Isotropic energy storage flywheel rotor

• US 6,122,993 A
• Filed: 01/26/1998
• Issued: 09/26/2000
• Est. Priority Date: 01/26/1998
• Status: Expired due to Fees

• Current Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Original Assignee: Alliedsignal Inc. (Honeywell International Inc.)
• Inventors: Moody, John, Narasimhan, Dave, Morris, Robert C., Coronato, Patrick
• Primary Examiner(s): Battista, Mary Ann
• Application Number:
  US09/013,656
• Time in Patent Office: 974 Days
• Field of Search: 74/572
• US Class Current: 74/572.11
• CPC Class Codes: F16F 15/305 made of plastics, e.g. fibre reinforced plastics [FRP] , i.e. characterised by their special construction from such materials
• CPC Class Codes: Y02E 60/16 Mechanical energy storage, e.g. flywheels or pressurised fluids
• CPC Class Codes: Y10T 74/2119 Structural detail, e.g., material, configuration, superconductor, discs, laminated, etc.

Abstract

An energy storage flywheel having a benign failure mode, the rotor of which is constructed of a brittle, high specific strength, isotropic solid.

Claims

1. An energy storage or momentum control flywheel comprising a rotor fabricated from a single body of a non-composite, non-laminated, high specific strength, brittle, isotropic solid material with strength great enough to insure complete fragmentation immediately after the onset of mechanical failure.

2. The flywheel rotor of claim 1 wherein said rotor is a disc of thickness t and radius R.

3. The flywheel rotor of claim 1 wherein the rotor is an annular ring of thickness t in the axial direction.

4. The flywheel rotor of claim 1 wherein the rotor shape is a surface of revolution having a thickness t, wherein the thickness t is greatest along the axis of rotation and decreases with increasing radius in a hyperbolic or an exponential manner so as to reduce or eliminate the spatial variation of centrifugally induced stresses.

5. The flywheel rotor of claim 1 wherein the material of construction of the rotor is a single crystal body.

6. The flywheel rotor of claim 5 wherein the single crystal body is a single crystal of silicon.

7. The flywheel rotor of claim 5 in wherein the single crystal body is a metal oxide single crystal.

8. The flywheel rotor of claim 7 wherein the metal oxide is selected from the group consisting of sapphire and oxide garnets.

9. The flywheel rotor of claim 1 wherein the material of construction of the rotor is a silicate glass.

10. The flywheel rotor of claim 1 wherein the material of construction of the rotor is a glass-ceramic.

11. The flywheel rotor of claim 10 wherein the glass-ceramic is microcrystalline material.

12. An energy storage flywheel rotor fabricated from a single body of a non-composite, non-laminated, high specific strength, brittle, isotropic solid material wherein the entire surface of said rotor comprises a layer in surface compression with maximum surface or near-surface compressive elastic strains, in directions parallel to said surface, in the range of 0.02 to 0.4%, so as to impart surface damage tolerance to the brittle body.

13. The flywheel rotor of claim 12 wherein the material of construction of the rotor is silicate glass.

14. The flywheel rotor of claim 13 wherein the compression layer is produced by rapidly cooling the surface of a silicate glass body brought to a semi-viscous state by heating.

15. The flywheel rotor of claim 13 wherein the silicate glass is s-glass.

16. The flywheel rotor of claim 13 wherein the silicate glass is e-glass.

17. The flywheel rotor of claim 13 wherein the silicate glass is flint glass or soda lime glass.

18. The flywheel rotor of claim 12 wherein said single body of the rotor is an alkali containing aluminosilicate glass.

19. The flywheel rotor of claim 12 comprising a core region and a laminated surface layer resulting in a state of surface compression.

20. The flywheel of claim 12 wherein the rotor is yttrium aluminum garnet and the surface compression layer is yttrium aluminum garnet with a rare earth element selected from the group consisting of holmium, dysprosium, terbium, gadolinium, europium, samarium, neodymium, praseodymium, and lanthanum and mixtures thereof.

21. The flywheel rotor of claim 12 wherein the rotor is monocrystalline silicon and the surface compression layer is a silicon germanium alloy.

22. The flywheel rotor of claim 12 wherein the surface of the rotor is chemically polished and coated with a polymeric layer to provide mechanical protection to the surface.