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51. 发明公开

EP1134640A3 Attitude control system for a spacecraft 有权
标题翻译：对于空间飞行器位置控制
公开(公告)号：EP1134640A3
公开(公告)日：2004-08-11
申请号：EP00309213.7
申请日：2000-10-19
申请人： Astrium Limited
发明人： Holt, Antony Philip
IPC分类号： G05D1/08 , B64G1/24
CPC分类号： B64G1/283 , B64G1/28 , B64G1/36 , B64G1/361 , B64G1/363 , G05D1/0883
摘要： Attitude is controlled using reaction wheels (or other reaction means) taking as the control signal the inertial momentum vector of the spacecraft, based on the estimated momentum of the structure of the spacecraft and the sensed momentum of the reaction means, to provide more accurate control than hitherto.

52. 发明公开

EP1425216A1 AIRCRAFT STRUCTURAL COMPONENTS 有权
标题翻译：建筑部品 - 飞机
公开(公告)号：EP1425216A1
公开(公告)日：2004-06-09
申请号：EP02788063.2
申请日：2002-07-11
申请人： BAE Systems PLC
发明人： GAITONDE, John, Martin,Airbus UK limited
IPC分类号： B64C1/14 , B64C3/26
CPC分类号： B64C3/26 , B64C1/1446 , Y10T428/24273
摘要： A structural component such as wing skin (1) for an aircraft is formed generally of a first composite fibre and matrix material exhibiting a first tensile modulus in respect of tensile stress and a first tolerance of strain resulting from such stress. One or more openings (5, 6, 7) are provided in the component and the material of a portion of the component bounding the opening(s) is a second composite fibre and matrix material. The second material exhibits a second tensile modulus in respect of tensile stress that is smaller than the first tensile modulus of the first material and a second tolerance of strain resulting from such stress that is greater than the first tolerance of strain of the first material.

53. 发明公开

EP1373067A1 TURBULENT FLOW DRAG REDUCTION 有权
标题翻译：涡流场减阻
公开(公告)号：EP1373067A1
公开(公告)日：2004-01-02
申请号：EP02718320.1
申请日：2002-03-26
申请人： BAE Systems PLC
发明人： SCOTT, Simon Joseph,Bae Systems (Operations) Ltd , JOHNSON, Graham A.,Bae Systems (Operations) Ltd , THORNTON, Edward
IPC分类号： B64C23/00
CPC分类号： B64C23/005 , Y02T50/166
摘要： The present invention relates to apparatus for influencing fluid flow over a surface, and more particularly, but not exclusively, to turbulent boundary layer flow drag reduction for an aircraft. The present invention provides such apparatus including a plasma generator comprising a first electrode (7) and a signal generator (18), the apparatus being operable to drive the first electrode (7) with a pulsed signal generated by the signal generator (18) thereby to cause a change in direction of the flow of the fluid over the surface.

54. 发明公开

EP1307763A1 METHOD OF INTERFERENCE SUPPRESSION IN A RADAR SYSTEM 审中-公开
标题翻译：法故障抑制雷达系统
公开(公告)号：EP1307763A1
公开(公告)日：2003-05-07
申请号：EP01960882.7
申请日：2001-08-10
申请人： Alenia Marconi Systems Limited
发明人： LANGSFORD, Peter,Alenia Marconi Systems Limited
IPC分类号： G01S7/28
CPC分类号： G01S7/2813 , G01S7/36
摘要： The invention relates to a method of interference suppression in a radar system (10) and also to a system (10) operating according to the method. The system (10) incorporates a first antenna (40) and associated electronic circuits for emitting interrogating radar radiation towards a remote scene (S). Moreover, the system (10) also incorporates a second antenna (45) and associated electronic circuits for receiving interrogating radiation reflected from the scene (S) and generating correponding first and second processed signals. The first and second processed signals correspond to a broader main beam response of the antenna (45) and to a narrower main beam response thereof respectively. By mutually comparing the first and second processed signals, the system (10) is operable to identify those second processed signals affected by interference from the scene (S). The system (10) also incorporates electronic units (430, 440) operable to calculate adaptive weights for modifying the narrower response to steer its nulls in directions of interfering sources in the scene (S) when the narrower response is used to generate an overall output from the system (10), the units operable to selectively use second signal samples identified as being subject to interference for calculating the adaptive weights. The system (10) is operable to store its first and second signals for a period not less than that associated with updating the adaptive weights, thereby providing the system (10) with enhanced interference suppresssion characteristics.

