Energy storage apparatus

• US 4,077,678 A
• Filed: 07/30/1976
• Issued: 03/07/1978
• Est. Priority Date: 07/30/1976
• Status: Expired due to Term

• Current Assignee: United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration
• Original Assignee: United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration
• Inventors: Studer, Philip A., Evans, Harold E.
• Primary Examiner(s): Skudy, R.
• Application Number:
  US05/710,035
• Time in Patent Office: 585 Days
• Field of Search: 310/178, 310/153, 310/74, 310/154, 310/67, 310/269, 308/10, 322/4, 322/48, 322/49
• US Class Current: 310/90.5
• CPC Class Codes: F16C 2361/55 Flywheel systems
• CPC Class Codes: F16C 2380/28 Motor, generator coupled with a flywheel
• CPC Class Codes: F16C 32/0465 with permanent magnets provided in the magnetic circuit of the electromagnets
• CPC Class Codes: F16C 32/048 with active support of two degrees of freedom, e.g. radial magnetic bearings
• CPC Class Codes: F16F 15/3156 Arrangement of the bearings
• CPC Class Codes: H02K 7/025 for power storage
• CPC Class Codes: H02K 7/09 with magnetic bearings
• CPC Class Codes: Y02E 60/16 Mechanical energy storage, e.g. flywheels or pressurised fluids

Abstract

An energy storage device comprises a flywheel rotor in the form of a spokeless ring of filamentary, composite material rotating around a ring-shaped stator. Along the inner rim of the rotor, there is a layer of magnetically soft iron that forms homopolar, salient pole pairs. An ironless armature winding mounted on the stator extends into an air gap formed between the pole pairs. To bring the rotor up to speed, alternating current is supplied to the armature winding using electronic commutation. The armature current interacts with flux in the air gap to create a force acting to rotate the rotor. During coast down, current may be tapped from the rotor using commutation diodes. The rotor and stator are maintained in axial alignment to each other by magnetic flux produced by a permanent magnet in the stator. An electromagnet incorporated in the stator modulates permanent magnet flux to compensate for any eccentricity between the stator and the rotor that may develop during rotation.

Claims

1. An energy storage apparatus comprising:

a stator;

a flywheel rotor including a spokeless, continuous ring portion, and a plurality of salient pole members distributed along an inner rim of said ring portion, a first air gap being formed between opposed pairs of said pole members;

said flywheel rotor being rotatable around an outer rim of said stator, a second air gap being formed between said stator and said rotor;

stationary armature means extending into said first air gap;

means for supplying alternating current to said armature means in a motor mode of operation, said alternating current interacting with magnetic flux in said first air gap to cause rotation of said rotor;

means for withdrawing alternating current from said armature means in a generator mode of operation; and

magnetic bearing means for magnetically supporting said rotor in axial and radial alignment to said stator, including;

first permanent magnet means incorporated in said stator for establishing a steady state flux in said second air gap, and

sets of opposed salient teeth within said rotor and said stator, respectively, said steady state flux passing through said second air gap between said opposed salient teeth for maintaining said rotor and said stator in axial alignment to one another.

2. The apparatus of claim 1, wherein said armature means is mounted to said stator.

3. The apparatus of claim 1, wherein said stator comprises a continuous ring member.

4. The apparatus of claim 1, wherein said rotor ring portion is formed of a filamentary wound, composite material, and said poles are formed of iron.

5. The apparatus of claim 1, wherein said bearing means further includes first electromagnet means incorporated in said stator for establishing a dynamic flux in said second air gap, said dynamic flux tending to maintain said rotor and stator in radial alignment to each other by reducing any eccentricity of said rotor with respect to said stator.

6. The apparatus of claim 5, including means for monitoring a size of said second air gap and means responsive to said monitoring means for energizing said first electromagnet means to compensate for any eccentricity of said second air gap.

7. The apparatus of claim 5, wherein said first electromagnet means is continuously controlled.

8. The apparatus of claim 1, wherein an inner rim of said rotor contains a circumferential slot defining said first air gap, pairs of said pole members being radially aligned in facing relationship to each other within said slot.

9. The apparatus of claim 8, wherein said pole members are formed of magnetically soft iron, thereby providing unidirectional flux between said opposed ones of said pole members.

10. The apparatus of claim 8, wherein said stator includes second permanent magnet means for establishing a steady state flux through said first air gap and said armature, and further includes second electromagnet means in shunt with said second permanent magnet means for establishing a control flux through said armature.

11. The apparatus of claim 1, wherein said first permanent magnet means includes a plurality of permanent magnets equispaced from each other along said stator.

12. The apparatus of claim 10, wherein said second permanent magnet means includes a single ring-shaped permanent magnet disposed along and concentric to said ring-shaped stator.

13. The apparatus of claim 5, wherein said first electromagnet means is wound around said first permanent magnet means.

14. The apparatus of claim 1, wherein said rotor and said stator are located within an air evacuated, enclosed module.