Thermal management assembly comprising bulk graphene material
US-2015253089-A1 · Sep 10, 2015 · US
US2016209133A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016209133-A1 |
| Application number | US-201615084098-A |
| Country | US |
| Kind code | A1 |
| Filing date | Mar 29, 2016 |
| Priority date | Dec 27, 2013 |
| Publication date | Jul 21, 2016 |
| Grant date | — |
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The present invention discloses a thermally conductive composite sheet, including a first aluminum alloy layer, at least one graphite sheet, an aluminum alloy frame, and a second aluminum alloy layer, where the aluminum alloy frame is provided with at least one opening; the graphite sheet is positioned inside the opening of the aluminum alloy frame; the aluminum alloy frame and the graphite sheet are sandwiched between the first aluminum alloy layer and the second aluminum alloy layer; the first aluminum alloy layer is diffusion-bonded to the graphite sheet and the aluminum alloy frame; the second aluminum alloy layer is diffusion-bonded to the graphite sheet and the aluminum alloy frame; and the graphite sheet is cladded by the first aluminum alloy layer, the second aluminum alloy layer, and the aluminum alloy frame, to form a unity.
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What is claimed is: 1 . A thermally conductive composite sheet, comprising: a first aluminum alloy layer, at least one graphite sheet, an aluminum alloy frame, and a second aluminum alloy layer, wherein the aluminum alloy frame is provided with at least one opening; the graphite sheet is positioned inside the opening of the aluminum alloy frame; the aluminum alloy frame and the graphite sheet are sandwiched between the first aluminum alloy layer and the second aluminum alloy layer; the first aluminum alloy layer is diffusion-bonded to the graphite sheet and the aluminum alloy frame; the second aluminum alloy layer is diffusion-bonded to the graphite sheet and the aluminum alloy frame; and the graphite sheet is cladded by the first aluminum alloy layer, the second aluminum alloy layer, and the aluminum alloy frame, to form a unity. 2 . The thermally conductive composite sheet according to claim 1 , wherein materials of the first aluminum alloy layer, the second aluminum alloy layer, and the aluminum alloy frame are the same. 3 . The thermally conductive composite sheet according to claim 1 , wherein a thickness of the first aluminum alloy layer is 0.26 millimeters to 1.0 millimeters. 4 . The thermally conductive composite sheet according to claim 1 , wherein a thickness of the second aluminum alloy layer is 0.26 millimeters to 1.0 millimeters. 5 . The thermally conductive composite sheet according to claim 1 , wherein there is one opening inside the aluminum alloy frame, there is also one graphite sheet, and the graphite sheet is accommodated inside the opening. 6 . The thermally conductive composite sheet according to claim 1 , wherein there are multiple openings inside the aluminum alloy frame, there are also multiple graphite sheets, and each graphite sheet is correspondingly accommodated inside one opening. 7 . A thermally conductive composite sheet, comprising: a first aluminum alloy layer, at least one graphite sheet, a first transition layer, a second transition layer, an aluminum alloy frame, and a second aluminum alloy layer, wherein the aluminum alloy frame is provided with at least one opening; the graphite sheet is positioned inside the opening of the aluminum alloy frame; the aluminum alloy frame and the graphite sheet are sandwiched between the first aluminum alloy layer and the second aluminum alloy layer; the first transition layer is disposed between the graphite sheet and the first aluminum alloy layer; the second transition layer is disposed between the second aluminum alloy layer and the graphite sheet; the first aluminum alloy layer and the first transition layer are diffusion-bonded; the first transition layer and the graphite sheet are diffusion-bonded; the graphite sheet and the second transition layer are diffusion-bonded; the second transition layer and the second aluminum alloy layer are diffusion-bonded; and two opposite sides of the aluminum alloy frame are separately diffusion-bonded to the first aluminum alloy layer and the second aluminum alloy layer, so that the first transition layer, the second transition layer, and the graphite sheet are cladded by the first aluminum alloy layer, the second aluminum alloy layer, and the aluminum alloy frame, to form a unity. 