CA2327492C - Magnetically suspended flywheel system - Google Patents

Magnetically suspended flywheel system Download PDF

Info

Publication number
CA2327492C
CA2327492C CA2327492A CA2327492A CA2327492C CA 2327492 C CA2327492 C CA 2327492C CA 2327492 A CA2327492 A CA 2327492A CA 2327492 A CA2327492 A CA 2327492A CA 2327492 C CA2327492 C CA 2327492C
Authority
CA
Canada
Prior art keywords
shaped
magnet
assembly
ring
rotor
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CA2327492A
Other languages
French (fr)
Other versions
CA2327492A1 (en
Inventor
Go Simon Sunatori
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CA2327492A priority Critical patent/CA2327492C/en
Publication of CA2327492A1 publication Critical patent/CA2327492A1/en
Application granted granted Critical
Publication of CA2327492C publication Critical patent/CA2327492C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C39/00Relieving load on bearings
    • F16C39/06Relieving load on bearings using magnetic means
    • F16C39/063Permanent magnets
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K7/00Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/02Additional mass for increasing inertia, e.g. flywheels
    • H02K7/025Additional mass for increasing inertia, e.g. flywheels for power storage
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02NELECTRIC MACHINES NOT OTHERWISE PROVIDED FOR
    • H02N15/00Holding or levitation devices using magnetic attraction or repulsion, not otherwise provided for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2361/00Apparatus or articles in engineering in general
    • F16C2361/55Flywheel systems
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/16Mechanical energy storage, e.g. flywheels or pressurised fluids

Abstract

A magnetically suspended flywheel system comprises a housing, a stator assembly, and a rotor assembly. The stator assembly comprises a ring-shaped stator magnet having a substantially triangular cross section. The rotor assembly comprises a vertical shaft, a cone-shaped rotor magnet having a substantially triangular cross section, and a flywheel. The ring-shaped stator magnet has the same sense of magnetisation as the cone-shaped rotor magnet. The ring-shaped stator magnet forms inverse heart-shaped magnetic flux lines, and the cone-shaped rotor magnet forms heart-shaped magnetic flux lines. An upward magnetic repulsion force between the inverse heart-shaped magnetic flux lines of the ring-shaped stator magnet and the heart-shaped magnetic flux lines of the cone-shaped rotor magnet equals a downward gravitational force by the rotor assembly in order to passively suspend the rotor assembly so that the rotor assembly is capable of rotating around the central axis of rotation. This invention relates to flywheel systems, and the principal use of the invention is for kinetic energy storage systems.

Description

Description Title = Magnetically Suspended Flywheel System Technical Field = This invention relates to flywheel systems, more particularly to a magnetic flywheel system.

Background Art = There are many instances where it would be desirable to be able to use a magnetic force in order to suspend a flywheel for a low-friction operation.

= A number of patents disclose flywheel systems having active magnetic suspension systems, or superconducting magnetic bearings comprising low-temperature superconductors or high-temperature superconductors using Meissner effect, in order to circumvent Earnshaw's Theorem and to levitate a flywheel with static stability.

= Canadian Patent 2 190 298 discloses "Magnetically Levitated Axleless Wheel System". This prior art has a magnetically levitated wheel made of permanent magnets, but it does not have a flywheel for kinetic energy storage.

= U.S. Patent 4 382 245 discloses "Levitation device", or Levitron (Trade Mark). This prior art has a dish-shaped permanent magnet in one form with an upper surface of a first polarity and a lower surface of a second polarity disposed in co-axial relationship to a second magnet having the opposite polar relationships.

= U.S. Patent 5 495 221 discloses "Dynamically stable magnetic suspension/bearing system". This prior art contains magnetic subsystems which act together to support a rotating element in a state of dynamic equilibrium.

= U.S. Patent 5 760 506 discloses "Flywheels for energy storage". This prior art has a bearing assembly including a bulk high temperature superconductive magnet that provides lateral stability to the flywheel.

= These prior art arrangements do not have a passive magnetic suspension system which operates at room temperature, and uses permanent magnets to form a cone-shaped well in a toroidal magnetic field.

Description of the Invention = It is a primary object of the invention to provide a flywheel system which has a passive magnetic suspension system.

= It is another object of the invention to provide a flywheel system which operates at room temperature.

= It is another object of the invention to provide a flywheel system which uses permanent magnets in order to form a cone-shaped well in a toroidal magnetic field.

