WO1997036361B1 - Active electromagnetic damping system for spindle motors - Google Patents
Active electromagnetic damping system for spindle motorsInfo
- Publication number
- WO1997036361B1 WO1997036361B1 PCT/US1997/004277 US9704277W WO9736361B1 WO 1997036361 B1 WO1997036361 B1 WO 1997036361B1 US 9704277 W US9704277 W US 9704277W WO 9736361 B1 WO9736361 B1 WO 9736361B1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- radial
- spin axis
- ofthe
- central shaft
- shaft
- Prior art date
Links
- 230000003534 oscillatory Effects 0.000 claims 4
- 230000000087 stabilizing Effects 0.000 claims 2
- 230000000875 corresponding Effects 0.000 claims 1
- 238000006073 displacement reaction Methods 0.000 claims 1
- 238000004804 winding Methods 0.000 claims 1
Abstract
A method of damping resonances in a rotating system is disclosed, which includes developing a representation of vibrating movement in the rotating system, taking the derivative of that representation and applying an out-of-phase active damping force based on the derivative to the rotating system to damp out the movement.
Claims
AMENDED CLAIMS
[received by the International Bureau on 25 September 1997 (25.09.97); original claims 1 , 4, 5, 14-16, 19 and 21 amended; original claims 2 and 3 cancelled, remaining claims unchanged (5 pages)]
1. A method of damping resonances in a rotating system comprising a spindle
motor having a central shaft defining the central, rotational axis ofthe system and supporting at least one disc which is subject to said undamped vibrating movement; developing a representation of vibrating movement in the rotating system;
taking the derivative of that representation;
applying an out-of-phase active, radial damping force based on said derivative to said
rotating system to damp out said movement.
4. A method as claimed in claim 1 wherein the vibrating movement is defined as a function of two angular rotations α and β which are radial and orthogonal to one another.
5. A method as claimed in claim 14 wherein the vibrating movement is defined as a function of two angular rotations α and β which are radial and orthogonal to one another.
6. A method as claimed in claim 4 wherein said active damping system introduces two radial damping forces which are proportional to the derivatives ofthe angular rotation α and β.
7. A method as claimed in claim 5 wherein said active damping system introduces two radial damping forces which are proportional to the derivatives ofthe angular rotation α and β
8. A method as claimed in claim 6 wherein the radial damping forces are applied to said central shaft below said discs.
9. A method as claimed in claim 7 wherein the radial damping forces are applied to said central shaft below said discs.
10. A method as claimed in claim 8 wherein the central shaft is supported on upper
and lower bearings, and a center of mass ofthe system is defined between the bearings.
1 1. A method as claimed in claim 9 wherein the central shaft is supported on upper and lower bearings, and a center of mass ofthe system is defined between the bearings
12. A method as claimed in claim 10 wherein said central shaft supports a rotor
magnet which rotates with said shaft, said radial active damping forces being applied to said shaft
13. A method as claimed in claim 11 wherein said central shaft supports a rotor magnet which rotates with said shaft, said radial active damping forces being applied to said shaft.
14. A method of micropositioning ofthe spin axis or damping mechanical vibration
in a rotating system comprising a spindle motor having a central shaft defining a central rotational axis
of the spindle motor corresponding to said spin axis applying a rotating force vector created by an
actuator and controlled by the position ofthe spin axis as measured by a sensing device, wherein:
a) the force being in phase quadrature with respect to the measured position or displacement of said spin axis; and b) the force being proportional to the velocity of movement of the spin axis position
and in phase opposite to said velocity
15 A method of stabilizing the central spin axis of a rotating system in a given position, said rotating system comprising a spindle motor having a central shaft defining the central spin axis; a rotor mounted on said shaft comprising an inertial load and bearing means to support said rotor for rotation relative to said shaft including developing a representation ofthe position of said spin axis or the oscillatory movements of said spin axis; and
analyzing said representation to calculate and generate radial forces which in turn stabilize the position ofthe spin axis and dampen oscillatory movements of said axis.
16. A method as claimed in claim 15 wherein the forces applied are established to be
proportional to either a derivative of position ofthe rotor or a velocity of oscillatory movement of said rotor.
17. A method as claimed in claim 16 wherein the rotating system includes an
electromagnetic actuator, and the method includes applying the forces utilizing said electromagnetic actuator.
18. A method as claimed in claim 17 wherein said electromagnetic actuator comprises stationary windings and rotating magnets surrounding said spin axis, and said method includes energizing said stationary winding to apply said forces to dampen said oscillatory movements
19. A method as claimed in claim 18 wherein said rotating system includes said motor
surrounding said spin axis and comprising magnets and windings rotating relative to one another.
20. A method as claimed in claim 19 wherein the magnets of said motor and the magnets of said stabilizing actuator are a common set of magnets.
21. A method as claimed in claim 20 wherein the rotating system is said spindle motor having a central shaft comprising said spin axis and defining the central rotational axis ofthe rotating system, and wherein said rotating system inertial load comprises at least one disc which is subject to
said undamped vibrating movement.
22. A method as claimed in claim 21 wherein the vibrating movement is defined as a
function of two angular rotations α and β which are radial and orthogonal to one another
23. A method as claimed in claim 22 wherein the radial damping forces are applied to
said central shaft below said discs.
