CN107381555B - A kind of three-dimensional grapheme of structure-controllable and its preparation method of composite material - Google Patents
A kind of three-dimensional grapheme of structure-controllable and its preparation method of composite material Download PDFInfo
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- CN107381555B CN107381555B CN201710677410.3A CN201710677410A CN107381555B CN 107381555 B CN107381555 B CN 107381555B CN 201710677410 A CN201710677410 A CN 201710677410A CN 107381555 B CN107381555 B CN 107381555B
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- 239000002131 composite material Substances 0.000 title claims abstract description 65
- 238000002360 preparation method Methods 0.000 title claims abstract description 30
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 155
- 229910021389 graphene Inorganic materials 0.000 claims abstract description 152
- 239000002184 metal Substances 0.000 claims abstract description 109
- 229910052751 metal Inorganic materials 0.000 claims abstract description 109
- 239000011347 resin Substances 0.000 claims abstract description 88
- 229920005989 resin Polymers 0.000 claims abstract description 88
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 77
- 239000000463 material Substances 0.000 claims abstract description 46
- 238000000034 method Methods 0.000 claims abstract description 45
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 42
- 229910052802 copper Inorganic materials 0.000 claims abstract description 41
- 239000010949 copper Substances 0.000 claims abstract description 41
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 38
- 238000004519 manufacturing process Methods 0.000 claims abstract description 22
- 238000005229 chemical vapour deposition Methods 0.000 claims abstract description 11
- 239000000126 substance Substances 0.000 claims abstract description 11
- 239000011248 coating agent Substances 0.000 claims abstract description 7
- 238000000576 coating method Methods 0.000 claims abstract description 7
- 239000000243 solution Substances 0.000 claims description 40
- 229920003229 poly(methyl methacrylate) Polymers 0.000 claims description 28
- 239000004926 polymethyl methacrylate Substances 0.000 claims description 28
- 239000000654 additive Substances 0.000 claims description 22
- 230000000996 additive effect Effects 0.000 claims description 22
- 230000007797 corrosion Effects 0.000 claims description 22
- 238000005260 corrosion Methods 0.000 claims description 22
- 239000004205 dimethyl polysiloxane Substances 0.000 claims description 22
- 229920000435 poly(dimethylsiloxane) Polymers 0.000 claims description 22
- 230000008569 process Effects 0.000 claims description 16
- 239000000919 ceramic Substances 0.000 claims description 13
- 229910010293 ceramic material Inorganic materials 0.000 claims description 13
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 claims description 12
- 238000011049 filling Methods 0.000 claims description 12
- 238000010438 heat treatment Methods 0.000 claims description 12
- 239000002002 slurry Substances 0.000 claims description 12
- VEXZGXHMUGYJMC-UHFFFAOYSA-N Hydrochloric acid Chemical compound Cl VEXZGXHMUGYJMC-UHFFFAOYSA-N 0.000 claims description 11
- ROOXNKNUYICQNP-UHFFFAOYSA-N ammonium persulfate Chemical compound [NH4+].[NH4+].[O-]S(=O)(=O)OOS([O-])(=O)=O ROOXNKNUYICQNP-UHFFFAOYSA-N 0.000 claims description 10
- -1 polydimethylsiloxane Polymers 0.000 claims description 9
- 239000000805 composite resin Substances 0.000 claims description 8
- 238000005245 sintering Methods 0.000 claims description 8
- 229910018072 Al 2 O 3 Inorganic materials 0.000 claims description 7
- 238000001513 hot isostatic pressing Methods 0.000 claims description 7
- 238000000465 moulding Methods 0.000 claims description 7
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 claims description 5
- 239000004743 Polypropylene Substances 0.000 claims description 5
- 229910001870 ammonium persulfate Inorganic materials 0.000 claims description 5
- 238000007772 electroless plating Methods 0.000 claims description 5
- 229910017604 nitric acid Inorganic materials 0.000 claims description 5
- 229920001155 polypropylene Polymers 0.000 claims description 5
- 229910021578 Iron(III) chloride Inorganic materials 0.000 claims description 4
- 239000004696 Poly ether ether ketone Substances 0.000 claims description 4
- 239000004952 Polyamide Substances 0.000 claims description 4
- 239000004698 Polyethylene Substances 0.000 claims description 4
- 239000004372 Polyvinyl alcohol Substances 0.000 claims description 4
- XECAHXYUAAWDEL-UHFFFAOYSA-N acrylonitrile butadiene styrene Chemical compound C=CC=C.C=CC#N.C=CC1=CC=CC=C1 XECAHXYUAAWDEL-UHFFFAOYSA-N 0.000 claims description 4
- 239000003822 epoxy resin Substances 0.000 claims description 4
- 238000001746 injection moulding Methods 0.000 claims description 4
- RBTARNINKXHZNM-UHFFFAOYSA-K iron trichloride Chemical compound Cl[Fe](Cl)Cl RBTARNINKXHZNM-UHFFFAOYSA-K 0.000 claims description 4
- 229920002647 polyamide Polymers 0.000 claims description 4
- 229920000647 polyepoxide Polymers 0.000 claims description 4
- 229920002530 polyetherether ketone Polymers 0.000 claims description 4
- 229920000573 polyethylene Polymers 0.000 claims description 4
- 229920002451 polyvinyl alcohol Polymers 0.000 claims description 4
- 238000000935 solvent evaporation Methods 0.000 claims description 4
- 239000004793 Polystyrene Substances 0.000 claims description 3
- 229910004298 SiO 2 Inorganic materials 0.000 claims description 3
- 229910010413 TiO 2 Inorganic materials 0.000 claims description 3
- 229910003465 moissanite Inorganic materials 0.000 claims description 3
- 239000003960 organic solvent Substances 0.000 claims description 3
- 239000004417 polycarbonate Substances 0.000 claims description 3
- 229910010271 silicon carbide Inorganic materials 0.000 claims description 3
- KXGFMDJXCMQABM-UHFFFAOYSA-N 2-methoxy-6-methylphenol Chemical compound [CH]OC1=CC=CC([CH])=C1O KXGFMDJXCMQABM-UHFFFAOYSA-N 0.000 claims description 2
- 239000005011 phenolic resin Substances 0.000 claims description 2
- 229920001568 phenolic resin Polymers 0.000 claims description 2
- 229920000515 polycarbonate Polymers 0.000 claims description 2
- 229920002223 polystyrene Polymers 0.000 claims description 2
- 229920003048 styrene butadiene rubber Polymers 0.000 claims description 2
- 235000013870 dimethyl polysiloxane Nutrition 0.000 claims 3
- BZHJMEDXRYGGRV-UHFFFAOYSA-N Vinyl chloride Chemical compound ClC=C BZHJMEDXRYGGRV-UHFFFAOYSA-N 0.000 claims 1
- CXQXSVUQTKDNFP-UHFFFAOYSA-N octamethyltrisiloxane Chemical compound C[Si](C)(C)O[Si](C)(C)O[Si](C)(C)C CXQXSVUQTKDNFP-UHFFFAOYSA-N 0.000 claims 1
- 238000004987 plasma desorption mass spectroscopy Methods 0.000 claims 1
- 238000004528 spin coating Methods 0.000 claims 1
- 238000007747 plating Methods 0.000 abstract description 35
- 238000010276 construction Methods 0.000 abstract 1
- 239000010410 layer Substances 0.000 description 71
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 44
- 239000001257 hydrogen Substances 0.000 description 28
- 229910052739 hydrogen Inorganic materials 0.000 description 28
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 26
- 229910052786 argon Inorganic materials 0.000 description 22
- 238000005516 engineering process Methods 0.000 description 18
- 239000007789 gas Substances 0.000 description 17
- WSFSSNUMVMOOMR-UHFFFAOYSA-N Formaldehyde Chemical compound O=C WSFSSNUMVMOOMR-UHFFFAOYSA-N 0.000 description 12
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 12
- 230000001681 protective effect Effects 0.000 description 12
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 10
- 238000004140 cleaning Methods 0.000 description 9
- 238000001816 cooling Methods 0.000 description 9
- 238000001723 curing Methods 0.000 description 9
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 8
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 8
- 230000003213 activating effect Effects 0.000 description 8
- 239000003638 chemical reducing agent Substances 0.000 description 8
- 239000011159 matrix material Substances 0.000 description 8
- 230000003472 neutralizing effect Effects 0.000 description 8
- 230000001235 sensitizing effect Effects 0.000 description 8
- HSFWRNGVRCDJHI-UHFFFAOYSA-N alpha-acetylene Natural products C#C HSFWRNGVRCDJHI-UHFFFAOYSA-N 0.000 description 7
- 125000002534 ethynyl group Chemical group [H]C#C* 0.000 description 7
- 239000007788 liquid Substances 0.000 description 7
- 230000000737 periodic effect Effects 0.000 description 7
- 239000012298 atmosphere Substances 0.000 description 6
- 238000010992 reflux Methods 0.000 description 6
- VZGDMQKNWNREIO-UHFFFAOYSA-N tetrachloromethane Chemical compound ClC(Cl)(Cl)Cl VZGDMQKNWNREIO-UHFFFAOYSA-N 0.000 description 6
- 239000003795 chemical substances by application Substances 0.000 description 5
- 150000001879 copper Chemical class 0.000 description 5
- ORTQZVOHEJQUHG-UHFFFAOYSA-L copper(II) chloride Chemical compound Cl[Cu]Cl ORTQZVOHEJQUHG-UHFFFAOYSA-L 0.000 description 5
- 238000000151 deposition Methods 0.000 description 5
- 230000008021 deposition Effects 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 150000002815 nickel Chemical class 0.000 description 5
- LGQLOGILCSXPEA-UHFFFAOYSA-L nickel sulfate Chemical compound [Ni+2].[O-]S([O-])(=O)=O LGQLOGILCSXPEA-UHFFFAOYSA-L 0.000 description 5
- 229910000363 nickel(II) sulfate Inorganic materials 0.000 description 5
- 238000007788 roughening Methods 0.000 description 5
- PPBRXRYQALVLMV-UHFFFAOYSA-N Styrene Chemical compound C=CC1=CC=CC=C1 PPBRXRYQALVLMV-UHFFFAOYSA-N 0.000 description 4
- RDOXTESZEPMUJZ-UHFFFAOYSA-N anisole Chemical compound COC1=CC=CC=C1 RDOXTESZEPMUJZ-UHFFFAOYSA-N 0.000 description 4
- 239000007864 aqueous solution Substances 0.000 description 4
- 238000006243 chemical reaction Methods 0.000 description 4
- 229910000365 copper sulfate Inorganic materials 0.000 description 4
- ARUVKPQLZAKDPS-UHFFFAOYSA-L copper(II) sulfate Chemical compound [Cu+2].[O-][S+2]([O-])([O-])[O-] ARUVKPQLZAKDPS-UHFFFAOYSA-L 0.000 description 4
- 230000006872 improvement Effects 0.000 description 4
- 239000007769 metal material Substances 0.000 description 4
