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公开(公告)号：US20110283826A1
公开(公告)日：2011-11-24
申请号：US12782547
申请日：2010-05-18
申请人： Porter Davis
发明人： Porter Davis
CPC分类号： B64G1/286
摘要： A control moment gyroscope assembly including, but not limited to, a rotor that includes a shaft, a primary rim and a web that connects the shaft to the primary rim. The rotor is made from a metal material and is adapted to spin about the shaft. The control moment gyroscope assembly further includes a secondary rim that is made of the metal material and that is disposed around the rotor. The secondary rim is configured to compress the rotor in the direction of the shaft.
摘要翻译： 控制力矩陀螺仪组件包括但不限于包括轴，主缘和将轴连接到主轮缘的腹板的转子。 转子由金属材料制成并适于围绕轴旋转。 控制力矩陀螺仪组件还包括由金属材料制成并且设置在转子周围的次级边缘。 次级轮缘构造成沿着轴的方向压缩转子。
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公开(公告)号：US20100101341A1
公开(公告)日：2010-04-29
申请号：US12258170
申请日：2008-10-24
申请人： Brian P. Bunch , Steve Mowry , Paul Ferguson
发明人： Brian P. Bunch , Steve Mowry , Paul Ferguson
IPC分类号： G01C19/06
CPC分类号： H01Q3/08 , Y10T74/1225
摘要： Gimbal power systems and methods are operable to provide power to a device attached to the gimbal. An exemplary embodiment is configured to rotate a rotational member of the gimbal system about an axis, wherein a stator of a rotary power transformer affixed to the rotational member rotates about the axis, and wherein an end of an electrical connection coupled to a power connector of a rotor winding of the rotary power transformer remains substantially stationary as the stator of the rotary power transformer rotates about the axis.
摘要翻译： 云台电力系统和方法可操作以向连接到万向节的设备提供电力。 一个示例性实施例被配置为围绕一个轴线旋转万向节系统的旋转构件，其中固定到旋转构件的旋转动力变压器的定子围绕轴线旋转，并且其中电连接的一端与电力连接器 当旋转动力变压器的定子围绕轴旋转时，旋转动力变压器的转子绕组保持基本上静止。
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公开(公告)号：US20100064828A1
公开(公告)日：2010-03-18
申请号：US12212401
申请日：2008-09-17
IPC分类号： G01C19/06
CPC分类号： B64G1/286 , Y10T74/12 , Y10T74/1229 , Y10T74/1282 , Y10T74/1289 , Y10T74/1296
摘要： A rotor assembly is provided for deployment within the inner gimbal assembly of a control moment gyroscope (CMG). In one embodiment, the rotor assembly includes a rotor shell, a rotor shaft fixedly coupled to the rotor shell, and a rotor rim. The rotor rim includes an annular body and a strain relief member. A first end portion of the strain relief member is fixedly coupled to the annular body, and a second end portion of the strain relief member is fixedly coupled to the rotor shell to form a rim-shell joinder interface. The strain relief member has a flexibility sufficient to reduce the mechanical stress experienced by the rim-shell joinder interface during operation of the CMG.
摘要翻译： 提供转子组件用于展开在控制力矩陀螺仪（CMG）的内部万向节组件内。 在一个实施例中，转子组件包括转子壳体，固定地联接到转子壳体的转子轴和转子轮缘。 转子轮辋包括环形体和应变消除部件。 应变消除构件的第一端部固定地联接到环形体，并且应变消除构件的第二端部固定地联接到转子壳体以形成边缘 - 壳体接合界面。 应变消除构件具有足够的灵活性，以降低在操作CMG期间轮辋 - 壳接合界面所经历的机械应力。
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公开(公告)号：US07181987B2
公开(公告)日：2007-02-27
申请号：US10428761
申请日：2003-05-02
申请人： Peter Winston Hamady
发明人： Peter Winston Hamady
CPC分类号： A63B21/22 , A63B21/222 , F03G3/00 , G01C19/04 , G01C19/24 , Y10T74/1204 , Y10T74/1207 , Y10T74/1221 , Y10T74/1229 , Y10T74/1254 , Y10T74/1282
摘要： A precessional device having independent control of the output torque generated by the device and the oscillation race of the device is disclosed. The device comprises a rotor supported by an axle wherein the ends of the axle are supported by a circular race. The circular race is rotatable, and may be driven by, for example, a motor, thereby controlling the oscillation rate of the device independently of the output torque arising front the rotation rate of the rotor. The motor may be controlled by a control program that adjusts the rotation rate of the circular race to modify the shape of the resistance curve.
