CN107553996A - A kind of heat-conductive composite material of multilayer fibre reinforced and preparation method thereof - Google Patents

A kind of heat-conductive composite material of multilayer fibre reinforced and preparation method thereof Download PDF

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CN107553996A
CN107553996A CN201610517225.3A CN201610517225A CN107553996A CN 107553996 A CN107553996 A CN 107553996A CN 201610517225 A CN201610517225 A CN 201610517225A CN 107553996 A CN107553996 A CN 107553996A
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heat
composite material
fibre reinforced
conductive composite
multilayer
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张娜
朱月华
王海波
蒋利华
卓宁泽
何清洋
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Nanjing Tech University
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Nanjing Tech University
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Abstract

The invention discloses a kind of heat-conductive composite material of multilayer fibre reinforced and preparation method thereof, the heat-conductive composite material of the multilayer fibre reinforced is made up of semi-solid preparation thermal conductive adhesive composition and multilayer carbon fibre reinforcement, the number of plies of multilayer carbon fiber is more than 2 layers, semi-solid preparation thermal conductive adhesive composition is by epoxy resin, curing agent, heat filling, anti-current glue filler and dispersant composition, the mass ratio of epoxy resin and curing agent is 100: 10~100, the mass fraction of heat filling is 10~50, the mass fraction of anti-current glue filler is 10~30, the mass fraction of dispersant is 1~5.The heat-conductive composite material of the present invention uses multilayer carbon fibre reinforced cloth, in addition to as forming skeleton, also advantageously improves heat conductivility;Natural graphite flakes are aligned, not only increase the thermal conductivity of heat-conductive composite material, while also reduce production cost, of the invention method is simple, is applicable to manufacture on a large scale.

Description

A kind of heat-conductive composite material of multilayer fibre reinforced and preparation method thereof
Technical field
The present invention relates to a kind of heat-conductive composite material of multilayer fibre reinforced and preparation method thereof, refer in particular to it is a kind of have lead Heat-conductive composite material of heat and adhesive property and preparation method thereof.
Background technology
Heat dissipation problem turns into the bottleneck for limiting numerous industry developments.Especially as integrated technology in electronics industry and assembling skill The continuous renewal development of art, electronic component and electronic equipment small, integrated and densification, working frequency are anxious Increase severely plus, now heat caused by electronic equipment accumulates rapidly, at a temperature of use environment, for ensure electronic component it is long when Between high reliability normal work, propose higher and higher requirement for the heat conductivility of adhesive for playing cementation.
Epoxy resin is the macromolecule matrix for being commonly used for heat conduction stick, and it has excellent physical and mechanical properties and caking property Can, while solidification temperature scope is wide, crosslink density is easily controllable, and solidification process does not produce small molecule by-product, thus shrinkage factor It is low.But epoxy resin still has its weak point while many excellent properties be present, as thermal conductivity factor is low, only 0.2W/ Mk, heat conductivility is poor, greatly limit its application in high-tech sector.Significantly improve leading for adhesive Hot, main path is exactly the filling heat conduction component into polymer, and such as patent CN 102719210A, to describe a kind of ultralow temperature exhausted Edge heat conduction adhesive, heat filling are made up of metal powder and nonmetallic heat conductive powder, and the thermal conductive adhesive thermal conductivity factor of preparation is Improve, but be no more than 1W/mk, and also add the weight of heat-conducting glue, being not suitable for Aeronautics and Astronautics etc. has special want to weight The field asked uses.Patent CN201110346213.6 describes a kind of BN as heat filling, the epoxy half of glass-fiber-fabric enhancing Cured sheets and its manufacture method, thermal conductivity factor can reach 3.5W/mk, be the thermally conductive sheets of individual layer glass-fiber-fabric enhancing, in microwave tube In use, heat conductivility can't reach requirement on constant power pipe.
The unique sheet crystal structure of natural flake graphite, the characteristics of causing its heat conductivility that anisotropy is presented, i.e., High-termal conductivity along graphite flake layer direction and the low heat conductivity perpendicular to graphite flake layer direction.In its face thermal conductivity 140~ 500W/mk, and interlayer direction thermal conductivity is only 3~10W/mk or so.
