JPH0428531A - Prepreg coating method using double-layer primer - Google Patents
Prepreg coating method using double-layer primerInfo
- Publication number
- JPH0428531A JPH0428531A JP2133930A JP13393090A JPH0428531A JP H0428531 A JPH0428531 A JP H0428531A JP 2133930 A JP2133930 A JP 2133930A JP 13393090 A JP13393090 A JP 13393090A JP H0428531 A JPH0428531 A JP H0428531A
- Authority
- JP
- Japan
- Prior art keywords
- layer
- primer
- prepreg
- cured
- coating layer
- 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.)
- Granted
Links
- 238000000576 coating method Methods 0.000 title claims abstract description 22
- 239000010410 layer Substances 0.000 claims abstract description 30
- 239000000203 mixture Substances 0.000 claims abstract description 23
- 239000000853 adhesive Substances 0.000 claims abstract description 21
- 230000001070 adhesive effect Effects 0.000 claims abstract description 21
- 239000003795 chemical substances by application Substances 0.000 claims abstract description 21
- 229920000647 polyepoxide Polymers 0.000 claims abstract description 21
- 239000003822 epoxy resin Substances 0.000 claims abstract description 20
- 239000000463 material Substances 0.000 claims abstract description 20
- 239000011247 coating layer Substances 0.000 claims abstract description 19
- 229910000831 Steel Inorganic materials 0.000 claims abstract description 18
- 239000010959 steel Substances 0.000 claims abstract description 18
- 239000011342 resin composition Substances 0.000 claims abstract description 15
- 239000012779 reinforcing material Substances 0.000 claims abstract description 11
- 239000000835 fiber Substances 0.000 claims abstract description 9
- 239000007788 liquid Substances 0.000 claims abstract description 9
- 229920000768 polyamine Polymers 0.000 claims abstract description 8
- 229920006295 polythiol Polymers 0.000 claims abstract description 7
- 239000007787 solid Substances 0.000 claims abstract description 5
- 229920005989 resin Polymers 0.000 claims description 6
- 239000011347 resin Substances 0.000 claims description 6
- 239000011248 coating agent Substances 0.000 abstract description 15
- 230000007547 defect Effects 0.000 abstract 1
- 230000035939 shock Effects 0.000 abstract 1
- 238000005260 corrosion Methods 0.000 description 16
- 230000007797 corrosion Effects 0.000 description 13
- 238000000034 method Methods 0.000 description 8
- IISBACLAFKSPIT-UHFFFAOYSA-N bisphenol A Chemical compound C=1C=C(O)C=CC=1C(C)(C)C1=CC=C(O)C=C1 IISBACLAFKSPIT-UHFFFAOYSA-N 0.000 description 6
- -1 modified aliphatic amines Chemical class 0.000 description 6
- 239000003973 paint Substances 0.000 description 6
- 239000000945 filler Substances 0.000 description 5
- 239000000843 powder Substances 0.000 description 5
- PXKLMJQFEQBVLD-UHFFFAOYSA-N bisphenol F Chemical compound C1=CC(O)=CC=C1CC1=CC=C(O)C=C1 PXKLMJQFEQBVLD-UHFFFAOYSA-N 0.000 description 4
- 238000001035 drying Methods 0.000 description 4
- 229920002635 polyurethane Polymers 0.000 description 4
- 239000004814 polyurethane Substances 0.000 description 4
- 229930185605 Bisphenol Natural products 0.000 description 3
- LYCAIKOWRPUZTN-UHFFFAOYSA-N Ethylene glycol Chemical compound OCCO LYCAIKOWRPUZTN-UHFFFAOYSA-N 0.000 description 3
- DNIAPMSPPWPWGF-UHFFFAOYSA-N Propylene glycol Chemical compound CC(O)CO DNIAPMSPPWPWGF-UHFFFAOYSA-N 0.000 description 3
- 239000002253 acid Substances 0.000 description 3
- 150000001412 amines Chemical class 0.000 description 3