摘要翻译： 公开了一种具有独立控制装置产生的输出转矩和装置摆动轨迹的进动装置。 该装置包括由轴支撑的转子，其中轴的端部由圆形座圈支撑。 圆弧可以旋转，并且可以由例如电动机驱动，从而独立于在转子旋转速度之前产生的输出转矩来控制装置的振荡速率。 电动机可以通过调节圆弧的旋转速度来控制以修改电阻曲线的形状的控制程序来控制。
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公开(公告)号：US07111522B2
公开(公告)日：2006-09-26
申请号：US10788745
申请日：2004-02-26
CPC分类号： H02K7/025 , Y02E60/16 , Y10T74/1282 , Y10T74/2119 , Y10T74/2191
摘要： A containment vessel used to enclose an energy storage flywheel system during certification testing of the energy storage flywheel system includes a plurality of concentrically disposed vessels. One or more intermediate shields are freely disposed within an outer shield, and an inner shield is freely disposed within the intermediate shields. The inner shield includes a deflector rim disposed proximate one of its ends that is configured to absorb the energy of ejected material, in the highly unlikely event of a flywheel failure during testing.
摘要翻译： 用于在能量存储飞轮系统的认证测试期间封闭储能飞轮系统的安全壳体包括多个同心设置的容器。 一个或多个中间屏蔽件自由地设置在外屏蔽件内，并且内屏蔽件自由地设置在中间屏蔽件内。 内屏蔽件包括靠近其端部之一设置的偏转器边缘，其构造成在测试期间在飞轮故障的极不可能的情况下吸收喷射材料的能量。
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公开(公告)号：US20050125111A1
公开(公告)日：2005-06-09
申请号：US10681853
申请日：2003-10-06
申请人： J. Bonn , Mason Peck
发明人： J. Bonn , Mason Peck
CPC分类号： G01C19/30 , B64G1/286 , G01C19/065 , G05D1/0883 , Y10T74/1204 , Y10T74/1218 , Y10T74/1221
摘要： Methods and apparatus are provided for reorienting control moment gyros (CMGs) to compensate for CMG failure or change in spacecraft (S/C) mass properties or mission. An improved CMG comprises a drive means for rotating the CMG around an axis not parallel to the CMG gimbal axis. Releasable clamps lock the CMG to the spacecraft except during CMG array reorientation. CMGs arrays are combined with attitude sensors, a command module, memory for storing data and programs, CMG drivers and sensors (preferably for each CMG axis), and a controller coupling these elements. The method comprises determining whether a CMG has failed or the S/C properties or mission changed, identifying the working CMGs of the array, determining a new array reorientation for improved spacecraft control, unlocking, reorienting and relocking the CMGs in the array and updating the S/C control parameters for the new array orientation.
摘要翻译： 提供了方法和装置，用于重新定向控制力矩陀螺（CMG），以补偿CMG故障或航天器（S / C）质量属性或任务的变化。 改进的CMG包括用于围绕不平行于CMG万向轴的轴线旋转CMG的驱动装置。 除了在CMG阵列重新定向之外，可拆卸的夹具将CMG锁定到航天器。 CMG阵列与姿态传感器，命令模块，用于存储数据和程序的存储器，CMG驱动器和传感器（优选为每个CMG轴）组合，以及耦合这些元件的控制器。 该方法包括确定CMG是否发生故障或S / C属性或任务改变，识别阵列的工作CMG，确定用于改进的航天器控制，解锁，重定向和重新锁定阵列中的CMG的新阵列重定向，并更新 新数组方向的S / C控制参数。
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公开(公告)号：US4916957A
公开(公告)日：1990-04-17
申请号：US191504
申请日：1988-05-09
申请人： Thomas R. Quermann
发明人： Thomas R. Quermann
CPC分类号： G01C19/06 , G01C19/28 , Y10T74/1257 , Y10T74/1275
摘要： A gyroscopic rate sensor has a motor driven shaft on which is mounted a flexible disc rotor enclosed in a gas-filled housing with a rotating rigid plate, also mounted on the shaft, to provide viscous gaseous restraint. A rotating capacitive plate assembly referenced to the drive motor spin axis provides a stable electrical output signal proportional to periodic deflections of the disc rotor. By perforating the disc rotor near the spin axis, spring restraint is minimized while the squeeze film damping provides improved dynamic response.