Asphalt base carbon fiber is a kind of using coal asphalt or petroleum asphalt as special type of the phosphorus content made of raw material more than 92% Fiber, there is the excellent combination property such as high intensity, high-modulus, high heat conduction, corrosion-resistant, can be widely applied to Aero-Space, state The fields such as anti-, industry.The heat conductivility of asphalt base carbon fiber is very excellent, and thermal conductivity is in 100~1000W/mk, even more It is high.Japanese Unexamined Patent Publication 2010-53224 data describes one kind fibre reinforced, BN, Al2O3Epoxy half as heat filling is solid 5.0W/mk can be arrived by changing piece and its manufacture method, thermal conductivity factor.
The content of the invention
It is high it is an object of the invention to overcome the deficiencies of the prior art and provide a kind of thermal conductivity factor, while have excellent The heat-conductive composite material of stick performance, the heat-conductive composite material is by semi-solid preparation thermal conductive adhesive composition and multilayer fibre reinforced Material forms, and the number of plies of multilayer carbon fiber is more than 2 layers, and semi-solid preparation thermal conductive adhesive composition is by epoxy resin, curing agent, heat conduction The mass ratio of filler, anti-current glue filler and dispersant composition, epoxy resin and curing agent is 100: 10~100, heat filling Mass fraction be 10~50, the mass fraction of anti-current glue filler is 10~30, and the mass fraction of dispersant is 1~5.
Described carbon fibre reinforcement is asphalt base carbon fiber, is to spin asphalt or coal tar asphalt through melting Silk, solidification, carbonization and other processes, finally made of 1600 DEG C~3000 DEG C high-temperature process and graphitization, a diameter of the 5 of carbon fiber ~10um, the length of carbon fiber is 20~25mm.
Described heat filling is natural flake graphite, and thermal conductivity is about 60~220W/mk, material diameter scope is 0.15~ 0.55mm。
Described anti-current glue filler is one or both of kaolin and preparing spherical SiO 2 mixture, and particle size range is 1~3um.
Described dispersant is anionic dispersing agents.
Described epoxy resin is in liquid bisphenol A types epoxy resin, solid-state bisphenol A type epoxy resin fat, phenolic resin One or two mixing, curing agent are the mixing of one or both of organoborane amine, dicyandiamide, modified anhydride.
It is a further object to provide a kind of preparation method of the heat-conductive composite material of multilayer fibre reinforced, bag Include following steps:
(1) preparation of carbon fibre reinforced cloth:By 80~90g/m2Carbon fiber is weighed, with the multiple washing and filtering of 95% alcohol And 60 DEG C of drying in vacuum drying chamber, copied with short net tilting wet method and network structure is made, be immersed in water miscible phenolic aldehyde ring In the binding agent of oxygen tree fat and Polyamine Type curing agent composition, after 120 DEG C predrying, then under 180 DEG C, 10~15MPa pressure Compacting 5~10 seconds, handled 3 minutes at 150 DEG C afterwards, carbon fibre reinforced cloth is made;
(2) preparation of semi-solid preparation thermal conductive adhesive mixture:Epoxy resin and curing agent are weighed in proportion, after stirring Heat filling, anti-current jelly and dispersant are added, is again stirring for after being well mixed, carries out vacuum defoamation;
(3) preparation of the heat-conductive composite material of multilayer fibre reinforced:One layer of demoulding is sprayed in the mould bottom surface customized Agent, the thick semi-solid preparation thermal conductive adhesive mixtures of one layer of 0.1~0.4mm are poured into, with orientation compression roll along parallel to mould base The direction extruding adhesive mixture at bottom, makes graphite flakes be arranged parallel to the direction of mold base, then after extrusion mixed Laminate spreads one layer of carbon fibre reinforced cloth prepared, and it is gluing then to pour into the thick semi-solid preparation heat conduction of one layer of 0.1~0.4mm again Agent composition, the step of repetition above, after the completion of last layer of semi-solid preparation thermal conductive adhesive mixture is suppressed, in 100~180 DEG C dry 2~4 hours, that is, the heat-conductive composite material of multilayer fibre reinforced is made;
(4) cutting and use of heat-conductive composite material:The plane aligned perpendicular to graphite, carried out by the width used Cutting, the heat-conductive composite material needed is made, in use, being put by graphite flake in heat-conductive composite material perpendicular to the direction of bonding plane Put among two bonding planes, at 150~210 DEG C, heating 30~120min solidifications.
The excellent effect of the present invention is:
Using multilayer carbon fibre reinforced cloth, in addition to as heat-conductive composite material forming skeleton, can also further improve Heat conductivility;Natural graphite flakes are aligned, while effectively solving device heat dissipation problem, also reduces and is produced into This, of the invention method is simple, is applicable to manufacture on a large scale.