- MTHSVFCYNBDYFN-UHFFFAOYSA-N diethylene glycol Chemical compound OCCOCCO MTHSVFCYNBDYFN-UHFFFAOYSA-N 0.000 description 3
- LNEPOXFFQSENCJ-UHFFFAOYSA-N haloperidol Chemical compound C1CC(O)(C=2C=CC(Cl)=CC=2)CCN1CCCC(=O)C1=CC=C(F)C=C1 LNEPOXFFQSENCJ-UHFFFAOYSA-N 0.000 description 3
- 239000000049 pigment Substances 0.000 description 3
- 229920005862 polyol Polymers 0.000 description 3
- 150000003077 polyols Chemical class 0.000 description 3
- 125000003396 thiol group Chemical group [H]S* 0.000 description 3
- JOYRKODLDBILNP-UHFFFAOYSA-N Ethyl urethane Chemical compound CCOC(N)=O JOYRKODLDBILNP-UHFFFAOYSA-N 0.000 description 2
- VZCYOOQTPOCHFL-OWOJBTEDSA-N Fumaric acid Chemical compound OC(=O)\C=C\C(O)=O VZCYOOQTPOCHFL-OWOJBTEDSA-N 0.000 description 2
- PEDCQBHIVMGVHV-UHFFFAOYSA-N Glycerine Chemical compound OCC(O)CO PEDCQBHIVMGVHV-UHFFFAOYSA-N 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- PPBRXRYQALVLMV-UHFFFAOYSA-N Styrene Chemical compound C=CC1=CC=CC=C1 PPBRXRYQALVLMV-UHFFFAOYSA-N 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 2
- 150000007513 acids Chemical class 0.000 description 2
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 2
- WNLRTRBMVRJNCN-UHFFFAOYSA-N adipic acid Chemical compound OC(=O)CCCCC(O)=O WNLRTRBMVRJNCN-UHFFFAOYSA-N 0.000 description 2
- 150000004982 aromatic amines Chemical class 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 238000005470 impregnation Methods 0.000 description 2
- 239000012784 inorganic fiber Substances 0.000 description 2
- QQVIHTHCMHWDBS-UHFFFAOYSA-N isophthalic acid Chemical compound OC(=O)C1=CC=CC(C(O)=O)=C1 QQVIHTHCMHWDBS-UHFFFAOYSA-N 0.000 description 2
- 239000010445 mica Substances 0.000 description 2
- 229910052618 mica group Inorganic materials 0.000 description 2
- 238000002156 mixing Methods 0.000 description 2
- 239000000178 monomer Substances 0.000 description 2
- 229920003986 novolac Polymers 0.000 description 2
- 239000000123 paper Substances 0.000 description 2
- 239000004848 polyfunctional curative Substances 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- 239000002904 solvent Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 239000000758 substrate Substances 0.000 description 2
- VZCYOOQTPOCHFL-UHFFFAOYSA-N trans-butenedioic acid Natural products OC(=O)C=CC(O)=O VZCYOOQTPOCHFL-UHFFFAOYSA-N 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- IVSZLXZYQVIEFR-UHFFFAOYSA-N 1,3-Dimethylbenzene Natural products CC1=CC=CC(C)=C1 IVSZLXZYQVIEFR-UHFFFAOYSA-N 0.000 description 1
- SMZOUWXMTYCWNB-UHFFFAOYSA-N 2-(2-methoxy-5-methylphenyl)ethanamine Chemical compound COC1=CC=C(C)C=C1CCN SMZOUWXMTYCWNB-UHFFFAOYSA-N 0.000 description 1
- JAHNSTQSQJOJLO-UHFFFAOYSA-N 2-(3-fluorophenyl)-1h-imidazole Chemical compound FC1=CC=CC(C=2NC=CN=2)=C1 JAHNSTQSQJOJLO-UHFFFAOYSA-N 0.000 description 1
- QTWJRLJHJPIABL-UHFFFAOYSA-N 2-methylphenol;3-methylphenol;4-methylphenol Chemical compound CC1=CC=C(O)C=C1.CC1=CC=CC(O)=C1.CC1=CC=CC=C1O QTWJRLJHJPIABL-UHFFFAOYSA-N 0.000 description 1
- UPMLOUAZCHDJJD-UHFFFAOYSA-N 4,4'-Diphenylmethane Diisocyanate Chemical compound C1=CC(N=C=O)=CC=C1CC1=CC=C(N=C=O)C=C1 UPMLOUAZCHDJJD-UHFFFAOYSA-N 0.000 description 1
- QTBSBXVTEAMEQO-UHFFFAOYSA-M Acetate Chemical compound CC([O-])=O QTBSBXVTEAMEQO-UHFFFAOYSA-M 0.000 description 1
- NIXOWILDQLNWCW-UHFFFAOYSA-M Acrylate Chemical compound [O-]C(=O)C=C NIXOWILDQLNWCW-UHFFFAOYSA-M 0.000 description 1
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 1
- 244000025254 Cannabis sativa Species 0.000 description 1
- 235000012766 Cannabis sativa ssp. sativa var. sativa Nutrition 0.000 description 1
