介质壁上的感应金属网格。一个或多个网格中的每一个包括压缩网格臂并被调谐以允许在上部和下部频率的带通传输。

8. 发明公开

EP2212198A4 METHODS AND APPARATUS FOR TRANSFORMING UNMANNED AERIAL VEHICLE 有权
标题翻译： VERFAHREN UND VORRICHTUNG ZUR VERWANDLUNG EINES UNBEMANNTEN LUFTFAHRZEUGS
公开(公告)号：EP2212198A4
公开(公告)日：2016-05-11
申请号：EP08845839
申请日：2008-10-31
申请人： RAYTHEON CO
发明人： KINSEY LLOYD E , KRANKING PATRICK D
IPC分类号： B64C39/02 , B64C29/02
CPC分类号： B64C39/024 , B64C29/02 , B64C2201/028 , B64C2201/084 , B64C2201/088

9. 发明公开

EP2188805A4 SENSOR FOR EYE-SAFE AND BODY-FIXED SEMI-ACTIVE LASER GUIDANCE 有权
标题翻译：传感器眼安全和车身固定半主动激光指南
公开(公告)号：EP2188805A4
公开(公告)日：2016-01-27
申请号：EP08857524
申请日：2008-08-14
申请人： RAYTHEON CO
发明人： ANDRESSEN CLARENCE C
IPC分类号： G09G5/00 , G01J1/42 , H04N5/347
CPC分类号： H04N5/347 , F41G7/226 , F41G7/2293 , G01J1/4228 , H04N5/335

10. 发明公开

EP2165387A4 HIGH POWER PHASED ARRAY ANTENNA SYSTEM 有权
标题翻译：与相高效控天线阵系统
公开(公告)号：EP2165387A4
公开(公告)日：2015-12-02
申请号：EP08768679
申请日：2008-06-20
申请人： RAYTHEON CO
发明人： BROWN KENNETH W , AHRENS FREDERICK A
IPC分类号： H01Q1/36 , H03F3/60 , H04B1/44
CPC分类号： H01Q25/005 , H01Q21/0025 , H01Q21/061 , H03F1/0277 , H03F3/24 , H03F3/602 , H03F3/68 , H03F2200/192 , H03F2200/198
摘要： Embodiments of a switchable high-power transmit module to selectively provide a high-power microwave signal in excess of one kilowatt to one of first and second output paths are disclosed herein. The module includes a switch to receive a lower-power microwave signal from a source, a first ninety-degree coupler for directing power from the switch to first and second paths, a first high-power amplifier disposed in the first path, a second high-power amplifier disposed in the second path, and a second ninety-degree coupler to receive output signals of the first and second amplifiers. The switch is configured to selectively couple the lower-power microwave signal between first and second input ports of the first ninety-degree coupler. When the switch couples the lower-power microwave signal to a selected one of the input ports of the first coupler, signals generated by the first and second high-power amplifiers are combined in the second ninety-degree coupler to provide the high-power microwave output signal on only one of the output paths.

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