公开(公告)号：US3951000A

公开(公告)日：1976-04-20

申请号：US458005

申请日：1974-04-04

Applicant: Lincoln S. Ferriss ,  Robert M. Hohenstein

Inventor： Lincoln S. Ferriss ,  Robert M. Hohenstein

IPC: G01C19/08 ,  H02N1/00 ,  G01C19/28

CPC classification number: H02N1/004 ,  G01C19/08 ,  Y10T74/1275

Abstract: An electrostatic motor which is well suited for an electrostatic gyro rotor spin up, spin down system which provides positive starting at any rotor position, choice of clock-wise or counter-clockwise rotation, spin up and spin down modes with automatic coast and stop modes, choice of full speed along with having zero induced rotor voltage and non-displacemental force generation is shown.

Abstract translation: 一种非常适合静电陀螺转子旋转的静电马达，旋转下降系统，可在任何转子位置提供正向启动，选择时钟方向或逆时针旋转，自旋和自动降档模式，具有自动惯性和停止模式 示出了全速选择以及具有零感应转子电压和非排量力产生。

公开(公告)号：US3446081A

公开(公告)日：1969-05-27

申请号：US3446081D

申请日：1967-03-08

Applicant: FABRICATION D INSTR DE MESURE

Inventor： OGER RENE

IPC: G01C19/08 ,  G01C19/16 ,  H02K1/18 ,  H02K5/24

CPC classification number: G01C19/08 ,  G01C19/16 ,  H02K1/185 ,  H02K5/24 ,  Y10T74/12 ,  Y10T74/1282

公开(公告)号：US3274837A

公开(公告)日：1966-09-27

申请号：US19950262

申请日：1962-06-01

Applicant: FENTON RALPH V ,  ISELY WILLIAM H

Inventor： FENTON RALPH V ,  ISELY WILLIAM H

IPC: G01C19/04 ,  G01C19/08

CPC classification number: G01C19/04 ,  G01C19/08 ,  Y10T74/1229 ,  Y10T74/1282

公开(公告)号：US3238432A

公开(公告)日：1966-03-01

申请号：US17862762

申请日：1962-03-09

Applicant: SPERRY RAND CORP

Inventor： AMBERGER DONALD J

IPC: G01C19/08 ,  H02P9/10 ,  H02P25/02

CPC classification number: G01C19/08 ,  H02P9/10 ,  H02P25/024 ,  Y10T74/1282

公开(公告)号：US2810843A

公开(公告)日：1957-10-22

申请号：US61399956

申请日：1956-10-04

Applicant: GASACCUMULATOR SVENSKA AB

Inventor： CARL-ERIK

IPC: G01C19/08 ,  H02K29/00 ,  H02M3/338 ,  H02M7/5383 ,  H02P6/14

CPC classification number: G01C19/08 ,  H02K29/00 ,  H02M3/338 ,  H02M7/5383 ,  H02P6/14 ,  Y10S74/06 ,  Y10T74/1275

公开(公告)号：US20210017001A1

公开(公告)日：2021-01-21

申请号：US17043435

申请日：2019-03-27

Applicant: VERTON IP PTY LTD

Inventor： Stanley Thomson ,  Andrew Miller ,  Patrick Taylor ,  Gerrard Hickson ,  Tom Koorts

IPC: B66C13/06 ,  G01C19/08 ,  G01C19/18

Abstract: A gyroscopic module comprises at least one gyroscopic rotor rotatably mounted to a support, wherein the at least one gyroscopic rotor is driven by at least one first power source and at least one gimbal frame is coupled to the support of the at least one gyroscopic rotor. The gyroscopic module comprises at least one slew bearing coupled to the at least one gimbal frame to change an orientation of the at least one gyroscopic rotor, wherein the at least one slew bearing is driven by at least one second power source mounted to the at least one gimbal frame.

公开(公告)号：US20170261321A1

公开(公告)日：2017-09-14

申请号：US15529491

申请日：2015-07-23

Applicant: Goertek, Inc.