- 235000012765 Cannabis sativa ssp. sativa var. spontanea Nutrition 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 206010007269 Carcinogenicity Diseases 0.000 description 1
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- 229920000742 Cotton Polymers 0.000 description 1
- 208000006558 Dental Calculus Diseases 0.000 description 1
- 239000004593 Epoxy Substances 0.000 description 1
- 239000004606 Fillers/Extenders Substances 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- CERQOIWHTDAKMF-UHFFFAOYSA-N Methacrylic acid Chemical compound CC(=C)C(O)=O CERQOIWHTDAKMF-UHFFFAOYSA-N 0.000 description 1
- ISWSIDIOOBJBQZ-UHFFFAOYSA-N Phenol Chemical compound OC1=CC=CC=C1 ISWSIDIOOBJBQZ-UHFFFAOYSA-N 0.000 description 1
- LGRFSURHDFAFJT-UHFFFAOYSA-N Phthalic anhydride Natural products C1=CC=C2C(=O)OC(=O)C2=C1 LGRFSURHDFAFJT-UHFFFAOYSA-N 0.000 description 1
- 239000004962 Polyamide-imide Substances 0.000 description 1
- 239000004698 Polyethylene Substances 0.000 description 1
- 239000004642 Polyimide Substances 0.000 description 1
- 239000004721 Polyphenylene oxide Substances 0.000 description 1
- 239000004734 Polyphenylene sulfide Substances 0.000 description 1
- OFOBLEOULBTSOW-UHFFFAOYSA-N Propanedioic acid Natural products OC(=O)CC(O)=O OFOBLEOULBTSOW-UHFFFAOYSA-N 0.000 description 1
- 229910052581 Si3N4 Inorganic materials 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 239000001361 adipic acid Substances 0.000 description 1
- 235000011037 adipic acid Nutrition 0.000 description 1
- 125000001931 aliphatic group Chemical group 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- OHJMTUPIZMNBFR-UHFFFAOYSA-N biuret Chemical compound NC(=O)NC(N)=O OHJMTUPIZMNBFR-UHFFFAOYSA-N 0.000 description 1
- 229910052796 boron Inorganic materials 0.000 description 1
- JHIWVOJDXOSYLW-UHFFFAOYSA-N butyl 2,2-difluorocyclopropane-1-carboxylate Chemical compound CCCCOC(=O)C1CC1(F)F JHIWVOJDXOSYLW-UHFFFAOYSA-N 0.000 description 1
- 235000009120 camo Nutrition 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 230000007670 carcinogenicity Effects 0.000 description 1
- 231100000260 carcinogenicity Toxicity 0.000 description 1
- 239000004359 castor oil Substances 0.000 description 1
- 235000019438 castor oil Nutrition 0.000 description 1
- 235000005607 chanvre indien Nutrition 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 229930003836 cresol Natural products 0.000 description 1
- 235000014113 dietary fatty acids Nutrition 0.000 description 1
- 125000005442 diisocyanate group Chemical group 0.000 description 1
- 239000003085 diluting agent Substances 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 239000000194 fatty acid Substances 0.000 description 1
- 229930195729 fatty acid Natural products 0.000 description 1
- 239000001530 fumaric acid Substances 0.000 description 1
- 235000011187 glycerol Nutrition 0.000 description 1
- ZEMPKEQAKRGZGQ-XOQCFJPHSA-N glycerol triricinoleate Natural products CCCCCC[C@@H](O)CC=CCCCCCCCC(=O)OC[C@@H](COC(=O)CCCCCCCC=CC[C@@H](O)CCCCCC)OC(=O)CCCCCCCC=CC[C@H](O)CCCCCC ZEMPKEQAKRGZGQ-XOQCFJPHSA-N 0.000 description 1
- 239000011487 hemp Substances 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000007774 longterm Effects 0.000 description 1
- 239000002075 main ingredient Substances 0.000 description 1
- VZCYOOQTPOCHFL-UPHRSURJSA-N maleic acid Chemical compound OC(=O)\C=C/C(O)=O VZCYOOQTPOCHFL-UPHRSURJSA-N 0.000 description 1
- 239000011976 maleic acid Substances 0.000 description 1