- 239000000178 monomer Substances 0.000 description 4
- 229910052757 nitrogen Inorganic materials 0.000 description 4
- 239000001488 sodium phosphate Substances 0.000 description 4
- 229910000162 sodium phosphate Inorganic materials 0.000 description 4
- RYFMWSXOAZQYPI-UHFFFAOYSA-K trisodium phosphate Chemical compound [Na+].[Na+].[Na+].[O-]P([O-])([O-])=O RYFMWSXOAZQYPI-UHFFFAOYSA-K 0.000 description 4
- MQRWBMAEBQOWAF-UHFFFAOYSA-N acetic acid;nickel Chemical compound [Ni].CC(O)=O.CC(O)=O MQRWBMAEBQOWAF-UHFFFAOYSA-N 0.000 description 3
- 229940078494 nickel acetate Drugs 0.000 description 3
- 239000011148 porous material Substances 0.000 description 3
- 239000000843 powder Substances 0.000 description 3
- 239000002356 single layer Substances 0.000 description 3
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 2
- VGGSQFUCUMXWEO-UHFFFAOYSA-N Ethene Chemical compound C=C VGGSQFUCUMXWEO-UHFFFAOYSA-N 0.000 description 2
- 239000005977 Ethylene Substances 0.000 description 2
- UQSXHKLRYXJYBZ-UHFFFAOYSA-N Iron oxide Chemical compound [Fe]=O UQSXHKLRYXJYBZ-UHFFFAOYSA-N 0.000 description 2
- MCMNRKCIXSYSNV-UHFFFAOYSA-N Zirconium dioxide Chemical compound O=[Zr]=O MCMNRKCIXSYSNV-UHFFFAOYSA-N 0.000 description 2
- 229920000122 acrylonitrile butadiene styrene Polymers 0.000 description 2
- 239000004676 acrylonitrile butadiene styrene Substances 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 229940116318 copper carbonate Drugs 0.000 description 2
- OPQARKPSCNTWTJ-UHFFFAOYSA-L copper(ii) acetate Chemical compound [Cu+2].CC([O-])=O.CC([O-])=O OPQARKPSCNTWTJ-UHFFFAOYSA-L 0.000 description 2
- RSJOBNMOMQFPKQ-UHFFFAOYSA-L copper;2,3-dihydroxybutanedioate Chemical compound [Cu+2].[O-]C(=O)C(O)C(O)C([O-])=O RSJOBNMOMQFPKQ-UHFFFAOYSA-L 0.000 description 2
- GEZOTWYUIKXWOA-UHFFFAOYSA-L copper;carbonate Chemical compound [Cu+2].[O-]C([O-])=O GEZOTWYUIKXWOA-UHFFFAOYSA-L 0.000 description 2
- 230000007547 defect Effects 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 238000005530 etching Methods 0.000 description 2
- 230000004927 fusion Effects 0.000 description 2
- 150000002431 hydrogen Chemical class 0.000 description 2
- UZKWTJUDCOPSNM-UHFFFAOYSA-N methoxybenzene Substances CCCCOC=C UZKWTJUDCOPSNM-UHFFFAOYSA-N 0.000 description 2
- 238000000016 photochemical curing Methods 0.000 description 2
- 239000004800 polyvinyl chloride Substances 0.000 description 2
- 238000003860 storage Methods 0.000 description 2
- ZAMOUSCENKQFHK-UHFFFAOYSA-N Chlorine atom Chemical compound [Cl] ZAMOUSCENKQFHK-UHFFFAOYSA-N 0.000 description 1
- 206010070834 Sensitisation Diseases 0.000 description 1
- 230000004913 activation Effects 0.000 description 1
- 238000005054 agglomeration Methods 0.000 description 1
- 230000002776 aggregation Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 125000004432 carbon atom Chemical group C* 0.000 description 1
- 239000001569 carbon dioxide Substances 0.000 description 1
- 229910002092 carbon dioxide Inorganic materials 0.000 description 1
- 238000006555 catalytic reaction Methods 0.000 description 1
- 238000003486 chemical etching Methods 0.000 description 1
- 239000000460 chlorine Substances 0.000 description 1
- 229910052801 chlorine Inorganic materials 0.000 description 1
- 239000013078 crystal Substances 0.000 description 1
- 229960003280 cupric chloride Drugs 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 239000006262 metallic foam Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006386 neutralization reaction Methods 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 239000012994 photoredox catalyst Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920000915 polyvinyl chloride Polymers 0.000 description 1
- 238000004886 process control Methods 0.000 description 1
- 230000008313 sensitization Effects 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 239000000758 substrate Substances 0.000 description 1
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- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
- C04B35/48—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on zirconium or hafnium oxides, zirconates, zircon or hafnates
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- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
- C04B35/10—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics based on aluminium oxide
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- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
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- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/01—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on oxide ceramics
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- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/52—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbon, e.g. graphite
- C04B35/522—Graphite
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- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
- C04B35/565—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on silicon carbide
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- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
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- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/10—Alloys containing non-metals
- C22C1/1005—Pretreatment of the non-metallic additives
- C22C1/101—Pretreatment of the non-metallic additives by coating
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
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- C22C1/00—Making non-ferrous alloys
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- C22C1/1036—Alloys containing non-metals starting from a melt
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- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/10—Alloys containing non-metals
- C22C1/1036—Alloys containing non-metals starting from a melt
- C22C1/1047—Alloys containing non-metals starting from a melt by mixing and casting liquid metal matrix composites
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- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C18/00—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
- C23C18/16—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by reduction or substitution, e.g. electroless plating
- C23C18/31—Coating with metals
- C23C18/32—Coating with nickel, cobalt or mixtures thereof with phosphorus or boron
- C23C18/34—Coating with nickel, cobalt or mixtures thereof with phosphorus or boron using reducing agents
- C23C18/36—Coating with nickel, cobalt or mixtures thereof with phosphorus or boron using reducing agents using hypophosphites
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- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C18/00—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating
- C23C18/16—Chemical coating by decomposition of either liquid compounds or solutions of the coating forming compounds, without leaving reaction products of surface material in the coating; Contact plating by reduction or substitution, e.g. electroless plating
- C23C18/31—Coating with metals
- C23C18/38—Coating with copper
- C23C18/40—Coating with copper using reducing agents
- C23C18/405—Formaldehyde
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- Organic Chemistry (AREA)
- Materials Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Structural Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- General Chemical & Material Sciences (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Composite Materials (AREA)
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Abstract
Description
技术领域technical field
本发明属于石墨烯复合材料制备领域,更具体地,涉及一种结构可控的三维石墨烯及其复合材料的制备方法。The invention belongs to the field of preparation of graphene composite materials, and more specifically relates to a preparation method of three-dimensional graphene with controllable structure and a composite material thereof.
背景技术Background technique
石墨烯是由单层碳原子构成的二维(2D)晶体材料,具有极其优异的电、光、热及机械性能和超高的比表面积,赋予其在纳米材料、生物工程、精细化工、能量存储等科学领域非常重要的应用前景。由石墨烯制备的复合材料,也因其对原有材料力学、导热、导电性能的改进而备受关注。Graphene is a two-dimensional (2D) crystal material composed of a single layer of carbon atoms. It has very important application prospects in scientific fields such as storage. Composite materials prepared from graphene have also attracted much attention because of their improvements in the mechanical, thermal and electrical properties of the original materials.
然而,2D单层石墨烯片之间存在强烈的相互作用力,极易发生聚集,我们通常所使用的石墨烯材料多以粉状形式存在,这导致其优异的比表面积及导热与导电特性受到限制。现有石墨烯复合材料的制备通常采用石墨烯粉末作为添加物,由于石墨烯分布的不可控性,造成复合材料石墨烯添加量较大(如导电塑料石墨烯添加量为4~10%)及复合材料性能优化受限(复合材料的力学性能随石墨烯添加量的增大,呈现出先增大后减小的变化趋势)。为了解决这一难题,研究者将多片石墨烯连接在一起形成三维蜂窝状骨架结构,即三维(3D)石墨烯。3D石墨烯除具有石墨烯固有的理化性质外,其丰富的孔隙、超轻的密度、大比表面积、低导热系数、高导电率、良好的力学可压缩性和结构稳定性等性能赋予该材料在储氢、催化、传感技术、超级电容器及柔性/可伸缩导电复合材料等领域具有较单层石墨烯更优的性能和更广阔的应用前景。However, there is a strong interaction force between 2D single-layer graphene sheets, and it is easy to aggregate. The graphene materials we usually use are mostly in the form of powder, which leads to its excellent specific surface area and thermal and electrical conductivity. limit. The preparation of existing graphene composite materials usually adopts graphene powder as an additive, and due to the uncontrollability of graphene distribution, the amount of graphene added to the composite material is relatively large (such as the amount of graphene added in conductive plastics is 4 to 10%) and The performance optimization of composite materials is limited (the mechanical properties of composite materials show a trend of first increasing and then decreasing with the increase of graphene addition). To solve this problem, the researchers connected multiple sheets of graphene together to form a three-dimensional honeycomb skeleton structure, that is, three-dimensional (3D) graphene. In addition to the inherent physical and chemical properties of graphene, 3D graphene has abundant pores, ultra-light density, large specific surface area, low thermal conductivity, high electrical conductivity, good mechanical compressibility and structural stability. Compared with single-layer graphene, it has better performance and broader application prospects in the fields of hydrogen storage, catalysis, sensing technology, supercapacitors and flexible/stretchable conductive composite materials.