Inventor： Tingkai Zhang

IPC: G01C19/26 ,  B81B7/00 ,  G01C19/08

CPC classification number: G01C19/26 ,  B81B7/0003 ,  B81B7/008 ,  G01C19/08 ,  G01C19/56 ,  G01C19/5684 ,  G01C19/5691 ,  G01C19/5733 ,  G01P9/02

Abstract: The present invention is related to a triaxial micro-electromechanical gyroscope, comprising: a ring-shaped detection capacitor located at the center; two sets of driving capacitors located at outer sides of the ring-shaped detection capacitor and symmetrically distributed at two sides of an origin along a y-axis; two sets of second detection capacitors located at the outer sides of the ring-shaped detection capacitor respectively and symmetrically distributed at the two sides of the origin along an x-axis; and a linkage part connected with movable polar plates of the driving capacitors, movable polar plates of the second detection capacitors, and an outer edge of ring-shaped upper polar plates of the ring-shaped detection capacitor, respectively. The triaxial micro-electromechanical gyroscope provided by the present invention adopts a single structure design, and integrates capacitive electrostatic driving and differential capacitive detection.

公开(公告)号：US20140352462A1

公开(公告)日：2014-12-04

申请号：US13886257

申请日：2013-05-02

Applicant: Walter E. Wood

Inventor： Walter E. Wood

IPC: G01C19/08 ,  G01C19/16

CPC classification number: F03G7/10 ,  Y10T74/1282

Abstract: A gyroscopic apparatus, having application as prime mover, has a pair, or alternatively multiple pairs, of flywheels disposed opposite one another. A pivot axis of the flywheels lies in a position midway between the flywheels for each pair. Each flywheel has its own separate electric motor or engine. A drive arrangement operates to spin the assembly unit about a second axis, in the same plane, but perpendicular to the flywheel pair axis.

Abstract translation: 作为原动机的陀螺仪装置具有彼此相对设置的一对或多对飞轮。 飞轮的枢转轴位于每对飞轮之间的中间位置。 每个飞轮都有自己独立的电动机或发动机。 驱动装置用于在同一平面内绕组合单元旋转第二轴线，但垂直于飞轮对轴线。

公开(公告)号：US20120199697A1

公开(公告)日：2012-08-09

申请号：US13321086

申请日：2010-05-19

Applicant: Vivek Nagabhushan ,  Norman G. Fitz-Coy ,  Frederick Aaron Leve

Inventor： Vivek Nagabhushan ,  Norman G. Fitz-Coy ,  Frederick Aaron Leve

IPC: B64G1/28 ,  G05D1/08 ,  G01C19/08 ,  B64G1/10

CPC classification number: B64G1/286 ,  B64G1/428 ,  Y10T74/1282

Abstract: Various embodiments of the present invention include an attitude control system for use with small satellites. According to various embodiments, the system allows rapid retargeting (e.g., high slew rates) and full three-axis attitude control of small satellites using a compact actuation system. In certain embodiments, the compact actuation system includes a plurality of single-gimbaled control moment gyroscopes (SGCMG) arranged in a pyramidal configuration that are disposed within a small satellite.

Abstract translation: 本发明的各种实施例包括用于小卫星的姿态控制系统。 根据各种实施例，该系统允许使用紧凑的致动系统来对小型卫星进行快速重新定向（例如高转换速率）和全三轴姿态控制。 在某些实施例中，紧凑型致动系统包括布置在金字塔形配置中的多个单平衡控制力矩陀螺仪（SGCMG），其布置在小型卫星内。

公开(公告)号：US20070131044A1

公开(公告)日：2007-06-14

申请号：US11290773

申请日：2005-11-30

Applicant: Chen-Chung Wu

Inventor： Chen-Chung Wu

IPC: G01C19/08 ,  F21L13/00

CPC classification number: A63H1/24 ,  Y10T74/12

Abstract: An electromagnetic gyro comprises a gyro body which defines a resonance circuit and at least one LED; and a base forming a self-excitation multivibrator; wherein said resonance circuit creates an alternating current induced by a variation magnetic field founded by said self-excitation multivibrator. In accordance with the present invention the electricity energy has been passed by the coupling among the windings to make the rotating gyro body light, without adding a battery therein. The circuit construction is also simple. These LEDs have high luminance through different combination of colors of which can achieve wonderful effect when the gyro body rotates. As a further improvement, there adds at least one LED in the base thereby having a function of illumination.

Abstract translation: 电磁陀螺仪包括限定谐振电路的陀螺仪和至少一个LED; 和形成自激多谐振荡器的基座; 其中所述谐振电路产生由所述自激多谐振荡器建立的变化磁场引起的交流电流。 根据本发明，通过绕组之间的耦合使电能通过，以使旋转陀螺仪体轻，而不在其中添加电池。 电路结构也很简单。 这些LED通过不同的颜色组合具有高亮度，当陀螺仪旋转时，其可以实现精彩的效果。 作为进一步的改进，在基底中添加至少一个LED，从而具有照明功能。