- LVHBHZANLOWSRM-UHFFFAOYSA-N methylenebutanedioic acid Natural products OC(=O)CC(=C)C(O)=O LVHBHZANLOWSRM-UHFFFAOYSA-N 0.000 description 1
- 239000004745 nonwoven fabric Substances 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 239000005011 phenolic resin Substances 0.000 description 1
- 239000013034 phenoxy resin Substances 0.000 description 1
- 229920006287 phenoxy resin Polymers 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 239000004014 plasticizer Substances 0.000 description 1
- 229920000233 poly(alkylene oxides) Polymers 0.000 description 1
- 229920002312 polyamide-imide Polymers 0.000 description 1
- 229920002857 polybutadiene Polymers 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 229920000570 polyether Polymers 0.000 description 1
- 229920000573 polyethylene Polymers 0.000 description 1
- 229920001721 polyimide Polymers 0.000 description 1
- 229920000098 polyolefin Polymers 0.000 description 1
- 229920000069 polyphenylene sulfide Polymers 0.000 description 1
- 150000007519 polyprotic acids Polymers 0.000 description 1
- 229920005749 polyurethane resin Polymers 0.000 description 1
- HJWLCRVIBGQPNF-UHFFFAOYSA-N prop-2-enylbenzene Chemical compound C=CCC1=CC=CC=C1 HJWLCRVIBGQPNF-UHFFFAOYSA-N 0.000 description 1
- 229920006395 saturated elastomer Polymers 0.000 description 1
- 238000007790 scraping Methods 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 150000005846 sugar alcohols Polymers 0.000 description 1
- 239000012209 synthetic fiber Substances 0.000 description 1
- 229920002994 synthetic fiber Polymers 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
- DVKJHBMWWAPEIU-UHFFFAOYSA-N toluene 2,4-diisocyanate Chemical compound CC1=CC=C(N=C=O)C=C1N=C=O DVKJHBMWWAPEIU-UHFFFAOYSA-N 0.000 description 1
- 229920006337 unsaturated polyester resin Polymers 0.000 description 1
- AVWRKZWQTYIKIY-UHFFFAOYSA-N urea-1-carboxylic acid Chemical compound NC(=O)NC(O)=O AVWRKZWQTYIKIY-UHFFFAOYSA-N 0.000 description 1
- 229920001567 vinyl ester resin Polymers 0.000 description 1
- 125000000391 vinyl group Chemical group [H]C([*])=C([H])[H] 0.000 description 1
- 229920002554 vinyl polymer Polymers 0.000 description 1
- 210000002268 wool Anatomy 0.000 description 1
- 239000002759 woven fabric Substances 0.000 description 1
- DGVVWUTYPXICAM-UHFFFAOYSA-N β‐Mercaptoethanol Chemical compound OCCS DGVVWUTYPXICAM-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B82—NANOTECHNOLOGY
- B82Y—SPECIFIC USES OR APPLICATIONS OF NANOSTRUCTURES; MEASUREMENT OR ANALYSIS OF NANOSTRUCTURES; MANUFACTURE OR TREATMENT OF NANOSTRUCTURES
- B82Y30/00—Nanotechnology for materials or surface science, e.g. nanocomposites
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Nanotechnology (AREA)
- Condensed Matter Physics & Semiconductors (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Materials Engineering (AREA)
- Crystallography & Structural Chemistry (AREA)
- Composite Materials (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
- Manufacture Of Macromolecular Shaped Articles (AREA)
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Paints Or Removers (AREA)
- Preventing Corrosion Or Incrustation Of Metals (AREA)
Abstract
Description
【発明の詳細な説明】
[産業上の利用分野]
本発明は、海洋鋼構造物等の乾湿交番部に重防食被覆を
施すためのプリプレグ被覆方法及びそれに用いるプリプ
レグ被覆材に関するものである。DETAILED DESCRIPTION OF THE INVENTION [Industrial Application Field] The present invention relates to a prepreg coating method for applying a heavy corrosion protection coating to a wet/dry alternating section of a marine steel structure, etc., and a prepreg coating material used therein.
