Systems and methods for leadless power coupling for cryogenic environments

Patent metadata

Field	Value
Publication number	US-12334253-B2
Application number	US-202117548589-A
Country	US
Kind code	B2
Filing date	Dec 12, 2021
Priority date	Jun 4, 2021
Publication date	Jun 17, 2025
Grant date	Jun 17, 2025

Abstract

In examples, provided are leadless power couplers that include (1) a thermal insulating system having an outer wall and an inner wall, (2) a first electrically conductive winding located outside the thermal insulating system, where the first electrically conductive winding is configured to create a varying magnetic field, (3) a plurality of second electrically conductive windings located inside the thermal insulating system and configured to couple to the varying magnetic field, the plurality of second electrically conductive windings being superconductors, (4) a plurality of cryogenic rectifiers, each cryogenic rectifier being coupled to a respective second electrically conductive winding in the plurality of second electrically conductive windings, and (5) a plurality of cryogenic cables coupled between respective outputs of the plurality of cryogenic rectifiers and respective loads.

First claim

What is claimed is:

1. A leadless power coupler for a cryogenic environment, comprising:
a first thermal insulating system having a wall defining a cavity therein;
a first electrically conductive winding located outside of the first thermal insulating system, wherein the first electrically conductive winding is configured to create a varying magnetic field;
a plurality of second electrically conductive windings located inside the first thermal insulating system and configured to couple to the varying magnetic field, wherein the plurality of second electrically conductive windings are superconductors;
a plurality of cryogenic rectifiers, wherein each cryogenic rectifier is coupled to a respective second electrically conductive winding in the plurality of second electrically conductive windings; and
a plurality of cryogenic cables coupled between respective outputs of the plurality of cryogenic rectifiers and respective loads,
wherein:
the first thermal insulating system is configured thermally in a bus topology; and
the first electrically conductive winding, the plurality of second electrically conductive windings, the plurality of cryogenic rectifiers, and the plurality of cryogenic cables are configured electrically in a star topology with the first electrically conductive winding at a center of the star topology.

2. The leadless power coupler for a cryogenic environment of claim 1 , wherein the wall is comprised of at least one of fiberglass, epoxy, porcelain, carbon fiber, or a composite thereof.

3. The leadless power coupler for a cryogenic environment of claim 1 , wherein the first electrically conductive winding is at ambient temperature.

4. The leadless power coupler for a cryogenic environment of claim 1 , wherein a first number of windings in the first electrically conductive winding and a second number of windings in the plurality of second electrically conductive windings has a ratio of 5:1 or greater.

5. The leadless power coupler for a cryogenic environment of claim 1 , wherein the first electrically conductive winding and the plurality of second electrically conductive windings are at least one of cylindrical windings, flat windings, or pancake coil windings.

6. The leadless power coupler for a cryogenic environment of claim 1 , wherein no electrical conductors couple, through the wall, the first electrically conductive winding to the plurality of second electrically conductive windings.

7. The leadless power coupler for a cryogenic environment of claim 1 , wherein the respective loads are located outside of the first thermal insulating system.

8. The leadless power coupler for a cryogenic environment of claim 1 , wherein the respective loads comprise a rack-mounted power distribution unit.

9. The leadless power coupler for a cryogenic environment of claim 1 , wherein the respective loads comprise a computer.

10. The leadless power coupler for a cryogenic environment of claim 1 , wherein the respective loads comprise a superconducting magnet comprising coils of superconducting wire.

11. The leadless power coupler for a cryogenic environment of claim 1 , wherein the respective loads comprise a motor.

12. The leadless power coupler for a cryogenic environment of claim 1 , wherein the respective loads are configured to normally operate at ambient temperature.

13. The leadless power coupler for a cryogenic environment of claim 1 , further comprising a circuit breaker coupled between a second electrically conductive winding in the plurality of second electrically conductive windings and a respective cryogenic rectifier in the plurality of cryogenic rectifiers.

14. The leadless power coupler for a cryogenic environment of claim 1 , further comprising a second thermal insulating system, wherein the first electrically conductive winding is located inside of the second thermal insulating system.

15. The leadless power coupler for a cryogenic environment of claim 1 , further comprising a frequency upconverter coupled to the first electrically conductive winding and configured to increase a frequency of an alternating current input to the first electrically conductive winding.

16. The leadless power coupler for a cryogenic environment of claim 1 , further comprising:
an aircraft wing, wherein at least a portion of the first thermal insulating system is located inside the aircraft wing; and
an aircraft electric propulsion motor, wherein the electric propulsion motor is a respective load in the respective loads.

17. A method for supplying electrical power via a leadless power coupler for a cryogenic environment, comprising:
applying an input alternating current through a first electrically conductive winding to create a varying magnetic field, wherein the first electrically conductive winding is located outside of a thermal insulating system and the thermal insulating system comprises a wall defining a cavity therein;
inducing, using the varying magnetic field, a plurality of output alternating currents in a plurality of respective second electrically conductive windings, wherein the plurality of second electrically conductive windings are located inside the thermal insulating system and the plurality of second electrically conductive windings are in a superconducting state;
rectifying, using a plurality of cryogenic rectifiers, the plurality of output alternating currents into a plurality of respective direct currents, wherein each cryogenic rectifier is coupled to a respective second electrically conductive winding in the plurality of second electrically conductive windings; and
conducting the plurality of respective direct currents to respective loads via a plurality of respective cryogenic cables coupled between respective outputs of the plurality of cryogenic rectifiers and the respective loads,
wherein:
the thermal insulating system is configured thermally in a bus topology; and
the first electrically conductive winding, the plurality of second electrically conductive windings, the plurality of cryogenic rectifiers, and the plurality of cryogenic cables are configured electrically in a star topology with the first electrically conductive winding at a center of the star topology.

18. The method of claim 17 , further comprising increasing a frequency of the input alternating current prior to applying the input alternating current through the first electrically conductive winding.

19. The method of claim 17 , wherein in a respective load in the respective loads is at least one of a superconducting motor or a superconducting generator, and further comprising conducting a respective direct current in the respective direct currents to a brushless exciter of at least one of the superconducting motor or the superconducting generator.

Assignees

• Univ Florida State Res Found Inc
• Univ Florida State

Inventors

• Steurer Michael
• Graber Lukas
• Pamidi Sastry
• Shi Yanjun
• Cheatham Peter
• Kim Chul Han

Classifications

• B64D27/24

  using steam or spring force (jet aircraft B64D27/16) · CPC title

• B64D35/02

  specially adapted for specific power plants · CPC title

• H05K7/1492

  having electrical distribution arrangements, e.g. power supply or data communications · CPC title

• H01F6/065

  Feed-through bushings, terminals and joints (leading of conductors or axles through casings of transformers H01F27/04) · CPC title

• H01F6/04

  Cooling · CPC title