Brief description of the drawings:
Fig. 1 is a kind of preparation flow figure of the heat-conductive composite material of multilayer fibre reinforced.
Fig. 2 is a kind of heat-conductive composite material structural representation of multilayer fibre reinforced, wherein 1 is multilayer fibre reinforced Heat-conductive composite material, 11 be semi-solid preparation thermal conductive adhesive composition, and 12 be carbon fibre reinforced cloth, and 2 be anti-current glue filler, and 3 are Epoxy resin cure sizing material, 4 be crystalline flake graphite, and 5 be the mould for scribbling remover, and 6 be orientation compression roll.
Fig. 3 is that a kind of heat-conductive composite material of multilayer fibre reinforced uses schematic diagram, wherein 1 is multilayer fibre reinforced Heat-conductive composite material, 2 for bonding matrix.
Embodiment
Epoxy resin involved in the present invention, curing agent, dispersant are bought from Wuxi Ren Ze chemical products Co., Ltd, Crystalline flake graphite purchase is limited from the source carbon graphite material of Shenzhen's crystalline substance from Qingdao Jin Tao graphite Co., Ltd, carbon fibre material purchase Company, anti-current glue filler are bought from Chemical Reagent Co., Ltd., Sinopharm Group.
The invention will be further described with reference to embodiments, but the implementation of the present invention is not limited to this.
Embodiment 1
(1) preparation of carbon fibre reinforced cloth:By 80g/m2Weigh carbon fiber, with the multiple washing and filtering of 95% alcohol and 60 DEG C of drying, are copied with short net tilting wet method and network structure are made, be immersed in water miscible epoxy novolac tree in vacuum drying chamber In the binding agent of fat and Polyamine Type curing agent composition, after 120 DEG C predrying, then suppressed 10 seconds under 180 DEG C, 10MPa pressure Clock, handled 3 minutes at 150 DEG C afterwards, carbon fibre reinforced cloth is made;
(2) preparation of semi-solid preparation thermal conductive adhesive mixture:Weigh 40g liquid bisphenols A types epoxy resin and 4g organic borons Amine hardener, 5g 0.55mm 3 μm of natural flake graphite, 5g kaolin and 0.6g dispersants are stirring evenly and then adding into, then It is secondary be uniformly mixed after, carry out vacuum defoamation;
(3) preparation of the heat-conductive composite material of multilayer fibre reinforced:One layer of demoulding is sprayed in the mould bottom surface customized Agent, the thick semi-solid preparation thermal conductive adhesive mixtures of one layer of 0.4mm are poured into, adhesive is extruded along the direction parallel to mold base Mixture, one layer of carbon fibre reinforced cloth prepared is then spread above mixture after extrusion, then pours into one layer of 0.4mm again Thick semi-solid preparation thermal conductive adhesive mixture, the step of repetition above, in last layer of semi-solid preparation thermal conductive adhesive mixture pressure After the completion of system, dried in 140 DEG C 3 hours, that is, the heat-conductive composite material of multilayer fibre reinforced is made;
(4) cutting and use of heat-conductive composite material:The plane aligned perpendicular to graphite, carried out by the width used Cutting, the heat-conductive composite material needed is made, in use, by graphite flake in thermally conductive sheet composite perpendicular to the direction of bonding plane It is placed among two bonding planes, at 180 DEG C, heating 90min solidifications.
Embodiment 2
(1) preparation of carbon fibre reinforced cloth:By 90g/m2Weigh carbon fiber, with the multiple washing and filtering of 95% alcohol and 60 DEG C of drying, are copied with short net tilting wet method and network structure are made, be immersed in water miscible epoxy novolac tree in vacuum drying chamber In the binding agent of fat and Polyamine Type curing agent composition, after 120 DEG C predrying, then suppressed 5 seconds under 180 DEG C, 15MPa pressure Clock, handled 3 minutes at 150 DEG C afterwards, carbon fibre reinforced cloth is made;
(2) preparation of semi-solid preparation thermal conductive adhesive mixture:Weigh 20g liquid bisphenol A types epoxy resin, 20g Solid Doubles Phenol A types epoxy resin and 40g modified anhydride curing agent, are stirring evenly and then adding into 3 μm of 20g 0.55mm natural flake graphites, 8g Silica and 2g dispersants, be again stirring for it is well mixed after, carry out vacuum defoamation;
(3) preparation of the heat-conductive composite material of multilayer fibre reinforced:One layer of demoulding is sprayed in the mould bottom surface customized Agent, the thick semi-solid preparation thermal conductive adhesive mixtures of one layer of 0.3mm are poured into, adhesive is extruded along the direction parallel to mold base Mixture, one layer of carbon fibre reinforced cloth prepared is then spread above mixture after extrusion, then pours into one layer of 0.3mm again Thick semi-solid preparation thermal conductive adhesive mixture, the step of repetition above, in last layer of semi-solid preparation thermal conductive adhesive mixture pressure After the completion of system, dried in 100 DEG C 2 hours, that is, the heat-conductive composite material of multilayer fibre reinforced is made;
(4) cutting and use of heat-conductive composite material:The plane aligned perpendicular to graphite, carried out by the width used Cutting, the heat-conductive composite material needed is made, in use, being put by graphite flake in heat-conductive composite material perpendicular to the direction of bonding plane Put among two bonding planes, at 150 DEG C, heating 120min solidifications.
