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公开(公告)号：EP0274004B1
公开(公告)日：1992-03-11
申请号：EP87113491.2
申请日：1987-09-15
发明人： Porat, Itzhak , Netzer, Ehud , Rosenberg, Jehuda , Netzer, Yishai
IPC分类号： G01C19/42
CPC分类号： G01C19/42 , G01C19/28 , Y10T74/1264 , Y10T74/1293
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2.发明公开
公开(公告)号：EP2239822A2
公开(公告)日：2010-10-13
申请号：EP10157573.6
申请日：2010-03-24
发明人： Yang, Wei
CPC分类号： H01S5/14 , G01C19/66 , G01C19/665 , H01S3/0816 , H01S3/083 , H01S3/10092 , H01S5/18311 , Y10T74/1264
摘要： A interferometric optical gyroscope includes an active resonator comprising a half cavity vertical cavity surface emitting laser (half-VCSEL) operating as one of the mirrors that form the ring resonator. The half-VCSEL includes a bottom mirror stack and active layers formed on the bottom mirror stack and has a surface opposite the bottom mirror stack. Lack of a top mirror stack typically found in a VCSEL prevents the half-VCSEL from lasing, thus the half-VCSEL forms a reflective amplifier for the light circulating in the resonator. A single or multiple external light sources can be used to induce two counterpropagating beams in the resonator. Higher finesse due to the internal gain in the resonator enhances the sensitivity of the gyroscope.
摘要翻译： 干涉光学陀螺仪包括有源谐振器，其包括作为形成环形谐振器的反射镜之一工作的半空腔垂直腔表面发射激光器（半VCSEL）。 半VCSEL包括底部反射镜堆叠和形成在底部反射镜堆叠上并且具有与底部反射镜叠层相对的表面的有源层。 缺少通常在VCSEL中发现的顶部镜像堆栈可防止半VCSEL发光，因此半VCSEL形成在谐振器中循环的光的反射放大器。 可以使用单个或多个外部光源来诱导谐振器中的两个反向传播光束。 由于谐振器内部增益引起的更高的精细度提高了陀螺仪的灵敏度。
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公开(公告)号：EP0485695B1
公开(公告)日：1994-07-20
申请号：EP91113536.6
申请日：1991-08-13
发明人： Krieger, Dietmar
IPC分类号： G01D5/26
CPC分类号： G02B6/3604 , G01D5/347 , G02B6/3532 , G02B6/3594 , G02B6/3598 , Y10T74/1264
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公开(公告)号：EP0517861A1
公开(公告)日：1992-12-16
申请号：EP91912613.0
申请日：1991-02-26
申请人： AlliedSignal Inc.
发明人： PONA, Joseph, Jr.
IPC分类号： G01C19
CPC分类号： G01C19/28 , G01C19/42 , Y10T74/1264
摘要： Détecteur miniature à vitesse angulaire, porteur de liquide, à deux degrés de liberté, utilisé en premier lieu pour des applications tactiques, comprenant un rotor porteur de liquide hydrodynamique sphérique, un moteur-couple magnétique permanent et un capteur optique. Tous ces éléments sont disposés de manière à fournir deux axes d'information sur la vitesse angulaire dans un petit boîtier. Les composants individuels peuvent être préassemblés sous forme de sous-ensembles, et stockés et testés individuellement en vue du montage final.
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公开(公告)号：EP0485695A1
公开(公告)日：1992-05-20
申请号：EP91113536.6
申请日：1991-08-13
发明人： Krieger, Dietmar
IPC分类号： G01D5/26
CPC分类号： G02B6/3604 , G01D5/347 , G02B6/3532 , G02B6/3594 , G02B6/3598 , Y10T74/1264
摘要： Der optoelektrische Meßabgriff ist für einen Meßwertgeber geeignet, der in einer um eine Achse drehbaren Halterung beweglich angeordnet ist, wobei die Auslenkung des Meßwertgebers aus einer Anfangsposition als Meßwertwert erfaßt wird. Der Meßwertgeber weist dazu auf einer der Drehachse der Halterung zugewandten Seite eine mit unterschiedlichen optischen Eigenschaften in Codeform versehene Skala (10) auf. In einer axialen Bohrung (3,1) der Drehachse ist zumindest ein Lichtwellenleiter (9) angeordnet , dessen eines Ende auf die Skala und dessen anderes Ende auf ein optoelektrisches Bauelement (8) gerichtet ist, wobei das optoelektrische Bauelement (8) mit einem die Drehachse der Halterung lagernden Gehäuseteil (1) fest verbunden ist.
摘要翻译： 光电测量仪器适用于可移动地布置在可围绕轴线旋转的保持器中的测量值发射器，测量值发射器从初始位置的偏转被检测为测量值。 为此，测量值发射器在与保持器的旋转轴线相对的一侧呈现具有代码形式的不同光学特性的标尺（10）。 在旋转轴的轴向孔（3,1）中，布置有至少一个光波导（9），其一端指向标尺，另一端指向光电元件（8） ，光电部件（8）永久地连接到支撑保持器的旋转轴线的壳体部分（1）。 ...