8 . The thermally conductive composite sheet according to claim 7 , wherein materials of the first aluminum alloy layer, the second aluminum alloy layer, and the aluminum alloy frame are the same. 9 . The thermally conductive composite sheet according to claim 7 , wherein a thickness of the first aluminum alloy layer is 0.26 millimeters to 1.0 millimeters. 10 . The thermally conductive composite sheet according to claim 7 , wherein a thickness of the second aluminum alloy layer is 0.26 millimeters to 1.0 millimeters. 11 . The thermally conductive composite sheet according to claim 7 , wherein there is one opening inside the aluminum alloy frame, there is also one graphite sheet, and the graphite sheet is accommodated inside the opening. 12 . The thermally conductive composite sheet according to claim 7 , wherein there are multiple openings inside the aluminum alloy frame, there are also multiple graphite sheets, and each graphite sheet is correspondingly accommodated inside one opening. 13 . The thermally conductive composite sheet according to claim 7 , wherein the first transition layer is made of titanium or an alloy comprising titanium. 14 . The thermally conductive composite sheet according to claim 7 , wherein the second transition layer is made of titanium or an alloy comprising titanium. 15 . The thermally conductive composite sheet according to claim 7 , wherein a thickness of the first transition layer is 20 micrometers to 40 micrometers. 16 . The thermally conductive composite sheet according to claim 7 , wherein a thickness of the second transition layer is 20 micrometers to 40 micrometers. 17 . A method for making a thermally conductive composite sheet, the method comprising: providing two aluminum alloy sheets and one aluminum alloy frame, wherein the aluminum alloy frame is provided with at least one opening, and performing mechanical treatment and chemical treatment on the aluminum alloy sheets and the aluminum alloy frame, so as to decrease roughness of surfaces of the aluminum alloy sheets and a surface of the aluminum alloy frame, and obtain active aluminum alloy surfaces; providing at least one graphite sheet; placing the graphite sheet inside the opening of the aluminum alloy frame, separately placing the aluminum alloy sheets on two opposite sides of the aluminum alloy frame and the graphite sheet to form a laminated structure, placing the laminated structure inside a furnace chamber, and vacuumizing the furnace chamber; and heating and pressurizing the laminated structure, and performing diffusion-bonding between the aluminum alloy frame in which the graphite sheet is placed and the two aluminum alloy sheets, so as to obtain a thermally conductive composite sheet. 18 . The method for making a thermally conductive composite sheet according to claim 17 , wherein performing mechanical treatment comprises grinding and polishing, so as to decrease roughness of the surfaces of the aluminum alloy sheets and the surface of the aluminum alloy frame. 19 . The method for making a thermally conductive composite sheet according to claim 17 , wherein performing chemical treatment comprises acid cleaning and alkaline cleaning, so as to obtain the active aluminum alloy surfaces. 20 . The method for making a thermally conductive composite sheet according to claim 17 , wherein the furnace chamber is vacuumized until an intensity of pressure is 5×10−3 Pa to 7×10−3 Pa. 21 . The method for making a thermally conductive composite sheet according to claim 17 , wherein when diffusion-bonding is performed between the aluminum alloy frame in which the graphite sheet is placed and the two aluminum alloy sheets, a temperature inside the furnace chamber is increased to 530 degrees Celsius to 590 degrees Celsius, and a pressure of 10 MPa to 15 MPa is applied to the laminated structure, so that diffusion-bonding is performed between surfaces of the graphite sheet and the aluminum alloy sheets that are in contact with each other. 22 . The method for making a thermally conductive composite sheet according to claim 17 , wherein there are multiple openings inside the aluminum alloy frame, there are also multiple graphite sheets, and each grap
having a heterogeneous or anisotropic structure, e.g. powder or fibres in a matrix, wire mesh or porous structures (H10W40/254, H10W40/251 take precedence) · CPC title
Fillings or auxiliary members in containers or in encapsulations for thermal protection or control · CPC title
Metallic materials (H10W40/254, H10W40/257, H10W40/255, H10W40/251, H10W40/253 take precedence) · CPC title
having a laminate or multilayered structure, e.g. direct bond copper [DBC] ceramic substrates · CPC title
Assembling together parts thereof · CPC title
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