为此,现有技术中已经对其提出了一些解决方案。例如,CN102674321A中公开了一种用化学气相沉积法在三维泡沫镍模板表面沉积石墨烯薄膜,并经溶除多孔金属基底后得到多孔泡沫状石墨烯,不过,该方法采用泡沫金属作为模板,其中的孔隙特性及石墨烯片层的取向均无法得到有效控制;CN105776186A公开了一种采用SLM成形金属模板,生长制备结构可控的三维石墨烯多孔材料制备方法,该方法以SLM增材制造技术制备金属模板生长石墨烯,SLM制备的金属模板表面质量较差,因此制备的石墨烯质量较差,难以应用于复合材料的制备;CN106349658A、CN105749865A和CN106349658A所公布的三维石墨烯复合材料的制备方法,均是以粉末态三维石墨烯为复合剂,石墨烯分散性得到一定改善,但仍会发生团聚,且石墨烯片层取向无法实现调控。For this reason, some solutions have been proposed in the prior art. For example, CN102674321A discloses a graphene film deposited on the surface of a three-dimensional foamed nickel template by chemical vapor deposition, and obtains porous foamed graphene after dissolving the porous metal substrate. However, the method uses metal foam as a template, wherein Both the pore characteristics and the orientation of graphene sheets cannot be effectively controlled; CN105776186A discloses a method for preparing a three-dimensional graphene porous material with controllable growth and structure by using SLM forming metal templates. The method is prepared by SLM additive manufacturing technology Metal template growth graphene, the metal template surface quality prepared by SLM is relatively poor, so the prepared graphene quality is relatively poor, is difficult to be applied to the preparation of composite material; CN106349658A, CN105749865A and CN106349658A announced the preparation method of three-dimensional graphene composite material Both use powdered three-dimensional graphene as the composite agent, and the dispersion of graphene has been improved to a certain extent, but agglomeration still occurs, and the orientation of graphene sheets cannot be adjusted.
发明内容Contents of the invention
针对现有技术的以上缺陷或改进需求,本发明提供了一种结构可控的三维石墨烯及其复合材料的制备方法,通过三维模板的设计制造成形、化学镀金属层质量的调控以及石墨烯的生长等环节进行研究和设计,由此解决了三维石墨烯及其复合材料外部形状和内部结构不可控的的技术问题。In view of the above defects or improvement needs of the prior art, the present invention provides a method for preparing three-dimensional graphene and its composite materials with controllable structure, through the design and manufacture of three-dimensional templates, the regulation and control of the quality of the electroless metal layer and the graphene The growth and other links of the graphene are studied and designed, thus solving the technical problem of uncontrollable external shape and internal structure of three-dimensional graphene and its composite materials.
为实现上述目的,按照本发明的一个方面,提供了一种结构可控的三维石墨烯制备方法,其特征在于,该方法包括以下步骤:In order to achieve the above object, according to one aspect of the present invention, a method for preparing three-dimensional graphene with controllable structure is provided, wherein the method comprises the following steps:
(a)针对待制备三维石墨烯所需的三维结构构建CAD模型,将该CAD模型通过增材制造得到相应结构的三维树脂结构;(a) Constructing a CAD model for the three-dimensional structure required for the preparation of three-dimensional graphene, and obtaining a three-dimensional resin structure of the corresponding structure through additive manufacturing of the CAD model;
(b)将步骤(a)中获得的三维树脂结构采用化学镀方法在表面镀铜或镍金属层,由此得到表面有金属镀层的树脂结构,利用化学腐蚀或热处理的方法去除该金属镀层的树脂结构中的树脂材料,得到镀铜或镍的三维结构模板;(b) the three-dimensional resin structure obtained in the step (a) is plated with a copper or nickel metal layer on the surface by an electroless plating method, thereby obtaining a resin structure with a metal coating on the surface, and removing the metal coating by chemical corrosion or heat treatment Resin material in the resin structure to obtain a three-dimensional structure template plated with copper or nickel;
(c)在步骤(b)获得的三维结构金属模板上采用化学气相沉积法生成石墨烯,由此得到所需的三维石墨烯。(c) using a chemical vapor deposition method to generate graphene on the three-dimensional structure metal template obtained in step (b), thereby obtaining the desired three-dimensional graphene.
进一步优选地,步骤(a)中,所述增材制造的步骤包括光固化、熔融沉积和激光选区烧结。Further preferably, in step (a), the step of additive manufacturing includes photocuring, fusion deposition and laser selective sintering.
进一步优选地,步骤(b)中,所述化学镀方法镀铜时采用的镀铜液为硫酸铜、氯化铜、碱式碳酸铜、酒石酸铜或醋酸铜中的一种或组合;所述化学镀方法镀镍时采用的镀镍液为硫酸镍或乙酸镍中的一种或组合;且所述金属镀层的层厚度范围为1μm~50μm。Further preferably, in the step (b), the copper plating solution adopted during the copper plating by the electroless plating method is one or a combination of copper sulfate, copper chloride, basic copper carbonate, copper tartrate or copper acetate; The nickel plating solution used in electroless nickel plating is one or a combination of nickel sulfate or nickel acetate; and the thickness of the metal plating layer ranges from 1 μm to 50 μm.
进一步优选地,步骤(b)中,所述去除树脂材料的方法采用化学腐蚀或热处理,其中,所述化学腐蚀采用丙酮、乙醇或四氯化碳作为腐蚀剂,所述热处理的温度为300℃~900℃。Further preferably, in step (b), the method for removing the resin material adopts chemical corrosion or heat treatment, wherein the chemical corrosion uses acetone, ethanol or carbon tetrachloride as the etchant, and the temperature of the heat treatment is 300° C. to 900°C.
进一步优选地,步骤(c)中,所述化学气相沉积所使用的碳源为甲烷、乙烯、乙炔或苯乙烯中的一种或组合。Further preferably, in step (c), the carbon source used in the chemical vapor deposition is one or a combination of methane, ethylene, acetylene or styrene.
按照本发明的另一个方面,提供了一种三维石墨烯复合金属材料的制备方法,其特征在于,该制备方法包括下列步骤:针对由权利要求1-5任一项所制得的三维石墨烯,采用铸造或热等静压的方式将金属填充至其内部结构的空隙中,由此制得三维石墨烯复合金属材料。According to another aspect of the present invention, a method for preparing a three-dimensional graphene composite metal material is provided, characterized in that the preparation method comprises the following steps: for the three-dimensional graphene prepared by any one of claims 1-5 , using casting or hot isostatic pressing to fill the metal into the voids of its internal structure, thereby preparing a three-dimensional graphene composite metal material.
按照本发明的又一个方面,提供了一种三维石墨烯复合树脂的制备方法,其特征在于,该制备方法包括下列步骤:According to another aspect of the present invention, a kind of preparation method of three-dimensional graphene composite resin is provided, it is characterized in that, this preparation method comprises the following steps:
(c1)针对由权利要求1-5任一项所制得的三维石墨烯,在其表面旋凃一层树脂支撑层,然后浸入腐蚀液中直至该三维石墨烯的金属模板完全溶解,得到带有支撑层的三维石墨烯,其中,所述树脂支撑层材料采用聚甲基丙烯酸甲酯(PMMA)或聚二甲基硅氧烷(PDMS);所述腐蚀液采用盐酸、硫酸、硝酸、氯化铁或过硫酸铵中的一种或组合,腐蚀过程温度范围为30℃~90℃;(c1) For the three-dimensional graphene obtained by any one of claims 1-5, spin-coat a layer of resin support layer on its surface, and then immerse in the corrosion solution until the metal template of the three-dimensional graphene is completely dissolved to obtain a band Three-dimensional graphene with a support layer, wherein the resin support layer material adopts polymethyl methacrylate (PMMA) or polydimethylsiloxane (PDMS); the corrosion solution adopts hydrochloric acid, sulfuric acid, nitric acid, chlorine One or a combination of iron oxide or ammonium persulfate, the temperature range of the corrosion process is 30°C to 90°C;
(c2)采用注塑、溶剂蒸发的方法使树脂材料填充至所述带有支撑层的三维石墨烯的空隙中,由此制得三维石墨烯复合树脂材料。(c2) Filling the resin material into the voids of the three-dimensional graphene with the support layer by means of injection molding and solvent evaporation, thereby preparing a three-dimensional graphene composite resin material.
进一步优选地,在步骤(c2)中,所述树脂材料为PMMA、PDMS、聚酰胺(PA)、聚乙烯(PE)、聚丙烯(PP)、聚氯乙烯(PVC)、聚碳酸酯(PC)、丙烯腈-苯乙烯-丁二烯共聚物(ABS)、聚苯乙烯(PS)、环氧树脂(EP)、酚醛树脂(PF)、聚醚醚酮(PEEK)或聚乙烯醇(PVA)中的一种或组合。Further preferably, in step (c2), the resin material is PMMA, PDMS, polyamide (PA), polyethylene (PE), polypropylene (PP), polyvinyl chloride (PVC), polycarbonate (PC ), acrylonitrile-styrene-butadiene copolymer (ABS), polystyrene (PS), epoxy resin (EP), phenolic resin (PF), polyether ether ketone (PEEK) or polyvinyl alcohol (PVA ) in one or a combination.
