IP Library › Granted Patent US 11,035,621
Granted Patent B2
US 11,035,621 · App. 16/431,870 · Granted Jun 15, 2021

Electronics cooling with multi-phase heat exchange and heat spreader

Inventors: Stefano Lassini (Lowell, MI); Brian Rush (Niskayuna, NY); Daniel Erno (Niskayuna, NY); William Dwight Gerstler (Niskayuna, NY)
Assignee: GE Aviation Systems LLC
F28D15/04F28D7/0025F28D7/0066F28D9/0093F28D15/0233F28D15/0266F28D15/0275F28D20/021F28F1/045F28F7/02H01L23/427H05K7/20309H05K7/20318H05K7/20336F28F2270/00Y02E60/14
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Quick Facts
Patent No.
US 11,035,621
App. No.
16/431,870
Granted
Jun 15, 2021
Kind
B2
Abstract

One example aspect of the present disclosure is directed to a system for cooling a surface. The system can include a housing. The housing can include an evaporator portion. The housing can include at least one trifurcated heat exchange portion. The at least one trifurcated heat exchange portion can include a condenser portion coupled to the evaporator portion. The at least one trifurcated heat exchange portion can include a coolant portion substantially surrounded by the condenser portion. The at least one trifurcated heat exchange portion can include a phase change material portion substantially surrounding the condenser portion.

Claims (43)

1. A multi-domain heat exchanger, comprising:

a coolant portion defining a coolant domain therein;

a condenser portion surrounding the coolant portion, the condenser portion and the coolant portion defining a condenser domain therebetween;

a housing surrounding the condenser portion, the housing and the condenser portion defining a phase change material domain therebetween; and

an evaporator portion defining a vapor chamber, the vapor chamber fluidly communicating with the condenser domain;

wherein the coolant portion, the condenser portion, and the housing define an array of unit cells, the array of unit cells separating the coolant domain from the condenser domain and separating the condenser domain from the phase change material domain.

2. The multi-domain heat exchanger of claim 1 , wherein the coolant portion comprises hydrodynamic furcations that divide the coolant domain.

3. The multi-domain heat exchanger of claim 1 , wherein the condenser portion comprises hydrodynamic furcations that divide the condenser domain and/or the phase change material domain.

4. The multi-domain heat exchanger of claim 1 , comprising:

a plurality of nested furcated domains, the plurality of nested furcated domains defined at least in part by the coolant portion and the condenser portion.

5. The multi-domain heat exchanger of claim 4 , wherein the plurality of nested furcated domains comprises the coolant domain, the condenser domain, and the phase change material domain.

6. The multi-domain heat exchanger of claim 1 , wherein the condenser portion comprises a wicking structure.

7. The multi-domain heat exchanger of claim 1 , comprising:

a vacuum shroud surrounding at least a portion of the housing, the vacuum shroud and the housing defining a vacuum domain therebetween.

8. A cooling system, comprising:

an evaporator section defining a vapor chamber;

a condenser section defining a condenser domain, the condenser section operably coupled to the evaporator section, the condenser section comprising a multi-domain heat exchanger, the multi-domain heat exchanger comprising:

a coolant portion defining a coolant domain therein;

a condenser portion surrounding the coolant portion, the condenser portion and the coolant portion defining a condenser domain therebetween, the condenser domain fluidly communicating with the vapor chamber; and

a housing surrounding the condenser portion, the housing and the condenser portion defining a phase change material domain therebetween;

wherein the coolant portion, the condenser portion, and the housing define an array of unit cells, the array of unit cells separating the coolant domain from the condenser domain and separating the condenser domain from the phase change material domain.

9. The cooling system of claim 8 , wherein the coolant portion comprises hydrodynamic furcations that divide the coolant domain.

10. The cooling system of claim 8 , wherein the condenser portion comprises hydrodynamic furcations that divide the condenser domain and/or the phase change material domain.

11. The cooling system of claim 8 , comprising:

a plurality of nested furcated domains, the plurality of nested furcated domains defined at least in part by the coolant portion and the condenser portion.

12. The cooling system of claim 11 , wherein the plurality of nested furcated domains comprises the coolant domain, the condenser domain, and the phase change material domain.

13. The cooling system of claim 8 , wherein the condenser portion comprises a wicking structure.

14. The cooling system of claim 8 , comprising:

a vacuum shroud surrounding at least a portion of the housing, the vacuum shroud and the housing defining a vacuum domain therebetween.

15. A method of cooling a component, the method comprising:

evaporating working fluid with an evaporator section defining a vapor chamber, transferring heat from the evaporator section to evaporating working fluid in the vapor chamber;

condensing working fluid with a condenser section defining a condenser domain, transferring heat from the condensing working fluid to the condenser section, the condenser section operably coupled to the evaporator section, the condenser section comprising a multi-domain heat exchanger, the multi-domain heat exchanger comprising:

a coolant portion defining a coolant domain therein;

a condenser portion surrounding the coolant portion, the condenser portion and the coolant portion defining a condenser domain therebetween, the condenser domain fluidly communicating with the vapor chamber; and

a housing surrounding the condenser portion, the housing and the condenser portion defining a phase change material domain therebetween;

wherein the coolant portion, the condenser portion, and the housing define an array of unit cells, the array of unit cells separating the coolant domain from the condenser domain and separating the condenser domain from the phase change material domain.

16. The method of claim 15 , comprising:

flowing evaporated working fluid from the evaporator section to the condenser section at least in part using a pressure gradient between the evaporator section and the condenser section.

17. The method of claim 15 , comprising:

flowing condensed working fluid from the condenser section to the evaporator section at least in part using capillary force provided by a wicking structure in the condenser domain.

18. The method of claim 15 , wherein the coolant portion and the condenser portion define at least a portion of a plurality of nested furcated domains.

19. The method of claim 18 , wherein the plurality of nested furcated domains comprises the coolant domain, the condenser domain, and the phase change material domain.

20. The method of claim 15 , thermally insulating at least a portion of the array of unit cells using a vacuum shroud surrounding at least a portion of the housing, the vacuum shroud and the housing defining a vacuum domain therebetween.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 5, 2019
From: LASSINI, STEFANO; RUSH, BRIAN; ERNO, DANIEL; GERSTLER, WILLIAM DWIGHT
To: GE AVIATION SYSTEMS LLC
Reel/Frame 049375/0351 →
Continuity (3)
Continuation 15497520 · Apr 26, 2017
Provisional Application 62352862 · Jun 21, 2016
Related Publication 20190285356A1 · Sep 19, 2019
Cited By (1)
US 12,352,510