JP2008169245A - Heat dissipation material and manufacturing method thereof - Google Patents
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- JP2008169245A JP2008169245A JP2007001448A JP2007001448A JP2008169245A JP 2008169245 A JP2008169245 A JP 2008169245A JP 2007001448 A JP2007001448 A JP 2007001448A JP 2007001448 A JP2007001448 A JP 2007001448A JP 2008169245 A JP2008169245 A JP 2008169245A
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- 238000004519 manufacturing process Methods 0.000 title claims abstract description 16
- 230000017525 heat dissipation Effects 0.000 title claims description 30
- 239000011347 resin Substances 0.000 claims abstract description 78
- 229920005989 resin Polymers 0.000 claims abstract description 78
- 239000000919 ceramic Substances 0.000 claims abstract description 65
- 239000002184 metal Substances 0.000 claims abstract description 27
- 229910052751 metal Inorganic materials 0.000 claims abstract description 27
- 239000002131 composite material Substances 0.000 claims abstract description 23
- 239000011148 porous material Substances 0.000 claims abstract description 10
- 239000002002 slurry Substances 0.000 claims description 31
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 27
- 238000000034 method Methods 0.000 claims description 18
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- 238000002360 preparation method Methods 0.000 claims description 2
- 238000011049 filling Methods 0.000 abstract description 8
- 239000002245 particle Substances 0.000 description 12
- 230000005855 radiation Effects 0.000 description 11
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 7
- 238000005470 impregnation Methods 0.000 description 6
- 238000005245 sintering Methods 0.000 description 6
- 239000010410 layer Substances 0.000 description 5
- 238000000859 sublimation Methods 0.000 description 4
- 230000008022 sublimation Effects 0.000 description 4
- 229910018072 Al 2 O 3 Inorganic materials 0.000 description 3
- OKKJLVBELUTLKV-UHFFFAOYSA-N Methanol Chemical compound OC OKKJLVBELUTLKV-UHFFFAOYSA-N 0.000 description 3
- 239000011888 foil Substances 0.000 description 3
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- 238000001816 cooling Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
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- 239000002905 metal composite material Substances 0.000 description 1
- 239000002923 metal particle Substances 0.000 description 1
- 239000011812 mixed powder Substances 0.000 description 1
- 229920001721 polyimide Polymers 0.000 description 1
- 229920001195 polyisoprene Polymers 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 239000003505 polymerization initiator Substances 0.000 description 1
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Abstract
Description
本発明は放熱材及びその製造方法に関し、詳しくは電子部品用の放熱デバイス等に用いられる放熱材及びその製造方法に関する。 The present invention relates to a heat radiating material and a manufacturing method thereof, and more particularly to a heat radiating material used for a heat radiating device for an electronic component and the like and a manufacturing method thereof.
パーソナルコンピュータやモバイル電子機器の高機能化に伴い、CPU等の発熱源の発熱量が飛躍的に増大しており、放熱デバイスの高性能化が求められている。
放熱手法の一つとして簡易でかつ効果的な方法は、発熱源の表面に放熱シートを貼り付けて放熱する方法である。該放熱シートは、一般的には樹脂中に高熱伝導率の粒子を分散した材料である(特許文献1)。高熱伝導率粒子としては、熱伝導率が400W/mK程度あるAgやCuなどの金属粒子、Al2O3やAlNなどのセラミックス粒子が用いられることが多いが、共通する課題がある。
As the functions of personal computers and mobile electronic devices increase, the amount of heat generated by a heat source such as a CPU has increased dramatically, and there is a need for higher performance of heat dissipation devices.
A simple and effective method for dissipating heat is a method of dissipating heat by attaching a heat dissipating sheet to the surface of the heat source. The heat radiating sheet is generally a material in which particles having high thermal conductivity are dispersed in a resin (Patent Document 1). As the high thermal conductivity particles, metal particles such as Ag and Cu having a thermal conductivity of about 400 W / mK, and ceramic particles such as Al 2 O 3 and AlN are often used, but there are common problems.
これらの複合材料において高い熱伝導率を発現させるためには、複合材料中で高熱伝導率の分散粒子が、少なくともそれらの粒子の一部が互いに接触している必要がある。すなわち、粒子が互いに接触せず、孤立した粒子分散型組織になった場合、複合材料の熱伝導率は極めて低くなる。
分散粒子同士を接触させるためには、粒子の体積含有率を50%以上にまで高くしなければならないが、この場合は逆に樹脂の特徴である柔軟性が損なわれてしまい、放熱シートが熱源に隙間無く密着できなくなり、放熱性が低下する。
予め高気孔率のセラミックス多孔体を焼結法で作製しておき、該多孔体中に樹脂を装填する方法も考えられるが、気孔率の高いセラミックス多孔体は非常にもろく、焼結後の形状維持が困難である。
In order to develop high thermal conductivity in these composite materials, it is necessary that dispersed particles having high thermal conductivity in the composite material have at least a part of the particles in contact with each other. That is, when the particles do not contact each other and become an isolated particle dispersed structure, the thermal conductivity of the composite material becomes extremely low.
