CN107446304B - The method of phenolic resin preimpregnation material and its manufacture phenolic composite - Google Patents
The method of phenolic resin preimpregnation material and its manufacture phenolic composite Download PDFInfo
- Publication number
- CN107446304B CN107446304B CN201610366860.6A CN201610366860A CN107446304B CN 107446304 B CN107446304 B CN 107446304B CN 201610366860 A CN201610366860 A CN 201610366860A CN 107446304 B CN107446304 B CN 107446304B
- Authority
- CN
- China
- Prior art keywords
- phenolic resin
- prepreg
- phenolic
- resin
- composite
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 239000000463 material Substances 0.000 title claims abstract description 102
- KXGFMDJXCMQABM-UHFFFAOYSA-N 2-methoxy-6-methylphenol Chemical compound [CH]OC1=CC=CC([CH])=C1O KXGFMDJXCMQABM-UHFFFAOYSA-N 0.000 title claims abstract description 94
- 229920001568 phenolic resin Polymers 0.000 title claims abstract description 93
- 239000005011 phenolic resin Substances 0.000 title claims abstract description 92
- 239000002131 composite material Substances 0.000 title claims abstract description 49
- 238000000034 method Methods 0.000 title claims abstract description 43
- ISWSIDIOOBJBQZ-UHFFFAOYSA-N phenol group Chemical group C1(=CC=CC=C1)O ISWSIDIOOBJBQZ-UHFFFAOYSA-N 0.000 title claims abstract description 36
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 19
- 229920005989 resin Polymers 0.000 claims abstract description 41
- 239000011347 resin Substances 0.000 claims abstract description 41
- 239000004744 fabric Substances 0.000 claims abstract description 40
- 239000002562 thickening agent Substances 0.000 claims abstract description 26
- 230000004888 barrier function Effects 0.000 claims abstract description 21
- 230000008569 process Effects 0.000 claims abstract description 8
- 238000003475 lamination Methods 0.000 claims description 34
- 239000011162 core material Substances 0.000 claims description 32
- 238000007789 sealing Methods 0.000 claims description 31
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 claims description 29
- -1 phenolic aldehyde Chemical class 0.000 claims description 27
- 238000005470 impregnation Methods 0.000 claims description 26
- 238000001035 drying Methods 0.000 claims description 25
- 238000002360 preparation method Methods 0.000 claims description 22
- 239000007789 gas Substances 0.000 claims description 21
- 230000008719 thickening Effects 0.000 claims description 20
- 239000012745 toughening agent Substances 0.000 claims description 19
- 235000019441 ethanol Nutrition 0.000 claims description 18
- LYCAIKOWRPUZTN-UHFFFAOYSA-N Ethylene glycol Chemical compound OCCO LYCAIKOWRPUZTN-UHFFFAOYSA-N 0.000 claims description 17
- 239000002253 acid Substances 0.000 claims description 14
- OSGAYBCDTDRGGQ-UHFFFAOYSA-L calcium sulfate Chemical compound [Ca+2].[O-]S([O-])(=O)=O OSGAYBCDTDRGGQ-UHFFFAOYSA-L 0.000 claims description 14
- 150000007942 carboxylates Chemical class 0.000 claims description 14
- 238000003860 storage Methods 0.000 claims description 14
- CPLXHLVBOLITMK-UHFFFAOYSA-N Magnesium oxide Chemical group [Mg]=O CPLXHLVBOLITMK-UHFFFAOYSA-N 0.000 claims description 13
- 238000007711 solidification Methods 0.000 claims description 11
- 230000008023 solidification Effects 0.000 claims description 11
- DNIAPMSPPWPWGF-UHFFFAOYSA-N Propylene glycol Chemical compound CC(O)CO DNIAPMSPPWPWGF-UHFFFAOYSA-N 0.000 claims description 9
- 239000000203 mixture Substances 0.000 claims description 9
- NBIIXXVUZAFLBC-UHFFFAOYSA-N Phosphoric acid Chemical group OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 claims description 8
- 229920003987 resole Polymers 0.000 claims description 8
- 239000005062 Polybutadiene Substances 0.000 claims description 7
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 7
- 238000010438 heat treatment Methods 0.000 claims description 7
- 239000000395 magnesium oxide Substances 0.000 claims description 7
- 229920002857 polybutadiene Polymers 0.000 claims description 7
- BIKXLKXABVUSMH-UHFFFAOYSA-N trizinc;diborate Chemical compound [Zn+2].[Zn+2].[Zn+2].[O-]B([O-])[O-].[O-]B([O-])[O-] BIKXLKXABVUSMH-UHFFFAOYSA-N 0.000 claims description 7
- JYEUMXHLPRZUAT-UHFFFAOYSA-N 1,2,3-triazine Chemical compound C1=CN=NN=C1 JYEUMXHLPRZUAT-UHFFFAOYSA-N 0.000 claims description 6
- 229920001730 Moisture cure polyurethane Polymers 0.000 claims description 6
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 claims description 6
- ZJCCRDAZUWHFQH-UHFFFAOYSA-N Trimethylolpropane Chemical compound CCC(CO)(CO)CO ZJCCRDAZUWHFQH-UHFFFAOYSA-N 0.000 claims description 6
- WNROFYMDJYEPJX-UHFFFAOYSA-K aluminium hydroxide Chemical compound [OH-].[OH-].[OH-].[Al+3] WNROFYMDJYEPJX-UHFFFAOYSA-K 0.000 claims description 6
- 239000004327 boric acid Substances 0.000 claims description 6
- QYCDATSIIJDLGY-UHFFFAOYSA-N imidazolidine;1,3-oxazolidine Chemical compound C1CNCN1.C1COCN1 QYCDATSIIJDLGY-UHFFFAOYSA-N 0.000 claims description 6
- JEIPFZHSYJVQDO-UHFFFAOYSA-N iron(III) oxide Inorganic materials O=[Fe]O[Fe]=O JEIPFZHSYJVQDO-UHFFFAOYSA-N 0.000 claims description 6
- WRYCSMQKUKOKBP-UHFFFAOYSA-N Imidazolidine Chemical compound C1CNCN1 WRYCSMQKUKOKBP-UHFFFAOYSA-N 0.000 claims description 5
- WYNCHZVNFNFDNH-UHFFFAOYSA-N Oxazolidine Chemical compound C1COCN1 WYNCHZVNFNFDNH-UHFFFAOYSA-N 0.000 claims description 5
- KGBXLFKZBHKPEV-UHFFFAOYSA-N boric acid Chemical compound OB(O)O KGBXLFKZBHKPEV-UHFFFAOYSA-N 0.000 claims description 5
- BRPQOXSCLDDYGP-UHFFFAOYSA-N calcium oxide Chemical compound [O-2].[Ca+2] BRPQOXSCLDDYGP-UHFFFAOYSA-N 0.000 claims description 5
- 239000000292 calcium oxide Substances 0.000 claims description 5
- ODINCKMPIJJUCX-UHFFFAOYSA-N calcium oxide Inorganic materials [Ca]=O ODINCKMPIJJUCX-UHFFFAOYSA-N 0.000 claims description 5
- 239000006229 carbon black Substances 0.000 claims description 5
- 150000004893 oxazines Chemical class 0.000 claims description 5
- 229920000137 polyphosphoric acid Polymers 0.000 claims description 5
- 239000000565 sealant Substances 0.000 claims description 5
- 238000010583 slow cooling Methods 0.000 claims description 5
- 240000007182 Ochroma pyramidale Species 0.000 claims description 4
- 239000004372 Polyvinyl alcohol Substances 0.000 claims description 4
- 229910000147 aluminium phosphate Inorganic materials 0.000 claims description 4
- LNDKRVOOYMEYTC-UHFFFAOYSA-N buta-1,3-dien-1-ol Chemical compound OC=CC=C LNDKRVOOYMEYTC-UHFFFAOYSA-N 0.000 claims description 4
- 239000006260 foam Substances 0.000 claims description 4
- 229920001451 polypropylene glycol Polymers 0.000 claims description 4
- 229920002451 polyvinyl alcohol Polymers 0.000 claims description 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 4
- WHOZNOZYMBRCBL-OUKQBFOZSA-N (2E)-2-Tetradecenal Chemical compound CCCCCCCCCCC\C=C\C=O WHOZNOZYMBRCBL-OUKQBFOZSA-N 0.000 claims description 3