Embodiment 3
(1) preparation of carbon fibre reinforced cloth:By 85g/m2Weigh carbon fiber, with the multiple washing and filtering of 95% alcohol and 60 DEG C of drying, are copied with short net tilting wet method and network structure are made, be immersed in water miscible epoxy novolac tree in vacuum drying chamber In the binding agent of fat and Polyamine Type curing agent composition, after 120 DEG C predrying, then suppressed 8 seconds under 180 DEG C, 12MPa pressure Clock, handled 3 minutes at 150 DEG C afterwards, carbon fibre reinforced cloth is made;
(2) preparation of semi-solid preparation thermal conductive adhesive mixture:Weigh 30g liquid bisphenol A types epoxy resin, 10g phenolic aldehyde rings Oxygen tree fat and 4g dicy-curing agents, be stirring evenly and then adding into 10g 0.15mm natural flake graphites, 1 μm of 4g kaolin and 1g dispersants, it is again stirring for after being well mixed, carries out vacuum defoamation;
(3) preparation of the heat-conductive composite material of multilayer fibre reinforced:One layer of demoulding is sprayed in the mould bottom surface customized Agent, the thick semi-solid preparation thermal conductive adhesive mixtures of one layer of 0.1mm are poured into, adhesive is extruded along the direction parallel to mold base Mixture, one layer of carbon fibre reinforced cloth prepared is then spread above mixture after extrusion, then pours into one layer of 0.1mm again Thick semi-solid preparation thermal conductive adhesive mixture, the step of repetition above, in last layer of semi-solid preparation thermal conductive adhesive mixture pressure After the completion of system, dried in 180 DEG C 4 hours, that is, the heat-conductive composite material of multilayer fibre reinforced is made;
(4) cutting and use of heat-conductive composite material:The plane aligned perpendicular to graphite, carried out by the width used Cutting, the heat-conductive composite material needed is made, in use, being put by graphite flake in heat-conductive composite material perpendicular to the direction of bonding plane Put among two bonding planes, at 210 DEG C, heating 30min solidifications.
Embodiment 4
(1) preparation of carbon fibre reinforced cloth:By 80g/m2Weigh carbon fiber, with the multiple washing and filtering of 95% alcohol and 60 DEG C of drying, are copied with short net tilting wet method and network structure are made, be immersed in water miscible epoxy novolac tree in vacuum drying chamber In the binding agent of fat and Polyamine Type curing agent composition, after 120 DEG C predrying, then suppressed 10 seconds under 180 DEG C, 15MPa pressure Clock, handled 3 minutes at 150 DEG C afterwards, carbon fibre reinforced cloth is made;
(2) preparation of semi-solid preparation thermal conductive adhesive mixture:Weigh 30g liquid bisphenol A types epoxy resin, 10g Solid Doubles Phenol A types epoxy resin and 20g modified anhydrides, 3g dicy-curing agents, it is stirring evenly and then adding into the natural scale stones of 15g 0.25mm Ink, 12g1 μm of silica and 0.4g dispersants, it is again stirring for after being well mixed, carries out vacuum defoamation;
(3) preparation of the heat-conductive composite material of multilayer fibre reinforced:One layer of demoulding is sprayed in the mould bottom surface customized Agent, the thick semi-solid preparation thermal conductive adhesive mixtures of one layer of 0.2mm are poured into, adhesive is extruded along the direction parallel to mold base Mixture, one layer of carbon fibre reinforced cloth prepared is then spread above mixture after extrusion, then pours into one layer of 0.2mm again Thick semi-solid preparation thermal conductive adhesive mixture, the step of repetition above, in last layer of semi-solid preparation thermal conductive adhesive mixture pressure After the completion of system, dried in 150 DEG C 2 hours, that is, the heat-conductive composite material of multilayer fibre reinforced is made;
(4) cutting and use of heat-conductive composite material:The plane aligned perpendicular to graphite, carried out by the width used Cutting, the heat-conductive composite material needed is made, in use, being put by graphite flake in heat-conductive composite material perpendicular to the direction of bonding plane Put among two bonding planes, at 180 DEG C, heating 60min solidifications.
