Manufacturing method for a finished product of a heat sink composite having heat dissipation function

11213877 ยท 2022-01-04

Assignee

Inventors

Cpc classification

International classification

Abstract

The invention relates to a manufacturing process for a heat dissipation heat sink composite having heat dissipation function and a manufacturing method for a finished product thereof. It comprises the steps of rolling a first heat conductive material and a substrate to adhere the first heat conductive material to the substrate for fixation; adhering a second heat conductive material to the substrate for combination; and rolling the second heat conductive material and the substrate for firmly combination and fixation to complete the manufacturing of a composite material.

Claims

1. A manufacturing method for a finished product of a heat sink composite having a heat dissipation function, comprising the following steps of: (a) cutting a heat sink composite in order to form a plurality of heat sink composites; (b) after the cutting, arranging the plurality of heat sink composites to form an array of heat sink composites; (c) binding and fixing the array of heat sink composites by a heat-resistant insulating tape; and (d) bonding the array of heat sink composites to a component, to be cooled, by use of an insulating silicone elastic interface material.

2. A manufacturing method for a finished product of a heat sink composite having a heat dissipation function, comprising the following steps of: (a) arranging a plurality of heat sink composites, having a predetermined size, in an array in order to form an array of heat sink composites; (b) winding the array of heat sink composites to a predetermined number of layers and binding and fixing the array of heat sink composites by a heat-resistant insulating tape; (c) after winding, cutting the array of heat sink composites into a desired size to form a sized array of heat sink composites; (d) axially encapsulating the sized array of heat sink composites; and (e) bonding the sized array of heat sink composites to a component, to be cooled, by use of an insulating silicone elastic interface material.

3. The manufacturing method for a finished product of the heat sink composite having heat dissipation function as claimed in claim 2, further comprising a step of moving the array of heat sink composites into a vacuum annealing furnace for reduction and annealing after the step (b) and before the step (c) as claimed in claim 2.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a flow chart showing a manufacturing process for a heat sink composite having heat dissipation function according to the present invention;

(2) FIG. 2 is a schematic diagram showing a manufacturing process for a heat sink composite having heat dissipation function according to the present invention;

(3) FIG. 3 is a sectional view showing a heat sink composite having heat dissipation function according to the present invention;

(4) FIG. 4 is a first schematic diagram showing a heat sink composite bound and fixed by a heat-resistant insulating tape to be further cut to a size as needed;

(5) FIG. 5 is a second schematic diagram showing a heat sink composite bound and fixed by a heat-resistant insulating tape to be further cut to a size as needed;

(6) FIG. 6 is a schematic diagram showing a plurality of heat sink composites bonded to an insulating silicone elastic interface material for contacting a component to be cooled;

(7) FIG. 7 is a schematic diagram showing a first embodiment for a plurality of heat sink composites wound to a predetermined number of layers;

(8) FIG. 8 is a schematic diagram showing a second embodiment for a plurality of heat sink composites wound to a predetermined number of layers;

(9) FIG. 9 is a schematic diagram showing the first embodiment for the plurality of heat sink composites further bonded to two insulating silicone elastic interface materials for contacting a component to be cooled;

(10) FIG. 10 is a schematic diagram showing the second embodiment for the plurality of heat sink composites further bonded to two insulating silicone elastic interface materials for contacting a component to be cooled.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT

(11) Hereinafter, an exemplary embodiment of the present invention will be described in detail with reference to the accompanying drawings.

(12) As showed in FIG. 1 and FIG. 2, a manufacturing process for a heat sink composite having heat dissipation function according to the present invention is disclosed. It mainly comprises the following steps of:

(13) (a) transferring a first heat conductive material (1) and a substrate (2); preferably, the first heat conductive material (1) is selected from a group consisting of graphite oxide, graphene oxide and carbon materials with functional groups and shaped as a thin film, a flake or a roll, and the substrate (2) is a metal film, a metal mesh, a metal sheet, an inorganic film, an inorganic mesh, an organic film, an organic mesh or a non-woven fabric;

(14) (b) rolling the first heat conductive material (1) and the substrate (2) under a high pressure by a rolling mechanism (3) to adhere the substrate (2) on one side of the first heat conductive material (1) for fixation;

(15) (c) spraying the other side of the first heat conductive material (1) with an organic or inorganic phase change material (5) by a spraying mechanism (4) for firmly combining the phase change material (5) to the first heat conductive material (1);

(16) (d) adhering one side of a second heat conductive material (7) to the substrate (2) by use of its inherent functional groups for combination, or by use of spraying an organic adhesive (6) on an outer surface of the substrate (2) for drying to form adhesiveness and for further bonding the organic adhesive (6) to the second heat conductive material (7), and then rolling the second heat conductive material (7) and the substrate (2) by a high pressure to be firmly bonded to each other so as to complete the preparation of a heat sink composite (A); preferably, the second heat conductive material (7) is selected from a group consisting of graphite oxide, graphene oxide and carbon materials with functional groups and shaped as a thin film, a flake or a roll; and

(17) (e) spraying the other side of the second heat conductive material (7) with an organic or inorganic phase change material (5) for firmly combining the phase change material (5) to the second heat conductive material (7) as shown in FIG. 3.

(18) In use of the present invention, referring to FIG. 4 and FIG. 5, a heat sink composite (A) is cut into a size as needed, and then the plurality of heat sink composites (A) of various sizes are combined and arranged to form an array. A heat-resistant insulating tape (8) is used to bind and fix the plurality of heat sink composites (A) to be further cut into a size as needed. Referring to FIG. 6, an insulating silicone elastic interface material (9) is used to bond the plurality of heat sink composites (A) to a component to be cooled so as to achieve excellent heat dissipation.

(19) Referring to FIG. 7 and FIG. 8, in step (a), a plurality of heat sink composites (A) having a predetermined size are arranged to form an array and then one ends of the plurality of heat sink composites (A) are fixed to a roll for winding. In step (b), after the plurality of heat sink composites (A) are wound up to a predetermined number of layers, a heat-resistant insulating tape (8) is used to bind and fix the plurality of heat sink composites (A). The plurality of heat sink composites (A) are taken off from the roll and then transferred into a vacuum annealing furnace for reduction and annealing. In step (c), after cooled down to room temperature, the plurality of heat sink composites (A) are transferred into a cutting mechanism for cutting into a size as needed. In step (d), the plurality of heat sink composites (A) are axially encapsulated. Finally, in step (e), the plurality of heat sink composites (A) are bonded to a component (B) to be cooled by use of an insulating silicone elastic interface material (9) as shown in FIG. 9 and FIG. 10 so as to achieve excellent heat dissipation.

(20) Compared with the technique available now, the present invention has the following advantages:

(21) 1. The present invention increases efficiency of 3-dimentional heat dissipation and conduction and electromagnetic radiation absorption.

(22) 2. The present invention avoids the occurrence of oxidative damage, so it can maintain a long service life with high performance.

(23) 3. The present invention is easy to process and manufacture and has low loss and high yield rate, so it can reduce manufacturing cost.

(24) 4. The present invention has no environmental damage during the production process and achieves environmental friendly effect due to its recyclability.