Liquid nitrogen-based cooling system
11306957 · 2022-04-19
Assignee
Inventors
Cpc classification
F25B19/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F17C2223/0161
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J2270/904
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25D3/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J2210/42
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J3/04412
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F25B9/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25J3/04
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25B9/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25B9/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F25D3/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A liquid nitrogen-based cooling system features a cooling circuit and a liquid nitrogen-based heat sink. Heat absorbed by fluid flowing in the cooling circuit is subsequently absorbed by liquid nitrogen within the heat sink, which causes the liquid nitrogen to vaporize. The vaporized nitrogen is condensed back to liquid form, e.g., by means of a helium-based cryo-refrigeration system. The heat-sink includes at least a first vessel that contains the liquid nitrogen, with the cooling circuit including a series of coils passing around the first vessel in heat-exchanging contact with an exterior surface thereof so that heat can be transferred into the liquid nitrogen. The first vessel and coils may be contained within a second, outer vessel that minimizes heat transfer from the ambient environment to the fluid flowing in the cooling circuit and the liquid nitrogen within the first vessel.
Claims
1. A liquid nitrogen-based cooling system, comprising: a heat sink containing a first heat-absorbing medium comprising a supply of liquid nitrogen; a closed-loop cooling circuit through which circulates a non-cryogenic second heat-absorbing medium, the closed-loop cooling circuit being configured and arranged such that the second heat-absorbing medium flows toward and absorbs heat from a device or region to be cooled and then back toward the heat sink, the closed-loop cooling circuit further being arranged in heat-exchanging relationship with the heat sink such that the heat absorbed by the second heat-absorbing medium is transferred to the liquid nitrogen, thereby causing a portion of the liquid nitrogen to vaporize within the heat sink; and a refrigeration subsystem arranged relative to the heat sink to condense nitrogen that has vaporized within the heat sink back into liquid nitrogen and return the condensed nitrogen to the supply of liquid nitrogen; wherein the heat sink comprises at least a first vessel in which the liquid and vaporized nitrogen are confined, such that the nitrogen cycles between its liquid and vapor phases within the confines of the first vessel, and a plurality of coils arranged in heat-transferring relationship with the liquid nitrogen, the plurality of coils forming a portion of the closed-loop cooling circuit through which the second heat-absorbing medium circulates; wherein the first vessel is a double-wall vessel and the plurality of coils are arranged on the exterior of the double-wall vessel, thereby transferring heat with the liquid nitrogen.
2. The cooling system of claim 1, wherein the plurality of coils pass around an exterior surface of the first vessel.
3. The cooling system of claim 1, wherein the first vessel and the plurality of coils are disposed within a second, outer vessel, with at least a partial vacuum between the first and second vessels and at least a portion of the coils being disposed within the at least partial vacuum.
4. The cooling system of claim 1, wherein the refrigeration subsystem comprises a helium-based cryo-refrigeration system having a cold head that extends into an interior region within the first vessel, the cold head providing a surface on which the vaporized nitrogen condenses back into liquid nitrogen.
5. The cooling system of claim 1, wherein the second heat-absorbing medium comprises propylene glycol.
6. The cooling system of claim 5, wherein the second heat-absorbing medium comprises a mixture of propylene glycol and one or more anticorrosive agents.
7. A method for cooling a device or region of space requiring cooling, comprising: circulating a heat-absorbing medium within a closed-loop cooling circuit, the heat-absorbing medium flowing in a direction from a heat sink toward the device or region of space requiring cooling and back toward the heat sink, the heat sink comprising a double-wall vessel containing therein a supply of liquid nitrogen; causing or allowing heat to be transferred from the device or region of space requiring cooling to the heat-absorbing medium that is circulating within the closed-loop cooling circuit; transporting the heat, via the heat-absorbing medium, to the heat sink; causing or allowing the heat being transported by the heat-absorbing medium to be transferred from the heat-absorbing medium to the liquid nitrogen contained within the double-wall vessel by coils that pass around an exterior of the double-wall vessel to thereby transfer heat to the liquid nitrogen and cause at least a portion of the liquid nitrogen to vaporize within the double-wall vessel; removing heat from the vaporized nitrogen to thereby cause the vaporized nitrogen to condense back to liquid form; and returning the nitrogen that has been condensed back to liquid form to the supply of liquid nitrogen contained within the double-wall vessel, wherein the nitrogen cycles between its liquid and vapor phases within and limited to the confines of the double-wall vessel.