= A magnetically suspended flywheel system comprises a housing, a stator assembly, and a rotor assembly. The stator assembly comprises a ring-shaped stator magnet having a substantially triangular cross section. The rotor assembly comprises a vertical shaft, a cone-shaped rotor magnet having a substantially triangular cross section, and a flywheel. The ring-shaped stator magnet has the same sense of magnetisation as the cone-shaped rotor magnet. The ring-shaped stator magnet forms inverse heart-shaped magnetic flux lines, and the cone-shaped rotor magnet forms heart-shaped magnetic flux lines. An upward magnetic repulsion force between the inverse heart-shaped magnetic flux lines of the ring-shaped stator magnet and the heart-shaped magnetic flux lines of the cone-shaped rotor magnet equals a downward gravitational force by the rotor assembly in order to passively suspend the rotor assembly so that the rotor assembly is capable of rotating around the central axis of rotation.

Brief Description of the Figures in the Drawings = In drawings which illustrate embodiments of the invention:

o Figure 1 marked "Prior Art" is a sectional side view of a conventional magnetically suspended flywheel system;

o Figure 2 marked "Prior Art" is a sectional top view of a conventional magnetically suspended flywheel system;

o Figure 3 marked "Prior Art" is a schematic diagram of a conventional magnetically suspended flywheel system;

o Figure 4 is a sectional side view of one embodiment of a magnetically suspended flywheel system according to the invention;

o Figure 5 is a sectional top view of one embodiment of a magnetically suspended flywheel system according to the invention;

o Figure 6 is a schematic diagram of one embodiment of a magnetically suspended flywheel system according to the invention;

o Figure 7 is a sectional side view of another embodiment of a magnetically suspended flywheel system according to the invention;
o Figure 8 is a sectional top view of another embodiment of a magnetically suspended flywheel system according to the invention;
and o Figure 9 is a schematic diagram of another embodiment of a magnetically suspended flywheel system according to the invention.
Modes for Carrying Out the Invention = One conventional flywheel system shown in Figure 1 in sectional side view marked "Prior Art" and Figure 2 in sectional top view marked "Prior Art"
comprises a housing 1-0, a stator assembly, and a rotor assembly.

= The stator assembly comprises a ring-shaped stator magnet 1-1, securely attached to the housing 1-0.
= The rotor assembly has a central axis of rotation, and is co-axially placed relative to the stator assembly. The rotor assembly comprises a vertical shaft 1-2 made of a non-magnetic material, a disc-shaped rotor magnet 1-3, and a flywheel 1-4 made of a ferromagnetic material such as iron (Fe), cobalt (Co) or nickel (Ni) so that the rotor assembly can be set in motion by an external prime mover magnetically coupled to the flywheel. The vertical shaft 1-2 has a top portion and a bottom portion.
The disc-shaped rotor magnet 1-3 is securely attached to the top portion of the vertical shaft 1-2. The flywheel 1-4 is securely attached to the bottom portion of the vertical shaft 1-2.

= The ring-shaped stator magnet 1-1 has the opposite sense of magnetisation to the disc-shaped rotor magnet 1-3. The ring-shaped stator magnet 1-1 forms magnetic flux lines, and the disc-shaped rotor magnet 1-3 forms magnetic flux lines. An upward magnetic repulsion force (Fm) between the magnetic flux lines of the ring-shaped stator magnet 1-1 and the magnetic flux lines of the disc-shaped rotor magnet 1-3 equal a downward gravitational force (Fg) by the rotor assembly in order to passively suspend the rotor assembly so that the rotor assembly is capable of rotating around the central axis of rotation, as shown in the schematic diagram of Figure 3 marked "Prior Art".

= Magnetic flux lines flowing in a same direction indicate a stable pattern, while magnetic flux lines flowing in opposite directions indicate an unstable pattern. The unstable magnetic flux line patterns at the air gap between the ring-shaped stator magnet 1-1 and the disc-shaped rotor magnet 1-3 in Figure 3 provide axial stability and radial instability. Although the diameter of the ring-shaped stator magnet 1-1 is different from the diameter of the disc-shaped rotor magnet 1-3, an eddy-current stabiliser 1-5 is required in order to overcome the radial instability. The gravitational force is used to suppress "tilt" and "whirl" instabilities.

= In one embodiment of the invention shown in Figure 4 in sectional side view and Figure 5 in sectional top view, a flywheel system comprises a housing 2-0, a stator assembly, and a rotor assembly.

= The stator assembly comprises a ring-shaped stator magnet 2-1 having a substantially triangular cross section, securely attached to the housing 2-0.