In order to bring the dispersed particles into contact with each other, the volume content of the particles must be increased to 50% or more. In this case, however, the flexibility that is characteristic of the resin is impaired, and the heat dissipation sheet becomes a heat source. It becomes impossible to adhere to the gap without any gap, and the heat dissipation is reduced.
A method of preparing a porous ceramic body with a high porosity by a sintering method in advance and loading a resin into the porous body is also conceivable, but a ceramic porous body with a high porosity is very brittle and has a shape after sintering. It is difficult to maintain.
本発明は上記問題を解決すべく、熱伝導率が高い放熱材及びその製造方法を提供することを課題とする。 This invention makes it a subject to provide the thermal radiation material with high heat conductivity, and its manufacturing method in order to solve the said problem.
本発明はこの課題を解決すべくされたものであり、樹脂の含有量が大きい場合でも高い熱伝導率と柔軟性を持つ放熱材とその製法に関し、下記の特徴を持つ。
(1)セラミックス多孔体と第二成分としての樹脂または金属からなる吸熱部と放熱部とを有する複合材料であって、該セラミックス多孔体中において吸熱部から放熱部へ配向するように設けたマクロ孔に樹脂または金属を充填させた第二成分の連続相と、該配向させた他の第二成分の連続相とを連結するミクロ孔を有し、当該ミクロ孔に樹脂または金属を充填させた連結相とを有する複合材料からなることを特徴とする放熱材。
(2)前記第二成分が樹脂であることを特徴とする上記(1)に記載の放熱材。
(3)前記第二成分の体積含有率が放熱材中50〜90%であることを特徴とする上記(1)又は(2)に記載の放熱材。
The present invention has been made to solve this problem, and has the following characteristics regarding a heat radiating material having high thermal conductivity and flexibility even when the resin content is large and a method for producing the same.
(1) A composite material having a ceramic porous body and a heat absorbing portion and a heat radiating portion made of a resin or metal as a second component, the macro provided in the ceramic porous body so as to be oriented from the heat absorbing portion to the heat radiating portion It has micropores that connect the continuous phase of the second component in which the holes are filled with resin or metal and the continuous phase of the other second component that is oriented, and the micropores are filled with resin or metal A heat dissipation material comprising a composite material having a connected phase.
(2) The heat dissipation material as described in (1) above, wherein the second component is a resin.
(3) The heat radiation material according to (1) or (2), wherein the volume content of the second component is 50 to 90% in the heat radiation material.
(4)前記第二成分の連続相となるマクロ孔の直径が5〜100μmであることを特徴とする上記(1)〜(3)のいずれか一に記載の放熱材。
(5)前記ミクロ孔の平均細孔径が、0.1〜5μmであることを特徴とする上記(1)〜(4)のいずれか一に記載の放熱材。
(6)前記セラミックス多孔体の熱伝導率が、20W/mK以上であることを特徴とする上記(1)〜(5)のいずれか一に記載の放熱材。
(7)引張伸び率が50%以上の樹脂を前記第二成分として使用することを特徴とする上記(1)〜(6)のいずれか一に記載の放熱材。
(8)放熱材の表面の少なくとも一部に粘着層が形成されたことを特徴とする上記(1)〜(7)のいずれか一に記載の放熱材。
(4) The heat dissipation material as described in any one of (1) to (3) above, wherein a diameter of a macropore serving as a continuous phase of the second component is 5 to 100 μm.
(5) The heat dissipation material according to any one of (1) to (4), wherein an average pore diameter of the micropores is 0.1 to 5 μm.
(6) The heat dissipation material according to any one of (1) to (5) above, wherein the ceramic porous body has a thermal conductivity of 20 W / mK or more.
(7) The heat dissipation material as described in any one of (1) to (6) above, wherein a resin having a tensile elongation of 50% or more is used as the second component.
(8) The heat radiation material according to any one of (1) to (7), wherein an adhesive layer is formed on at least a part of the surface of the heat radiation material.
(9)セラミックス原料粉末を水中に分散させるスラリー調整工程と、得られたスラリーを特定方向から凍結させ氷の成長を促す工程と、凍結したスラリーを真空凍結乾燥し氷を昇華させ、マクロ孔を有する成形体を作る工程と、氷を昇華させた成形体を加熱処理により焼成し、前記成形体中にミクロ孔を形成する工程、および該マクロ孔およびミクロ孔中に第二成分である樹脂または金属を充填する工程とを有することを特徴とする放熱材の製造方法。
(10)前記第二成分が樹脂であることを特徴とする上記(9)に記載の放熱材の製造方法。
(9) Slurry preparation step for dispersing ceramic raw material powder in water, step of freezing the obtained slurry from a specific direction to promote ice growth, vacuum freeze-drying the frozen slurry to sublimate ice, A step of making a molded body having, a step of baking a molded body sublimated with ice by heat treatment to form micropores in the molded body, and a resin or a second component in the macropores and micropores or And a step of filling with a metal.