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公开(公告)号：EP0274004A3
公开(公告)日：1989-08-30
申请号：EP87113491.2
申请日：1987-09-15
发明人： Porat, Itzhak , Netzer, Ehud , Rosenberg, Jehuda , Netzer, Yishai
IPC分类号： G01C19/42
CPC分类号： G01C19/42 , G01C19/28 , Y10T74/1264 , Y10T74/1293
摘要： A gymballess, two axis rate gyroscope in which an inertia rotor is keyed on the electric motor shaft. The motor shaft comprises a flexible part (flexure shaft) adapted to flex upon precession of the inertia rotor in consequence of an angular velocity input around either of two axes normal to each other and both normal to the rotor spin axis, and an end portion extending beyond the inertia rotor in a direction away from the electric motor (deflector). The gyroscope further comprises non-contacting measuring means in association with said deflector for detecting any deflection thereof.
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公开(公告)号：EP2239822A3
公开(公告)日：2016-07-13
申请号：EP10157573.6
申请日：2010-03-24
发明人： Yang, Wei
CPC分类号： H01S5/14 , G01C19/66 , G01C19/665 , H01S3/0816 , H01S3/083 , H01S3/10092 , H01S5/18311 , Y10T74/1264
摘要： A interferometric optical gyroscope includes an active resonator comprising a half cavity vertical cavity surface emitting laser (half-VCSEL) operating as one of the mirrors that form the ring resonator. The half-VCSEL includes a bottom mirror stack and active layers formed on the bottom mirror stack and has a surface opposite the bottom mirror stack. Lack of a top mirror stack typically found in a VCSEL prevents the half-VCSEL from lasing, thus the half-VCSEL forms a reflective amplifier for the light circulating in the resonator. A single or multiple external light sources can be used to induce two counterpropagating beams in the resonator. Higher finesse due to the internal gain in the resonator enhances the sensitivity of the gyroscope.
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公开(公告)号：EP1532048B1
公开(公告)日：2008-12-03
申请号：EP03751893.3
申请日：2003-08-22
发明人： MEFFE, Marc, E.
CPC分类号： B64G1/286 , Y10T74/125 , Y10T74/1254 , Y10T74/1261 , Y10T74/1264
摘要： The present invention provides a control moment gyroscope (100) that overcomes many of the limitations of the prior art. The control moment gyroscope (100) provides a radial actuator mechanism (110) to provide rotation to an inner gimbal assembly (102) around a gimbal axis. The radial actuator mechanism comprises a circular ring (111) at the midpoint of the gimbal axis, the circular ring (111) extending around the outer periphery of the inner gimbal assembly housing. The radial actuator mechanism (110) rotates the inner gimbal assembly (102) around the gimbal axis through the use of a non-contact motor that provides rotational force directly to the outer perimeter of the inner gimbal assembly (102). Because the inner gimbal assembly (102) is rotated from the midpoint of the gimbal axis, a torque module assembly at the end of the gimbal axis is not required. Thus, the overall length of the control moment gyroscope (100) can be reduced. Additionally, the cost and life limiting attributes of the torque module assembly can be eliminated, and the operational bandwidth of the gyroscope (100) increased. Finally, because the inner gimbal assembly (102) is rotated from the outer perimeter, the torque provided to the inner gimbal assembly (102) is naturally increased by the leverage arm of the inner gimbal assembly (102).
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公开(公告)号：EP1532048A1
公开(公告)日：2005-05-25
申请号：EP03751893.3
申请日：2003-08-22
发明人： MEFFE, Marc, E.
CPC分类号： B64G1/286 , Y10T74/125 , Y10T74/1254 , Y10T74/1261 , Y10T74/1264
摘要： The present invention provides a control moment gyroscope (100) that overcomes many of the limitations of the prior art. The control moment gyroscope (100) provides a radial actuator mechanism (110) to provide rotation to an inner gimbal assembly (102) around a gimbal axis. The radial actuator mechanism comprises a circular ring (111) at the midpoint of the gimbal axis, the circular ring (111) extending around the outer periphery of the inner gimbal assembly housing. The radial actuator mechanism (110) rotates the inner gimbal assembly (102) around the gimbal axis through the use of a non-contact motor that provides rotational force directly to the outer perimeter of the inner gimbal assembly (102). Because the inner gimbal assembly (102) is rotated from the midpoint of the gimbal axis, a torque module assembly at the end of the gimbal axis is not required. Thus, the overall length of the control moment gyroscope (100) can be reduced. Additionally, the cost and life limiting attributes of the torque module assembly can be eliminated, and the operational bandwidth of the gyroscope (100) increased. Finally, because the inner gimbal assembly (102) is rotated from the outer perimeter, the torque provided to the inner gimbal assembly (102) is naturally increased by the leverage arm of the inner gimbal assembly (102).
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公开(公告)号：EP0517861B1
公开(公告)日：1994-05-25
申请号：EP91912613.6
申请日：1991-02-26
申请人： AlliedSignal Inc.
发明人： PONA, Joseph, Jr.
IPC分类号： G01C19/42
CPC分类号： G01C19/28 , G01C19/42 , Y10T74/1264
摘要： A miniature two degree of freedom fluid bearing angular rate sensor used primarily for tactical applications includes a spherical hydrodynamic fluid bearing rotor, a permanent magnet motor/torquer, and an optical pick-off, all of which are arranged to provide two axes of rate information in a small package. The individual components can be pre-assembled as sub-assemblies, and individually stocked and tested for final assembly.
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