8. The cooling system of claim 1, wherein the second heat-absorbing medium circulates in liquid form.
9. The cooling system of claim 1, wherein the first vessel comprises an insulating material between the two walls of the double-wall.
10. The cooling system of claim 9, wherein the insulating material comprises an aerogel.
11. The cooling system of claim 1, wherein the double-wall regulates heat transfer into and out of the first vessel.
12. A liquid nitrogen-based cooling system, comprising: a heat sink containing a first heat-absorbing medium comprising a supply of liquid nitrogen; a closed-loop cooling circuit through which circulates a second heat-absorbing medium, the closed-loop cooling circuit being configured and arranged such that the second heat-absorbing medium flows toward and absorbs heat from a device or region to be cooled and then back toward the heat sink, the closed-loop cooling circuit further being arranged in heat-exchanging relationship with the heat sink such that the heat absorbed by the second heat-absorbing medium is transferred to the liquid nitrogen, thereby causing a portion of the liquid nitrogen to vaporize within the heat sink; and a refrigeration subsystem arranged relative to the heat sink to condense nitrogen that has vaporized within the heat sink back into liquid nitrogen and return the condensed nitrogen to the supply of liquid nitrogen; wherein the heat sink comprises at least a first vessel in which the liquid and vaporized nitrogen are confined, such that the nitrogen cycles between its liquid and vapor phases within the confines of the first vessel, the first vessel being a double-wall vessel, and a plurality of coils arranged in heat-transferring relationship around the exterior of the first vessel to transfer heat with the liquid nitrogen, the plurality of coils forming a portion of the closed-loop cooling circuit through which the second heat-absorbing medium circulates.
13. The cooling system of claim 12, wherein the second heat-absorbing medium comprises a non-cryogen.
14. The cooling system of claim 13, wherein the second heat-absorbing medium comprises propylene glycol.
15. The cooling system of claim 12, wherein the first vessel further comprises an insulator between the double walls of the double-wall.
16. The cooling system of claim 15, wherein the insulator comprises an aerogel.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) These and other features of the invention will become clearer in view of the description below and the accompanying figures, in which:
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DETAILED DESCRIPTION OF EMBODIMENTS
(10) An embodiment of a cooling system 10 in accordance with the invention is illustrated in the figures. As illustrated in
(11) Further details of the liquid nitrogen-based heat sink 14 are illustrated in
(12) As further illustrated in
(13) As the liquid nitrogen absorbs heat, it vaporizes into the headspace within the vessel 26. As noted above, the nitrogen vapor is cooled by the cold head 18 of helium-based cryo-refrigeration system 20—the cold head 18 extends into the interior of the first vessel 26—and condenses back into liquid form, which drips back into the supply of liquid nitrogen.
(14) Furthermore, the first vessel 26 and surrounding coils 28 are suitably contained within a second, outer vessel 30. Like the first vessel 26, the second vessel 30 also suitably has a double-wall construction, with the space between the inner and outer walls of the second vessel 30 being filled with an insulating material such as an aerogel. Additionally, at least a partial vacuum is suitably drawn in the space 32 between the first and second vessels 26, 30, i.e., the space in which the coils 28 are located. The combination of (partial) vacuum between the walls of the first and second vessels 26, 30 and insulating material such as aerogel between the inner and outer walls of the second, outer vessel 30 significantly limits—perhaps even eliminating—heat transfer into the propylene glycol in the coils 26 from the ambient atmosphere.
(15) Based on models we have conducted, it costs significantly less to cool a large-scale system using a cooling system as described above than it costs to cool the same system using a conventional cooling system. For example, according to our calculations, a large-scale server system with 350,000 watts of computing power requires 1.2 million BTU of cooling capability. Current technology like that described in the background section above requires 352,000 watts to run a suitably sized cooling system at a cost (based on local energy rates) of almost $22,000 per month, whereas a system as per the invention only requires 2,500 watts (to drive the circulation pump 18 and the cryo-refrigeration unit 20) to run a suitably sized system at a cost on the order of $155 per month. Such savings are deemed to be highly significant.