(10) The method for manufacturing a heat dissipation material as described in (9) above, wherein the second component is a resin.
本発明による放熱材は、一方向に配向したマクロ孔を持つセラミックス多孔体を出発として用いるため、セラミックス多孔体中へ樹脂や金属が含浸されやすく、結果として熱伝導率が高い複合材料が得られる。また、特にセラミックス多孔体に樹脂を含浸させた場合には、柔軟な複合材料を得ることができる。 Since the heat dissipation material according to the present invention uses a ceramic porous body having macropores oriented in one direction as a starting material, the ceramic porous body is easily impregnated with resin or metal, and as a result, a composite material having high thermal conductivity is obtained. . In particular, when a porous ceramic body is impregnated with a resin, a flexible composite material can be obtained.
本発明に係る放熱材は連続相と連結相とを有する複合材料かなる。連続相とは、セラミックス多孔体中の吸熱部から放熱部へと配向して貫通するマクロ孔に第二成分としての樹脂又は金属が充填された構造をしている。さらにマクロ孔同士は、樹脂又は金属が充填されたミクロ孔(連結相)によって連結されている。また、本発明に係る放熱材において、吸熱部とは、放熱材が発熱部材に貼りつけられた際に熱を吸収する部位を意味し、放熱部とは放熱材から熱を逃がす部位を意味する。吸熱部から吸収された熱は樹脂、金属又はセラミックスを介して放熱部へと伝わり外部へと放熱される。したがって、本発明に係る放熱材をシート状にした場合には、発熱部位に貼りつけられた一方の面が吸熱部となり、対向する面が放熱部となる。 The heat dissipating material according to the present invention is a composite material having a continuous phase and a connected phase. The continuous phase has a structure in which a resin or metal as a second component is filled in macropores that are oriented and penetrated from the heat absorbing portion to the heat radiating portion in the ceramic porous body. Furthermore, the macropores are connected by micropores (connection phase) filled with resin or metal. In the heat dissipation material according to the present invention, the heat absorption part means a part that absorbs heat when the heat dissipation material is attached to the heat generating member, and the heat dissipation part means a part that releases heat from the heat dissipation material. . The heat absorbed from the heat absorbing part is transferred to the heat radiating part through the resin, metal or ceramics and radiated to the outside. Therefore, when the heat dissipating material according to the present invention is formed into a sheet shape, one surface attached to the heat generating portion is a heat absorbing portion, and the opposite surface is a heat dissipating portion.
本発明に係る放熱材の放熱部にはCu箔、Al箔のような金属箔や、ポリイミド等の樹脂箔による第二基材が設けられていることが好ましい。このような第二基材により、複合材料から伝えられた熱は第二基材の厚み方向に加えて、面内方向にも伝達されるので、放熱効果が極めて大きくなる。さらに、第二基材の最表面に熱放射層が設けられていると、熱放射層の表面からの輻射によっても放熱できるので好ましい。熱放射層としては、熱を赤外線として大気中に放射できるものであれば特に限定されない。セラミックス等も好ましく用いることができる。また、吸熱部に粘着シートが設けられていると、発熱部への貼り付けが容易になる。 It is preferable that the heat radiating portion of the heat radiating material according to the present invention is provided with a second base material made of a metal foil such as Cu foil or Al foil or a resin foil such as polyimide. With such a second base material, the heat transferred from the composite material is also transferred in the in-plane direction in addition to the thickness direction of the second base material, so that the heat dissipation effect becomes extremely large. Furthermore, it is preferable that a heat radiation layer is provided on the outermost surface of the second base material because heat can be radiated by radiation from the surface of the heat radiation layer. The heat radiation layer is not particularly limited as long as it can radiate heat into the atmosphere as infrared rays. Ceramics or the like can also be preferably used. Moreover, when the heat-absorbing part is provided with an adhesive sheet, it can be easily attached to the heat generating part.
次に、本発明の複合材料とその製法の一例について説明する。
本発明の放熱材は、予め高い気孔率を持つセラミックス多孔体を作製しておき、該多孔体の細孔内部へ樹脂を充填させることで得られる。
セラミックス多孔体の製法は、凍結乾燥法と呼ばれるものであり、セラミックス原料粉末を水中に分散させるスラリー調整工程と、得られたスラリーを特定方向から凍結させ氷の成長を促す工程と、凍結したスラリーを真空凍結乾燥し氷を昇華させ、マクロ孔を有する成形体を作る工程と、氷を昇華させた成形体を加熱処理により焼成し、前記成形体中にミクロ孔を形成する工程からなる。(特許文献2参照)
このようにして作製した多孔体中に樹脂を充填することで本発明の放熱材は作製できる。
Next, an example of the composite material of the present invention and its manufacturing method will be described.
The heat dissipating material of the present invention is obtained by preparing a ceramic porous body having a high porosity in advance and filling a resin inside the pores of the porous body.