- CTQNGGLPUBDAKN-UHFFFAOYSA-N O-Xylene Chemical compound CC1=CC=CC=C1C CTQNGGLPUBDAKN-UHFFFAOYSA-N 0.000 claims description 3
- 239000002202 Polyethylene glycol Substances 0.000 claims description 3
- SRSXLGNVWSONIS-UHFFFAOYSA-N benzenesulfonic acid Chemical compound OS(=O)(=O)C1=CC=CC=C1 SRSXLGNVWSONIS-UHFFFAOYSA-N 0.000 claims description 3
- 229940092714 benzenesulfonic acid Drugs 0.000 claims description 3
- 238000013461 design Methods 0.000 claims description 3
- 238000000605 extraction Methods 0.000 claims description 3
- WXZMFSXDPGVJKK-UHFFFAOYSA-N pentaerythritol Chemical compound OCC(CO)(CO)CO WXZMFSXDPGVJKK-UHFFFAOYSA-N 0.000 claims description 3
- 229940044654 phenolsulfonic acid Drugs 0.000 claims description 3
- WVDDGKGOMKODPV-ZQBYOMGUSA-N phenyl(114C)methanol Chemical compound O[14CH2]C1=CC=CC=C1 WVDDGKGOMKODPV-ZQBYOMGUSA-N 0.000 claims description 3
- 229920001223 polyethylene glycol Polymers 0.000 claims description 3
- ISIJQEHRDSCQIU-UHFFFAOYSA-N tert-butyl 2,7-diazaspiro[4.5]decane-7-carboxylate Chemical compound C1N(C(=O)OC(C)(C)C)CCCC11CNCC1 ISIJQEHRDSCQIU-UHFFFAOYSA-N 0.000 claims description 3
- JOXIMZWYDAKGHI-UHFFFAOYSA-N toluene-4-sulfonic acid Chemical compound CC1=CC=C(S(O)(=O)=O)C=C1 JOXIMZWYDAKGHI-UHFFFAOYSA-N 0.000 claims description 3
- 229920001807 Urea-formaldehyde Polymers 0.000 claims description 2
- 239000003610 charcoal Substances 0.000 claims description 2
- 239000003795 chemical substances by application Substances 0.000 claims description 2
- ODGAOXROABLFNM-UHFFFAOYSA-N polynoxylin Chemical compound O=C.NC(N)=O ODGAOXROABLFNM-UHFFFAOYSA-N 0.000 claims description 2
- 230000002194 synthesizing effect Effects 0.000 claims 2
- LSNNMFCWUKXFEE-UHFFFAOYSA-M Bisulfite Chemical compound OS([O-])=O LSNNMFCWUKXFEE-UHFFFAOYSA-M 0.000 claims 1
- XSTXAVWGXDQKEL-UHFFFAOYSA-N Trichloroethylene Chemical compound ClC=C(Cl)Cl XSTXAVWGXDQKEL-UHFFFAOYSA-N 0.000 claims 1
- OBNDGIHQAIXEAO-UHFFFAOYSA-N [O].[Si] Chemical compound [O].[Si] OBNDGIHQAIXEAO-UHFFFAOYSA-N 0.000 claims 1
- 150000001335 aliphatic alkanes Chemical class 0.000 claims 1
- 125000005909 ethyl alcohol group Chemical group 0.000 claims 1
- 239000002699 waste material Substances 0.000 abstract description 7
- 239000007788 liquid Substances 0.000 abstract description 3
- 238000009826 distribution Methods 0.000 abstract description 2
- 239000012530 fluid Substances 0.000 abstract description 2
- 230000002401 inhibitory effect Effects 0.000 abstract description 2
- 230000035699 permeability Effects 0.000 abstract description 2
- 238000001723 curing Methods 0.000 description 30
- 239000010408 film Substances 0.000 description 24
- 239000003063 flame retardant Substances 0.000 description 11
- 239000010410 layer Substances 0.000 description 11
- 239000000243 solution Substances 0.000 description 11
- 239000005060 rubber Substances 0.000 description 8
- RNFJDJUURJAICM-UHFFFAOYSA-N 2,2,4,4,6,6-hexaphenoxy-1,3,5-triaza-2$l^{5},4$l^{5},6$l^{5}-triphosphacyclohexa-1,3,5-triene Chemical compound N=1P(OC=2C=CC=CC=2)(OC=2C=CC=CC=2)=NP(OC=2C=CC=CC=2)(OC=2C=CC=CC=2)=NP=1(OC=1C=CC=CC=1)OC1=CC=CC=C1 RNFJDJUURJAICM-UHFFFAOYSA-N 0.000 description 7
- 238000007598 dipping method Methods 0.000 description 7
- 229920001971 elastomer Polymers 0.000 description 7
- 239000002904 solvent Substances 0.000 description 7
- HEMHJVSKTPXQMS-UHFFFAOYSA-M Sodium hydroxide Chemical compound [OH-].[Na+] HEMHJVSKTPXQMS-UHFFFAOYSA-M 0.000 description 6
- 150000002148 esters Chemical class 0.000 description 6
- 238000003912 environmental pollution Methods 0.000 description 5
- 239000003292 glue Substances 0.000 description 5
- 238000000465 moulding Methods 0.000 description 5
- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 description 4
- 230000000052 comparative effect Effects 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 239000003365 glass fiber Substances 0.000 description 4
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 3
- 239000000835 fiber Substances 0.000 description 3
- 238000002386 leaching Methods 0.000 description 3
- 239000003960 organic solvent Substances 0.000 description 3
- 229910052698 phosphorus Inorganic materials 0.000 description 3
- 239000011574 phosphorus Substances 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 238000011074 autoclave method Methods 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- YCIMNLLNPGFGHC-UHFFFAOYSA-N catechol Chemical group OC1=CC=CC=C1O YCIMNLLNPGFGHC-UHFFFAOYSA-N 0.000 description 2
- 238000002485 combustion reaction Methods 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 239000003085 diluting agent Substances 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 235000011187 glycerol Nutrition 0.000 description 2
- 230000010354 integration Effects 0.000 description 2
- 238000002955 isolation Methods 0.000 description 2
- RCHKEJKUUXXBSM-UHFFFAOYSA-N n-benzyl-2-(3-formylindol-1-yl)acetamide Chemical compound C12=CC=CC=C2C(C=O)=CN1CC(=O)NCC1=CC=CC=C1 RCHKEJKUUXXBSM-UHFFFAOYSA-N 0.000 description 2
- 229920001343 polytetrafluoroethylene Polymers 0.000 description 2
- 239000004810 polytetrafluoroethylene Substances 0.000 description 2
- 238000004080 punching Methods 0.000 description 2
- GHMLBKRAJCXXBS-UHFFFAOYSA-N resorcinol Chemical compound OC1=CC=CC(O)=C1 GHMLBKRAJCXXBS-UHFFFAOYSA-N 0.000 description 2
- 239000002356 single layer Substances 0.000 description 2
- 239000000779 smoke Substances 0.000 description 2
- 238000003786 synthesis reaction Methods 0.000 description 2
- 229920001169 thermoplastic Polymers 0.000 description 2
- 230000001988 toxicity Effects 0.000 description 2
- 231100000419 toxicity Toxicity 0.000 description 2
- HVLLSGMXQDNUAL-UHFFFAOYSA-N triphenyl phosphite Chemical compound C=1C=CC=CC=1OP(OC=1C=CC=CC=1)OC1=CC=CC=C1 HVLLSGMXQDNUAL-UHFFFAOYSA-N 0.000 description 2
- DGXAGETVRDOQFP-UHFFFAOYSA-N 2,6-dihydroxybenzaldehyde Chemical compound OC1=CC=CC(O)=C1C=O DGXAGETVRDOQFP-UHFFFAOYSA-N 0.000 description 1
- WKBOTKDWSSQWDR-UHFFFAOYSA-N Bromine atom Chemical compound [Br] WKBOTKDWSSQWDR-UHFFFAOYSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- IMROMDMJAWUWLK-UHFFFAOYSA-N Ethenol Chemical compound OC=C IMROMDMJAWUWLK-UHFFFAOYSA-N 0.000 description 1
- XXFKYQVWZOJMRR-UHFFFAOYSA-N OC1=CC=C(C=C1)C(C)(C)C1=CC=C(C=C1)O.[Br] Chemical compound OC1=CC=C(C=C1)C(C)(C)C1=CC=C(C=C1)O.[Br] XXFKYQVWZOJMRR-UHFFFAOYSA-N 0.000 description 1
- BPQQTUXANYXVAA-UHFFFAOYSA-N Orthosilicate Chemical compound [O-][Si]([O-])([O-])[O-] BPQQTUXANYXVAA-UHFFFAOYSA-N 0.000 description 1
- 239000004698 Polyethylene Substances 0.000 description 1
- HXMUYYHTXVEPPM-UHFFFAOYSA-N [S].CC1=C(C=CC=C1)C Chemical compound [S].CC1=C(C=CC=C1)C HXMUYYHTXVEPPM-UHFFFAOYSA-N 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- 229910021502 aluminium hydroxide Inorganic materials 0.000 description 1
- 229910000410 antimony oxide Inorganic materials 0.000 description 1