= The rotor assembly has a central axis of rotation, and is co-axially placed relative to the stator assembly. The rotor assembly comprises a vertical shaft 2-2 made of a non-magnetic material, a cone-shaped rotor magnet 2-3 having a substantially triangular cross section, and a flywheel 2-4 made of a non-magnetic material. The vertical shaft 2-2 has a top portion and a bottom portion. The cone-shaped rotor magnet 2-3 is securely attached to the top portion of the vertical shaft 2-2. The flywheel 2-4 is securely attached to the bottom portion of the vertical shaft 2-2.

= Unlike the conventional flywheel system, the ring-shaped stator magnet 2-1 has the same sense of magnetisation as the cone-shaped rotor magnet 2-3. The ring-shaped stator magnet 2-1 forms inverse heart-shaped magnetic flux lines, and the cone-shaped rotor magnet 2-3 forms heart-shaped magnetic flux lines. An upward magnetic repulsion force (Fm) between the inverse heart-shaped magnetic flux lines of the ring-shaped stator magnet 2-1 and the heart-shaped magnetic flux lines of the cone-shaped rotor magnet 2-3 equals a downward gravitational force (Fg) by the rotor assembly in order to passively suspend the rotor assembly so that the rotor assembly is capable of rotating around the central axis of rotation, as shown in the schematic diagram of Figure 6.

= Magnetic flux lines flowing in a same direction indicate a stable pattern, while magnetic flux lines flowing in opposite directions indicate an unstable pattern. The stable magnetic flux line patterns at the air gap between the ring-shaped stator magnet 2-1 and the cone-shaped rotor magnet 2-3 in Figure 6 provide axial stability and radial stability. These stabilities are due to a cone-shaped well in a toroidal magnetic field, which is formed by a concentrated first magnetic pole and a distributed second magnetic pole. The stable force field counters any overturning tendencies of the magnets. The gravitational force is used to suppress "tilt" and "whirl" instabilities.

= The equilibrium in this configuration is analogous to the Lagrange Points between gravitational bodies in space.

= Preferably, the ring-shaped stator magnet 2-1 of the stator assembly and the cone-shaped rotor magnet 2-3 of the rotor assembly are made of rare-earth permanent magnet, which is an electrical insulator so that eddy current is not induced during operation.

= The ring-shaped stator magnet 2-1 of the stator assembly may consist of a plurality of ring-shaped magnets having different diameters, concentrically stacked together.

= The cone-shaped rotor magnet 2-3 of the rotor assembly may consist of a plurality of disc-shaped magnets having different diameters, concentrically stacked together.

= In another embodiment of the invention shown in Figure 7 in sectional side view and Figure 8 in sectional top view, a flywheel system comprises a housing 3-0, a stator assembly, and a rotor assembly.

= The stator assembly comprises a cone-shaped stator magnet 3-1 having a substantially triangular cross section, securely attached to the housing 3-0.

= The rotor assembly has a central axis of rotation, and is co-axially placed relative to the stator assembly. The rotor assembly comprises a vertical shaft 3-2 made of a non-magnetic material, a ring-shaped rotor magnet 3-3 having a substantially triangular cross section, and a flywheel 3-4 made of a ferromagnetic material such as iron (Fe), cobalt (Co) or nickel (Ni) so that the rotor assembly can be set in motion by an external prime mover magnetically coupled to the flywheel. The vertical shaft 3-2 has a top portion and a bottom portion. The ring-shaped rotor magnet 3-3 is securely attached to the top portion of the vertical shaft 3-2. The flywheel 3-4 is securely attached to the bottom portion of the vertical shaft 3-2.

= Unlike the conventional flywheel system, the cone-shaped stator magnet 3-1 has the same sense of magnetisation as the ring-shaped rotor magnet 3-3. The cone-shaped stator magnet 3-1 forms inverse heart-shaped magnetic flux lines, and the ring-shaped rotor magnet 3-3 forms heart-shaped magnetic flux lines. An upward magnetic repulsion force (Fm) between the inverse heart-shaped magnetic flux lines of the cone-shaped stator magnet 3-1 and the heart-shaped magnetic flux lines of the ring-shaped rotor magnet 3-3 equals a downward gravitational force (Fg) by the rotor assembly in order to passively suspend the rotor assembly so that the rotor assembly is capable of rotating around the central axis of rotation, as shown in the schematic diagram of Figure 9.

= Magnetic flux lines flowing in a same direction indicate a stable pattern, while magnetic flux lines flowing in opposite directions indicate an unstable pattern. The stable magnetic flux line patterns at the air gap between the cone-shaped stator magnet 3-1 and the ring-shaped rotor magnet 3-3 in Figure 9 provide axial stability and radial stability. These stabilities are due to a cone-shaped well in a toroidal magnetic field, which is formed by a concentrated first magnetic pole and a distributed second magnetic pole. The stable force field counters any overturning tendencies of the magnets. The gravitational force is used to suppress "tilt" and "whirl" instabilities.