The method for producing a ceramic porous body is called a freeze-drying method, a slurry adjustment step of dispersing ceramic raw material powder in water, a step of freezing the obtained slurry from a specific direction to promote ice growth, and a frozen slurry Are formed by vacuum freeze-drying and sublimating ice to form a molded body having macropores, and a process of baking the molded body with ice sublimated by heat treatment to form micropores in the molded body. (See Patent Document 2)
The heat dissipating material of the present invention can be produced by filling a resin in the produced porous body.
図1に示すように、本発明の放熱材のベースとなるセラミックス多孔体の製造方法は、セラミックス原料粉末を水中に分散させてスラリーを調整する工程(工程1)、該スラリーを特定方向(図面の矢印方向)から凍結させ氷の成長を促す工程(工程2)、凍結したスラリーを真空凍結乾燥して氷を昇華させ、マクロ孔を有する成形体を作る工程(工程3)、氷を昇華させた成形体を加熱処理により焼成し、成形体を構成する骨格中にミクロ孔を形成する工程(工程4)によって作製することを特徴とする。 As shown in FIG. 1, the manufacturing method of the ceramic porous body used as the base of the heat dissipating material of the present invention includes a step of adjusting a slurry by dispersing ceramic raw material powder in water (step 1), and the slurry in a specific direction (drawing). The process of freezing from the direction of the arrow) to promote ice growth (process 2), the process of making the formed slurry with macropores by sublimating the frozen slurry by vacuum freeze-drying (process 3), and sublimating the ice The formed body is fired by heat treatment, and is produced by a step (step 4) of forming micropores in the skeleton constituting the formed body.
工程1に用いるセラミックス原料粉末は、多孔質体の骨格を形成するための原料であり、焼結可能なセラミックスを含有していれば特にその材料は限定されないが、放熱材として好ましいのは、熱伝導率が20W/mK以上のセラミックスである。セラミックス多孔体に樹脂を含浸して複合材料にした場合、複合材料の熱伝導率はほとんど全てセラミックスによって決定されてしまう。セラミックスの熱伝導率がこれより小さい場合、放熱材としての利点が小さくなる。熱伝導率は高いほど好ましく、Al2O3、SiC、ZnO、Si3N4、AlN等が候補となる。セラミックススラリーには必要に応じ焼結助剤を添加しても良い。 The ceramic raw material powder used in step 1 is a raw material for forming the skeleton of the porous body, and the material is not particularly limited as long as it contains a sinterable ceramic. A ceramic having a conductivity of 20 W / mK or more. When a ceramic porous body is impregnated with a resin to form a composite material, almost all the thermal conductivity of the composite material is determined by the ceramic. When the thermal conductivity of ceramics is smaller than this, the advantage as a heat dissipation material becomes small. Higher thermal conductivity is preferable, and Al 2 O 3 , SiC, ZnO, Si 3 N 4 , AlN, and the like are candidates. If necessary, a sintering aid may be added to the ceramic slurry.
スラリー中のセラミックスの体積含有率は10〜50%が好ましい。セラミックスの体積含有率が10%を下回ると昇華後の成形体の形状維持製が損なわれて、樹脂を充填処理する際に崩壊する場合がある。また、50%を超えるとセラミックス多孔体の気孔率が小さくなり、樹脂充填後の複合材料の柔軟性が損なわれる。したがって、本発明のセラミックス多孔体と第二成分としての樹脂若しくは金属との複合材料からなる放熱材には、50〜90体積%の樹脂若しくは金属を含有させることができる。 The volume content of ceramics in the slurry is preferably 10 to 50%. If the volume content of the ceramic is less than 10%, the shape-maintaining product of the formed body after sublimation may be damaged, and the ceramic may collapse when the resin is filled. On the other hand, if it exceeds 50%, the porosity of the ceramic porous body becomes small, and the flexibility of the composite material after resin filling is impaired. Therefore, 50-90 volume% resin or metal can be contained in the heat dissipation material which consists of the composite material of the ceramic porous body of this invention and the resin or metal as a 2nd component.
次に工程2について説明する。工程2では、前述のスラリーを一方向から凍結させることで、水成分が凍結方向に平行に凍結し、スラリー中に霜柱状の氷が形成される。具体的には、以下のように行えばよい。例えば、スラリーを注入した容器を低温に保ったアルコールなどの冷媒を収容された溶液槽に底面のみを浸漬し静置する。アルコールとしてはメタノールやエタノールが好ましい。冷却槽の温度は少なくとも水の凝固点以下に保たれている必要がある。またスラリーを入れる容器は、例えば底面を熱伝導性の良い金属で側面を熱伝導性の低い樹脂系材料などで作製する。スラリー容器の上部を解放し大気と接するようにしておくと、調度霜柱が形成されるようにスラリー底部より垂直方向上方に向かって氷の柱が成長する。 Next, step 2 will be described. In step 2, the above-described slurry is frozen from one direction, so that the water component is frozen in parallel with the freezing direction, and frost column-shaped ice is formed in the slurry. Specifically, it may be performed as follows. For example, only the bottom surface is immersed in a solution tank containing a refrigerant such as alcohol in which the container into which the slurry is poured is kept at a low temperature and is allowed to stand. As the alcohol, methanol and ethanol are preferable. The temperature of the cooling tank needs to be kept at least below the freezing point of water. Moreover, the container which puts a slurry is produced, for example with a resin-type material etc. with a low heat conductivity in the side surface with a metal with good heat conductivity. When the upper part of the slurry container is released so as to be in contact with the atmosphere, an ice column grows upward in the vertical direction from the bottom of the slurry so that an adjusted frost column is formed.