- 125000003118 aryl group Chemical group 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 229910052788 barium Inorganic materials 0.000 description 1
- DSAJWYNOEDNPEQ-UHFFFAOYSA-N barium atom Chemical compound [Ba] DSAJWYNOEDNPEQ-UHFFFAOYSA-N 0.000 description 1
- RQPZNWPYLFFXCP-UHFFFAOYSA-L barium dihydroxide Chemical compound [OH-].[OH-].[Ba+2] RQPZNWPYLFFXCP-UHFFFAOYSA-L 0.000 description 1
- 229910001863 barium hydroxide Inorganic materials 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 125000005619 boric acid group Chemical group 0.000 description 1
- GDTBXPJZTBHREO-UHFFFAOYSA-N bromine Substances BrBr GDTBXPJZTBHREO-UHFFFAOYSA-N 0.000 description 1
- 229910052794 bromium Inorganic materials 0.000 description 1
- 150000007516 brønsted-lowry acids Chemical class 0.000 description 1
- 150000007528 brønsted-lowry bases Chemical class 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 239000003054 catalyst Substances 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 235000019504 cigarettes Nutrition 0.000 description 1
- 239000004927 clay Substances 0.000 description 1
- 238000009833 condensation Methods 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 239000007822 coupling agent Substances 0.000 description 1
- 238000000280 densification Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000007865 diluting Methods 0.000 description 1
- 238000010790 dilution Methods 0.000 description 1
- 239000012895 dilution Substances 0.000 description 1
- ASMQGLCHMVWBQR-UHFFFAOYSA-M diphenyl phosphate Chemical group C=1C=CC=CC=1OP(=O)([O-])OC1=CC=CC=C1 ASMQGLCHMVWBQR-UHFFFAOYSA-M 0.000 description 1
- 235000013399 edible fruits Nutrition 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 239000002657 fibrous material Substances 0.000 description 1
- 238000004079 fireproofing Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 229910052736 halogen Inorganic materials 0.000 description 1
- 150000002367 halogens Chemical class 0.000 description 1
- 208000021760 high fever Diseases 0.000 description 1
- 239000012943 hotmelt Substances 0.000 description 1
- 125000002887 hydroxy group Chemical group [H]O* 0.000 description 1
- WGCNASOHLSPBMP-UHFFFAOYSA-N hydroxyacetaldehyde Natural products OCC=O WGCNASOHLSPBMP-UHFFFAOYSA-N 0.000 description 1
- 125000002632 imidazolidinyl group Chemical group 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000001802 infusion Methods 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- AXZKOIWUVFPNLO-UHFFFAOYSA-N magnesium;oxygen(2-) Chemical compound [O-2].[Mg+2] AXZKOIWUVFPNLO-UHFFFAOYSA-N 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 239000012528 membrane Substances 0.000 description 1
- 239000003595 mist Substances 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- QJGQUHMNIGDVPM-UHFFFAOYSA-N nitrogen group Chemical group [N] QJGQUHMNIGDVPM-UHFFFAOYSA-N 0.000 description 1
- 239000011368 organic material Substances 0.000 description 1
- VTRUBDSFZJNXHI-UHFFFAOYSA-N oxoantimony Chemical compound [Sb]=O VTRUBDSFZJNXHI-UHFFFAOYSA-N 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 230000036314 physical performance Effects 0.000 description 1
- 239000000049 pigment Substances 0.000 description 1
- 238000006068 polycondensation reaction Methods 0.000 description 1
- 229920000573 polyethylene Polymers 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 229920002379 silicone rubber Polymers 0.000 description 1
- 150000003384 small molecules Chemical class 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 229920002725 thermoplastic elastomer Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
- 239000010456 wollastonite Substances 0.000 description 1
- 229910052882 wollastonite Inorganic materials 0.000 description 1
- 239000002023 wood Substances 0.000 description 1
- 239000008096 xylene Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08L—COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
- C08L61/00—Compositions of condensation polymers of aldehydes or ketones; Compositions of derivatives of such polymers
- C08L61/04—Condensation polymers of aldehydes or ketones with phenols only
- C08L61/06—Condensation polymers of aldehydes or ketones with phenols only of aldehydes with phenols
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B21/00—Layered products comprising a layer of wood, e.g. wood board, veneer, wood particle board
- B32B21/10—Next to a fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B25/00—Layered products comprising a layer of natural or synthetic rubber
- B32B25/04—Layered products comprising a layer of natural or synthetic rubber comprising rubber as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B25/08—Layered products comprising a layer of natural or synthetic rubber comprising rubber as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B25/00—Layered products comprising a layer of natural or synthetic rubber
- B32B25/10—Layered products comprising a layer of natural or synthetic rubber next to a fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B25/00—Layered products comprising a layer of natural or synthetic rubber
- B32B25/20—Layered products comprising a layer of natural or synthetic rubber comprising silicone rubber
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
- B32B27/08—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/12—Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B27/00—Layered products comprising a layer of synthetic resin
- B32B27/32—Layered products comprising a layer of synthetic resin comprising polyolefins
-
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Abstract
The invention discloses the methods of a kind of phenolic resin preimpregnation material and its manufacture phenolic composite, and prepreg includes following components in parts by weight: 50~65 parts of fabric, 20~48 parts of phenolic resin, 1~5 part of thickener.The method of phenolic resin preimpregnation material manufacture phenolic composite uses the cured technique of vacuum bag, uses microporous barrier in the process, and the micropore size of the microporous barrier is 0.1~10um, and with a thickness of between 2~300um, porosity is 50%~80%;Since micropore size is up to ten thousand times of fluid molecule diameter, hundred times smaller than drop diameter, therefore there is excellent moisture-inhibiting, ventilative and anti-drop permeability, escaping gas is extracted when to vacuumize, and liquid resin component will not be extracted, avoiding resin from being extracted leads to the non-uniform problem of resin distribution, reduces waste of material and waste.
Description
Technical field
The invention belongs to technical field of composite materials, and in particular to a kind of phenolic resin preimpregnation material, phenolic resin preimpregnation material
Preparation method and prepreg manufacture phenolic composite method.