按照本发明的又一个方面,提供了一种三维石墨烯复合陶瓷的制备方法,其特征在于,该制备方法包括下列步骤:According to another aspect of the present invention, a kind of preparation method of three-dimensional graphene composite ceramics is provided, it is characterized in that, this preparation method comprises the following steps:
(d1)针对由权利要求1-5任一项所制得的三维石墨烯,在其表面旋凃一层树脂支撑层,然后浸入腐蚀液中直至将该三维石墨烯的金属模板完全溶解,由此得到带有支撑层的三维石墨烯,其中,所述树脂支撑层材料采用聚甲基丙烯酸甲酯(PMMA)或聚二甲基硅氧烷(PDMS);所述腐蚀液采用盐酸、硫酸、硝酸、氯化铁或过硫酸铵中的一种或组合,腐蚀过程温度范围为30℃~90℃;(d1) for the three-dimensional graphene obtained by any one of claims 1-5, spin-coat a layer of resin support layer on its surface, then immerse in the corrosion solution until the metal template of the three-dimensional graphene is completely dissolved, by This obtains the three-dimensional graphene that has support layer, wherein, described resin support layer material adopts polymethyl methacrylate (PMMA) or polydimethylsiloxane (PDMS); Described corrosion solution adopts hydrochloric acid, sulfuric acid, One or a combination of nitric acid, ferric chloride or ammonium persulfate, the temperature range of the corrosion process is 30°C to 90°C;
(d2)采用填充陶瓷浆料、胶态成型的方法,将陶瓷材料填充至所述带有支撑层的三维石墨烯空隙中,然后采用有机溶剂腐蚀或热处理的方法去除该初步陶瓷复合材料中的树脂支撑层,并采用填充陶瓷浆料、胶态成型的方法再次填充陶瓷材料,最后对再次填充的产物进行热等静压或常压烧结,由此制得三维石墨烯复合陶瓷材料。(d2) Filling the ceramic material into the three-dimensional graphene voids with the support layer by filling ceramic slurry and colloidal molding, and then removing the carbon dioxide in the preliminary ceramic composite material by organic solvent corrosion or heat treatment. The resin support layer is filled with ceramic slurry and colloidal molding method to refill the ceramic material, and finally the refilled product is subjected to hot isostatic pressing or normal pressure sintering to obtain a three-dimensional graphene composite ceramic material.
进一步优选地,在步骤(d2)中,所述陶瓷浆料材料选用Al2O3、ZrO2、TiO2、SiO2或SiC中的一种或组合。Further preferably, in step (d2), the ceramic slurry material is selected from one or a combination of Al 2 O 3 , ZrO 2 , TiO 2 , SiO 2 or SiC.
总体而言,通过本发明所构思的以上技术方案与现有技术相比,能够取得下列有益效果:Generally speaking, compared with the prior art, the above technical solutions conceived by the present invention can achieve the following beneficial effects:
1、本发明通过采用增材制造结合化学镀金属层做为模板,采用化学气相沉积在金属模板上生长三维石墨烯,能够按照需求设计制备特定形状及结构的三维石墨烯复合材料,能够有效克服现有技术中所存在的石墨烯复合材料中石墨烯分布不均匀、石墨烯片层取向不可控的缺陷,为三维石墨烯复合材料性能的提升奠定基础;1. The present invention uses additive manufacturing combined with electroless metal plating layer as a template, and uses chemical vapor deposition to grow three-dimensional graphene on the metal template, and can design and prepare three-dimensional graphene composite materials with specific shapes and structures according to requirements, which can effectively overcome The defects of uneven distribution of graphene and uncontrollable orientation of graphene sheets in graphene composite materials existing in the prior art lay the foundation for improving the performance of three-dimensional graphene composite materials;
2、以增材制造结合化学镀制备金属模板用于化学气相沉积三维石墨烯,由于化学镀金属表面质量优于增材制造直接成形金属模板表面质量,因此,本发明技术有利于生长高质量三维石墨烯,有利于三维石墨烯复合材料的制备及性能提升;2. Using additive manufacturing combined with electroless plating to prepare metal templates for chemical vapor deposition of three-dimensional graphene, since the surface quality of electroless metal plating is better than that of additive manufacturing directly formed metal templates, the technology of the present invention is conducive to the growth of high-quality three-dimensional graphene Graphene is conducive to the preparation and performance improvement of three-dimensional graphene composite materials;
3、本方法具有操作简便制备周期短和适应面广等特点,尤其适于按照需要设计,制备内部石墨烯复合结构可获得有效、精密控制的高质量、多功能三维石墨烯复合材料产品。3. This method has the characteristics of simple operation, short preparation period and wide application range, and is especially suitable for designing according to needs. The preparation of internal graphene composite structures can obtain effective and precisely controlled high-quality, multifunctional three-dimensional graphene composite material products.
附图说明Description of drawings
图1是按照本发明的优选实施例所构建的结构可控的三维石墨烯及其复合材料的制备方法流程图。Fig. 1 is a flow chart of the preparation method of three-dimensional graphene and its composite material with controllable structure constructed according to a preferred embodiment of the present invention.
具体实施方式Detailed ways
为了使本发明的目的、技术方案及优点更加清楚明白,以下结合附图及实施例,对本发明进行进一步详细说明。应当理解,此处所描述的具体实施例仅仅用以解释本发明,并不用于限定本发明。此外,下面所描述的本发明各个实施方式中所涉及到的技术特征只要彼此之间未构成冲突就可以相互组合。In order to make the object, technical solution and advantages of the present invention more clear, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention. In addition, the technical features involved in the various embodiments of the present invention described below can be combined with each other as long as they do not constitute a conflict with each other.
本发明提供的一种结构可控的三维石墨烯复合材料制备方法,结合增材制造、化学镀和CVD技术制备出符合设计要求结构可控的三维石墨烯材料,然后通过添加相应复合材料组分作为支撑填充材料,同时配置腐蚀液溶解或热处理分解的方法去除掉复合材料中不需要的组分,最终制备出结构可控的三维石墨烯复合金属、树脂、陶瓷材料。A method for preparing a structure-controllable three-dimensional graphene composite material provided by the present invention combines additive manufacturing, chemical plating and CVD technology to prepare a three-dimensional graphene material that meets the design requirements and structure controllable, and then adds the corresponding composite material components As a supporting filling material, at the same time dissolving corrosive liquid or heat treatment to decompose to remove unnecessary components in the composite material, and finally prepare three-dimensional graphene composite metal, resin, and ceramic materials with controllable structure.
具体包括以下步骤:Specifically include the following steps:
(1)构建所需三维多孔结构的CAD模型,并对其外部形状和内部结构分别进行设计;(1) Construct the CAD model of the required three-dimensional porous structure, and design its external shape and internal structure respectively;
步骤(1)中所述CAD模型呈现有序排列的周期性多孔结构或者按照设计需求排列的相互连通三维结构,并且其单元尺寸在0.1~10mm之间,孔隙率在30~99%之间可调。The CAD model described in step (1) presents an ordered periodic porous structure or an interconnected three-dimensional structure arranged according to design requirements, and its unit size is between 0.1-10mm, and the porosity is between 30-99%. Tune.
(2)基于步骤(1)所构建的CAD模型,通过光固化、熔融沉积或激光选区烧结增材制造技术制得相应形状的三维树脂结构;(2) Based on the CAD model constructed in step (1), a three-dimensional resin structure of corresponding shape is obtained by photocuring, fused deposition or laser selective sintering additive manufacturing technology;
步骤(2)中所述增材制造技术包括光固化、熔融沉积、激光选区烧结技术;成形制备的三维结构为树脂材料。The additive manufacturing technology described in step (2) includes light curing, fusion deposition, and laser selective sintering technologies; the three-dimensional structure prepared by forming is a resin material.
(3)通过化学镀铜或者化学镀镍工艺,在步骤(2)所制备的三维树脂结构表面镀铜或镍金属层;其中所采用的镀铜或镀镍工艺包含树脂结构清洗、粗化、中和、敏化、活化后,采用镀铜液或镀镍液在处理后树脂结构表面镀铜或镍金属层,镀得的金属层厚度在1~50μm之间。然后将镀有金属层的树脂结构利用化学腐蚀或热处理的方法去除树脂材料,得到铜或镍三维结构模板;(3) Copper or nickel metal layer is plated on the surface of the three-dimensional resin structure prepared in step (2) by electroless copper plating or electroless nickel plating process; wherein the copper plating or nickel plating process adopted includes resin structure cleaning, roughening, After neutralization, sensitization and activation, a copper or nickel plating solution is used to plate a copper or nickel metal layer on the surface of the treated resin structure, and the thickness of the plated metal layer is between 1 and 50 μm. Then, the resin structure coated with the metal layer is removed by chemical corrosion or heat treatment to obtain a copper or nickel three-dimensional structure template;
步骤(3)中所采用的镀铜液以硫酸铜、氯化铜、碱式碳酸铜、酒石酸铜、醋酸铜为铜盐;采用的镀镍液以硫酸镍、乙酸镍为镍盐;镀得的金属层厚度控制在1~50μm之间。The copper plating liquid adopted in the step (3) is copper salt with copper sulfate, cupric chloride, basic copper carbonate, copper tartrate, copper acetate; The nickel plating liquid that adopts is nickel salt with nickel sulfate, nickel acetate; The thickness of the metal layer is controlled between 1 and 50 μm.
步骤(3)中所采用的化学腐蚀方法为采用丙酮、乙醇、四氯化碳腐蚀树脂模板;热处理方法为在300~900℃下分解去除树脂结构。The chemical etching method used in step (3) is to corrode the resin template with acetone, ethanol, and carbon tetrachloride; the heat treatment method is to decompose and remove the resin structure at 300-900° C.
(4)通过化学气相沉积法在步骤(3)所制得的金属模板上生长石墨烯:在此过程中,将金属模板放入CVD管式炉中,通入氩气作为保护气体;然后在通入氩气条件下,加热样品至反应温度;到达反应温度后通入氩气和氢气保温;然后通入甲烷和氢气、并保持管式炉内压强,开始进行化学气相沉积反应;反应结束后在通入氩气和氢气条件下将样品冷却至室温,由此制得生长在所述金属模板上的三维石墨烯;(4) grow graphene on the prepared metal template of step (3) by chemical vapor deposition: in this process, metal template is put into CVD tube furnace, feeds argon as shielding gas; Then in Under the condition of feeding argon, heat the sample to the reaction temperature; after reaching the reaction temperature, feed argon and hydrogen to keep warm; then feed methane and hydrogen, and keep the pressure in the tube furnace, and start the chemical vapor deposition reaction; after the reaction The sample is cooled to room temperature under the condition of feeding argon and hydrogen, thereby preparing three-dimensional graphene grown on the metal template;
步骤(4)中化学气相沉积过程所使用碳源为甲烷、乙烯、乙炔、苯乙烯;在步骤(3)所制备的三维金属模板表面生长的石墨烯层数为1~20层。The carbon sources used in the chemical vapor deposition process in step (4) are methane, ethylene, acetylene, and styrene; the number of graphene layers grown on the surface of the three-dimensional metal template prepared in step (3) is 1-20 layers.