24. A method as claimed in claim 23 wherein the central shaft is supported on upper
and lower bearings, and a center of mass ofthe system is defined between the bearings
- -
25 A method as claimed in claim 24 wherein said central shaft supports a rotor magnet which rotates with said shaft, said radial active damping forces being applied to said shaft
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9818259A GB2325534B (en) | 1996-03-26 | 1997-03-19 | Active electromagnetic damping system for spindle motors |
US09/029,044 US6140790A (en) | 1996-03-26 | 1997-03-19 | Active electromagnetic damping system for spindle motors |
DE19781660T DE19781660T1 (en) | 1996-03-26 | 1997-03-19 | Active, electromagnetic damping system for spindle motors |
JP9534469A JP2000507335A (en) | 1996-03-26 | 1997-03-19 | Active electromagnetic damping system for spindle motor |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US1417896P | 1996-03-26 | 1996-03-26 | |
US60/014,178 | 1996-03-26 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO1997036361A1 WO1997036361A1 (en) | 1997-10-02 |
WO1997036361B1 true WO1997036361B1 (en) | 1997-11-06 |
Family
ID=21763976
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US1997/004277 WO1997036361A1 (en) | 1996-03-26 | 1997-03-19 | Active electromagnetic damping system for spindle motors |
Country Status (6)
Country | Link |
---|---|
US (1) | US6140790A (en) |
JP (2) | JP2000507335A (en) |
KR (1) | KR100371993B1 (en) |
DE (1) | DE19781660T1 (en) |
GB (1) | GB2325534B (en) |
WO (1) | WO1997036361A1 (en) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7123431B2 (en) * | 2002-07-30 | 2006-10-17 | International Business Machines Corporation | Precise positioning of media |
DE10302531B4 (en) * | 2003-01-20 | 2007-02-08 | Minebea Co., Ltd. | Measuring device and measuring method for electric motors |
JP2004341608A (en) * | 2003-05-13 | 2004-12-02 | Mitsutoyo Corp | Machinery |
EP1621785A1 (en) * | 2004-07-30 | 2006-02-01 | Mecos Traxler AG | Method and apparatus for controlling a magnetic bearing device |
US7370524B2 (en) * | 2004-08-13 | 2008-05-13 | Lawrence Livermore National Security, Llc | Adaptive vibration control using synchronous demodulation with machine tool controller motor commutation |
US7525266B2 (en) * | 2006-01-30 | 2009-04-28 | Honeywell International Inc. | Inverter loop latch with integrated AC detection reset |
DE102006042539C5 (en) * | 2006-09-11 | 2016-10-20 | Gottfried Wilhelm Leibniz Universität Hannover | Work spindle and method for operating a work spindle |
CN102292771A (en) | 2009-02-10 | 2011-12-21 | 富士通株式会社 | Library device and control method thereof |
US9638508B2 (en) | 2012-02-01 | 2017-05-02 | Seagate Technology Llc | Offset reduction for displacement sensor |
US9482510B2 (en) | 2012-02-01 | 2016-11-01 | Seagate Technology, Llc | Noise measurement for measured displacement |
US9310179B2 (en) | 2012-02-01 | 2016-04-12 | Seagate Technology Llc | Spindle force actuator |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3608383A (en) * | 1970-02-04 | 1971-09-28 | Us Army | Single axis rate gyro and piezotransistor angular rate detector |
US3974434A (en) * | 1974-03-08 | 1976-08-10 | Electronic Engineering Company Of California | Stepping motor signal circuit |
US3891285A (en) * | 1974-05-13 | 1975-06-24 | Rockwell International Corp | Electrostatic bearing sensing and control circuitry |
US4352481A (en) * | 1980-03-13 | 1982-10-05 | Hughes Aircraft Company | Apparatus and method for electronic damping of resonances |
FR2561738B1 (en) * | 1984-03-26 | 1986-08-22 | Europ Propulsion | METHOD AND DEVICE FOR REDUCING THE VIBRATION OF ROTATING MACHINES EQUIPPED WITH AN ACTIVE MAGNETIC SUSPENSION |
US4848169A (en) * | 1987-05-22 | 1989-07-18 | Honeywell, Inc. | Two axis rate gyro apparatus |
JPS6446015A (en) * | 1987-08-08 | 1989-02-20 | Shinko Electric Co Ltd | Control apparatus of magnetic bearing |
JPH0332338A (en) * | 1989-06-26 | 1991-02-12 | Shimadzu Corp | Magnetic bearing formed integrally with motor |
CA1332969C (en) * | 1989-09-29 | 1994-11-08 | Francois Paquet | Analog torque rebalance loop for a tuned rotor gyroscope |
US5272815A (en) * | 1990-11-14 | 1993-12-28 | Tokimec Inc. | Gyro compass |
JP3463218B2 (en) * | 1993-12-24 | 2003-11-05 | 光洋精工株式会社 | Magnetic bearing device |
JP3550584B2 (en) * | 1995-04-21 | 2004-08-04 | 正 深尾 | Electromagnetic rotating machine |
-
1997
- 1997-03-19 US US09/029,044 patent/US6140790A/en not_active Expired - Lifetime
- 1997-03-19 JP JP9534469A patent/JP2000507335A/en not_active Ceased
- 1997-03-19 WO PCT/US1997/004277 patent/WO1997036361A1/en active IP Right Grant
- 1997-03-19 GB GB9818259A patent/GB2325534B/en not_active Expired - Fee Related
- 1997-03-19 DE DE19781660T patent/DE19781660T1/en not_active Withdrawn
- 1997-03-19 KR KR10-1998-0707458A patent/KR100371993B1/en not_active IP Right Cessation
-
2009
- 2009-03-04 JP JP2009050819A patent/JP4980386B2/en not_active Expired - Lifetime
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