Background technique
Phenolic resin is the artificial resin of first commercial applications in human history, because it is with good heat resistance
Energy, flame retardant property, corrosion resistance (except oxidisability bronsted lowry acids and bases bronsted lowry), high-temperature creep resistance, are all widely applied, such as so far
It is used to prepare a variety of heat resistant articles, anticorrosion material, fire proofing etc..
After phenolic resin curing, aromatic ring is fine and close on molecular structure, encounters high fever and burns the layer of charcoal of densification easy to form, slows down
Intrusion of the heat to material internal, has also completely cut off the entrance of oxygen;The cigarette that the calory burning released when therefore burning is low, discharges
Mist is few, and the toxicity of smog is low, shows excellent flame retardant property (FST).Due to the anti-flammability of phenolic resin itself
Can be splendid, so not needing to add various fire retardants as other flame-retarded resins, such as halogen, nitrogenous class, containing Phosphorus;Or tree
The elements such as nitrogen, phosphorus are introduced in the molecular structure of rouge.From various countries to the toxicity requirements of material, such as Britain's rail traffic standard
BS6853 Appendix D, Boeing standard BSS7239, all to CO, CO2、HF、HCl、HBr、HCN、NO2、SO2The release of eight kinds of gases is dense
Degree is strictly limited.Phenolic resin does not need outer addition fire retardant, so general performance comes out due to the flame-retarding characteristic of itself
FST performance be optimal in all organic materials.
Phenolic resin is usually used in preparing aviation, the interior material in rail traffic with its excellent flame retardant property.But phenolic aldehyde
Material has its weakness, that is, belongs to fragile material, poor toughness;In addition, material can discharge hydrone during curing molding, these
Moisture is generally difficult to whole discharges, and causing material internal, there are many micropores, to influence the mechanical strength of phenolic materials.Therefore
Around phenolic materials toughening and intensity is improved, numerous researchers have carried out a large amount of research to it, also achieved many achievements.
In recent years, phenolic resin preimpregnation material is widely used in the preparation of aircraft interior material, phenolic resin preimpregnation material system
It is convenient to make product, product strength, flame retardant property are all more satisfactory.
There are mainly two types of ie in solution infusion process and Hot-melt film methods for the preparation method of prepreg.Solution dipping method is by fiber
Or fabric is after resin solution impregnates, the technique that the solvent in resin is vapored away, and prepreg is made to reach B-stage;The method
Production equipment less investment, the disadvantage is that prepreg resin content is difficult to control accurately, a large amount of solvent volatilizations form environmental pollution.Heat
Melten gel embrane method is the glue film that the resin of melting is made to uniform ground first, then by glue film and fiber or fabric in certain temperature
With compound dipping is carried out under pressure, obtain qualified prepreg;This technological advantage is that resin content control is accurate, fugitive constituent is few, nothing
Environmental pollution;The disadvantage is that equipment investment is high.
For solution dipping method, equipment is simple, less investment, simple production process, as long as being avoided that solvent volatilizees, reduction is waved
Hair part content controls prepreg resin content, can form the solution dipping method of improvement.
101735551 A(application number 200810180315.3 of Chinese patent literature CN) one kind is disclosed with high temperature power
The heat-insulation composite material and preparation method thereof of performance is learned, is a kind of phenolic aldehyde prepreg on the material, main component is barium phenol
Urea formaldehyde, ethyl alcohol and high strength glass fiber sheet.First high strength glass fiber sheet is cut out and is heat-treated when preparation, by barium phenolic aldehyde
Resin and ethyl alcohol are mixed into resin adhesive liquid according to 60:40, dry drying after impregnation, obtain phenolic composite prepreg.
It is fire-retardant that 102731960 B of Chinese patent literature CN (application number 201210211451.0) discloses a kind of high tenacity
The preparation method of phenolic aldehyde prepreg composite, by introducing thermoplastic polymer and rubber toughener into phenolic resin,
The toughness of composite material is substantially increased, while introducing bromine/Sb system fire retardant and compensating under flame retardant property caused by toughener
The problem of drop;Ethyl alcohol is used as diluent in disclosed preimpregnation preparation method for material simultaneously, makes phenolic resin, toughener, four
The mixed viscosity of bromine bisphenol-A, antimony oxide is lower, is suitble to the impregnation to fibrous material.
104194256 A(application number 201410330863.6 of Chinese patent literature CN) in disclose a kind of toughening type ring
Protect the glass fibre prepreg cloth of phenolic resin, including following component: Environmental protection phenol formaldehyde resin, alkali-free glass fiber cloth, coupling agent KH-560,
Inner pattern releasing agent applicable, pigment, silica, industrial alcohol, graphite, wollastonite.
Existing solution dipping method prepares in the technology of phenolic resin preimpregnation material and uses ethyl alcohol in above-mentioned three applications
As solvent.Phenolic resin curing belongs to polycondensation reaction, can generate small molecule water, and volatilization remains in material not the part gone out
In, micropore is formed, to have an adverse effect to material mechanical performance and flame retardant property, so most of phenolic aldehyde prepregs all select
With molecular weight phenolic resin as high as possible, to reduce the yield of phenolic aldehyde prepreg moisture when solidifying;But phenolic resin
Molecular weight is higher, and viscosity is bigger, is more difficult to be impregnated with glass-fiber-fabric, so all employing ethyl alcohol in above patent document as solvent
Or referred to as diluent, the viscosity for reducing phenolic resin go on smoothly impregnation.After completing impregnation, the ethyl alcohol used will lead to
The problems such as crossing heating evaporation to fall, doing so " a large amount of solvent volatilizations, environmental pollution " for just producing solution dipping method;Another party
Face, the ethyl alcohol in prepreg can not completely be discharged except prepreg, thus to the anti-flammability of phenolic composite have compared with
Big influence.
When manufacturing composite material with prepreg, optimal method is autoclave method, and autoclave method is (general simultaneously also in relation with true
Empty bag method) lower than 1%, product strength performance is best for the obtained porosity of composite product;But the cost of autoclave is very
It is high.Develop the outer curing method of tank, i.e. OoA method again in recent years, vacuum bag pressure method is exactly one of.Vacuum bag pressure method can save
The manufacture for removing high-cost autoclave uses common drying chamber.
Since laying can bring a certain amount of gas into existing vacuum bag pressure method technique, so in the curing process of prepreg
In, it is usually laid with isolation film with holes on the surface of prepreg, adds inhale rubber mat and airfelt above;It is convenient for so under vacuum,
Gas inside prepreg can be smoothly extracted.But it is also higher to inhale glue material cost, while the process for inhaling glue need to be specific
In temperature range, Resin Flow cannot be excessive, and otherwise resin is extracted excessively;Resin Flow can not be too small, otherwise gas
It is complete that body is not easy discharge;This requires the viscosity temperature characteristic of prepreg is extremely stable, so the control for inhaling glue process is very difficult.
Importantly, these moisture are taken out in a manner of steam by inhaling glue-line since phenolic aldehyde prepreg can discharge water in solidification
A certain amount of resin would generally be taken when out out of, cause resin content uneven, also result in waste of material and environmental pollution.
Summary of the invention
Technical problem to be solved by the invention is to provide a kind of phenol that the phenolic resin by low molecular weight, low viscosity is made
The method of urea formaldehyde prepreg, the preparation method of phenolic resin preimpregnation material and prepreg manufacture composite material.
The technical solution for realizing an object of the present disclosure is a kind of phenolic resin preimpregnation material, in parts by weight includes with the following group
Point: 50~65 parts of fabric, 20~48 parts of phenolic resin, 1~5 part of thickener.
The phenolic resin is resol, and viscosity is 300~1500mPas;The thickener be magnesia,
One of calcium oxide, calcium sulfate, nano-grade aluminum hydroxide, white carbon black, boric acid, zinc borate or more than one composition.