[従来技術と問題点]
従来、海洋鋼構造物の没水部、乾湿交番部、飛沫部など
の防食用被覆として、タールエポキシ樹脂塗料、厚膜ポ
リウレタン塗料、厚膜エポキシ樹脂塗料などが使用され
ている。[Prior art and problems] Conventionally, tar epoxy resin paints, thick film polyurethane paints, thick film epoxy resin paints, etc. have been used as anti-corrosion coatings for submerged parts, dry/wet alternating parts, splash parts, etc. of marine steel structures. ing.
しかしながら、タールエポキシ樹脂塗料は、防食性は比
較的よいが、耐衝撃性が極めて劣り、その結果塗膜が損
傷されやすく、且つ防食性の低下を招きやすい。また塗
膜の強度および硬度が低く、鋼構造物の運搬中や据付時
に破壊を起こしゃすく、しかも組成面からタールは臭気
、発ガン性等衛生上の問題を有しているので好ましくな
い。However, although tar epoxy resin paints have relatively good corrosion resistance, they have extremely poor impact resistance, and as a result, the coating film is easily damaged and the corrosion resistance is likely to deteriorate. In addition, the strength and hardness of the coating film is low, making it difficult to break during transportation or installation of steel structures, and tar is undesirable because it has hygienic problems such as odor and carcinogenicity due to its composition.
また、厚膜ポリウレタン塗料は、防食性、塗装作業性の
面で劣り、その上付着性においてもM粗性に欠けるとい
う問題を残している。Further, thick film polyurethane paints are inferior in terms of corrosion resistance and painting workability, and also have the problem of lacking M roughness in terms of adhesion.
さらに、厚膜エポキシ樹脂塗料は、塗装作業性、耐衝撃
性に劣り、しかも均一な厚膜を得にくいという作業性の
問題を有している。Further, thick film epoxy resin paints have problems in workability, such as poor coating workability and impact resistance, and difficulty in obtaining a uniform thick film.
[問題点を解決するための手段]
本発明者らは、従来の海洋鋼構造物の防食被覆に見られ
る問題点を解決すべく、鋭意検討を重ねた結果、特定の
プリプレグ被覆材を用いた新規な被覆方法を用いること
によりこれらの問題点が解決できることを見出し、本発
明を完成するに至った。[Means for Solving the Problems] In order to solve the problems found in conventional anti-corrosion coatings for marine steel structures, the inventors of the present invention have conducted intensive studies and have developed a method using a specific prepreg coating material. We have discovered that these problems can be solved by using a new coating method, and have completed the present invention.
かくして、本発明に従えば、
(i)鋼材表面に、ポリアミンを硬化剤とする常温で反
応硬化性のエポキシ樹脂プライマー組成物全塗布し、つ
いでポリチオールを硬化剤とする常温で反応硬化性のエ
ポキシ樹脂系プライマー組成物を塗布し、上層となる下
記プリプレグ被覆層との初期粘着力が0.!M/alI
+以上になるまで硬化させて接着性複層プライマー層を
形成し、(ii)該接着性プライマー層の上に、常温で
反応硬化性の液状樹脂組成物を繊維加工補強材に含浸さ
せて、永久変形可能な可塑性が発現する固体状になるま
で硬化させたプリプレグ被覆層を貼り合せ、ついで
(iii)該接着性複層プライマー層及び該プリプレグ
被覆層の両層を完全に密着硬化させることを特徴とする
プリプレグ被覆方法が提供される。Thus, according to the present invention, (i) an epoxy resin primer composition that is reactively curable at room temperature and uses a polyamine as a hardening agent is completely coated on the surface of the steel material, and then an epoxy resin primer composition that is reactively curable at room temperature and uses polythiol as a hardener is coated on the surface of the steel material; A resin-based primer composition is applied, and the initial adhesive strength with the upper prepreg coating layer shown below is 0. ! M/alI
(ii) on the adhesive primer layer, impregnating the fiber processing reinforcing material with a liquid resin composition that is reactively curable at room temperature; A prepreg coating layer that has been cured to a solid state exhibiting permanently deformable plasticity is bonded together, and then (iii) both the adhesive multilayer primer layer and the prepreg coating layer are completely bonded and cured. A featured prepreg coating method is provided.