(5)配置一定浓度的的腐蚀液,将步骤(4)所制得的产物先表面旋凃一层树脂支撑层,然后浸入配置的腐蚀液中,在30~90℃温度下回流直至将所述金属模板完全溶解:其中采用镀铜制备的铜金属模板使用FeCl3或(NH4)2S2O8溶液作为腐蚀液;采用镀镍制备的镍金属模板采用HCl溶液作为腐蚀液。得到带有支撑层的复合用三维石墨烯材料;(5) Prepare a certain concentration of corrosive liquid, spin-coat a layer of resin support layer on the surface of the product obtained in step (4), then immerse in the prepared corrosive liquid, and reflow at a temperature of 30-90°C until the The above metal templates are completely dissolved: the copper metal template prepared by copper plating uses FeCl 3 or (NH 4 ) 2 S 2 O 8 solution as the etching solution; the nickel metal template prepared by nickel plating uses HCl solution as the etching solution. A composite three-dimensional graphene material with a support layer is obtained;
步骤(5)中所述树脂支撑层为PMMA、PDMS;腐蚀液选自下列物质的一种或其混合:盐酸、硫酸、硝酸、氯化铁和过硫酸铵;腐蚀过程控制温度在30℃~90℃。The resin support layer described in step (5) is PMMA, PDMS; Corrosive solution is selected from one or its mixture of following substances: hydrochloric acid, sulfuric acid, nitric acid, ferric chloride and ammonium persulfate; Corrosion process control temperature is at 30 ℃~ 90°C.
(6)三维石墨烯复合金属材料的制备,将步骤(4)所制得的表面长有石墨烯的金属结构作为复合添加材料,采用铸造、热等静压的方法使金属填充模板空隙,制得三维石墨烯复合金属材料;(6) the preparation of three-dimensional graphene composite metal material, the metal structure that the surface that step (4) makes has graphene is long as composite additive material, adopts the method for casting, hot isostatic pressing to make metal fill template space, make Obtain three-dimensional graphene composite metal material;
步骤(6)中所述填充金属为铜或镍;三维石墨烯所占复合材料比例为0.01~10wt%。The filling metal in step (6) is copper or nickel; the proportion of three-dimensional graphene in the composite material is 0.01-10wt%.
(7)将带有树脂支撑层的三维石墨烯采用注塑、溶剂蒸发的方法使树脂材料填充模板空隙,制得三维石墨烯复合树脂材料;将带有树脂支撑层的三维石墨烯采用填充陶瓷浆料、胶态成型的方法,使陶瓷材料填充空隙,然后采用有机溶剂腐蚀或热处理的方法去除树脂支撑层,采用填充陶瓷浆料、胶态成型的方法填充空隙,再热等静压或常压烧结制得三维石墨烯复合陶瓷材料。(7) The three-dimensional graphene with the resin support layer is used for injection molding and solvent evaporation to make the resin material fill the template gap to obtain a three-dimensional graphene composite resin material; the three-dimensional graphene with the resin support layer is filled with ceramic slurry Material, colloidal molding method, so that the ceramic material fills the gap, and then use organic solvent corrosion or heat treatment to remove the resin support layer, fill the gap with ceramic slurry, colloidal molding method, and then hot isostatic pressing or normal pressure Sintering produces a three-dimensional graphene composite ceramic material.
步骤(7)中所述制备三维石墨烯复合树脂材料填充树脂为PMMA、PDMS、PA、PE、PP、PVC、PC、ABS、PS、EP、PF、PEEK、PVA中的一种;制备三维石墨烯复合陶瓷材料所填充材料为Al2O3、ZrO2、TiO2、SiO2、SiC;三维石墨烯所占复合材料比例为0.01~10wt%。Prepare the three-dimensional graphene composite resin material filling resin described in step (7) and be the one in PMMA, PDMS, PA, PE, PP, PVC, PC, ABS, PS, EP, PF, PEEK, PVA; Prepare three-dimensional graphite The filling material of the graphene composite ceramic material is Al 2 O 3 , ZrO 2 , TiO 2 , SiO 2 , SiC; the proportion of three-dimensional graphene in the composite material is 0.01-10 wt%.
综上所述,本发明的总体思路主要包括三个方面,一是按照材料设计需求建立CAD模型,通过增材制造和化学镀技术制备出符合CAD模型的金属模板;二是在制备的金属模板上采用CVD技术生长结构可控的三维石墨烯;三是通过添加相应复合材料组分作为支撑填充材料,同时配置腐蚀液溶解或热处理分解的方法去除掉复合材料中不需要的组分,最终制得符合设计需求,结构可控的三维石墨烯复合金属、树脂、陶瓷材料。In summary, the general idea of the present invention mainly includes three aspects. One is to establish a CAD model according to the material design requirements, and to prepare a metal template conforming to the CAD model through additive manufacturing and chemical plating technology; The first is to use CVD technology to grow three-dimensional graphene with controllable structure; the third is to add the corresponding composite material components as support filling materials, and at the same time configure corrosive solution to dissolve or heat treatment to decompose to remove unnecessary components in the composite material, and finally produce Three-dimensional graphene composite metal, resin, and ceramic materials with controllable structure must meet the design requirements.
下面将结合具体的实施例对本发明的方案进行进一步的说明。The solutions of the present invention will be further described below in conjunction with specific examples.
实施例1Example 1
(1)采用CAD软件,相应建立单元尺寸为0.1mm的三维多孔单元体,其中将该单元体阵列设计为孔隙率为30%,有序排列的周期性多孔结构,模型外部尺寸为50mm×50mm×10mm。(1) Use CAD software to establish a three-dimensional porous unit body with a unit size of 0.1mm. The unit body array is designed as a periodic porous structure with a porosity of 30% and an orderly arrangement. The external size of the model is 50mm×50mm ×10mm.
(2)采用光固化增材制造技术制备所构建的CAD模型的树脂结构。(2) The resin structure of the constructed CAD model was prepared by light-curing additive manufacturing technology.
(3)将所制备的树脂结构经清洗、粗化、中和、敏化、活化后,采用化学镀铜工艺在树脂结构表面镀铜金属层,化学镀铜液采用硫酸铜为铜盐,甲醛为还原剂,镀得的金属铜层厚度为1μm。将制得的镀有金属层的树脂结构浸泡在丙酮中,待树脂结构完全溶解后取出,再洗涤、烘干。(3) After cleaning, roughening, neutralizing, sensitizing, and activating the prepared resin structure, adopt an electroless copper plating process to plate a copper metal layer on the surface of the resin structure. The electroless copper plating solution uses copper sulfate as copper salt, and formaldehyde As a reducing agent, the thickness of the plated metal copper layer is 1 μm. Soak the prepared resin structure coated with the metal layer in acetone, take it out after the resin structure is completely dissolved, and then wash and dry it.
(4)将步骤(3)制得的金属模板放入CVD管式炉中,通入氩气作为保护气体;在氩气流量300sccm条件下,50分钟将样品加热至900℃;在氩气流量50sccm、氢气流量50sccm条件下在900℃保温35分钟;在氢气流量30sccm、甲烷气体流量10sccm,并管式炉内压强50Pa条件下,将金属模板在900℃保温15分钟;然后在氩气流量60sccm、氢气流量50sccm条件下冷却至室温,由此制得生长在金属模板上的三维石墨烯,石墨烯层数为1层。(4) Put the metal template prepared in step (3) into a CVD tube furnace, and feed argon as a protective gas; under the condition of argon flow rate of 300 sccm, the sample was heated to 900° C. in 50 minutes; Insulate at 900°C for 35 minutes under the conditions of 50sccm and hydrogen flow rate of 50sccm; under the conditions of hydrogen flow rate of 30sccm, methane gas flow rate of 10sccm, and tube furnace pressure of 50Pa, the metal template is kept at 900°C for 15 minutes; 1. Cooling to room temperature under the condition of a hydrogen flow rate of 50 sccm, thereby preparing three-dimensional graphene grown on a metal template, and the number of graphene layers is 1 layer.
(5)将表面生长石墨烯的铜结构放入模具中,在保护性气氛条件下浇注融化的铜填充空隙,冷却脱模,即得到三维石墨烯复合铜材料。测试结果表明,三维石墨烯按设计需求均匀的分布在复合铜基体内。(5) Putting the copper structure with graphene growing on the surface into a mold, pouring molten copper to fill the gaps under protective atmosphere conditions, cooling and demoulding, and obtaining a three-dimensional graphene composite copper material. The test results show that the three-dimensional graphene is uniformly distributed in the composite copper matrix according to the design requirements.
实施例2Example 2
(1)采用CAD软件,相应建立单元尺寸为10mm的三维多孔单元体,其中将该单元体阵列设计为孔隙率为99%,有序排列的周期性多孔结构,模型外部尺寸为100mm×100mm×100mm。(1) Using CAD software, a three-dimensional porous unit body with a unit size of 10mm is correspondingly established. The unit body array is designed as a periodic porous structure with a porosity of 99% and an orderly arrangement. The external size of the model is 100mm×100mm× 100mm.
(2)采用熔融沉积增材制造技术制备所构建的CAD模型的树脂结构。(2) The resin structure of the constructed CAD model was prepared by fused deposition additive manufacturing technology.