工程3では凍結したスラリーを容器ごと減圧下で凍結乾燥を行う。この操作により氷部分を液体(水)を経ないで直接昇華させ、前述の凍結方向にそろった昇華痕として成形体中に孔を形成する。
工程4は得られた成形体の焼成過程である。工程3で形成した成形体を注意深くスラリー容器から抜き取り、それぞれのセラミックスに適した温度および焼結時間で焼成する。焼成温度および時間は緻密化があまり進行しない条件で行うことが好ましい。これにより柱状の氷の昇華痕をマクロ孔とするセラミックス多孔体が作製される。このマクロ孔は前述の昇華痕に準じ、焼結体を一方向に貫通した連続孔となる。また、工程3において、スラリー中には柱状の氷以外に、この柱状の氷の径に比べ極めて径の小さな氷も作られる。この氷も第4の工程において凍結昇華されるために、このマクロ孔の壁面やセラミックス骨格内部にも氷が形成される。その結果、セラミックス骨格内部には微細孔が形成され、比表面積の大きな多孔質体になる。
In step 3, the frozen slurry is freeze-dried together with the container under reduced pressure. By this operation, the ice portion is directly sublimated without passing through the liquid (water), and holes are formed in the molded body as sublimation marks aligned in the above-described freezing direction.
Step 4 is a firing process of the obtained molded body. The formed body formed in step 3 is carefully extracted from the slurry container and fired at a temperature and sintering time suitable for each ceramic. The firing temperature and time are preferably performed under conditions where densification does not proceed much. As a result, a ceramic porous body having columnar ice sublimation marks as macropores is produced. This macro hole is a continuous hole penetrating the sintered body in one direction in accordance with the aforementioned sublimation mark. In step 3, in addition to the columnar ice, ice having an extremely small diameter compared to the columnar ice is also produced in the slurry. Since this ice is also frozen and sublimated in the fourth step, ice is also formed on the wall surface of the macropore and the ceramic skeleton. As a result, fine pores are formed inside the ceramic skeleton, and the porous body has a large specific surface area.
図2に示すように、骨格となるセラミックスのブロック間に隙間としてのマクロ孔(図面垂直方向に貫通する開気孔)が形成される。微細孔は骨格となるセラミックス組織の内部に形成される。前記マクロ孔の大きさは、スラリー調整時の水分量を調整することで制御可能である。また、焼結の温度や時間を調整することで、マクロ孔の大きさの微調整や、微細孔の大きさの調整を行うことも可能である。また、本発明に係る放熱材を図2に示すようなシート形状とする場合には、厚み(マクロ孔と平行な方向の長さ)は50μm〜200μmであることが好ましい。 As shown in FIG. 2, macropores (open pores penetrating in the vertical direction in the drawing) are formed as gaps between ceramic blocks serving as a skeleton. Micropores are formed inside the ceramic structure that serves as the skeleton. The size of the macropores can be controlled by adjusting the amount of water during slurry adjustment. Further, by adjusting the sintering temperature and time, it is possible to finely adjust the size of the macropores and the size of the micropores. Moreover, when making the heat dissipation material which concerns on this invention into a sheet | seat shape as shown in FIG. 2, it is preferable that thickness (length of a direction parallel to a macro hole) is 50 micrometers-200 micrometers.
最後に、セラミックス多孔体中に第二成分としての樹脂または金属を充填することにより本発明の放熱材が得られる。
樹脂の含浸は種々の方法で行うことが可能であるが、多孔質層に含浸させるためには、できるだけ粘性の低い樹脂が好ましい。例えば、紫外線硬化樹脂の内、低粘度の液体状樹脂を含浸させた後、紫外線を照射して硬化させる等の方法がある。
Finally, the heat radiating material of the present invention is obtained by filling the ceramic porous body with a resin or metal as the second component.
The impregnation of the resin can be performed by various methods, but in order to impregnate the porous layer, a resin having a viscosity as low as possible is preferable. For example, after impregnating a low-viscosity liquid resin among ultraviolet curable resins, there is a method of curing by irradiating ultraviolet rays.
