This application is a Continuation-in-Part of application Ser. No. 15/049,019, filed Feb. 20, 2016.
The present invention relates to a method of manufacturing a hexagonal boron nitride laminate which exhibits thermal conductivity of the hexagonal boron nitride laminate 10 to 40 W/m·K, which is significantly larger than that currently used in thermal management.
Increasing circuit density and miniaturization of the modern electronics make the highly efficient heat removal and dissipation ever more critical for reliable operation of the electronic devices and systems. Hence the industry is in an urgent need of novel thermally conductive materials suitable for various thermal management applications. It is especially beneficial if such materials are electrically insulating since it would make it possible to apply them directly on the electronic circuitry. Unfortunately, most of the economically viable insulating materials are characterized by low thermal conductivity, which seriously limits their application as efficient heat spreaders.
It has been long known that bulk hexagonal boron nitride (hBN) possess one of the highest basal plane thermal conductivities among other materials (up to 400 W/m·K at room temperature) and almost matches that of silver. The more recent interest in hBN has been motivated by the search of an electrically insulating counterpart of graphene suitable for thermal management applications. Apart from excellent dielectric properties, few atomic layer hBN crystals demonstrated high values of thermal conductivity approaching its bulk value, and ultimately predicted to exceed those. Considering the rare combination of the electrical insulating behaviour with exceptionally high thermal conductivity hexagonal boron nitride is a promising candidate for the next-generation thermal management materials. However to exploit the remarkable properties of the few-layer hBN crystals for practical applications would require thermally conductive layers to be either flexible or conformal with the surface, and to have little heat junction within channel in a preferred orientation. All of those requirements can be satisfied by obtaining laminates consistent of thin (preferable monolayer) hBN crystals. It has been demonstrated before that graphene laminates possess relatively high thermal conductivity (up to 100 W/m·K) alongside with perfect coating properties. Unfortunately, the number of potential thermal management applications of such graphene laminates is limited by their high electrical conductivity. On the other hand, hBN laminates are also expected to provide high thermal conductivity in conjunction with excellent electrical insulating properties, which can potentially become a paradigm changer for the electronic industry.
The present invention has arisen to mitigate and/or obviate the afore-described disadvantages.
The primary objective of the present invention is to provide a method of manufacturing a hexagonal boron nitride laminate which exhibits thermal conductivity of hexagonal boron nitride laminates 10 to 40 W/m·K
Another objective of the present invention is to provide a method of manufacturing a hexagonal boron nitride laminate in which a thermal conductivity of the hexagonal boron nitride laminate increase with the increasing mass density, which opens a way of fine tuning of its thermal properties.
To obtain above-mentioned objective, a method of manufacturing hexagonal boron nitride laminates provided by the present invention contains steps of:
a) Dissolve 30 wt % to 80 wt % dielectric polymers in solvent.
b) Mixing 20 wt % to 70 wt % h-BN powder to form a well-mixed h-BN coating slurry.
c) Coating slurry on a substrate and dried at 100-150° C. A layer of h-BN laminates was obtained after this process.
By the above manufacturing method, a flexible insulating film with thermal conductivity as high as 10 W/mK to 40 W/mK can be reached.
Moreover, the substrate of the hexagonal boron nitride laminatec can be directly etched or processed to form electric circuit.
On the other hand, if a free-standing hexagonal boron nitride laminate is needed, the substrate can be completely etched or detached.
A method of manufacturing a hexagonal boron nitride laminate according to a preferred embodiment of the present invention contains steps of:
a) Dissolve 30 wt % to 80 wt % dielectric polymers in solvent.
Preferably, the dielectric polymer is selected from groups comprising polyethylene terephthalate (PETP), polyphenylene sulfide (PPS), polyetherimide (PEI), polyetherether ketone (PEEK), polyetherketone (PEK), polyimide (PI), Polyvinylidene fluoride (PVDF), phenol resin and acrylic resins.
