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    • 1. 发明公开
    • TWO DEGREE OF FREEDOM GYRO HAVING AN AXIAL GAP PERMANENT MAGNET MOTOR
    • 陀螺仪用永磁电机两个自由度。
    • EP0025446A1
    • 1981-03-25
    • EP80900529.0
    • 1980-02-27
    • NORTHROP CORPORATION
    • GROHE, Lester R.
    • G01P15G01C19G01C21G01P9
    • G01C19/08G01C19/20G01C19/28Y10T74/1225Y10T74/125Y10T74/1275Y10T74/1282
    • Gyroscope a deux degres de liberte ayant un moteur (72) a aimants permanents, a entrefer axial. L'enceinte (14) du gyro supporte un stator ayant deux groupes de bobines enroulees en quadrature et connectees en serie (39a, 39b), (39c, 39d). L'axe principal de chaque bobine est parallele a un axe de reference de rotation (Z) avec lequel les premier (A) et second (B) axes d'entree sont mutuellement orthogonaux, chaque groupe de bobine etant dispose annulairement autour de l'axe de rotation de reference. Le rotor (42, 44) du moteur tourne autour d'un axe de rotation et peut se deplacer de maniere rotative autour des deux axes d'entree. Le rotor comprend un jeu d'aimants permanents (46, 48) supportes annulairement autour de l'axe de rotation, les moments magnetiques des aimants adjacents ayant des directions opposees et le flux provenant des aimants etant accouple aux bobines du stator. Une bague de retour de flux magnetique (50) complete le chemin de passage du flux au travers des bobines. Un reseau d'excitation (70) detecte les fem de retour dans les bobines et produit des signaux de commande pour entrainer des courants alternatifs ayant un dephasage relatif de 90o dans les bobines respectives mais etant en phase avec les fem de retour detectees dans les bobines respectives. Un autre reseau detecte le deplacement rotatif du rotor autour des axes d'entree et produit des signaux appropries pour des dispositifs de coupure (72, 76) qui servent a maintenir le rotor dans une position ou son axe de rotation coincide sensiblement avec l'axe de rotation de reference.
    • 2. 发明授权
    • TWO DEGREE OF FREEDOM GYRO HAVING A PERMANENT MAGNET MOTOR
    • 具有永磁电机的两度自由陀螺仪
    • EP0025446B1
    • 1985-08-14
    • EP80900529.1
    • 1980-02-27
    • NORTHROP CORPORATION
    • GROHE, Lester R.
    • G01C19/08G01C19/28G01C19/30G01P15/14
    • G01C19/08G01C19/20G01C19/28Y10T74/1225Y10T74/125Y10T74/1275Y10T74/1282
    • A two degree of freedom gyro having an axial gap, permanent magnet motor (72). The gyro housing (14) supports a stator having two sets of quadrature wound series-connected coils (39a, 39b) (39c, 39d). The principal axis of each coil is parallel to a spin reference axis (Z) with which first (A) and second (B) input axes are mutually orthogonal, each set of coils being annularly arranged about the spin reference axis. The rotor (42, 44) of the motor is rotatable about a spin axis and rotationally displaceable about the two input axes. The rotor includes a set of permanent magnets (46, 48) supported annularly about the spin axis, the magnetic moments of adjacent magnets being oppositely directed and the flux from the magnets is coupled to the stator coils. A magnetic flux return ring (50) completes the path for flux passing through the coils. An excitation network (70) detects back emf in the coils and generates control signals for driving alternate currents having a 90 relative phase shift in the respective coils but in phase with the detected back emf in the respective coils. A further network detects rotational displacement of the rotor about the input axes and generates appropriate signals for torquers (72, 76) which serve to maintain the rotor in a position where its spin axis is substantially coincident with the spin reference axis.
    • 4. 发明授权
    • GYROSCOPIC TORQUE CONVERTER
    • 回转扭矩转换器
    • EP2118520B1
    • 2011-11-02
    • EP07848750.1
    • 2007-12-27
    • Harrison, Duncan James
    • Harrison, Duncan James
    • F16H33/10
    • F16H33/10Y10T74/1218Y10T74/1225Y10T74/1236
    • A torque converter comprises a stationary mount, input and output shafts, a primary frame (301) supported by the stationary mount for rotation about a primary axis and coupled for rotation with one of the input and output shafts (302,303), a secondary frame (50) supported by the primary frame (301) for rotation about a secondary axis perpendicular to the primary axis and coupled for rotation with the other of the input and output shafts, a plurality of flywheels (10) supported by the secondary frame (50) with their spin axes disposed at an angle to one another in the same plane, or in mutually parallel planes, and torsional springs acting between the flywheels and the secondary frame to cause the flywheels to oscillate in use, so as to effect a gyroscopic torque coupling between the primary and secondary frames. An excitation system (110) is mounted on the primary frame (301) for applying to each flywheel (50) a periodic torque that varies with the angular velocity of the secondary frame and the angular position of the axis of the flywheel relative to the secondary axis, so as to cause each flywheel to oscillate at its natural frequency in response to relative rotation between the primary and secondary frames.