Preferably, further including 1~10 part of curing accelerator, the curing accelerator is imidazolidine, triazine, oxazole
Alkane, oxazines, imidazolidine-oxazolidine hybrid, the resorcinol of etherificate, one of the carboxylate of strong acid or more than one group
Close object.Wherein the strong acid of synthetic ester is phosphoric acid, polyphosphoric acids, phosphorous acid, sulfuric acid, benzene sulfonic acid, p-methyl benzenesulfonic acid, dimethylbenzene sulphur
One of acid, phenolsulfonic acid;The alcohol of synthetic ester be ethyl alcohol, ethylene glycol, polyethylene glycol, propylene glycol, polypropylene glycol, glycerine,
One of pentaerythrite, benzyl alcohol, trimethylolpropane, phenol.
It is selectable, it further include 1~8 part of toughener;The toughener is base polyurethane prepolymer for use as, methoxy radical siloxane, gathers
One of vinyl alcohol, end hydroxy butadiene, carboxyl-terminated polybutadiene.
The technical solution for realizing the second purpose of the invention is a kind of preparation method of phenolic resin preimpregnation material as described above,
The following steps are included:
1. weighed phenolic resin and thickener will be uniformly mixed for use in dispersator according to parts by weight;Phenolic aldehyde
Resin is resol, and viscosity is 300~1500mPas;Thickener is magnesia, calcium oxide, calcium sulfate, nanoscale
One of aluminium hydroxide, white carbon black, boric acid, zinc borate or more than one composition.
2. fabric is connected on impregnation unit;1. material that step is mixed pours into the resin storage tank of impregnation unit
In, resin storage tank temperature control system is at 25 DEG C~80 DEG C;
3. starting impregnation unit, after fabric is impregnated with resin in resin storage tank, extraction is moved through pressure roller, enters increasing with film carrier
Thick drying tunnel;Thickening drying tunnel temperature is 40 DEG C~95 DEG C, and the fabric after impregnation is 0.5~5h, thickening by the time of thickening drying tunnel
It finishes to obtain phenolic resin preimpregnation material.
As optional, 1. step also weighs 1~10 part of curing accelerator and/or 1~8 part of toughener, will be according to weight
The weighed phenolic resin of number, thickener, toughener and/or curing accelerator are uniformly mixed stand-by in dispersator.
The curing accelerator is between imidazolidine, triazine, oxazolidine, oxazines, imidazolidine-oxazolidine hybrid, etherificate
One of the carboxylate or more than one composition of benzenediol, strong acid;The toughener is base polyurethane prepolymer for use as, methoxyl group
One of siloxanes, polyvinyl alcohol, end hydroxy butadiene, carboxyl-terminated polybutadiene.
The technical solution for realizing third purpose of the present invention is that a kind of phenolic resin preimpregnation material manufacture phenolic aldehyde is compound
The method of material, using the cured technique of vacuum bag, comprising the following steps:
1. prepreg is cut by required size, remove release film, lamination is successively completed on mold, is then presoaking
Material surface is successively laid with porous release film, microporous barrier, gas permeable material;The micropore size of the microporous barrier is 0.1~10um, thickness
Between 2~300um, porosity is 50%~80%;The lamination refers to prepreg is successively completed after obtained stacked body, press
Design thickness and prepreg thickness in monolayer according to phenolic composite determine the number of plies of prepreg in lamination.
2. being laid with sealant tape in mold surrounding, one, vacuum tube is touched on gas permeable material, and other end connects external vacuum
Pipeline is completed vacuum bag film and is sealed.
3. mold is integrally put into drying chamber, vacuum pump is opened, keeps pressure in -0.085~-0.01MPa;Heating is opened,
90 DEG C~160 DEG C are slowly increased to, Slow cooling demoulds after the completion of material solidification, obtains cured composite material.
Optionally, when 1. step is laid with lamination, between the adjacent two layers prepreg among lamination be laid with foam core material or
Honeycomb core material or cork wood, two pieces of prepregs and in-between core material form sandwich structure.
Preferably, step also uses edge sealing member when 1. middle laying has the lamination of core material, the edge sealing member is upper and lower
The vertical face thickness of perforative integrated frame shape prefabricated component, the frame shape prefabricated component is identical as the thickness of core material, the width of frame be 1 to
10cm, edge sealing member are the prefabricated profiled phenolic composite of integration.Edge sealing member is bonded the surrounding that core material is arranged in, edge sealing member
Surrounding outer rim and composite element edge profile are in same facade;The prepreg lamination below core material is first completed when laying
It is laid with, places edge sealing member, the horizontal plane of spread prepreg and edge elevation are compacted with edge sealing member, then core material is filled in frame
In the frame of shape edge sealing member, continue the laying of the prepreg above core material and edge sealing member.
It as optional, is laid with before prepreg lamination on mold, is first successively laid with gas permeable material, microporous barrier, with holes
Isolation film.
The present invention has the effect of positive:
(1) phenolic resin of the invention preimpregnation material uses the phenolic aldehyde of low viscosity (viscosity is 300~1500mPas)
Resin is used directly for impregnation operation or under lower heating temperature since phenolic resin viscosity is low when preparing prepreg
Impregnation is carried out, when impregnation does not need using ethyl alcohol or other organic solvent diluting phenolic resin;After the completion of the impregnation of fabric,
The molecular weight that thickening improves phenolic resin is carried out at a certain temperature.Phenolic resin preimpregnation material of the invention solidifies in final molding
When the moisture that generates it is few, micropore quantity is few in the composite product prepared with prepreg, quality of item is high.
(2) it is easy to operate using the phenolic resin of low molecular weight to prepare prepreg by the present invention, due to not needing using ethyl alcohol
Or other organic solvents, therefore the preparation method of prepreg of the present invention solves a large amount of solvents existing for existing solution dipping method and waves
The problems such as hair, environmental pollution.In addition, due to, without ethyl alcohol or other organic solvents, avoiding answering for prepreg preparation in prepreg
The problem of fire block articles performance caused by dissolvent residual declines in laminate article.
(3) phenolic resin of the invention preimpregnation material uses the phenolic resin of low molecular weight as raw material, due in prepreg
The molecular weight that phenolic resin can be improved while thickening operation is carried out containing thickener, after impregnation;Thickening operation is easy to control, control
Thickening operation can control the molecular weight of phenolic resin in prepreg simultaneously, to obtain the prepreg of different tack sizes.
(4) curing accelerator uses allow prepreg at 100 DEG C~120 DEG C lower in prepreg of the invention
At a temperature of curing molding, the lower temperature be compared with the prior art in phenolic resin 130 DEG C~160 DEG C of relatively high solidification temperature
For degree;Lower solidification temperature greatly reduces energy consumption, and reduces the cost of mold.
(5) prepreg Storage period of the invention is long, can store 2 months at 25 DEG C.
(6) the cured technique of vacuum bag is used when manufacturing composite material using prepreg of the invention, the present invention is in the work
Microporous barrier is used in skill, the micropore size of the microporous barrier is 0.1~10um, with a thickness of between 2~300um, porosity is 50%~
80%;Since micropore size is up to ten thousand times of fluid molecule diameter, hundred times smaller than drop diameter, therefore have excellent moisture-inhibiting,
Ventilative and anti-drop permeability, so that escaping gas is extracted when vacuumizing, and liquid resin component will not be extracted, and be avoided
Resin, which is extracted, leads to the non-uniform problem of resin distribution, reduces waste of material and waste.
(7) it due to the use of microporous barrier when phenolic aldehyde prepreg of the invention manufactures composite material, reduces viscous to prepreg
The strict demand of temperature characteristics and solidification temperature.
(8) present invention uses prefabricated edge sealing member, can increase the intensity at composite product edge;Meanwhile may be used also
When being laid with solving prepreg, intractable property at the angle R that die edge horizontal plane intersects with facade makes composite wood obtained
Material component possesses intact edge quality.