摘要翻译： 陀螺仪速率传感器具有马达驱动轴，在该马达驱动轴上安装有柔性圆盘转子，该柔性圆盘转子封装在具有旋转刚性板的充气壳体中，旋转刚性板也安装在轴上，以提供粘性气体约束。 以驱动电动机旋转轴为参照的旋转电容板组件提供与盘式转子的周期性偏转成比例的稳定的电输出信号。 通过在旋转轴附近穿过圆盘转子，弹簧约束最小化，而挤压膜阻尼提供改进的动态响应。
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公开(公告)号：US4466299A
公开(公告)日：1984-08-21
申请号：US413265
申请日：1964-11-23
CPC分类号： G01C19/20 , Y10T74/12 , Y10T74/1229 , Y10T74/1282
摘要： A gyro assembly including a rotor, stator, hysteresis motor and conical hydrodynamic bearings for supporting the rotor relative to the stator.
摘要翻译： 包括转子，定子，滞后电动机和用于相对于定子支撑转子的锥形流体动力轴承的陀螺仪组件。
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公开(公告)号：US4343203A
公开(公告)日：1982-08-10
申请号：US812296
申请日：1977-07-01
IPC分类号： G01C19/06
CPC分类号： G01C19/06 , Y10T74/12 , Y10T74/1296
摘要： A gyroscopic rotor device is designed to eliminate any spin bearing outer raceway distortion and/or axial preload changes due to centrifugal and thermal effects in a bimetal rotor assembly by means of judicial geometric shaping of the rotor components. The shaping of the heavy metal motor rim and/or the lower density metal rotor spin bearing support web interface includes a discrete number of stress concentrating pads and an equal number of holes formed in the bearing web opposite each of the pads for isolating any strain induced within the bearing web from the spin bearing outer race.
摘要翻译： 陀螺转子装置被设计成通过转子部件的司法几何形状来消除由于双金属转子组件中的离心和热效应引起的旋转轴承外滚道变形和/或轴向预载变化。 重金属电机边缘和/或较低密度的金属转子旋转轴承支撑腹板界面的成形包括离散数量的应力集中垫和在轴承腹板中形成的相同数量的孔，与每个垫相对，用于隔离任何应变诱发 在旋转轴承外圈的轴承网内。
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公开(公告)号：US4299127A
公开(公告)日：1981-11-10
申请号：US103353
申请日：1979-12-13
申请人： E. Paul Shannon
发明人： E. Paul Shannon
IPC分类号： G01C19/06
摘要： Flexible-hub magnetic gyro wheel including a ring member comprising ferromagnetic material or the like and including a plurality of alternating magnetic poles circumferentially spaced about the ring member, a flexible hub affixed to the interior of the ring, and structure rigidly attaching the flexible hub to a drive shaft, such as the shaft of a motor or a shaft driven by a motor or other drive structure. The structure for rigidly attaching the flexible hub to a shaft consists of a set collar and a set washer on opposing sides of the center of the hub material whereby the set collar and set washer support the magnetic gyro wheel on an axially rotating shaft. The magnetic gyro wheel is suitable for use in a rate of turn indicator, a gyro, or other like instrument designed to sense and respond to a rate of turn or angular velocity applied to the instrument at a right angle to the spin axis of the magnetic gyro wheel. The magnetic gyro wheel can comprise one or more rings of magnetic material magnetized with alternating poles with the flexible hub attached thereto or can be fabricated from a plurality of magnets held together in such a way as to achieve the characteristics of the magnetized ring or rings described above. As one alternative the magnetic gyro wheel can also be made of a flexible magnetic material magnetized with alternate magnetic domains on one or both sides of the wheel or upon the periphery of the wheel.
摘要翻译： 柔性毂式磁陀螺轮，包括包括铁磁材料等的环构件，并且包括围绕环构件周向间隔开的多个交变磁极，固定到环的内部的柔性毂，以及将柔性毂刚性地附接到 驱动轴，例如电动机的轴或由电动机或其它驱动结构驱动的轴。 用于将柔性轮毂刚性地连接到轴的结构包括在毂材料的中心的相对侧上的固定套环和套圈，由此套圈和固定垫圈将磁陀螺轮支撑在轴向旋转的轴上。 磁陀螺轮适用于转向指示器，陀螺仪或其他类似仪器的速率，其设计用于感测并响应与磁体的旋转轴成直角的施加到仪器的转动速度或角速度 陀螺轮。 磁性陀螺轮可以包括一个或多个被磁化的磁性材料环，其具有连接到其上的柔性毂的交替的磁极，或者可以由保持在一起的多个磁体制成，以实现所描述的磁化环或环的特性 以上。 作为一种替代方案，磁陀螺轮也可以由在轮的一侧或两侧上或在车轮周边上用交替磁畴磁化的柔性磁性材料制成。
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