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公开(公告)号：EP0952446A2
公开(公告)日：1999-10-27
申请号：EP99302311.8
申请日：1999-03-25
发明人： Beardmore, Geoffrey
IPC分类号： G01N27/10
CPC分类号： G01N29/28 , G01N29/07 , G01N29/223 , G01N29/262 , G01N2291/0231 , G01N2291/044 , G01N2291/106 , G01N2291/2694 , G10K11/34
摘要： An aircraft has several ultrasonic phased arrays 2 and 3 acoustically bonded to parts of its structure 1 to be monitored. The arrays 2 and 4 are energized to produce an ultrasonic beam that scans the structure in two planes. A monitor 6 receives the output from the arrays produced by reflection of energy from discontinuities within the structure 1. When there is a change in these outputs, the monitor 6 signals a pilot display unit 11 and a flight control system 8 such that the aircraft flight envelope can be restricted to minimize damage.
摘要翻译： 飞机具有多个超声相控阵列2和3声学结合到其结构1的待监视部分。 阵列2和4被激励以产生在两个平面中扫描结构的超声波束。 监视器6接收由结构1内的不连续性反射产生的阵列的输出。当这些输出发生变化时，监视器6发信号通知飞行员显示单元11和飞行控制系统8，使飞行器飞行 可以限制信封，以尽量减少损坏。
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公开(公告)号：EP0952446A3
公开(公告)日：2005-01-19
申请号：EP99302311.8
申请日：1999-03-25
发明人： Beardmore, Geoffrey
CPC分类号： G01N29/28 , G01N29/07 , G01N29/223 , G01N29/262 , G01N2291/0231 , G01N2291/044 , G01N2291/106 , G01N2291/2694 , G10K11/34
摘要： An aircraft has several ultrasonic phased arrays 2 and 3 acoustically bonded to parts of its structure 1 to be monitored. The arrays 2 and 4 are energized to produce an ultrasonic beam that scans the structure in two planes. A monitor 6 receives the output from the arrays produced by reflection of energy from discontinuities within the structure 1. When there is a change in these outputs, the monitor 6 signals a pilot display unit 11 and a flight control system 8 such that the aircraft flight envelope can be restricted to minimize damage.
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公开(公告)号：EP0029667A1
公开(公告)日：1981-06-03
申请号：EP80303908.0
申请日：1980-11-03
发明人： Beardmore, Geoffrey
CPC分类号： F16C17/045 , B24B9/00 , F16C33/1015
摘要： A hydrodynamic gas-lubricated bearing comprises a rotor (1) with a smooth bearing surface (3), and a fixed bearing plate (2) with a grooved surface (4). The grooves (10) are of spiral configuration being separated by lands (13) the top surface (14) of each of which has a convex profile. The central portion (15) of the surface (14) is raised above the edges (17) so that wedge-shaped regions (18) are formed between the surface (3) of the rotor (1) on both sides of the central portion (15). The surface (4) of the fixed bearing plate (2) may be formed with an overall convex surface. The grooved surface (4) of the fixed bearing member (2) is made by forming a pattern of grooves (10) in a smooth blank and subsequently rounding off the top surface (14) of the lands (13) by rotating the bearing part under pressure against a soft abrasive cloth.
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公开(公告)号：EP0896352A1
公开(公告)日：1999-02-10
申请号：EP98305571.6
申请日：1998-07-14
发明人： Beardmore, Geoffrey
IPC分类号： H01J1/02
摘要： A gas discharge lamp has a tubular envelope (1) containing tubular electrodes (30) at opposite ends. An annular support member (40) of a compressible ceramic fibre is supported in a groove (33) around each electrode and is compressed against the inside surface of the envelope. Movement of the electrodes (30) relative to the envelope (1) is damped by the support member (40).