Preferably, the dielectric polymer is flexible after curing with thickness of the film ranging from 5 um to 200 um.
b) Mixing 20 wt % to 70 wt % h-BN powder to form a well-mixed h-BN coating slurry.
Preferably, the thickness of h-BN powders ranges from 0.34 nm to 500 nm, and the diameter is from 0.1 μm to 100 μm.
c) Coating slurry on a substrate and dried at 100° C. to 150° C. A layer of h-BN laminate was obtained after this process.
Preferably, the substrates are electrically conductive layers such as Cu or Al foils.
Preferably, the thickness of the conductive layer ranges from 10 um to 100 um.
Preferably, the conductive layer can be further etched or processed to form electric circuit.
Preferably, the conductive layer can be thoroughly etched or detached to attain a free-standing laminate.
In
The thermal conductivity κ of the investigated laminate has been calculated using equation
κ=αρCp, (1)
here α is the in-plane thermal diffusivity, ρ is the material density and Cp is the specific heat. All three parameters were independently determined in experiment.
The thermal diffusivity α as a function of temperature T has been measured by the laser flash method using commercially available system (Netzsch LFA 457). To measure the in-plane thermal diffusivity the special sample holder has been used, which accommodates the free-standing hBN membrane samples cut into a round shape of 22 mm in diameter. A small spot of about 5 mm in diameter at the back side of the sample is flash heated by the laser beam. The heat diffusion as a function of time is registered by the infrared detector along the top circumference of the membrane at 5 mm to 6 mm from the centre of the sample. To avoid undesirable reflections the sample and sample holder have been spray coated with graphite paint. During the measurements the sample chamber of the laser flash system was continuously purged with nitrogen gas at the rate of 30 nal/min. The sample specific heat Cp was measured by the differential scanning calorimeter (Netzsch DSC 404 F3) using sapphire as a reference sample. The mass density ρ was estimated by weighting the sample of the known dimensions with precision electronic balances.
To evaluate the effect of the membrane composition we measured the thermal conductivity κ as a function of temperature T for four hBN laminates with different mass density. As seen from
To better understand the influence of the material density on the thermal conductivity we studied the dependence of κ on ρ at room temperature. The density of the laminate samples was controlled in two different ways: (i) by using hBN flakes of different thickness (only limited variations of ρ could be achieved in this way), and (ii) by variation of the additional roller compression applied during preparation of the laminates. Both methods had the same effect on the thermal conductivity. The combined results of this study are presented in
After systematic SEM examination of the laminates of different density, we concluded that the density variations are mostly due to the variation in the size of empty voids present between stacked hBN flakes. The schematic representation of two laminates with different density is given in
To confirm our suggestions, we carried out modeling of the thermal flow in laminates with voids. Our numerical simulation was done using ABAQUS 2011 finite element analysis software package. In order to explore the relation between the effective thermal conductivity and the density of hBN laminates we simulated the steady-state heat transfer governed by equation
where Q is the heat flux and ∂T/∂t=0 (steady-state heat transfer). The modeled system was evaluated with the ABAQUS element type DC2D8 and represented by a strip of orderly stacked solid blocks of thermally conductive media with lateral size of 1 μm×1 μm and thickness of 10 nm, as show in
Here q is the total net heat flux through the cross section of the laminate, L is the total length of the laminate strip and ΔT is the temperature difference between hot and cold ends of the strip.
The result of the numerical simulation is shown by solid curves in
In conclusion, we demonstrated that hBN inks can be used to produce laminates with thermal conductivity as high as 20 W/m·K in the above mentioned embodiment, which is significantly larger than that for materials currently used in thermal management. We also show that the effective thermal conductivity can be adjusted by varying the laminate packing density. We also identify a potential way for further increase in of thermal conductance by improving the quality of the flake-to-flake interface. Being electrically insulating, hBN laminates can potentially open a new avenue for using the advanced thermal management materials.
As shown in
As illustrated in
Number | Date | Country | |
---|---|---|---|
Parent | 15049019 | Feb 2016 | US |
Child | 15630757 | US |