紫外線硬化樹脂の中で、硬化後でも柔らかい樹脂を用いることが好ましい、なぜなら、このような放熱シートには、熱源となる部品の形状に対する追従性が要求されるためである。すなわち、柔らかいほど、発熱部品の表面との隙間ができにくく、その隙間に存在する空気による熱輸送の損失が少ない。樹脂の柔らかさは、一般には引っ張り試験時の伸び率が目安になる。樹脂の伸び率としては50%以上が好ましい。例えば、主鎖がポリイソプレンからなり、主鎖の両端にアクリル系二重結合を持つウレタナンアクリレート系樹脂などがある。そのほかの樹脂でももちろんかまわない。 Among the ultraviolet curable resins, it is preferable to use a soft resin even after curing, because such a heat-dissipating sheet is required to follow the shape of a part that becomes a heat source. That is, the softer the harder is the gap with the surface of the heat-generating component, and the less the heat transport loss due to the air present in the gap. The softness of the resin is generally based on the elongation rate during the tensile test. The elongation percentage of the resin is preferably 50% or more. For example, there is a uretanane acrylate resin having a main chain made of polyisoprene and acrylic double bonds at both ends of the main chain. Of course, other resins may be used.
本発明に係る放熱材に使用されるセラミックス多孔体は、放熱するのと平行な方向に貫通したマクロ孔が配向している。さらに、該マクロ孔に、第二成分としての樹脂が充填して連続相を形成しており、さらには、ミクロ孔にも適度な量の樹脂が含浸されて、マクロ孔に含浸された樹脂の柱同士を互いに、適度な強さで結合させている。このため、樹脂の柱の長さ方向と垂直の方向に外力が加わった場合に(シート形状の場合は、シートの面内方向の加重)、樹脂柱とセラミックス部の界面で剥離が生じて、材料が破壊される現象を防止することができる。このような理由により、曲げ等の柔軟性に優れるという特徴を有し、発熱部材に隙間なく貼り付ける事が可能となる。また、マクロ孔に含浸された樹脂は、セラミックス部の放熱性を増大させる効果もある。
これに対して、通常のセラミックス多孔質体は三次元的に連結した構造になっているため、変形しにくく、複合材料とした場合に引っ張り伸び率が小さくなる。
In the ceramic porous body used for the heat dissipating material according to the present invention, the macro holes penetrating in the direction parallel to the heat dissipating are oriented. Furthermore, the macropores are filled with a resin as the second component to form a continuous phase. Further, an appropriate amount of resin is impregnated into the micropores, so that the macropores The columns are joined together with moderate strength. For this reason, when an external force is applied in the direction perpendicular to the length direction of the resin column (in the case of a sheet, the load in the in-plane direction of the sheet), peeling occurs at the interface between the resin column and the ceramic part, The phenomenon that the material is destroyed can be prevented. For this reason, it has a feature of excellent flexibility such as bending, and can be attached to the heat generating member without any gap. Further, the resin impregnated in the macropores has an effect of increasing the heat dissipation of the ceramic portion.
On the other hand, since a normal ceramic porous body has a three-dimensionally connected structure, it is difficult to be deformed, and the tensile elongation is reduced when a composite material is used.
樹脂を充填する場合、例えば図2に示すように、平板状のセラミックス多孔体の一面からのみ樹脂を含浸させることが望ましい。なぜなら、セラミックス多孔体の多くの面から含浸させると、含浸後に複合材料周囲の樹脂を除去する処理が加わり加工費が大きくなるためである。一面からのみ含浸する場合は、上面のみを研削等で除去できるので容易であり、また、予めセラミックス多孔体中に含浸される樹脂量を計算しておけば、余分な樹脂を用意する必要もなくなる場合もある。 When the resin is filled, for example, as shown in FIG. 2, it is desirable to impregnate the resin only from one surface of the flat plate-shaped ceramic porous body. This is because impregnation from many surfaces of the ceramic porous body adds processing for removing the resin around the composite material after impregnation and increases the processing cost. When impregnating only from one surface, it is easy because only the upper surface can be removed by grinding or the like, and if the amount of resin impregnated in the ceramic porous body is calculated in advance, it is not necessary to prepare extra resin. In some cases.
配向したマクロ孔を持つセラミックス多孔体の場合、液体状の樹脂は、まずマクロ孔に沿って含浸が進行する。マクロ孔への含浸が進行しながら、同時に、マクロ孔同士を繋いでいるミクロ孔にも含浸される。ミクロ孔の内、細孔径が小さすぎる細孔には樹脂の含浸が起こらないため、好ましくない。 In the case of a ceramic porous body having oriented macropores, the liquid resin is first impregnated along the macropores. While the macropores are being impregnated, the micropores connecting the macropores are simultaneously impregnated. Of the micropores, pores having too small pore diameters are not preferred because resin impregnation does not occur.
樹脂を充填させる前のセラミックス多孔体の作製において、スラリー全体を冷却してしまうと容器側面からの伝熱による氷の成長が起こる可能性があるために好ましくない。すなわち、一方向でなく、ランダムな方向にマクロ孔が形成された成形体となり、この構造が焼結体にそのまま反映される。このような構造の多孔体では、樹脂を十分に含浸させることができない。 In the production of the ceramic porous body before filling with the resin, it is not preferable that the whole slurry is cooled because ice may grow due to heat transfer from the side surface of the container. That is, it becomes a molded body in which macropores are formed not in one direction but in random directions, and this structure is reflected in the sintered body as it is. The porous body having such a structure cannot be sufficiently impregnated with resin.
