Cooling system for superconducting wind power generator

Patent metadata

Field	Value
Publication number	US-12580449-B2
Application number	US-202218685410-A
Country	US
Kind code	B2
Filing date	Aug 30, 2022
Priority date	Aug 31, 2021
Publication date	Mar 17, 2026
Grant date	Mar 17, 2026

Abstract

Techniques are described for a wind power generator in which a refrigerant such as liquid helium and/or helium gas is applied to superconducting magnets via thermally conductive flexible structures. These structures thermally couple the refrigerant channels to the magnets, and/or to a thermally conductive structure (e.g., metal plate) to which the magnets are thermally coupled. The thermally conductive flexible structures may be arranged so that motion of the magnets relative to the cryogenic channels that cool the structures during heating and/or cooling of the magnets does not result in damage to the thermal connection between the channels and the magnets. The stationary stage of the generator may house a cooling station, and transfer the refrigerant to the rotary stage via a suitable rotary union.

First claim

What is claimed is:

1 . A cooling system for a wind power generator, the cooling system comprising:
a stationary portion having a first inlet configured to receive a coolant gas from a coolant source, a first outlet configured to provide a gas to a rotary union inlet of a rotary union and a second inlet configured to receive a gas from a rotary union outlet of the rotary union with a temperature of the gas at the first outlet being less than a temperature of the gas at the second inlet, the stationary portion comprising:
a cryostat;
a thermal radiation shield disposed within in the cryostat;
a gas channel provided within the thermal radiation shield and having a first inlet corresponding to the first inlet of the stationary portion, a first outlet corresponding to the first outlet of the stationary portion and a second inlet corresponding to the second inlet of the stationary portion;
a first plurality of colds heads thermally coupled to the gas channel;
a compressor coupled to the first plurality of cold heads thermally coupled to the gas channel;
a first cold head of the first plurality of cold beads coupled to the thermal radiation shield;
a compressor coupled to the first cold head for the thermal radiation shield; and
a valve system coupled to the gas channel and configured to direct a flow of gas through the gas channel; and
a rotary portion comprising:
a gas inlet and a gas outlet with a cooling channel coupled between the gas inlet and the gas outlet, the cooling channel being configured to allow the gas to flow from the gas inlet of the rotary portion to the gas outlet of the rotary portion, and
a plurality of thermally conductive, flexible structures, each thermally conductive, flexible structure being thermally coupled to at least a portion of the rotary portion,
wherein the rotary union is coupled between the rotary portion and the stationary portion,
wherein the cooling channel of the rotary union is in fluid communication with the first outlet of the stationary portion and with the gas inlet of the rotary portion and in fluid communication with the gas outlet of the rotary portion and the second inlet of the stationary portion, and
wherein the plurality of thermally conductive, flexible structures is configured to allow for movement of the rotary portion.

2 . The cooling system of claim 1 , wherein the gas channel forms a loop such that gas entering the gas channel through the second inlet is provided to one or more of the first plurality of cold heads and cooled prior to being provided to the first outlet of the stationary portion.

3 . The cooling system of claim 1 , wherein the compressor is provided as a plurality of compressors with ones of the plurality of compressors coupled to ones of the first plurality of colds heads coupled to the gas channel such that each of the first plurality of colds heads has at least one compressor coupled thereto.

4 . The cooling system of claim 1 , wherein the compressor is provided as a first plurality of compressors such that each of the first plurality of compressors is coupled to a respective one of the first plurality of colds heads.

5 . The cooling system of claim 1 , further comprising a rotary union having the rotary union inlet in fluid communication with the first outlet of the stationary portion and having the rotary union outlet in fluid communication with the first inlet of the stationary portion.

6 . The cooling system of claim 1 , further comprising a helium cylinder coupled to the first inlet of the stationary portion.

7 . The cooling system of claim 2 , further comprising a rotary union having a first channel in fluid communication with the first outlet of the stationary portion and having a second channel.

8 . A generator comprising:
a plurality of high temperature superconducting (HTS) magnets arranged in a loop; a plurality of thermally conductive, flexible structures, each thermally conductive, flexible structure being thermally coupled to one or more of the plurality of HTS magnets in the loop, wherein the plurality of thermally conductive flexible structures is configured to allow for movement of the plurality of HTS magnets in the loop; and a cooling channel comprising:
an inlet portion;
a circumferential portion coupled to the inlet portion and thermally coupled to at least some of the plurality of thermally conductive, flexible structures; and
an outlet portion, wherein the cooling channel is configured to allow a gas to flow from the inlet portion to the outlet portion.

9 . The generator of claim 8 , wherein:
the inlet portion extends radially outward from a center region of the loop; and the outlet portion extends radially inward to the center region of the loop.

10 . The generator of claim 8 , further comprising one or more thermally conductive plates, and wherein each of the plurality of thermally conductive, flexible structure is thermally coupled to one or more of the plurality of HTS magnets in the loop via one or more of the one or more thermally conductive plates.

11 . The generator of claim 8 , further comprising an inlet manifold coupled to the inlet portion of the cooling channel and an outlet manifold coupled to the outlet portion of the cooling channel.

12 . The generator of claim 11 , further comprising a rotary union coupled to the inlet manifold and coupled to the outlet manifold.

13 . The generator of claim 12 , wherein:
the cooling channel is a first cooling channel, the circumferential portion of the first cooling channel is thermally coupled to first ones of the plurality of thermally conductive, flexible structures, and the generator further comprises a second cooling channel, the second cooling channel comprising:
an inlet portion extending radially outward from a center region of the loop;
a circumferential portion coupled to the inlet portion of the second cooling channel and thermally coupled to a second subset of the plurality of thermally conductive, flexible structures; and
an outlet portion coupled to the circumferential portion of the second cooling channel and extending radially inward to the center region of the loop.

14 . The generator of claim 8 , wherein each HTS magnet in the loop comprises a stack of HTS tapes.

15 . The generator of claim 8 , wherein each HTS magnet in the loop comprises a double pancake coil.

16 . The generator of claim 8 , wherein the plurality of thermally conductive, flexible structures each comprise a flexible radial tube.

17 . A wind power generator comprising:
a cooling system comprising:
a rotary portion having a rotary portion inlet and a rotary portion outlet with a cooling channel coupled between the rotary portion inlet and the rotary portion outlet;
a stationary portion having a stationary portion outlet and a stationary portion inlet, the stationary portion configured to provide cooled gas at the stationary portion outlet thereof;
a rotary union coupled between the rotary portion and stationary portion, the rotary union having a first channel in fluid communication with the stationary portion outlet of the stationary portion and with the rotary portion inlet of the rotary portion and having a second channel in fluid communication with the rotary portion outlet of the rotary portion and the stationary portion inlet of the stationary portion, wherein the cooling channel of the rotary portion is configured to allow the cooled gas to flow from the rotary portion inlet of the rotary portion to the rotary portion outlet of the rotary portion; and
a plurality of the

Assignees

• Massachusetts Inst Technology
• Commonwealth Fusion Systems Llc

Inventors

• Radovinsky Alexey
• Zhukovsky Alexander

Classifications

• H02K55/00

  Dynamo-electric machines having windings operating at cryogenic temperatures · CPC title

• H02K9/14

  wherein gaseous cooling medium circulates between the machine casing and a surrounding mantle · CPC title

• Y02E40/60

  Superconducting electric elements or equipment; Power systems integrating superconducting elements or equipment · CPC title

• Y02E10/72

  Wind turbines with rotation axis in wind direction · CPC title

• F05B2260/232

  characterised by the cooling medium · CPC title