= The equilibrium in this configuration is analogous to the Lagrange Points between gravitational bodies in space.

= Preferably, the cone-shaped stator magnet 3-1 of the stator assembly and the ring-shaped rotor magnet 3-3 of the rotor assembly are made of rare-earth permanent magnet, which is an electrical insulator so that eddy current is not induced during operation.

= The cone-shaped stator magnet 3-1 of the stator assembly may consist of a plurality of disc-shaped magnets having different diameters, concentrically stacked together.

= The ring-shaped rotor magnet 3-3 of the rotor assembly may consist of a plurality of ring-shaped magnets having different diameters, concentrically stacked together.

= The housing 2-0 in Figure 4 and the housing 3-0 in Figure 7 may be hermetically sealed in a partial vacuum in order to reduce air resistance by rotational movement of the rotor assembly.

= The flywheel system may further comprise a bearing assembly securely attached to the housing and to the vertical shaft in order to provide additional stability. The bearing assembly may be placed above the flywheel or below the flywheel. The bearing assembly may be a magnetic bearing or a mechanical bearing.

Claims (16)

1. A flywheel system, comprising:

.circle. a housing;

.circle. a stator assembly comprising:

~ a ring-shaped stator magnet having an equilaterally triangular cross section, the equilaterally triangular cross section having an angle of pi/3 radian (60 degrees), the ring-shaped stator securely attached to the housing; and .circle. a rotor assembly having a central axis of rotation, the rotor assembly co-axially placed relative to the stator assembly, comprising:

~ a vertical shaft made of a non-magnetic material, the vertical shaft having a top portion and a bottom portion;

~ a cone-shaped rotor magnet having an equilaterally triangular cross section, the equilaterally triangular cross section having an angle of pi/3 radian (60 degrees), the cone-shaped rotor magnet securely attached to the top portion of the vertical shaft; and ~ a flywheel made of a ferromagnetic material such as iron (Fe), cobalt (Co) or nickel (Ni) so that the rotor assembly can be set in motion by an external prime mover magnetically coupled to the flywheel, the flywheel securely attached to the bottom portion of the vertical shaft;

the ring-shaped stator magnet having the same sense of magnetisation as the cone-shaped rotor magnet, an upward magnetic repulsion force between the inverse heart-shaped magnetic flux lines of the ring-shaped stator magnet and the heart-shaped magnetic flux lines of the cone-shaped rotor magnet passively suspending the rotor assembly so that the rotor assembly is capable of rotating around the central axis of rotation.
2. The flywheel system as defined in claim 1, in which the ring-shaped stator magnet of the stator assembly is made of rare-earth permanent magnet.
3. The flywheel system as defined in claim 1, in which the ring-shaped stator magnet of the stator assembly consists of a plurality of ring-shaped magnets having different diameters, concentrically stacked together.
4. The flywheel system as defined in claim 1, in which the cone-shaped rotor magnet of the rotor assembly is made of rare-earth permanent magnet.
5. The flywheel system as defined in claim 1, in which the cone-shaped rotor magnet of the rotor assembly consists of a plurality of disc-shaped magnets having different diameters, concentrically stacked together.
6. A flywheel system, comprising:

.circle. a housing;

.circle. a stator assembly comprising:

~ a cone-shaped stator magnet having an equilaterally triangular cross section, the equilaterally triangular cross section having an angle of pi/3 radian (60 degrees), the cone-shaped stator magnet securely attached to the housing; and .circle. a rotor assembly having a central axis of rotation, the rotor assembly co-axially placed relative to the stator assembly, comprising:

~ a vertical shaft made of a non-magnetic material, the vertical shaft having a top portion and a bottom portion;

~ a ring-shaped rotor magnet having an equilaterally triangular cross section, the equilaterally triangular cross section having an angle of pi/3 radian (60 degrees), the ring-shaped rotor magnet securely attached to the top portion of the vertical shaft; and ~ a flywheel made of a ferromagnetic material such as iron (Fe), cobalt (Co) or nickel (Ni) so that the rotor assembly can be set in motion by an external prime mover magnetically coupled to the flywheel, the flywheel securely attached to the bottom portion of the vertical shaft;