(3)将所制备的树脂结构经清洗、粗化、中和、敏化、活化后,采用化学镀镍工艺在树脂结构表面镀铜金属层,化学镀镍液采用硫酸镍为镍盐,亚磷酸钠为还原剂,镀得的金属镍层厚度为50μm。将制得的镀有金属层的树脂结构在氮气保护气氛下900℃热处理3小时,将树脂结构分解去除。(3) After cleaning, coarsening, neutralizing, sensitizing and activating the prepared resin structure, adopt the electroless nickel plating process to plate a copper metal layer on the surface of the resin structure. The electroless nickel plating solution adopts nickel sulfate as nickel salt, sub Sodium phosphate is used as a reducing agent, and the thickness of the metal nickel layer plated is 50 μm. The prepared resin structure coated with the metal layer was heat-treated at 900° C. for 3 hours under a nitrogen protective atmosphere to decompose and remove the resin structure.
(4)将步骤(3)制得的金属模板放入CVD管式炉中,通入氩气作为保护气体;在氩气流量300sccm条件下,50分钟将样品加热至1050℃;在氩气流量50sccm、氢气流量50sccm条件下在1050℃保温35分钟;在氢气流量30sccm、乙炔气体流量50sccm,并管式炉内压强200Pa条件下,将金属模板在1100℃保温15分钟;然后在氩气流量60sccm、氢气流量50sccm条件下冷却至室温,由此制得生长在金属模板上的三维石墨烯,石墨烯层数为20层。(4) Put the metal template prepared in step (3) into a CVD tube furnace, and feed argon as a protective gas; under the condition of an argon flow of 300 sccm, the sample was heated to 1050° C. in 50 minutes; Insulate at 1050°C for 35 minutes under the conditions of 50sccm and hydrogen flow rate of 50sccm; under the conditions of hydrogen flow rate of 30sccm, acetylene gas flow rate of 50sccm, and tube furnace pressure of 200Pa, the metal template was kept at 1100°C for 15 minutes; 1. Cooling to room temperature under the condition of hydrogen flow rate of 50 sccm, thus producing three-dimensional graphene grown on the metal template, the number of graphene layers is 20 layers.
(5)配置3wt%的PMMA乙醇溶液,旋凃于制得的表面长有石墨烯的金属模板上,在150℃条件下保温30分钟使PMMA固化。配置3mol/L的FeCl3水溶液,将制得的产物浸入其中,在30℃温度下回流直至将所述金属模板完全溶解。(5) Configure 3 wt% PMMA ethanol solution, spin-coat on the prepared metal template with graphene on the surface, and keep the PMMA solidified at 150° C. for 30 minutes. Prepare a 3 mol/L FeCl 3 aqueous solution, immerse the prepared product in it, and reflux at a temperature of 30° C. until the metal template is completely dissolved.
(6)采用注塑的方法将融化的PMMA注入步骤(5)所制备材料的空隙里,冷却即得到三维石墨烯复合PMMA材料。测试结果表明,三维石墨烯按设计需求均匀的分布在复合PMMA基体内。(6) Inject the melted PMMA into the voids of the material prepared in step (5) by injection molding, and cool to obtain the three-dimensional graphene composite PMMA material. The test results show that the three-dimensional graphene is uniformly distributed in the composite PMMA matrix according to the design requirements.
实施例3Example 3
(1)采用CAD软件,相应建立间距为1mm的片层结构模型,片层厚度为1mm模型外部尺寸为50mm×50mm×50mm。(1) Using CAD software, correspondingly establish a sheet structure model with a spacing of 1 mm, and the external size of the model with a sheet thickness of 1 mm is 50 mm × 50 mm × 50 mm.
(2)采用激光选区烧结增材制造技术制备所构建的CAD模型的树脂结构。(2) The resin structure of the constructed CAD model was prepared by laser selective sintering additive manufacturing technology.
(3)将所制备的树脂结构经清洗、粗化、中和、敏化、活化后,采用化学镀铜工艺在树脂结构表面镀铜金属层,化学镀铜液采用氯化铜为铜盐,甲醛为还原剂,镀得的金属铜层厚度为3μm。将制得的镀有金属层的树脂结构浸泡在丙酮中,待树脂结构完全溶解后取出,再洗涤、烘干。(3) After cleaning, roughening, neutralizing, sensitizing and activating the prepared resin structure, adopt an electroless copper plating process to plate a copper metal layer on the surface of the resin structure, and the electroless copper plating solution adopts copper chloride as copper salt, Formaldehyde is used as a reducing agent, and the thickness of the plated metal copper layer is 3 μm. Soak the prepared resin structure coated with the metal layer in acetone, take it out after the resin structure is completely dissolved, and then wash and dry it.
(4)将步骤(3)制得的金属模板放入CVD管式炉中,通入氩气作为保护气体;在氩气流量300sccm条件下,50分钟将样品加热至1000℃;在氩气流量50sccm、氢气流量50sccm条件下在1000℃保温35分钟;在氢气流量30sccm、甲烷气体流量20sccm,并管式炉内压强130Pa条件下,将金属模板在1000℃保温15分钟;然后在氩气流量60sccm、氢气流量50sccm条件下冷却至室温,由此制得生长在金属模板上的三维石墨烯,石墨烯层数为3层。(4) Put the metal template prepared in step (3) into a CVD tube furnace, and feed argon as a protective gas; under the condition of an argon flow of 300 sccm, the sample was heated to 1000° C. in 50 minutes; 50sccm, hydrogen flow rate of 50sccm at 1000°C for 35 minutes; under the conditions of hydrogen flow rate of 30sccm, methane gas flow rate of 20sccm, and tube furnace pressure of 130Pa, the metal template was kept at 1000°C for 15 minutes; then argon flow rate of 60sccm 1. Cooling to room temperature under the condition of a hydrogen flow rate of 50 sccm, thus producing three-dimensional graphene grown on a metal template, and the number of graphene layers is 3 layers.
(5)配置3wt%的PMMA乙醇溶液,旋凃于制得的表面长有石墨烯的金属模板上,在100℃条件下保温30分钟使PMMA固化。配置3mol/L的FeCl3水溶液,将制得的产物浸入其中,在50℃温度下回流直至将所述金属模板完全溶解。(5) Configure 3wt% PMMA ethanol solution, spin-coat on the prepared metal template with graphene on the surface, and keep the PMMA solidified at 100° C. for 30 minutes. Prepare a 3 mol/L FeCl 3 aqueous solution, immerse the prepared product in it, and reflux at a temperature of 50° C. until the metal template is completely dissolved.
(6)采用胶态成型的方法将Al2O3料浆注入步骤(5)所制备材料的空隙里,加热固化,然后在600℃热处理3小时,将PMMA支撑层分解去除,将Al2O3料浆注入PMMA去除所产生的空隙,加热固化并高温烧结,即得到三维石墨烯复合Al2O3陶瓷材料。测试结果表明,三维石墨烯按设计需求均匀的分布在复合Al2O3基体内。(6) Inject the Al 2 O 3 slurry into the gap of the material prepared in step (5) by colloidal molding method, heat and solidify, and then heat-treat at 600°C for 3 hours to decompose and remove the PMMA support layer, and the Al 2 O 3 3 The slurry is injected into PMMA to remove the generated voids, heated and solidified and sintered at high temperature to obtain a three-dimensional graphene composite Al 2 O 3 ceramic material. The test results show that the three-dimensional graphene is uniformly distributed in the composite Al 2 O 3 matrix according to the design requirements.
实施例4Example 4
(1)采用CAD软件,相应建立单元尺寸为3mm的三维多孔单元体,其中将该单元体阵列设计为孔隙率为85%,有序排列的周期性多孔结构,模型外部尺寸为50mm×50mm×50mm。(1) Using CAD software, a three-dimensional porous unit body with a unit size of 3mm is correspondingly established. The unit body array is designed as a periodic porous structure with a porosity of 85% and an orderly arrangement. The external size of the model is 50mm×50mm× 50mm.
(2)采用光固化增材制造技术制备所构建的CAD模型的树脂结构。(2) The resin structure of the constructed CAD model was prepared by light-curing additive manufacturing technology.
(3)将所制备的树脂结构经清洗、粗化、中和、敏化、活化后,采用化学镀镍工艺在树脂结构表面镀铜金属层,化学镀铜液采用硫酸铜为铜盐,甲醛为还原剂,镀得的金属铜层厚度为5μm。将制得的镀有金属层的树脂结构在氮气保护气氛下300℃热处理5小时,将树脂结构分解去除。(3) After cleaning, coarsening, neutralizing, sensitizing, and activating the prepared resin structure, an electroless nickel plating process is used to plate a copper metal layer on the surface of the resin structure. The electroless copper plating solution adopts copper sulfate as copper salt, and formaldehyde As a reducing agent, the thickness of the plated metal copper layer is 5 μm. The prepared resin structure coated with the metal layer was heat-treated at 300° C. for 5 hours under a nitrogen protective atmosphere to decompose and remove the resin structure.
(4)将步骤(3)制得的金属模板放入CVD管式炉中,通入氩气作为保护气体;在氩气流量300sccm条件下,50分钟将样品加热至1050℃;在氩气流量50sccm、氢气流量50sccm条件下在1050℃保温35分钟;在氢气流量30sccm、乙炔气体流量50sccm,并管式炉内压强200Pa条件下,将金属模板在1100℃保温15分钟;然后在氩气流量60sccm、氢气流量50sccm条件下冷却至室温,由此制得生长在金属模板上的三维石墨烯,石墨烯层数为1层。(4) Put the metal template prepared in step (3) into a CVD tube furnace, and feed argon as a protective gas; under the condition of an argon flow of 300 sccm, the sample was heated to 1050° C. in 50 minutes; Insulate at 1050°C for 35 minutes under the conditions of 50sccm and hydrogen flow rate of 50sccm; under the conditions of hydrogen flow rate of 30sccm, acetylene gas flow rate of 50sccm, and tube furnace pressure of 200Pa, the metal template was kept at 1100°C for 15 minutes; 1. Cooling to room temperature under the condition of a hydrogen flow rate of 50 sccm, thereby preparing three-dimensional graphene grown on a metal template, and the number of graphene layers is 1 layer.