本製法により作製されるセラミックス多孔体の細孔径は、使用する原料粉末のサイズにより制御することができる。一般的にはマクロ孔の直径は5〜100μm程度である。ミクロ孔の直径は0.1〜5μm程度である。マクロ孔には樹脂はほぼ完全に含浸される。直径が1μm以下のミクロ孔には樹脂は含浸されにくい傾向がある。 The pore diameter of the ceramic porous body produced by this production method can be controlled by the size of the raw material powder used. In general, the diameter of the macropore is about 5 to 100 μm. The diameter of the micropore is about 0.1 to 5 μm. The macropores are almost completely impregnated with the resin. Micropores having a diameter of 1 μm or less tend not to be impregnated with resin.
本発明は、セラミックスと樹脂の複合材料のみに限らず、金属と樹脂の複合材料の製造にも用いることができる。金属としては、例えば、Cu単体、Ag単体等が好ましく用いることができるが、金属とセラミックスとの濡れ性を考慮するとTi入りの金属であることがより好ましい。Ti合金を使用し、セラミックスとの濡れ性が充分に高い場合には、溶融金属をセラミックスに含浸させる際に加圧する必要がなくなる。
また、含浸する樹脂として、柔軟で引っ張り伸び率の大きい樹脂を用いると、粘着層を用いずに発熱源に直接貼り付けることもできる。
The present invention can be used not only for the composite material of ceramics and resin, but also for the production of composite materials of metal and resin. As the metal, for example, Cu alone, Ag alone or the like can be preferably used, but considering the wettability between the metal and ceramic, a metal containing Ti is more preferable. When a Ti alloy is used and wettability with ceramics is sufficiently high, it is not necessary to apply pressure when impregnating the molten metal into the ceramics.
Further, when a resin that is flexible and has a high tensile elongation is used as the resin to be impregnated, the resin can be directly attached to the heat source without using the adhesive layer.
(実施例1)
<セラミックス多孔体の合成>
セラミック原料粉末としての各種平均粒径のZnO、Al2O3、AlN粉末、蒸留水を粉末の体積比が80〜60vol%となるように混合した。この混合粉末を10時間ボールミル混合した後、得られたスラリーを真空脱泡装置に入れ攪拌しながらスラリー中に存在する泡を除去した。
各スラリーを、図3に示す直径40mmに設計した分解式容器に流し込んだ。エタノールの温度を−50℃に設定してCu部のみが浸るように静かに浸漬し、およそ60分間保持し、スラリーを完全に凍らせた。このスラリー容器を取り出しアルコール分を良くふき取って真空凍結乾燥機に入れた。約20hr乾燥した後、成形体を容器から注意深く抜き出し、各種雰囲気、各種焼結温度で2時間焼結を行った。
(Example 1)
<Synthesis of porous ceramics>
ZnO, Al 2 O 3 , AlN powder and distilled water having various average particle diameters as ceramic raw material powder were mixed so that the volume ratio of the powder was 80-60 vol%. After this mixed powder was ball mill mixed for 10 hours, the resulting slurry was placed in a vacuum defoamer and the bubbles present in the slurry were removed while stirring.
Each slurry was poured into a decomposable container designed to have a diameter of 40 mm shown in FIG. The ethanol temperature was set to −50 ° C. and gently immersed so that only the Cu portion was immersed, and held for about 60 minutes to completely freeze the slurry. The slurry container was taken out and the alcohol content was thoroughly wiped off and placed in a vacuum freeze dryer. After drying for about 20 hours, the compact was carefully extracted from the container and sintered for 2 hours in various atmospheres and various sintering temperatures.
<樹脂の含浸>
樹脂として昭和高分子製のビニルエステル樹脂:商品名:リポキシPH−300Aを用いた。この樹脂に樹脂の1wt%の重合開始剤(IRGACRE184:チバ・スペシャルティ・ケミカルズ製)を添加、攪拌後、上記各種セラミックス多孔体表面に滴下した。これを真空オーブンに入れ、ロータリーポンプで真空にしながら室温で樹脂を含浸させた。
<Resin impregnation>
As the resin, Showa High Polymer vinyl ester resin: Trade name: Lipoxy PH-300A was used. A 1 wt% polymerization initiator (IRGACRE 184: manufactured by Ciba Specialty Chemicals) of the resin was added to this resin, stirred, and then dropped onto the surface of the above various ceramic porous bodies. This was placed in a vacuum oven and impregnated with resin at room temperature while being evacuated with a rotary pump.