Specific embodiment
(embodiment 1)
The phenolic resin preimpregnation material of the present embodiment includes following components: 58 parts of fabric, phenolic resin in parts by weight
39 parts, 2 parts of thickener, 1 part of curing accelerator.
Fabric in the present embodiment is 800g/m2Bi-axial fabric.
Phenolic resin is resol, and the catalyst of synthetic reaction is sodium hydroxide, viscosity is 300~
It is 900 mPas in 1500mPas(the present embodiment).
The thickener is magnesia, in calcium oxide, calcium sulfate, nano-grade aluminum hydroxide, white carbon black, boric acid, zinc borate
One or more kinds of compositions, the thickener of the present embodiment is calcium sulfate.
The curing accelerator is between imidazolidine, triazine, oxazolidine, oxazines, imidazolidine-oxazolidine hybrid, etherificate
One of the carboxylate or more than one composition of benzenediol, strong acid.
The carboxylate of strong acid uses after being diluted by ethylene glycol in curing accelerator;The strong acid of synthetic ester is phosphoric acid, poly phosphorus
One of acid, phosphorous acid, sulfuric acid, benzene sulfonic acid, p-methyl benzenesulfonic acid, xylene monosulfonic acid, phenolsulfonic acid;The alcohol of synthetic ester is second
Alcohol, ethylene glycol, polyethylene glycol, propylene glycol, polypropylene glycol, glycerine, pentaerythrite, benzyl alcohol, trimethylolpropane, in phenol
One kind.The curing accelerator of the present embodiment is the triphenyl phosphite and imidazolidine that mass ratio is 1: 1.
The present embodiment phenolic resin preimpregnation material preparation method the following steps are included:
1. will according to above-mentioned parts by weight it is weighed by phenolic resin, thickener and curing accelerator in dispersator
It is uniformly mixed stand-by.
2. bi-axial fabric is connected on impregnation unit;1. material that step is mixed pours into the resin of impregnation unit
In slot, resin storage tank temperature control system is 35 DEG C~80 DEG C (being 60 DEG C in the present embodiment).
3. starting impregnation unit, after bi-axial fabric is impregnated with resin in resin storage tank, extraction is moved through pressure roller, is entered with film carrier
Thicken drying tunnel.Thickening drying tunnel temperature is 40 DEG C~95 DEG C (being 85 DEG C in the present embodiment), and the fabric after impregnation passes through thickening drying tunnel
Time be 2h, thickening finishes to obtain the phenolic resin preimpregnation material of the present embodiment.
(embodiment 2)
Remaining is same as Example 1 for the phenolic resin preimpregnation material of the present embodiment, the difference is that further including 2 parts of toughening
Agent, toughener are base polyurethane prepolymer for use as.
In addition to the base polyurethane prepolymer for use as being previously mentioned, toughener can also be methoxy radical siloxane, polyvinyl alcohol, terminal hydroxy group
One of polybutadiene, carboxyl-terminated polybutadiene.
(embodiment 3)
The phenolic resin preimpregnation material of the present embodiment is composed of the following components in parts by weight: 55 parts of fabric, phenolic aldehyde tree
42 parts of rouge, 3 parts of thickener, 2 parts of curing accelerator.
Wherein fabric is 200g/m2Glass satin fabric.
Phenolic resin is the resol catalyzed and synthesized with barium hydroxide, viscosity 1200mPas.
Thickener is boric acid.
Curing accelerator is the carboxylate and oxazolidine of polyphosphoric acids and trimethylolpropane.
Remaining is same as Example 1 for the preparation method of the phenolic resin preimpregnation material of the present embodiment, the difference is that:
Step 2. resin storage tank temperature control system at 65 DEG C.
3. it is 90 DEG C that step thickens drying tunnel temperature, and the fabric after impregnation is 1h by the time of thickening drying tunnel.
(embodiment 4)
The phenolic resin preimpregnation material of the present embodiment is composed of the following components in parts by weight: 50 parts of fabric, phenolic aldehyde tree
45 parts of rouge, 2 parts of thickener, 3 parts of curing accelerator.
Wherein fabric is 400g/m2Carbon fiber plain cloth.
Phenolic resin is the resol with magnesium oxide catalyzed synthesis, viscosity 1000mPas.
Thickener is zinc borate.
Curing accelerator is diphenyl phosphate and triazine.
Remaining is same as Example 1 for the preparation method of the phenolic resin preimpregnation material of the present embodiment, the difference is that:
Step 2. resin storage tank temperature control system at 63 DEG C.
3. it is 90 DEG C that step thickens drying tunnel temperature, and the fabric after impregnation is 1h by the time of thickening drying tunnel.
(embodiment 5)
The phenolic resin preimpregnation material of the present embodiment is composed of the following components in parts by weight: 2 parts of fabric, phenolic resin
44 parts, 3 parts of thickener.
Wherein fabric is 400g/m2Twill.
Phenolic resin is the resol synthesized with ammonia-catalyzed, viscosity 1400mPas.
Thickener is magnesia.
Curing accelerator is carboxylate and imidazolidine-oxazolidine hybrid of polyphosphoric acids and trimethylolpropane.
Remaining is same as Example 1 for the preparation method of the phenolic resin preimpregnation material of the present embodiment, the difference is that:
Step 2. resin storage tank temperature control system at 60 DEG C.
3. it is 95 DEG C that step thickens drying tunnel temperature, and the fabric after impregnation is 1h by the time of thickening drying tunnel.
(embodiment 6)
The phenolic resin preimpregnation material of the present embodiment is composed of the following components in parts by weight: 51 parts of fabric, phenolic aldehyde tree
41 parts of rouge, 2 parts of thickener, 3 parts of curing accelerator, 3 parts of toughener.
Wherein fabric is 500g/m2Bi-axial fabric.
Phenolic resin be Chinese patent literature CN 104356325A(application number 201410593338.2) disclosed in nanometer layer
The modified phenolic resin of shape silicate clay, viscosity 600mPas.
Thickener is the white carbon black and nano-grade aluminum hydroxide that mass ratio is 1:1.
Curing accelerator is the carboxylate and resorcinolformaldehyde resin of polyphosphoric acids and trimethylolpropane.
Toughener is methoxy radical siloxane.
Remaining is same as Example 1 for the preparation method of the phenolic resin preimpregnation material of the present embodiment, the difference is that:
Step 2. resin storage tank temperature control system at 60 DEG C.
3. it is 93 DEG C that step thickens drying tunnel temperature, and the fabric after impregnation is 0.5h by the time of thickening drying tunnel.
(embodiment 7)
The phenolic resin preimpregnation material of the present embodiment is composed of the following components in parts by weight: 50 parts of fabric, phenolic aldehyde tree
45 parts of rouge, 1 part of thickener, 2 parts of curing accelerator, 2 parts of toughener.
Wherein fabric is 250g/m2Twill.
Phenolic resin is the resol with sodium hydroxide catalyzed synthesis, viscosity 1000mPas.
Thickener is the calcium sulfate and zinc borate that mass ratio is 1:1.
Curing accelerator is the carboxylate of strong acid, and the acid of synthetic ester is phosphoric acid, and the alcohol of synthetic ester is polypropylene glycol;When use
It is used after carboxylate spent glycol dilution, the mass ratio of carboxylate and ethylene glycol is 5:1.
Toughener is carboxyl-terminated polybutadiene.
Remaining is same as Example 1 for the preparation method of the phenolic resin preimpregnation material of the present embodiment, the difference is that:
Step 2. resin storage tank temperature control system at 60 DEG C.
3. it is 9 DEG C that step thickens drying tunnel temperature, and the fabric after impregnation is 1h by the time of thickening drying tunnel.
Embodiment 1 to 7, which thickens the material finished, can be made into the soft solid coiled material for possessing different viscosity, illustrate thickening effect
Fruit is ideal, reaches the Typical physical performance of prepreg.