(5)配置PDMS固化液,聚合单体和固化剂以10:1的质量比混合,旋凃于制得的表面长有石墨烯的金属模板上,在80℃条件下保温30分钟使PDMS聚合固化。配置3mol/L的(NH4)2S2O8溶液,将制得的产物浸入其中,在30℃温度下回流直至将所述金属模板完全溶解。(5) Configure the PDMS curing liquid, mix the polymerized monomer and the curing agent at a mass ratio of 10:1, spin-coat on the prepared metal template with graphene on the surface, and keep the temperature at 80°C for 30 minutes to polymerize PDMS solidify. Prepare a 3 mol/L (NH 4 ) 2 S 2 O 8 solution, immerse the prepared product in it, and reflux at a temperature of 30° C. until the metal template is completely dissolved.
(6)配置PDMS固化液,聚合单体和固化剂以10:1的质量比混合,将PDMS固化液注入步骤(5)所制备材料的空隙里,冷却即得到三维石墨烯复合PDMS材料。测试结果表明,三维石墨烯按设计需求均匀的分布在复合PDMS基体内。(6) Prepare the PDMS solidified solution, mix the polymerized monomer and the solidified agent at a mass ratio of 10:1, inject the PDMS solidified solution into the gap of the material prepared in step (5), and cool to obtain the three-dimensional graphene composite PDMS material. The test results show that the three-dimensional graphene is uniformly distributed in the composite PDMS matrix according to the design requirements.
实施例5Example 5
(1)采用CAD软件,相应建立单元尺寸为0.2mm的三维多孔单元体,其中将该单元体阵列设计为孔隙率为50%,有序排列的周期性多孔结构,模型外部尺寸为10mm×10mm×10mm。(1) Use CAD software to establish a three-dimensional porous unit body with a unit size of 0.2 mm. The unit body array is designed as a periodic porous structure with a porosity of 50% and an orderly arrangement. The external size of the model is 10 mm×10 mm ×10mm.
(2)采用光固化增材制造技术制备所构建的CAD模型的树脂结构。(2) The resin structure of the constructed CAD model was prepared by light-curing additive manufacturing technology.
(3)将所制备的树脂结构经清洗、粗化、中和、敏化、活化后,采用化学镀镍工艺在树脂结构表面镀镍金属层,化学镀镍液采用乙酸镍为镍盐,亚磷酸钠为还原剂,镀得的金属镍层厚度为10μm。将制得的镀有金属层的树脂结构浸泡在四氯化碳中,待树脂结构完全溶解后取出,再洗涤、烘干。(3) After cleaning, roughening, neutralizing, sensitizing and activating the prepared resin structure, the electroless nickel plating process is used to plate a nickel metal layer on the surface of the resin structure. The electroless nickel plating solution adopts nickel acetate as nickel salt, sub Sodium phosphate is used as the reducing agent, and the thickness of the metal nickel layer is 10 μm. The prepared resin structure coated with the metal layer is soaked in carbon tetrachloride, taken out after the resin structure is completely dissolved, then washed and dried.
(4)将步骤(3)制得的金属模板放入CVD管式炉中,通入氩气作为保护气体;在氩气流量300sccm条件下,50分钟将样品加热至1000℃;在氩气流量50sccm、氢气流量50sccm条件下在1000℃保温30分钟;在氢气流量30sccm、甲烷气体流量10sccm,并管式炉内压强50Pa条件下,将金属模板在900℃保温15分钟;然后在氩气流量60sccm、氢气流量50sccm条件下冷却至室温,由此制得生长在金属模板上的三维石墨烯,石墨烯层数为5层。(4) Put the metal template prepared in step (3) into a CVD tube furnace, and feed argon as a protective gas; under the condition of an argon flow of 300 sccm, the sample was heated to 1000° C. in 50 minutes; Insulate at 1000°C for 30 minutes under the condition of 50sccm, hydrogen flow rate of 50sccm; under the conditions of hydrogen flow rate of 30sccm, methane gas flow rate of 10sccm, and tube furnace pressure of 50Pa, the metal template is kept at 900°C for 15 minutes; 1. Cooling to room temperature under the condition of a hydrogen flow rate of 50 sccm, thus preparing a three-dimensional graphene grown on a metal template, and the number of graphene layers is 5 layers.
(5)将表面生长石墨烯的镍结构放入模具中,在保护性气氛条件下填充镍金属粉,采用热等静压技术使材料致密化,冷却脱模,即得到三维石墨烯复合镍材料。测试结果表明,三维石墨烯按设计需求均匀的分布在复合镍基体内。(5) Put the nickel structure with graphene growing on the surface into the mold, fill it with nickel metal powder under protective atmosphere conditions, use hot isostatic pressing technology to densify the material, cool and demould, and obtain the three-dimensional graphene composite nickel material . The test results show that the three-dimensional graphene is uniformly distributed in the composite nickel matrix according to the design requirements.
实施例6Example 6
(1)采用CAD软件,相应建立单元尺寸为0.1mm的三维多孔单元体,其中将该单元体阵列设计为孔隙率为90%,有序排列的周期性多孔结构,模型外部尺寸为100mm×100mm×100mm。(1) Use CAD software to establish a three-dimensional porous unit body with a unit size of 0.1mm, in which the unit body array is designed as a periodic porous structure with a porosity of 90% and an orderly arrangement, and the external size of the model is 100mm×100mm ×100mm.
(2)采用熔融沉积增材制造技术制备所构建的CAD模型的树脂结构。(2) The resin structure of the constructed CAD model was prepared by fused deposition additive manufacturing technology.
(3)将所制备的树脂结构经清洗、粗化、中和、敏化、活化后,采用化学镀镍工艺在树脂结构表面镀铜金属层,化学镀镍液采用硫酸镍为镍盐,亚磷酸钠为还原剂,镀得的金属镍层厚度为25μm。将制得的镀有金属层的树脂结构在氮气保护气氛下800℃热处理4小时,将树脂结构分解去除。(3) After cleaning, coarsening, neutralizing, sensitizing and activating the prepared resin structure, adopt the electroless nickel plating process to plate a copper metal layer on the surface of the resin structure. The electroless nickel plating solution adopts nickel sulfate as nickel salt, sub Sodium phosphate is used as the reducing agent, and the thickness of the metal nickel layer is 25 μm. The prepared resin structure coated with the metal layer was heat-treated at 800° C. for 4 hours under a nitrogen protective atmosphere to decompose and remove the resin structure.
(4)将步骤(3)制得的金属模板放入CVD管式炉中,通入氩气作为保护气体;在氩气流量300sccm条件下,50分钟将样品加热至950℃;在氩气流量50sccm、氢气流量50sccm条件下在950℃保温35分钟;在氢气流量30sccm、乙炔气体流量50sccm,并管式炉内压强200Pa条件下,将金属模板在1100℃保温15分钟;然后在氩气流量60sccm、氢气流量50sccm条件下冷却至室温,由此制得生长在金属模板上的三维石墨烯,石墨烯层数为10层。(4) Put the metal template prepared in step (3) into a CVD tube furnace, and feed argon as a shielding gas; under the condition of an argon flow of 300 sccm, the sample was heated to 950° C. in 50 minutes; Insulate at 950°C for 35 minutes under the condition of 50sccm and hydrogen flow rate of 50sccm; under the conditions of hydrogen flow rate of 30sccm, acetylene gas flow rate of 50sccm, and tube furnace pressure of 200Pa, the metal template is kept at 1100°C for 15 minutes; then the argon flow rate is 60sccm 1. Cooling to room temperature under the condition of a hydrogen flow rate of 50 sccm, thereby preparing three-dimensional graphene grown on a metal template, and the number of graphene layers is 10 layers.
(5)配置3wt%的PMMA苯甲醚溶液,旋凃于制得的表面长有石墨烯的金属模板上,在100℃条件下保温40分钟使PMMA固化。配置3mol/L的FeCl3水溶液,将制得的产物浸入其中,在50℃温度下回流直至将所述金属模板完全溶解。(5) A 3wt% PMMA anisole solution was prepared, spin-coated on the prepared metal template with graphene on the surface, and kept at 100° C. for 40 minutes to solidify the PMMA. Prepare a 3 mol/L FeCl 3 aqueous solution, immerse the prepared product in it, and reflux at a temperature of 50° C. until the metal template is completely dissolved.
(6)将ZrO2料浆注入步骤(5)所制备材料的空隙里,加热固化,然后在900℃热处理2小时,将PMMA支撑层分解去除,再次将ZrO2料浆注入PMMA去除所产生的空隙,加热固化并采用热等静压烧结,即得到三维石墨烯复合ZrO2陶瓷材料。测试结果表明,三维石墨烯按设计需求均匀的分布在复合ZrO2基体内。(6) ZrO 2 slurry is injected into the gap of the material prepared in step (5), heated and solidified, then heat treated at 900°C for 2 hours, the PMMA support layer is decomposed and removed, and ZrO 2 slurry is injected into PMMA to remove the generated voids, heat solidified and sintered by hot isostatic pressing to obtain a three-dimensional graphene composite ZrO2 ceramic material. The test results show that the three-dimensional graphene is uniformly distributed in the composite ZrO 2 matrix according to the design requirements.
实施例7Example 7
(1)采用CAD软件,相应建立间距为3mm的片层结构模型,片层厚度为0.5mm模型外部尺寸为30mm×30mm×30mm。(1) Using CAD software, correspondingly establish a sheet structure model with a spacing of 3mm, and a sheet thickness of 0.5mm. The external dimensions of the model are 30mm×30mm×30mm.
(2)采用激光选区烧结增材制造技术制备所构建的CAD模型的树脂结构。(2) The resin structure of the constructed CAD model was prepared by laser selective sintering additive manufacturing technology.
(3)将所制备的树脂结构经清洗、粗化、中和、敏化、活化后,采用化学镀铜工艺在树脂结构表面镀铜金属层,化学镀铜液采用氯化铜为铜盐,甲醛为还原剂,镀得的金属铜层厚度为2μm。将制得的镀有金属层的树脂结构浸泡在乙醇中,待树脂结构完全溶解后取出,再洗涤、烘干。(3) After cleaning, roughening, neutralizing, sensitizing and activating the prepared resin structure, adopt an electroless copper plating process to plate a copper metal layer on the surface of the resin structure, and the electroless copper plating solution adopts copper chloride as copper salt, Formaldehyde is used as a reducing agent, and the thickness of the plated metal copper layer is 2 μm. Soak the prepared resin structure coated with the metal layer in ethanol, take it out after the resin structure is completely dissolved, then wash and dry.