Embodiment 5
(1) preparation of carbon fibre reinforced cloth:By 88g/m2Weigh carbon fiber, with the multiple washing and filtering of 95% alcohol and 60 DEG C of drying, are copied with short net tilting wet method and network structure are made, be immersed in water miscible epoxy novolac tree in vacuum drying chamber In the binding agent of fat and Polyamine Type curing agent composition, after 120 DEG C predrying, then suppressed 6 seconds under 180 DEG C, 13MPa pressure Clock, handled 3 minutes at 150 DEG C afterwards, carbon fibre reinforced cloth is made;
(2) preparation of semi-solid preparation thermal conductive adhesive mixture:Weigh 20g liquid bisphenol A types epoxy resin, 20g phenolic aldehyde rings Oxygen tree fat and 3g organoborane amines, 2g dicyandiamide agents, it is stirring evenly and then adding into 10g 0.40mm natural flake graphites, 2 μm of 8g Silica and 0.4g dispersants, it is again stirring for after being well mixed, carries out vacuum defoamation;
(3) preparation of the heat-conductive composite material of multilayer fibre reinforced:One layer of demoulding is sprayed in the mould bottom surface customized Agent, the thick semi-solid preparation thermal conductive adhesive mixtures of one layer of 0.3mm are poured into, adhesive is extruded along the direction parallel to mold base Mixture, one layer of carbon fibre reinforced cloth prepared is then spread above mixture after extrusion, then pours into one layer of 0.3mm again Thick semi-solid preparation thermal conductive adhesive mixture, the step of repetition above, in last layer of semi-solid preparation thermal conductive adhesive mixture pressure After the completion of system, dried in 170 DEG C 3 hours, that is, the heat-conductive composite material of multilayer fibre reinforced is made;
(4) cutting and use of heat-conductive composite material:The plane aligned perpendicular to graphite, carried out by the width used Cutting, the heat-conductive composite material needed is made, in use, being put by graphite flake in heat-conductive composite material perpendicular to the direction of bonding plane Put among two bonding planes, at 200 DEG C, heating 60min solidifications.

Claims (7)

1. a kind of heat-conductive composite material of multilayer fibre reinforced, it is characterised in that described heat-conductive composite material is by semi-solid preparation Thermal conductive adhesive composition and multilayer carbon fibre reinforcement composition, the number of plies of multilayer carbon fiber are more than 2 layers, semi-solid preparation heat-conducting glue Adhesive composition is made up of epoxy resin, curing agent, heat filling, anti-current glue filler and dispersant, epoxy resin and solidification The mass ratio of agent is 100: 10~100, and the mass fraction of heat filling is 10~50, the mass fraction of anti-current glue filler for 10~ 30, the mass fraction of dispersant is 1~5.
A kind of 2. heat-conductive composite material of multilayer fibre reinforced according to claim 1, it is characterised in that described carbon Fibre reinforced materials is asphalt base carbon fiber, is through works such as melt spinning, solidification, carbonizations by asphalt or coal tar asphalt Sequence, finally made of 1600 DEG C~3000 DEG C high-temperature process and graphitization, a diameter of 5~10um of carbon fiber, carbon fiber Length is 20~25mm.
3. the heat-conductive composite material of a kind of multilayer fibre reinforced according to claim 1, it is characterised in that described leads Hot filler is natural flake graphite, and thermal conductivity is about 60~220W/mk, and particle size range is 0.15~0.55mm.
4. the heat-conductive composite material of a kind of multilayer fibre reinforced according to claim 1, it is characterised in that described is anti- Gummosis filler is one or both of kaolin and preparing spherical SiO 2 mixture, and particle size range is 1~3um.
A kind of 5. heat-conductive composite material of multilayer fibre reinforced according to claim 1, it is characterised in that described point Powder is anionic dispersing agents.