Performance such as the following table 1 that the phenolic resin preimpregnation of embodiment 1 to embodiment 7 is expected:
Table 1
(embodiment 8, the method that material manufacture phenolic composite is presoaked by phenolic resin)
The present embodiment manufactures phenolic composite and uses the cured technique of vacuum bag, uses the phenolic resin prepolymer of embodiment 1
Leaching material, comprising the following steps:
1. successively completing gas permeable material, microporous barrier, porous release film on mold.
The gas permeable material is one of organic fabrix, inorganic fibre fabric;The micropore membrane material is thermoplastic
Property polyurethane, polytetrafluoroethylene (PTFE), one of silicon rubber, the micropore size of microporous barrier is 0.1~10um, with a thickness of 2~100um
Between, porosity is 50%~80%;Porous release film is polyethylene film, and aperture is 0.1~0.3mm, punching spacing is 3~
10mm。
2. the prepreg of embodiment 1 is cut by required size, remove release film, on the porous release film of step 1.
Complete lamination (prepreg of 3 layers of embodiment 1 is laid in the present embodiment).The lamination refers to the design according to phenolic composite
Thickness and prepreg thickness in monolayer determine the number of plies of prepreg in lamination, the stacked body obtained after prepreg is successively completed.
Further, during above-mentioned laying lamination, bubble can also be overlayed between the adjacent two layers prepreg among lamination
Foam core material or honeycomb core material or cork wood, make sandwich structure.
Further, edge sealing member is also used when being laid with the lamination for having core material, the edge sealing member is one up and down
Body frame shape prefabricated component, the thickness of the vertical guide of the frame shape prefabricated component is identical as the thickness of core material, and the width of frame is 1 to 10cm,
Edge sealing member is the prefabricated phenolic composite of integration.Edge sealing member is fitted in the edge of core material, the edge of edge sealing member
Profile and composite element edge profile are in same facade.The bottom prepreg lamination below core material is completed when laying
After laying, it will usually which needs are laid at the edge of these bottom prepregs along the facade of die edge upwards, die horizontal face
The prepreg at the angle R that intersects with edge elevation is easy to tilt, and places edge sealing member, with edge sealing member by the water of institute's shop fixtures layer prepreg
Then core material is filled in the frame of frame shape edge sealing member on the horizontal plane and facade of mold, continues core by plane and facade compacting
The laying of prepreg above material and edge sealing member.
Due to the setting of edge sealing member, in the vacuum in later period, core material surrounding is not allowed to be also easy to produce displacement and stitch
Gap, so that final composite element be avoided to generate cavitation damage in surrounding facade.
3. step 2. phenolic resin preimpregnation material lamination outer surface on be successively laid with porous release film, microporous barrier, thoroughly
Gas material, wherein microporous barrier needs completely to coat prepreg build-up surface.
4. being laid with sealant tape in mold surrounding, one, vacuum tube is touched on gas permeable material, and other end connects external vacuum
Pipeline is completed vacuum diaphragm and is sealed.
5. mold is integrally put into drying chamber, vacuum pump is opened, keeps pressure in -0.085~-0.01MPa;Heating is opened,
90 DEG C~160 DEG C (they being 100~120 DEG C in the present embodiment) are slowly increased to, and Slow cooling demoulds after the completion of material solidification, consolidate
The phenolic composite of change.
In prepreg used in the present embodiment due to containing curing accelerator, prepreg can 100 DEG C~120 DEG C compared with
Curing molding under low temperature, the lower temperature are 130 DEG C~160 DEG C of relatively high solidifications of middle phenolic resin compared with the prior art
For temperature;It is the case where for being free of curing accelerator in prepreg, higher at 130 DEG C~160 DEG C when preparing composite material
At a temperature of curing molding.
Likewise, according to the method described above, the prepreg of embodiment 2 to embodiment 7 is manufactured into phenolic composite plate;
To the method according to embodiment 8 by embodiment 1 to embodiment 7 prepreg manufacture composite material flat plate flame retardant property and machinery
Performance is detected:
(1) according to the stretching and punching of GB1447-2005, GB1451-2005 standard detection phenolic resin composite plate
Hit performance.
(2) 60 seconds vertical combustions.
Using VC-2 type vertical combustion analyzer, tested by BSS7230.
(3) smoke density.
Using SD-1 type smoke density case, tested by BSS7238.
Above-mentioned 3 testing results see the table below 2:
Table 2
Note: the embodiment 1 of the first row refers to multiple made of the prepreg of embodiment 1 according to the method for embodiment 8 in table 2
Condensation material plate, embodiment 2 to 7 is similarly.
(embodiment 9, the method that material manufacture phenolic composite is presoaked by phenolic resin)
The present embodiment manufactures phenolic composite and uses the cured technique of vacuum bag, uses the phenolic resin prepolymer of embodiment 1
Leaching material, comprising the following steps:
1. prepreg is cut by required size, remove release film, successively completes on mold and be made of 6 layers of prepreg
Lamination, be then successively laid with porous release film, microporous barrier, gas permeable material on prepreg surface;Wherein microporous barrier needs will be pre-
Leaching material build-up surface coats completely.The micropore size of the microporous barrier is 0.1~10um, with a thickness of between 2~300um, hole
Rate is 50%~80%;The lamination refers to prepreg is successively completed after obtained stacked body.
Further, during above-mentioned laying lamination, bubble can also be overlayed between the adjacent two layers prepreg among lamination
Foam core material or honeycomb core material or cork wood, make sandwich structure.
Further, edge sealing member described in embodiment 8 is also used when being laid with the lamination for having core material.
2. being laid with sealant tape in mold surrounding, one, vacuum tube is touched on gas permeable material, and other end connects external vacuum
Pipeline is completed vacuum diaphragm and is sealed.
3. mold is integrally put into drying chamber, vacuum pump is opened, keeps pressure in -0.085~-0.01MPa;Heating is opened,
90 DEG C~160 DEG C (being 120 DEG C in the present embodiment) are slowly increased to, Slow cooling demoulds after the completion of material solidification, obtains cured
Phenolic composite.
Compared with the preparation method of embodiment 8, the present embodiment only lamination side be laid with porous release film, microporous barrier and
Another side surface of gas permeable material, lamination is directly contacted with die surface, due to die surface be it is smooth, the present embodiment can be with
Obtain the composite material of side shiny surface.
For the preparation method of embodiment 8, due to the two sides of lamination be all provided with auxiliary material i.e. porous release film, microporous barrier and
Gas permeable material, therefore obtained composite material both side surface has a texture of auxiliary material, but when two sides are all laid with the mode of auxiliary material and prepare
Exhaust or steam discharge effect are more preferable.
For there is the case where core material in lamination, when laying, uses edge sealing member, on the one hand this is because the edge of core material
Opposite prepreg is fragile, increases intensity with edge sealing member;Using for another aspect edge sealing member makes in the vacuum in later period,
Core material surrounding is not allowed to be also easy to produce displacement and gap occurs, and lacks so that final composite element be avoided to generate hole in surrounding facade
It falls into.
(comparative example 1)
This comparative example manufactures phenolic composite and uses the cured technique of conventional vacuum bag, with the phenolic resin of embodiment 1
For prepreg, preparation process the following steps are included:
1. prepreg is cut by required size, remove release film, lamination is successively completed on mold (in this comparative example
Be 3 layers), then prepreg build-up surface successively porous release film, inhale rubber mat several layers, gas permeable material.
2. being laid with sealant tape in mold surrounding, one, vacuum tube is touched on gas permeable material, and other end connects external vacuum
Pipeline is completed vacuum bag film and is sealed.
3. mold is integrally put into drying chamber, vacuum pump is opened, keeps pressure in -0.085~-0.01MPa;Heating is opened,
120 DEG C are slowly increased to, Slow cooling demoulds after the completion of material solidification, obtains cured phenolic composite.
