IP Library Granted Patent US 11,570,933
Granted Patent B2
US 11,570,933 · App. 16/223,438 · Granted Jan 31, 2023

Exfoliated graphite materials and composite materials and devices for thermal management

Inventor: John Kenna (Surrey, CA)
Assignee: 0908905 B.C. Ltd.
H05K7/20509B23P15/26B32B3/266B32B9/007F28F1/14F28F3/02F28F21/02H01L21/4871H01L23/3672H01L23/373H01L23/433H05K7/2039H05K7/20472B23P2700/10B32B2264/108H01L23/3677H01L24/13H01L24/16H01L24/73H01L2224/13101H01L2224/16225H01L2224/73253H01L2924/0002H01L2924/16152H01L2924/16251Y10T29/4935
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Quick Facts
Patent No.
US 11,570,933
App. No.
16/223,438
Granted
Jan 31, 2023
Kind
B2
Abstract

Exfoliated graphite materials, and composite materials including exfoliated graphite, having enhanced through-plane thermal conductivity can be used in thermal management applications and devices. Methods for making such materials and devices involve processing exfoliated graphite materials such as flexible graphite to orient or re-orient the graphite flakes in one or more regions of the material.

Claims (26)

1. A method for making a composite material, said composite material comprising:

(i) a graphite material comprising a plurality of graphite flakes, and

(ii) a first sheet of perforated material comprising a plurality of apertures,

said method comprising:

embedding said first sheet of perforated material in said graphite material by pressing together said first sheet of perforated material and said graphite material, whereby said plurality of apertures in said first sheet of perforated material are substantially filled with said graphite material to produce a compressed layer of said graphite material on a first major surface of said first sheet of perforated material.

2. The method of claim 1 , wherein said graphite material is a flexible graphite sheet material, and said embedding said first sheet of perforated material in said graphite material comprises embedding said first sheet of perforated material in a first major surface of said flexible graphite sheet material by pressing together said first sheet of perforated material and said flexible graphite sheet material.

3. The method of claim 2 , wherein said first sheet of perforated material and said flexible graphite sheet material are pressed together in a calendering process.

4. The method of claim 3 , wherein said first sheet of perforated material is drawn from a roll of perforated sheet material, and said flexible graphite sheet material is drawn from a roll of flexible graphite sheet material.

5. The method of claim 2 , wherein said first sheet of perforated material and said flexible graphite sheet material are pressed together in a die press.

6. The method of claim 2 , wherein said composite material further comprises a second sheet of perforated material comprising a plurality of apertures, and said method further comprises:

embedding said second sheet of perforated material in a second major surface of said flexible graphite sheet material by pressing together said second sheet of perforated material and said flexible graphite sheet material, whereby said plurality of apertures in said second sheet of perforated material are substantially filled with said flexible graphite sheet material.

7. The method of claim 1 , wherein said composite material further comprises a second sheet of perforated material comprising a plurality of apertures, and said method further comprises:

embedding said second sheet of perforated material in said graphite material by pressing together said second sheet of perforated material and said graphite material, whereby said plurality of apertures in said second sheet of perforated material are substantially filled with said graphite material to produce a compressed layer of said graphite material between said first sheet of perforated material and said second sheet of perforated material.

8. The method of claim 1 , wherein said first sheet of perforated material and said graphite material are pressed together in a die press.

9. The method of claim 1 , further comprising forming said composite material into a non-planar shape.

10. The method of claim 1 , wherein said perforated material is a metal.

11. The method of claim 1 , wherein said perforated material is an adhesive film.

12. The method of claim 1 , wherein said perforated material is plastic.

13. The method of claim 1 , wherein said method comprises embedding said first sheet of perforated material in said graphite material by pressing together said first sheet of perforated material and said graphite material, whereby said plurality of apertures in said first sheet of perforated material are substantially filled with said graphite material so that said graphite material in said plurality of apertures is flush with a second major surface of said first sheet of perforated material.

14. The method of claim 1 , wherein said method comprises embedding said first sheet of perforated material in said graphite material by pressing together said first sheet of perforated material and said graphite material, whereby said plurality of apertures in said first sheet of perforated material are substantially filled with said graphite material and said graphite material protrudes above a second major surface of said first sheet of perforated material.

15. The method of claim 1 , wherein said method comprises making a plurality of discrete panels of said composite material and fastening said plurality of discrete panels together to form a heat dissipating enclosure having an interior surface and an exterior surface.

16. The method of claim 15 , wherein said first sheet of perforated material is a metal, and said plurality of discrete panels of said composite material are fastened together along the respective edges of each of said plurality of discrete panels by welding, soldering, brazing, or melting said metal.

17. The method of claim 15 , wherein said plurality of discrete panels forming said heat dissipating enclosure are oriented so that said first sheet of perforated material is located on said exterior surface of said heat dissipating enclosure, and said compressed layer of said graphite material is located on said interior surface of said heat dissipating enclosure.

18. The method of claim 7 , wherein said method comprises making a plurality of discrete panels of said composite material and fastening said plurality of discrete panels together to form a heat dissipating enclosure having an interior surface and an exterior surface.

19. The method of claim 18 , further comprising applying a protective coating to said exterior surface of said heat dissipating enclosure.

20. The method of claim 18 , further comprising applying an electrically insulating coating to said interior surface of said heat dissipating enclosure.

Assignments (3)
CHANGE OF NAME Recorded Jan 14, 2026
From: 0908905 B.C. LTD.
To: AFFINITY GRAPHITE LTD.
Reel/Frame 073467/0019 →
CHANGE OF NAME Recorded May 13, 2021
From: TERRELLA ENERGY SYSTEMS LTD.
To: 0908905 B.C. LTD.
Reel/Frame 056240/0159 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 30, 2019
From: KENNA, JOHN
To: TERRELLA ENERGY SYSTEMS LTD.
Reel/Frame 048187/0562 →
Continuity (6)
Continuation 15630323 · Jun 22, 2017
Continuation 15201347 · Jul 1, 2016
Continuation In Part 14583402 · Dec 26, 2014
Provisional Application 62035210 · Aug 8, 2014
Provisional Application 61921042 · Dec 26, 2013
Related Publication 20190124793A1 · Apr 25, 2019