IP Library Granted Patent US 9,932,226
Granted Patent B2
US 9,932,226 · App. 14/268,052 · Granted Apr 3, 2018

Composite material containing graphene

Inventor: Namsoo P. Kim (Bellevue, WA)
Assignee: The Boeing Company
B82Y30/00C09K5/14F28F21/02F28F21/081H01L23/373H01L23/3736H01L23/3737H01L2924/0002
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Quick Facts
Patent No.
US 9,932,226
App. No.
14/268,052
Granted
Apr 3, 2018
Kind
B2
Abstract

In one aspect, a composite material is disclosed herein that includes graphene platelets dispersed in a matrix. In some cases, the graphene platelets are randomly oriented within the matrix. The composite material can provide improved thermal conductivity and may be formed into heat spreaders or other thermal management devices to provide improved cooling to electronic, electrical components and semiconductor devices.

Claims (17)

1. A composite material comprising:

a metal matrix; and

a plurality of graphene platelets dispersed in the metal matrix;

wherein the graphene platelets are randomly oriented in the metal matrix,

wherein the graphene platelets have an average thickness of up to 10 nm, an average length of 1 μm to 1 cm, and an average width of 1 μm to 1 cm;

wherein the composite material includes the graphene platelets in an amount of 5% to 20% by volume, based on the total volume of the metal matrix; and

wherein the composite material exhibits a ductile-brittle transition temperature within 15% of the ductile-brittle transition temperature of the metal matrix without any graphene platelets and/or a tensile strength within 20% of the tensile strength of the metal matrix without any graphene platelets, and/or a tensile modulus within 20% of the tensile modulus of the metal matrix without any graphene platelets.

2. The composite material of claim 1 , wherein the metal matrix is thermally conductive.

3. The composite material of claim 1 , wherein the metal matrix comprises aluminum, an aluminum alloy, copper, a copper alloy, titanium, a titanium alloy, or a combination thereof.

4. The composite material of claim 1 , wherein the graphene platelets have an average thickness of 1 nm to 10 nm.

5. The composite material of claim 1 , wherein the graphene platelets have an average thickness of 0.3 nm to 1 nm.

6. The composite material of claim 1 , wherein the composite material exhibits a ductile-brittle transition temperature within 15% of the ductile-brittle transition temperature of the metal matrix without any graphene platelets.

7. The composite material of claim 1 , wherein the composite material exhibits a tensile strength within 20% of the tensile strength of the metal matrix without any graphene platelets.

8. The composite material of claim 1 , wherein the composite material exhibits a ductile-brittle transition temperature within 10% of the ductile-brittle transition temperature of the metal matrix without any graphene platelets and/or a tensile strength within 15% of the tensile strength of the metal matrix without any graphene platelets.

9. A thermally conductive material comprising the composite material of claim 1 .

10. A thermally conductive component comprising the thermally conductive material of claim 9 .

11. The thermally conductive component of claim 10 , wherein the thermally conductive component is a heat spreader or a heat sink.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 2, 2014
From: KIM, NAMSOO P.
To: THE BOEING COMPANY
Reel/Frame 032807/0527 →
Continuity (1)
Related Publication 20150315449A1 · Nov 5, 2015