55. 发明授权

EP0822139B1 Deployable radiators for spacecraft 失效
标题翻译：航天器部署散热器
公开(公告)号：EP0822139B1
公开(公告)日：2003-03-26
申请号：EP97305354.9
申请日：1997-07-17
申请人： MATRA MARCONI SPACE UK LIMITED
发明人： Dunbar, Neil William , McGoldrick, Philip David
IPC分类号： B64G1/50
CPC分类号： F28D15/043 , B64G1/50 , B64G1/503

56. 发明授权

EP1576408B1 DEFORMABLE MIRROR 失效
标题翻译：变形反射镜
公开(公告)号：EP1576408B1
公开(公告)日：2017-03-01
申请号：EP03789545.5
申请日：2003-12-18
申请人： BAE Systems PLC
发明人： GRIFFITH, Michael, Stewart , ARCHER, Nicholas, John , LAYCOCK, Leslie, Charles
IPC分类号： G02B26/06 , G02B26/08
CPC分类号： G02B26/0825 , G02B26/06

57. 发明授权

EP1485669B1 Ordnance with explosives liner and method of manufacture of the ordnance 有权
标题翻译：弹药案炸药和制造弹药的方法
公开(公告)号：EP1485669B1
公开(公告)日：2011-06-15
申请号：EP03744412.2
申请日：2003-03-06
申请人： BAE Systems PLC
发明人： White, Christopher , Bennett, Geoffrey , Thomas, Daniel Wayne , Crimmings, Gavin Michael , Johnson, David Conway
IPC分类号： F42B33/02
CPC分类号： F42B33/0285 , F42B33/0214
摘要： Described herein is a method of filling ordnance with explosive materials. An ordnance shell (2) comprises a cavity (32) filled with explosive material (10), the explosive material (10) being contained in a bag (36) located within the cavity (32).

58. 发明授权

EP1322903B1 DUAL-FREQUENCY MILLIMETER WAVE AND LASER RADIATION RECEIVER 有权
标题翻译： FOR两个频率爆炸毫米波和激光辐射接收器
公开(公告)号：EP1322903B1
公开(公告)日：2010-05-12
申请号：EP00981527.5
申请日：2000-12-05
申请人： Alenia Marconi Systems Incorporated
发明人： SANDERS, Ross, J. , SHMOLDAS, John, Dusan , WICKS, Dean, Arthur
IPC分类号： F41G7/22 , F41G7/00 , G01S13/86
CPC分类号： F41G7/226 , F41G7/008 , F41G7/2286 , F41G7/2293 , F42B30/006 , G01S3/00 , H01Q1/281 , H01Q3/16 , H01Q19/19

59. 发明授权

EP1522146B1 Time-interleaved sampler calibration method and apparatus 有权
标题翻译：用于校准的时间交织采样的方法和装置
公开(公告)号：EP1522146B1
公开(公告)日：2008-07-30
申请号：EP03761676.0
申请日：2003-06-24
申请人： BAE Systems PLC
发明人： WOOD, John Michael, BAE Systems ATC , COOTE, Nigel C.T.
IPC分类号： H03M1/10
CPC分类号： H03M1/1085 , H03M1/1038 , H03M1/1215
摘要： This invention relates to a method of calibrating a time-interleaved analogue-to-digital sampler (10) and to a method of performing analogue-to-digital conversion with a sampler (10) so calibrated. The invention provides a method of calibrating a sampler (10) comprising N time-interleaved ADCs (12a-d), the method comprising the steps of: (a) injecting in turn N calibration signals (13) into the sampler such that each calibration signal (13) occupies one of N related frequencies; (b) determining the input signal for each one of the N calibration frequencies (13); (c) measuring in the frequency domain the output at each of the N related frequencies for each one of the N calibration frequencies; and (d) determining the relationship that relates the input signal to the output at each of the N related frequencies for each one of the N calibration frequencies.

60. 发明公开

EP1927000A2 SENSOR DEVICE WITH BACKSIDE CONTACTS 有权
标题翻译： SENSOR背接触
公开(公告)号：EP1927000A2
公开(公告)日：2008-06-04
申请号：EP06779641.7
申请日：2006-09-19
申请人： BAE Systems plc
发明人： WARSOP, Clyde , PRESS, Andrew, Julian , HUCKER, Martyn, John
IPC分类号： G01P5/12 , G01F1/684
CPC分类号： G01F1/6845 , G01P5/12 , G01P13/025
摘要： A sensor device for sensing air flow speed at the exterior of an aircraft, comprising a substrate having an upper side on which is mounted a diaphragm over an aperture or recess in the substrate, the diaphragm being thermally and electrically insulative, and mounting on its upper surface a heating element comprising a layer of resistive material, and wherein electrical connections to the heating element are buried in the diaphragm and/or the substrate, and provide electrical terminals at the lower side of the substrate. The heating element is exposed to the environment, but the remaining electrical parts of the device are not exposed. Portions of a conductive substrate may be cut or etched away to define a conductive pillar. Signals may be transmitted through the conductive pillar from one surface carrying the sensor element to the other surface carrying contact pads.

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