摘要翻译： 气体放电灯具有在相对端包含管状电极（30）的管状外壳（1）。 可压缩陶瓷纤维的环形支撑构件（40）被支撑在围绕每个电极的凹槽（33）中并被压靠在外壳的内表面上。 电极（30）相对于外壳（1）的移动被支撑构件（40）阻尼。
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公开(公告)号：EP0802562A3
公开(公告)日：1997-12-17
申请号：EP97302056.3
申请日：1997-03-26
发明人： Beardmore, Geoffrey
摘要： A display 1 has a matrix array of cells 3 formed in a silicon plate 20 and each containing a tungsten strip filament 13. The cells 3 are filled with a halogen gas and are sealed by a double-glazed window 21 with an infra-red reflecting filter 22 to reflect heat back into the cell while allowing the transmission of visible radiation. The rear 6 of the plate 20 is treated to make it microporous and reduce its thermal conductivity
摘要翻译： 显示器1具有形成在硅板20中并且各自包含钨带细丝13的单元3的矩阵阵列。单元3填充有卤素气体，并且通过双层玻璃窗21密封，具有红外反射 过滤器22以将热量反射回到电池中，同时允许透射可见光。 处理板20的后部6以使其成为微孔并降低其热导率
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公开(公告)号：EP0802562A2
公开(公告)日：1997-10-22
申请号：EP97302056.3
申请日：1997-03-26
发明人： Beardmore, Geoffrey
摘要： A display 1 has a matrix array of cells 3 formed in a silicon plate 20 and each containing a tungsten strip filament 13. The cells 3 are filled with a halogen gas and are sealed by a double-glazed window 21 with an infra-red reflecting filter 22 to reflect heat back into the cell while allowing the transmission of visible radiation. The rear 6 of the plate 20 is treated to make it microporous and reduce its thermal conductivity
摘要翻译： 显示器1具有形成在硅板20中的单元3的矩阵阵列，并且每个单元包含钨条带细丝13.细胞3填充有卤素气体并且被具有红外反射的双层玻璃窗口21密封 过滤器22将热量反射回电池中，同时允许透射可见光辐射。 对板20的后部6进行处理以使其微孔并降低其导热性
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公开(公告)号：EP0847076A2
公开(公告)日：1998-06-10
申请号：EP97308883.4
申请日：1997-11-05
发明人： Beardmore, Geoffrey
IPC分类号： H01L21/00
CPC分类号： H01L21/67751 , H01L21/67201 , H01L21/67207 , H01L21/67276
摘要： A very compact silicon fabrication line has a number of process cells 20 to 25 all contained within a common outer enclosure 1. A semiconductor wafer 70 is loaded into the enclosure 1 through an air lock 10 and is mounted on a cap 56 supported under a carriage 80 movable along a rail 90 extending along the enclosure 1 between the different process cells 20 to 25. The cap 56 is lowered into sealing engagement with the open top 53, 54 of a cell 20 to 25 during each process.
摘要翻译： 非常紧凑的硅制造线具有多个处理单元20至25，其全部包含在公共外壳1内。半导体晶片70通过气锁10被装载到外壳1中，并且安装在支撑在托架下方的帽56上 80可沿着沿着外壳1在不同的处理单元20至25之间延伸的轨道90移动。在每个处理期间，帽56降低成与单元20至25的开口顶部53,54的密封接合。
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公开(公告)号：EP0029667B1
公开(公告)日：1983-12-28
申请号：EP80303908.0
申请日：1980-11-03
发明人： Beardmore, Geoffrey
CPC分类号： F16C17/045 , B24B9/00 , F16C33/1015
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公开(公告)号：EP0029655B1
公开(公告)日：1983-09-21
申请号：EP80303711.8
申请日：1980-10-21
发明人： Beardmore, Geoffrey
IPC分类号： G01C19/22
CPC分类号： G01C19/22 , Y10T74/125 , Y10T74/1279 , Y10T74/1282 , Y10T74/1293
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公开(公告)号：EP0029655A1
公开(公告)日：1981-06-03
申请号：EP80303711.8
申请日：1980-10-21
发明人： Beardmore, Geoffrey
IPC分类号： G01C19/22
CPC分类号： G01C19/22 , Y10T74/125 , Y10T74/1279 , Y10T74/1282 , Y10T74/1293
摘要： Gyroscope apparatus includes a tubular rotor (20) that is supported at opposite ends by bearings, such as a gas-lubricated bearing (1), for rotating about its axis (3). A gimbal ring (61) encircles the rotor and is resiliently supported with the rotor, for angular displacement about an axis (54) at right angles to the rotor axis (3), by a pair of flexure pivots (51 and 52) located intermediate the ends of the rotor. An inertia ring (72) is mounted concentrically with the gimbal ring (61) by another pair of flexure pivots (66 and 67) for angular displacement about an axis (73) at right angles to the rotor axis (3) and the axis of displacement (54) of the gimbal ring. The major part of each flexure pivot (51, 52 66, 67) is contained within the radial thickness of the gimbal ring. Displacement of the inertia ring is sensed by pick-offs (90 to 93) the output of which is used to control the restoring torque applied by torquers (80 to 83) located outwardly of the pick-offs.
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