Microporous barrier is not used in this comparative example, using the exhaust for inhaling rubber mat and carrying out solidification process, air that when laying carries secretly,
Solidify the steam released to be extracted by the hole of porous release film.
Rubber mat is inhaled in observation, the portion for inhaling rubber mat observes the resin for being solidified into rufous, is illustrated in air, steam
Fraction phenolic resin is carried in exhaust process secretly, these phenolic resin, which are accumulated in, inhales rubber mat layer, absorbs the suction of phenolic resin
Rubber mat cannot be recycled.The cured technique of traditional vacuum bag had both caused the waste of prepreg resin, also added into
Sheet and waste quantity.
Claims (9)
1. a kind of phenolic resin preimpregnation material, it is characterised in that in parts by weight include following components: 50~65 parts of fabric, phenol
20~48 parts of urea formaldehyde, 1~5 part of thickener, 1~10 part of curing accelerator;
The curing accelerator be imidazolidine, triazine, oxazolidine, oxazines, imidazolidine-oxazolidine hybrid, etherificate isophthalic two
One of the carboxylate or more than one composition of phenol, strong acid;
The strong acid for wherein synthesizing carboxylate is phosphoric acid, polyphosphoric acids, phosphorous acid, sulfuric acid, benzene sulfonic acid, p-methyl benzenesulfonic acid, dimethylbenzene
One of sulfonic acid, phenolsulfonic acid;The alcohol for synthesizing carboxylate is ethyl alcohol, ethylene glycol, polyethylene glycol, propylene glycol, polypropylene glycol, third
One of triol, pentaerythrite, benzyl alcohol, trimethylolpropane, phenol.
2. phenolic resin preimpregnation material according to claim 1, it is characterised in that: the phenolic resin is first rank phenolic aldehyde tree
Rouge, viscosity are 300~1500mPas;The thickener is magnesia, calcium oxide, calcium sulfate, nano-grade aluminum hydroxide, hard charcoal
One of black, boric acid, zinc borate or more than one composition.
Expect 3. being presoaked according to claim 1 to phenolic resin described in one of 2, it is characterised in that: further include 1~8 part of toughener;
The toughener is base polyurethane prepolymer for use as, methoxy radical siloxane, polyvinyl alcohol, end hydroxy butadiene, carboxyl-terminated polybutadiene
One of.
4. a kind of preparation method of phenolic resin preimpregnation material as described in claim 1, it is characterised in that the following steps are included:
1. will according to parts by weight weighed phenolic resin, thickener and curing accelerator in dispersator be uniformly mixed to
With;Phenolic resin is resol, and viscosity is 300~1500mPas;Thickener be magnesia, calcium oxide, calcium sulfate,
One of nano-grade aluminum hydroxide, white carbon black, boric acid, zinc borate or more than one composition;
2. fabric is connected on impregnation unit;1. material that step is mixed pours into the resin storage tank of impregnation unit,
Resin storage tank temperature control system is at 25 DEG C~80 DEG C;
3. starting impregnation unit, after fabric is impregnated with resin in resin storage tank, extraction is moved through pressure roller, enters thickening with film carrier and dries
Road;Thickening drying tunnel temperature is 40 DEG C~95 DEG C, and the fabric after impregnation is 0.5~5h by the time of thickening drying tunnel, and thickening finishes
Obtain phenolic resin preimpregnation material.
5. the preparation method of phenolic resin preimpregnation material according to claim 4, it is characterised in that: 1. step also weighs toughening
1~8 part of agent, will according to parts by weight weighed phenolic resin, thickener, toughener and curing accelerator in dispersator
It is uniformly mixed stand-by;
The curing accelerator be imidazolidine, triazine, oxazolidine, oxazines, imidazolidine-oxazolidine hybrid, etherificate isophthalic two
One of the carboxylate or more than one composition of phenol, strong acid;The toughener is base polyurethane prepolymer for use as, methoxyl group silicon oxygen
One of alkane, polyvinyl alcohol, end hydroxy butadiene, carboxyl-terminated polybutadiene.
6. a kind of method for presoaking material manufacture phenolic composite by phenolic resin described in claim 1, using vacuum bag pressure
Curing process, it is characterised in that the following steps are included:
1. prepreg is cut by required size, remove release film, lamination is successively completed on mold, then in prepreg table
Face is successively laid with porous release film, microporous barrier, gas permeable material;The micropore size of the microporous barrier is 0.1~10um, with a thickness of 2
Between~300um, porosity is 50%~80%;The lamination refers to the design thickness and preimpregnation material list according to phenolic composite
Thickness degree determines the number of plies of prepreg in lamination, the stacked body obtained after prepreg is successively completed;
2. being laid with sealant tape in mold surrounding, one, vacuum tube is touched on gas permeable material, and other end connects external vacuum pipeline,
It completes vacuum bag film and seals;
3. mold is integrally put into drying chamber, vacuum pump is opened, keeps pressure in -0.085~-0.01MPa;Heating is opened, slowly
90 DEG C~160 DEG C are risen to, Slow cooling demoulds after the completion of material solidification, obtains cured composite material.
7. the method for phenolic resin preimpregnation material manufacture phenolic composite according to claim 6, it is characterised in that: step
1. be laid with lamination, laying foam core material or honeycomb core material or cork wood between the adjacent two layers prepreg among lamination, two pieces
Prepreg and in-between core material form sandwich structure.
8. the method for phenolic resin preimpregnation material manufacture phenolic composite according to claim 7, it is characterised in that: step
1. edge sealing member is also used when being laid with the lamination for having core material in, the edge sealing member is upper and lower perforative integrated frame shape prefabricated component, envelope
Edge pieces is bonded the surrounding that core material is arranged in, and the edge profile of edge sealing member is with composite element edge profile same
Facade;
Prepreg lamination below core material is first completed when laying to be laid with, places edge sealing member, with edge sealing member by the water of spread prepreg
Core material, is then filled in the frame of frame shape edge sealing member by plane and edge elevation compacting, pre- above continuation core material and edge sealing member
Soak the laying of material.
9. the method for the preimpregnation material manufacture phenolic composite of the phenolic resin according to one of claim 6 to 8, feature exist
In: before being laid with prepreg lamination on mold, first successively it is laid with gas permeable material, microporous barrier, porous release film.
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CN108546488A (en) * | 2018-05-11 | 2018-09-18 | 南京宁丰化工设备有限公司 | A kind of composite plate high temperature resistant interleaving agent and preparation method thereof |
CN108841135B (en) * | 2018-06-01 | 2021-07-09 | 山东圣泉新材料股份有限公司 | Resin composition, SMC composite material, and preparation method and application thereof |
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CN114030202A (en) * | 2021-10-28 | 2022-02-11 | 常州百思通复合材料有限公司 | Method for producing thermosetting phenolic resin-based composite material |
CN115625897B (en) * | 2022-12-12 | 2023-03-28 | 北京玻钢院复合材料有限公司 | Toughening low-density hot-melt phenolic resin prepreg, composite material and preparation method |
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FR2620456B1 (en) * | 1987-09-15 | 1993-08-27 | Ceca Sa | NOVEL FORMO-PHENOLIC RESIN COMPOSITIONS FOR PREPARING PREPREGNATED MATS |
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CN101722706B (en) * | 2009-12-11 | 2012-12-26 | 中国航空工业集团公司北京航空材料研究院 | Process for pre-compacting prepreg overlay of resin-based composite material |
CN102731960B (en) * | 2012-06-18 | 2013-12-04 | 航天材料及工艺研究所 | Preparation method of high-toughness flame retardation phenolic prepreg composite material |
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CN105255101B (en) * | 2015-10-16 | 2018-03-09 | 航天材料及工艺研究所 | A kind of impact resistance, fireproof glass fibre reinforced phenolic sheet material and preparation method thereof |
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