(4)将步骤(3)制得的金属模板放入CVD管式炉中,通入氩气作为保护气体;在氩气流量300sccm条件下,50分钟将样品加热至1050℃;在氩气流量50sccm、氢气流量50sccm条件下在1050℃保温35分钟;在氢气流量30sccm、乙炔气体流量50sccm,并管式炉内压强200Pa条件下,将金属模板在1100℃保温15分钟;然后在氩气流量60sccm、氢气流量50sccm条件下冷却至室温,由此制得生长在金属模板上的三维石墨烯,石墨烯层数为1层。(4) Put the metal template prepared in step (3) into a CVD tube furnace, and feed argon as a protective gas; under the condition of an argon flow of 300 sccm, the sample was heated to 1050° C. in 50 minutes; Insulate at 1050°C for 35 minutes under the conditions of 50sccm and hydrogen flow rate of 50sccm; under the conditions of hydrogen flow rate of 30sccm, acetylene gas flow rate of 50sccm, and tube furnace pressure of 200Pa, the metal template was kept at 1100°C for 15 minutes; 1. Cooling to room temperature under the condition of a hydrogen flow rate of 50 sccm, thereby preparing three-dimensional graphene grown on a metal template, and the number of graphene layers is 1 layer.
(5)配置3wt%的PMMA苯甲醚溶液,旋凃于制得的表面长有石墨烯的金属模板上,在100℃条件下保温30分钟使PMMA固化。配置3mol/L的FeCl3水溶液,将制得的产物浸入其中,在50℃温度下回流直至将所述金属模板完全溶解。(5) A 3 wt % PMMA anisole solution was prepared, spin-coated on the prepared metal template with graphene on the surface, and kept at 100° C. for 30 minutes to solidify the PMMA. Prepare a 3 mol/L FeCl 3 aqueous solution, immerse the prepared product in it, and reflux at a temperature of 50° C. until the metal template is completely dissolved.
(6)采用溶剂蒸发的方法将PMMA溶液注入步骤(5)所制备材料的空隙里,蒸发溶剂固化,即得到三维石墨烯复合PMMA材料。测试结果表明,三维石墨烯按设计需求均匀的分布在复合PMMA基体内。(6) The PMMA solution is injected into the voids of the material prepared in step (5) by solvent evaporation, and the solvent is evaporated and solidified to obtain a three-dimensional graphene composite PMMA material. The test results show that the three-dimensional graphene is uniformly distributed in the composite PMMA matrix according to the design requirements.
实施例8Example 8
(1)采用CAD软件,相应建立单元尺寸为1mm的三维多孔单元体,其中将该单元体阵列设计为孔隙率为35%,有序排列的周期性多孔结构,模型外部尺寸为150mm×150mm×50mm。(1) Using CAD software, a three-dimensional porous unit body with a unit size of 1mm is correspondingly established. The unit body array is designed as a periodic porous structure with a porosity of 35% and an orderly arrangement. The external size of the model is 150mm×150mm× 50mm.
(2)采用光固化增材制造技术制备所构建的CAD模型的树脂结构。(2) The resin structure of the constructed CAD model was prepared by light-curing additive manufacturing technology.
(3)将所制备的树脂结构经清洗、粗化、中和、敏化、活化后,采用化学镀镍工艺在树脂结构表面镀铜金属层,化学镀镍液采用硫酸镍为镍盐,亚磷酸钠为还原剂,镀得的金属镍层厚度为20μm。将制得的镀有金属层的树脂结构在氮气保护气氛下600℃热处理5小时,将树脂结构分解去除。(3) After cleaning, coarsening, neutralizing, sensitizing and activating the prepared resin structure, adopt the electroless nickel plating process to plate a copper metal layer on the surface of the resin structure. The electroless nickel plating solution adopts nickel sulfate as nickel salt, sub Sodium phosphate is used as a reducing agent, and the thickness of the metal nickel layer is 20 μm. The prepared resin structure coated with the metal layer was heat-treated at 600° C. for 5 hours under a nitrogen protective atmosphere to decompose and remove the resin structure.
(4)将步骤(3)制得的金属模板放入CVD管式炉中,通入氩气作为保护气体;在氩气流量300sccm条件下,50分钟将样品加热至950℃;在氩气流量50sccm、氢气流量50sccm条件下在950℃保温35分钟;在氢气流量30sccm、乙炔气体流量50sccm,并管式炉内压强50Pa条件下,将金属模板在1100℃保温15分钟;然后在氩气流量60sccm、氢气流量50sccm条件下冷却至室温,由此制得生长在金属模板上的三维石墨烯,石墨烯层数为5层。(4) Put the metal template prepared in step (3) into a CVD tube furnace, and feed argon as a shielding gas; under the condition of an argon flow of 300 sccm, the sample was heated to 950° C. in 50 minutes; Insulate at 950°C for 35 minutes under the conditions of 50sccm and hydrogen flow rate of 50sccm; under the conditions of hydrogen flow rate of 30sccm, acetylene gas flow rate of 50sccm, and tube furnace pressure of 50Pa, the metal template was kept at 1100°C for 15 minutes; 1. Cooling to room temperature under the condition of a hydrogen flow rate of 50 sccm, thus preparing a three-dimensional graphene grown on a metal template, and the number of graphene layers is 5 layers.
(5)配置PDMS固化液,聚合单体和固化剂以10:1的质量比混合,旋凃于制得的表面长有石墨烯的金属模板上,在60℃条件下保温60分钟使PDMS聚合固化。配置3mol/L的硫酸溶液,将制得的产物浸入其中,在90℃温度下回流直至将所述金属模板完全溶解。(5) Configure the PDMS curing liquid, mix the polymerized monomer and curing agent at a mass ratio of 10:1, spin-coat on the prepared metal template with graphene on the surface, and keep the temperature at 60°C for 60 minutes to polymerize PDMS solidify. Prepare a 3 mol/L sulfuric acid solution, immerse the prepared product in it, and reflux at a temperature of 90° C. until the metal template is completely dissolved.
(6)配置PDMS固化液,聚合单体和固化剂以10:1的质量比混合,将PDMS固化液注入步骤(5)所制备材料的空隙里,冷却即得到三维石墨烯复合PDMS材料。测试结果表明,三维石墨烯按设计需求均匀的分布在复合PDMS基体内。(6) Configure the PDMS solidified solution, mix the polymerized monomer and the solidified agent at a mass ratio of 10:1, inject the PDMS solidified solution into the gap of the material prepared in step (5), and cool to obtain a three-dimensional graphene composite PDMS material. The test results show that the three-dimensional graphene is uniformly distributed in the composite PDMS matrix according to the design requirements.
本领域的技术人员容易理解,以上所述仅为本发明的较佳实施例而已,并不用以限制本发明,凡在本发明的精神和原则之内所作的任何修改、等同替换和改进等,均应包含在本发明的保护范围之内。It is easy for those skilled in the art to understand that the above descriptions are only preferred embodiments of the present invention, and are not intended to limit the present invention. Any modifications, equivalent replacements and improvements made within the spirit and principles of the present invention, All should be included within the protection scope of the present invention.
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WO2019192633A1 (en) * | 2018-04-06 | 2019-10-10 | Hermle Maschinenbau Gmbh | Method for producing a component, capsule for hot isostatic pressing and component arrangement |
CN108545723A (en) * | 2018-07-10 | 2018-09-18 | 中喜(宁夏)新材料有限公司 | The method of the preparation of biological alkyl graphene |
CN109095926A (en) * | 2018-08-01 | 2018-12-28 | 中国科学院上海硅酸盐研究所 | A kind of high-volume fractional graphene enhancing carborundum based material and preparation method thereof |
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CN109321770A (en) * | 2018-11-21 | 2019-02-12 | 上海交通大学 | A kind of nano-reinforced porous material and preparation method thereof |
CN110156482B (en) * | 2019-05-28 | 2020-12-29 | 西南交通大学 | A kind of copper-impregnated carbon sliding plate material and preparation method thereof |
CN111424257B (en) * | 2020-03-20 | 2021-07-13 | 西安交通大学 | A kind of three-dimensional network graphene with biomass structure and preparation method thereof |
CN114149002A (en) * | 2021-11-14 | 2022-03-08 | 西北工业大学 | Universal method for preparing nitrogen-doped graphene by 3d printing of recyclable metal salt |
CN115377520A (en) * | 2022-08-01 | 2022-11-22 | 西北工业大学宁波研究院 | Preparation method of nickel-iron battery and nickel-iron battery |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1608244A (en) * | 2001-11-30 | 2005-04-20 | 阿纳洛格装置公司 | Galois field multiply/ multiply-add/multiply accumulate |
CN103213980A (en) * | 2013-05-13 | 2013-07-24 | 中国科学院苏州纳米技术与纳米仿生研究所 | Preparation method of three-dimensional graphene or composite system thereof |
CN105776186A (en) * | 2014-12-25 | 2016-07-20 | 华中科技大学 | Method for preparing structure-controllable three-dimensional graphene porous material |
CN106433133A (en) * | 2016-08-23 | 2017-02-22 | 广东工业大学 | A polymer matrix/three-dimensional graphene thermal interface composite material and its preparation method and application |
-
2017
- 2017-08-09 CN CN201710677410.3A patent/CN107381555B/en active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1608244A (en) * | 2001-11-30 | 2005-04-20 | 阿纳洛格装置公司 | Galois field multiply/ multiply-add/multiply accumulate |
CN103213980A (en) * | 2013-05-13 | 2013-07-24 | 中国科学院苏州纳米技术与纳米仿生研究所 | Preparation method of three-dimensional graphene or composite system thereof |
CN105776186A (en) * | 2014-12-25 | 2016-07-20 | 华中科技大学 | Method for preparing structure-controllable three-dimensional graphene porous material |
CN106433133A (en) * | 2016-08-23 | 2017-02-22 | 广东工业大学 | A polymer matrix/three-dimensional graphene thermal interface composite material and its preparation method and application |
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