<樹脂の硬化>
その後、樹脂が含浸したセラミックス基板に波長が365nmの紫外線を50mW/cm2の光強度で照射して樹脂を硬化させた。
<熱伝導率測定>
樹脂含浸後の試料を、直径10mmに加工し、レーザーフラッシュ式熱伝導率測定装置により熱伝導率を測定した。引張試験片にも加工し、引張伸び率を測定した。
<Curing of resin>
Thereafter, the resin was cured by irradiating the ceramic substrate impregnated with the resin with ultraviolet light having a wavelength of 365 nm at a light intensity of 50 mW / cm 2 .
<Measurement of thermal conductivity>
The resin-impregnated sample was processed into a diameter of 10 mm, and the thermal conductivity was measured with a laser flash type thermal conductivity measuring device. Tensile specimens were also processed and the tensile elongation was measured.
比較として、平均粒径8.6μmのZnO粉末をプレス成形して成形体を作製し、温度800℃で2hr大気中で焼結させて、気孔率が50%の多孔体を作製した。これに、同様の方法で樹脂を含浸して複合材料とし、熱伝導率と引張伸び率を測定した。 As a comparison, a ZnO powder having an average particle size of 8.6 μm was press-molded to produce a compact, and sintered in the atmosphere at a temperature of 800 ° C. for 2 hours to prepare a porous body having a porosity of 50%. This was impregnated with a resin in the same manner to obtain a composite material, and the thermal conductivity and tensile elongation were measured.
結果を表1に示す。
本発明のセラミックス−樹脂複合材料層は高い熱伝導率と引張伸び率を示す。
比較品の引っ張り伸び率が小さいのは、樹脂が十分に含浸されなかったためと考えられる。
The results are shown in Table 1.
The ceramic-resin composite material layer of the present invention exhibits high thermal conductivity and tensile elongation.
The reason why the tensile elongation rate of the comparative product is small is considered that the resin was not sufficiently impregnated.
(実施例2)
<セラミックス多孔体の合成>
実施例1のものを用いた。
<金属の含浸>
純度99.9%の71wt%Cu−28wt%Ag−1wt%Ti合金のバルク体をセラミックス多孔体の上に乗せ、これを真空炉に入れ、900℃で2h加熱して溶融金属を含浸させた。
<熱伝導率測定>
樹脂含浸後の試料を、直径10mmに加工し、レーザーフラッシュ式熱伝導率測定装置により熱伝導率を測定した。
(Example 2)
<Synthesis of porous ceramics>
The one of Example 1 was used.
<Metal impregnation>
A bulk body of 71 wt% Cu-28 wt% Ag-1 wt% Ti alloy having a purity of 99.9% was placed on a ceramic porous body, placed in a vacuum furnace, and heated at 900 ° C. for 2 hours to impregnate the molten metal. .
<Measurement of thermal conductivity>
The resin-impregnated sample was processed into a diameter of 10 mm, and the thermal conductivity was measured with a laser flash type thermal conductivity measuring device.
比較として、平均粒径8.6μmのZnO粉末をプレス成形して成形体を作製し、温度800℃で2hr大気中で焼結させて、気孔率が50%の多孔体を作製した。これに、同様の方法で樹脂を含浸して複合材料とし、熱伝導率を測定した。
結果を表2に示す。
本発明のセラミックス−金属複合材料は高い熱伝導率を示す。
As a comparison, a ZnO powder having an average particle size of 8.6 μm was press-molded to produce a compact, and sintered in the atmosphere at a temperature of 800 ° C. for 2 hours to prepare a porous body having a porosity of 50%. This was impregnated with a resin in the same manner to obtain a composite material, and the thermal conductivity was measured.
The results are shown in Table 2.
The ceramic-metal composite material of the present invention exhibits high thermal conductivity.
Claims (10)
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Cited By (3)
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|---|---|---|---|---|
| EP2650914A3 (en) * | 2012-04-12 | 2014-05-14 | Chin Huan Ni | Heat dissipation module with multiple porosities |
| JP2017524240A (en) * | 2014-05-21 | 2017-08-24 | カデンツァ イノベーション,インコーポレイテッド | Lithium-ion battery with thermal runaway protection |
| CN113387719A (en) * | 2021-05-31 | 2021-09-14 | 安徽鼎元新材料有限公司 | Multilayer-structure anti-corrosion thermal insulation material and preparation method thereof |
-
2007
- 2007-01-09 JP JP2007001448A patent/JP2008169245A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2650914A3 (en) * | 2012-04-12 | 2014-05-14 | Chin Huan Ni | Heat dissipation module with multiple porosities |
| JP2017524240A (en) * | 2014-05-21 | 2017-08-24 | カデンツァ イノベーション,インコーポレイテッド | Lithium-ion battery with thermal runaway protection |
| US10651521B2 (en) | 2014-05-21 | 2020-05-12 | Cadenza Innovation, Inc. | Lithium ion battery with thermal runaway protection |
| CN113387719A (en) * | 2021-05-31 | 2021-09-14 | 安徽鼎元新材料有限公司 | Multilayer-structure anti-corrosion thermal insulation material and preparation method thereof |
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