Open-core flywheel architecture

Patent metadata

Field	Value
Publication number	US-11070107-B2
Application number	US-201715616395-A
Country	US
Kind code	B2
Filing date	Jun 7, 2017
Priority date	Apr 3, 2012
Publication date	Jul 20, 2021
Grant date	Jul 20, 2021

Abstract

Apparatuses, systems and methods are described for a flywheel system incorporating a rotor made from a high-strength material in an open-core flywheel architecture with a high-temperature superconductive (HTS) bearing technology to achieve the desired high energy density in the flywheel energy storage devices, to obtain superior results and performance, and that eliminates the material growth-matching problem and obviates radial growth and bending mode issues that otherwise occur at various high frequencies and speeds.

First claim

What is claimed is:

1. A flywheel rotor for use in a hollow open-core flywheel assembly for storing and releasing energy, said flywheel rotor comprising:
a rotor, the rotor having an inner surface and an outer surface;
at least one flexible upper stability permanent magnet affixed on the inner surface of the rotor;
at least one flexible lower stability permanent magnet affixed on the inner surface of the rotor;
wherein the rotor in use establishes an attractive force value in a position at rest between the flywheel rotor and a stator, said stator positioned in close proximity with the rotor, said stator comprising at least one stator magnet dimensioned wider than at least one of the at least one flexible upper stability permanent magnet;
wherein the at least one flexible upper stability permanent magnet and the at least one flexible lower stability permanent magnet are dimensioned to substantially maintain the attractive force value with the stator nearly uniformly as the rotor grows outward radially when the rotor is operating at circumferential velocities of from about 300 m/s to about 3000 m/s;
wherein the at least one flexible upper stability permanent magnet and the at least one flexible lower stability permanent magnet comprise FeBNd powder; and
wherein the at least one flexible upper stability permanent magnet and the at least one flexible lower stability permanent magnet comprise a material having a Young's modulus of from about 0.01 MPa to about 2 MPa.

2. The flywheel rotor of claim 1 , wherein the rotor rim comprises a material having a tensile strength of from about 2 GPa to about 20 GPa.

3. The flywheel rotor of claim 1 , wherein the rotor comprises a material selected from the group consisting of: carbon-fiber-containing material, glass-fiber containing material, metal-containing-material, and combinations thereof.

4. The flywheel rotor of claim 3 , wherein the material comprises a matrix of materials selected from the group consisting of: graphite, e-glass, S-glass, silica, aluminum, titanium, steel, and combinations thereof.

5. The flywheel rotor of claim 3 , wherein the carbon-fiber-containing material comprises a carbon nanotube-containing material.

6. The flywheel rotor of claim 5 , wherein the carbon nanotube-containing material comprises a single-walled carbon nanotube-containing material.

7. The flywheel rotor of claim 5 , wherein the carbon nanotube-containing material comprises a multi-walled carbon nanotube-containing material.

8. The flywheel rotor of claim 7 , wherein the multi-walled carbon nanotube-containing material has a density of about 0.2 gm/cm 3 and a minimal material strength of at least about 45 GPa.

9. The flywheel rotor of claim 7 , wherein the flywheel rotor comprises an energy density of at least about 473 Wh/kg.

10. The flywheel rotor of claim 7 , wherein the flywheel rotor comprises a wall strength of at least about 300 GPa.

11. The flywheel rotor of claim 7 , wherein the multi-walled carbon nanotube-containing material comprises a density ranging from about 0.2 g/cm 3 .

12. The flywheel rotor of claim 7 , wherein the multi-walled carbon nanotube-containing material comprises a material strength of about 45 GPa.

13. The flywheel rotor of claim 5 , wherein the carbon nanotubes comprise a physical wall strength ranging from about 150 to about 260 GPa.

14. The flywheel rotor of claim 5 , wherein the carbon nanotube-containing material comprises an effective wall thickness of about 0.34 nm.

15. The flywheel rotor of claim 1 , wherein the flexible upper stability bearing permanent magnet, and the flexible lower stability permanent magnet extend about the entire circumference of the inner surface of the rotor.

16. A vehicle comprising the flywheel rotor of claim 1 .

17. The vehicle of claim 16 , wherein the vehicle is an aircraft; a spacecraft; a terrestrial vehicle; a surface waterborne vehicle, or a sub-surface water-borne vehicle.

18. The flywheel rotor of claim 1 , wherein the rotor comprises a fiber composite rotor rim.

19. The flywheel rotor of claim 1 , wherein the at least one flexible upper stability permanent magnet a material having a Young's modulus of from about 0.01 MPa to about 2 MPa.

Assignees

• Boeing Co

Inventors

• Hull John R
• Strasik Michael
• Mittleider John A

Classifications

• Y02E60/16

  Mechanical energy storage, e.g. flywheels or pressurised fluids · CPC title

• H02K7/02

  Additional mass for increasing inertia, e.g. flywheels · CPC title

• F16C32/0438

  with a superconducting body, e.g. a body made of high temperature superconducting material such as YBaCuO · CPC title

• F16C32/0417

  for axial load mainly · CPC title

• F16C2360/45

  Turbo-molecular pumps · CPC title