    • 5. 发明公开
    • GYROSCOPIC TORQUE CONVERTER
    • 回转扭矩转换器
    • EP2118520A2
    • 2009-11-18
    • EP07848750.1
    • 2007-12-27
    • Harrison, Duncan James
    • Harrison, Duncan James
    • F16H33/10
    • F16H33/10Y10T74/1218Y10T74/1225Y10T74/1236
    • A torque converter comprises a stationary mount, input and output shafts, a primary frame (301) supported by the stationary mount for rotation about a primary axis and coupled for rotation with one of the input and output shafts (302,303), a secondary frame (50) supported by the primary frame (301) for rotation about a secondary axis perpendicular to the primary axis and coupled for rotation with the other of the input and output shafts, a plurality of flywheels (10) supported by the secondary frame (50) with their spin axes disposed at an angle to one another in the same plane, or in mutually parallel planes, and torsional springs acting between the flywheels and the secondary frame to cause the flywheels to oscillate in use, so as to effect a gyroscopic torque coupling between the primary and secondary frames. An excitation system (110) is mounted on the primary frame (301) for applying to each flywheel (50) a periodic torque that varies with the angular velocity of the secondary frame and the angular position of the axis of the flywheel relative to the secondary axis, so as to cause each flywheel to oscillate at its natural frequency in response to relative rotation between the primary and secondary frames.
    • 9. 发明公开
    • Control moment gyroscope based momentum control systems in small satellites
    • Gleroskop auf Grundlage von Impulsregelungssystemen in kleinen Satelliten
    • EP2263937A1
    • 2010-12-22
    • EP10159255.8
    • 2010-04-07
    • Honeywell International Inc.
    • McMickell, BrettBuchele, PaulGisler, Gary LynwoodAndrus, James
    • B64G1/28
    • B64G1/286Y10T74/1225Y10T74/1229Y10T74/1282
    • A self-contained momentum control system (MCS) for a spacecraft is provided for small satellites. The MCS features a miniaturized gyroscopic rotor with a rotational speed in excess of 20,000 RPM. The MCS includes at least three control moment gyroscopic mechanical assemblies (CMAs) rigidly mounted within a single enclosure, where each CMA mounted in an orientation whereby the longitudinal axis of each CMA is either orthogonal to every other CMA or is parallel to another CMA but in the opposite orientation. In order to further reduce the size of the MCS, an electronics package that is configured to interface command and control signals with and to provide power to the CMAs is included within the MCS enclosure. A plurality of shock isolation devices are used to secure each of the CMAs to the enclosure in order to reduce the launch load upon the CMAs thereby allowing the use of smaller rotor spin bearings. The MCS enclosure surrounding the CMAs and support structure is hermetically sealed.
    • 为小型卫星提供了一个用于航天器的独立动量控制系统(MCS)。 MCS具有转速超过20,000RPM的小型化陀螺转子。 MCS包括刚性地安装在单个外壳内的至少三个控制力矩陀螺机械组件(CMA),其中每个CMA以取向安装,由此每个CMA的纵向轴线与每隔一个CMA正交或者平行于另一个CMA, 相反的方向。 为了进一步减小MCS的尺寸,被配置为将命令和控制信号与CMA相连接并向其提供电力的电子装置包括在MCS机箱内。 使用多个防震隔离装置将每个CMA固定到外壳,以便减少CMA上的发射载荷,从而允许使用较小的转子旋转轴承。 围绕CMA和支撑结构的MCS外壳是密封的。
    • 10. 发明公开
    • STABILISING MEANS
    • 稳定手段
    • EP1917181A1
    • 2008-05-07
    • EP06774847.5
    • 2006-08-22
    • Technology Investment Company PTY Ltd.
    • ELMS, Anthony, Richard
    • B63B39/04B62D37/06G01C19/06
    • B62D37/06B63B39/04G01C19/16Y10T74/1221Y10T74/1225
    • A vehicle stabilising means comprising a cradle (23) supported from a mounting (17) to lie to one side of the mounting, a rotor (19) supported from the cradle between a pair of spaced supports (25) to be rotatably supported by the supports, a drive coupled to the rotor enabling the rotor to rotate at a substantially constant angular velocity, the rotor being rotatable about a first axis, the supports located to the side of the cradle remote from the mounting, the cradle further comprising a base (31) which is rotatably supported from the mounting to be rotatable around a second axis which is perpendicular to the first axis of rotation of the rotor and which intersects the first axis of the rotor, the mounting intended in use to be fixed to the vehicle such that in operation the mean orientation of the first and second axes are substantially perpendicular to the direction of the axis of stabilisation.
    • 一种车辆稳定装置,包括由安装件(17)支撑的支架(23)以位于支架的一侧,转子(19)在一对间隔开的支撑件(25)之间由支架支撑,以便由支架 支撑与所述转子耦合的驱动器,使得所述转子能够以基本恒定的角速度旋转,所述转子可围绕第一轴线旋转,所述支撑件位于所述支架的远离所述支架的一侧,所述支架进一步包括基座 31),所述支架从所述支架可旋转地支撑,以围绕垂直于所述转子的所述第一旋转轴线的第二轴线旋转,并且所述第二轴线与所述转子的第一轴线相交,所述支架在使用中被固定到车辆上 在操作中,第一和第二轴线的平均取向基本垂直于稳定轴线的方向。