A kind of 6. heat-conductive composite material of multilayer fibre reinforced according to claim 1, it is characterised in that described ring Oxygen tree fat is the mixing of one or both of liquid bisphenol A types epoxy resin, solid-state bisphenol A type epoxy resin fat, phenolic resin, Gu Agent is the mixing of one or both of organoborane amine, dicyandiamide, modified anhydride.
7. a kind of heat-conductive composite material of multilayer fibre reinforced, it is characterised in that described preparation method is according to the following steps Carry out:
(1) preparation of carbon fibre reinforced cloth:By 80~90g/m2Weigh carbon fiber, with the multiple washing and filtering of 95% alcohol and 60 DEG C of drying, are copied with short net tilting wet method and network structure are made, be immersed in water miscible epoxy novolac tree in vacuum drying chamber In the binding agent of fat and Polyamine Type curing agent composition, after 120 DEG C predrying, then 5 are suppressed under 180 DEG C, 10~15MPa pressure ~10 seconds, handled 3 minutes at 150 DEG C afterwards, carbon fibre reinforced cloth is made;
(2) preparation of semi-solid preparation thermal conductive adhesive mixture:Epoxy resin and curing agent are weighed in proportion, are stirring evenly and then adding into Heat filling, anti-current jelly and dispersant, it is again stirring for after being well mixed, carries out vacuum defoamation;
(3) preparation of the heat-conductive composite material of multilayer fibre reinforced:One layer of releasing agent is sprayed in the mould bottom surface customized, is fallen Enter the thick semi-solid preparation thermal conductive adhesive mixture of one layer of 0.1~0.4mm, with orientation compression roll along the side parallel to mold base To extruding adhesive mixture, graphite flakes are made to be arranged parallel to the direction of mold base, then on mixture after extrusion Face spreads one layer of carbon fibre reinforced cloth prepared, then pours into the thick semi-solid preparation thermal conductive adhesive mixing of one layer of 0.1~0.4mm again Thing, the step of repetition above, after the completion of last layer of semi-solid preparation thermal conductive adhesive mixture is suppressed, dry 2 in 100~180 DEG C ~4 hours, that is, the heat-conductive composite material of multilayer fibre reinforced is made.
(4) cutting and use of heat-conductive composite material:The plane aligned perpendicular to graphite, is cut by the width used Cut, the heat-conductive composite material needed is made, in use, being placed by graphite flake in heat-conductive composite material perpendicular to the direction of bonding plane Among two bonding planes, at 150~210 DEG C, heating 30~120min solidifications.
CN201610517225.3A 2016-07-01 2016-07-01 A kind of heat-conductive composite material of multilayer fibre reinforced and preparation method thereof Pending CN107553996A (en)

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CN108439983A (en) * 2018-04-16 2018-08-24 三峡大学 A kind of graphite ceramic compound pipe molding method
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CN113444499A (en) * 2021-06-25 2021-09-28 深圳市三科斯电子材料有限公司 Double-sided adhesive high-thermal-conductivity synthetic graphite flake and preparation method thereof
CN115416376A (en) * 2022-09-29 2022-12-02 上海昌海船舶技术有限公司 High-temperature-resistant high-strength heat-insulating cushion block and preparation method thereof
CN117135871A (en) * 2023-01-30 2023-11-28 荣耀终端有限公司 Composite material part, processing method thereof, part and electronic equipment

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Publication number Priority date Publication date Assignee Title
CN108439983A (en) * 2018-04-16 2018-08-24 三峡大学 A kind of graphite ceramic compound pipe molding method
CN109913185A (en) * 2019-03-11 2019-06-21 中国科学院合肥物质科学研究院 A kind of multilayered structure heat-conductive composite material and preparation method thereof containing heat conducting film
CN113444499A (en) * 2021-06-25 2021-09-28 深圳市三科斯电子材料有限公司 Double-sided adhesive high-thermal-conductivity synthetic graphite flake and preparation method thereof
CN113444499B (en) * 2021-06-25 2022-03-11 深圳市三科斯电子材料有限公司 Double-sided adhesive high-thermal-conductivity synthetic graphite flake and preparation method thereof
CN115416376A (en) * 2022-09-29 2022-12-02 上海昌海船舶技术有限公司 High-temperature-resistant high-strength heat-insulating cushion block and preparation method thereof
CN117135871A (en) * 2023-01-30 2023-11-28 荣耀终端有限公司 Composite material part, processing method thereof, part and electronic equipment

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Application publication date: 20180109