the cone-shaped stator magnet having the same sense of magnetisation as the ring-shaped rotor magnet, an upward magnetic repulsion force between the inverse heart-shaped magnetic flux lines of the cone-shaped stator magnet and the heart-shaped magnetic flux lines of the ring-shaped rotor magnet passively suspending the rotor assembly so that the rotor assembly is capable of rotating around the central axis of rotation.
7. The flywheel system as defined in claim 6, in which the cone-shaped stator magnet of the stator assembly is made of rare-earth permanent magnet.
8. The flywheel system as defined in claim 6, in which the cone-shaped stator magnet of the stator assembly consists of a plurality of disc-shaped magnets having different diameters, concentrically stacked together.
9. The flywheel system as defined in claim 6, in which the ring-shaped rotor magnet of the rotor assembly is made of rare-earth permanent magnet.
10. The flywheel system as defined in claim 6, in which the ring-shaped rotor magnet of the rotor assembly consists of a plurality of ring-shaped magnets having different diameters, concentrically stacked together.
11. The flywheel system as defined in claim 1 or claim 6, in which the housing is hermetically sealed in a partial vacuum in order to reduce air resistance by rotational movement of the rotor assembly.
12. The flywheel system as defined in claim 1 or claim 6, further comprising:
o a bearing assembly securely attached to the housing and to the vertical shaft;

in order to provide additional stability.
13. The flywheel system as defined in claim 12, in which the bearing assembly is placed above the flywheel.
14. The flywheel system as defined in claim 12, in which the bearing assembly is placed below the flywheel.
15. The flywheel system as defined in claim 12, in which the bearing assembly is a magnetic bearing.
16. The flywheel system as defined in claim 12, in which the bearing assembly is a mechanical bearing.
CA2327492A 2000-11-10 2000-11-10 Magnetically suspended flywheel system Expired - Fee Related CA2327492C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA2327492A CA2327492C (en) 2000-11-10 2000-11-10 Magnetically suspended flywheel system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA2327492A CA2327492C (en) 2000-11-10 2000-11-10 Magnetically suspended flywheel system

Publications (2)

Publication Number Publication Date
CA2327492A1 CA2327492A1 (en) 2002-05-10
CA2327492C true CA2327492C (en) 2011-07-12

Family

ID=4167813

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2327492A Expired - Fee Related CA2327492C (en) 2000-11-10 2000-11-10 Magnetically suspended flywheel system

Country Status (1)

Country Link
CA (1) CA2327492C (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012155170A1 (en) * 2011-05-13 2012-11-22 Empire Technology Development Llc Energy storage system
CN110266215B (en) * 2018-03-12 2021-08-27 李国坤 Vertical permanent magnetic suspension device
WO2021005522A1 (en) * 2019-07-08 2021-01-14 Azamour Investment Corporation Incorporated Rotary vane device
CN112505597B (en) * 2020-10-16 2021-10-22 横店集团东磁股份有限公司 Magnetic flux detection tool for annular permanent magnet

Also Published As

Publication number Publication date
CA2327492A1 (en) 2002-05-10

Similar Documents

Publication Publication Date Title
US6657344B2 (en) Passive magnetic bearing for a horizontal shaft
US5831362A (en) Magnet-superconductor flywheel and levitation systems
JP3121819B2 (en) Magnetic bearing device with permanent magnet that receives radial force applied to the shaft
CN101771308B (en) A kind of magnetic suspension rotor support system and magnetic suspension bearing and magnetic bias weight reducing device
IE850634L (en) Magnetic bearing
JP2008537872A (en) Method for stabilizing a magnetically levitated object
US6213737B1 (en) Damper device and turbomolecular pump with damper device
US6175175B1 (en) Levitation pressure and friction losses in superconducting bearings
JPH06510165A (en) High thrust and high stability magnet-superconductor system
US5540116A (en) Low-loss, high-speed, high-TC superconducting bearings
US4983869A (en) Magnetic bearing
WO2002035108A1 (en) Magnetic suspension bearing
CN101737425A (en) Monostable radial magnetic bearing with low power consumption and zero gravity action
CA2327492C (en) Magnetically suspended flywheel system
Post et al. Ambient-temperature passive magnetic bearings: Theory and design equations
EP0795226A4 (en)
US6369476B1 (en) High temperature superconductor bearings
JP3554070B2 (en) Superconducting magnetic bearing device
US20130207496A1 (en) System and method for performing magnetic levitation in an energy storage flywheel
WO1997009664A1 (en) Improvements in mixed-mu superconducting bearings
Komori et al. A hybrid-type superconducting magnetic bearing system with nonlinear control
CN108547868B (en) Semi-freedom degree radial magnetizing hybrid axial magnetic bearing
CN100547900C (en) Magnetic suspending wind turbine generator
US4643034A (en) Gyroscopically stabilized magnetic suspension system
JPH08296645A (en) Magnetic bearing device

Legal Events

Date Code Title Description
EEER Examination request
MKLA Lapsed

Effective date: 20131113