以下、本発明について具体的に説明する。The present invention will be specifically explained below.
本発明の方法における接着性複層プライマー層のII層
目の形成に用いるポリアミンを硬化剤とする常温で反応
硬化性のエポキシ樹脂系プライマー組成物は、従来から
公知の2液型工ポキシ樹脂系組成物が用いられる。エポ
キシ樹脂としては例えばビスフェノールA型、ビスフェ
ノールF型、ビスフェノールAD型、ノボラック型など
が、また硬化剤としては、たとえば変性脂肪族アミン、
変性芳香族アミンなど従来から公知の変性アミン系硬化
剤が用いられる。The epoxy resin primer composition, which is reactively curable at room temperature and uses polyamine as a curing agent, used to form the second layer of the adhesive multilayer primer layer in the method of the present invention is a conventionally known two-component engineered epoxy resin primer composition. A composition is used. Epoxy resins include bisphenol A type, bisphenol F type, bisphenol AD type, novolac type, etc., and curing agents include, for example, modified aliphatic amines,
Conventionally known modified amine curing agents such as modified aromatic amines are used.
本発明の方法における接着性複層プライマー層の第2層
目の形成に用いるポリチオールを硬化剤とする常温で反
応硬化性のエポキシ樹脂系プライマー組成物は、従来か
ら公知の2液型工ポキシ樹脂系組成物が用いられる。エ
ポキシ樹脂としては複層プライマー層のM1層目に用い
られるものすべて用いることができる。硬化剤は1分子
当り平均2個以上、好ましくは2〜3個のチオール基を
有するポリチオール系硬化剤が用いられ、例えばポリア
ルキレンオキシドの両末端にチオール基を有する硬化剤
、チオグリコールをジイソシア4−トを介してポリオー
ルに付加した硬化剤、ポリエポキシドに硬化水素を付加
しI;硬化剤など従来から公知のものが用いられる。The epoxy resin primer composition, which is reactively curable at room temperature and uses polythiol as a curing agent, used to form the second layer of the adhesive multilayer primer layer in the method of the present invention is a conventionally known two-component engineered poxy resin. based compositions are used. As the epoxy resin, all those used in the M1 layer of the multilayer primer layer can be used. As the curing agent, a polythiol-based curing agent having an average of 2 or more thiol groups, preferably 2 to 3 thiol groups per molecule is used. For example, a curing agent having thiol groups at both ends of polyalkylene oxide, thioglycol is diisocyanate. Conventionally known curing agents can be used, such as a curing agent added to a polyol via a curing agent, and a curing agent added to a polyepoxide with curing hydrogen.
接着性プライマーを複層にした理由は、ポリアミン硬化
剤を用いたエポキシ樹脂系プライマーは、鋼板素地に対
する密着性、防食性に優れているが、乾燥硬化過程での
プリプレグ被覆層との有効な初期密着力を発揮する期間
が短く、プリプレグの貼り付けのタイミングに余裕がな
い。他方、ポリチオール硬化剤を用いI;エポキシ樹脂
系プライマーは、乾燥硬化過程でのプリプレグ被覆層と
の初期密着力が大きく、曲率半径の小さい曲面鋼材への
プリプレグの貼り付けも可能である。このように初期密
着力を持続する時間が長いので、プリプレグの貼り付は
タイミングに制約が少ないが、反面鋼板素地に対する密
着性、防食性にやや劣る。The reason for using multiple layers of adhesive primers is that epoxy resin primers using polyamine hardeners have excellent adhesion and corrosion resistance to steel sheet substrates, but they do not have an effective initial bond with the prepreg coating layer during the drying and curing process. The period during which adhesive strength is exerted is short, and there is no margin for timing when applying the prepreg. On the other hand, an epoxy resin-based primer using a polythiol curing agent has a large initial adhesive strength with the prepreg coating layer during the drying and curing process, and it is also possible to attach the prepreg to a curved steel material with a small radius of curvature. Since the initial adhesion force is maintained for a long time as described above, there are few restrictions on the timing of attaching the prepreg, but on the other hand, the adhesion to the steel plate base and corrosion resistance are somewhat inferior.
本発明において、前記した2種類のプライマー組成物を
組み合せて複層プライマー層とすることにより、両者の
欠点がカバーされ、その特徴が活かされる。In the present invention, by combining the two types of primer compositions described above to form a multilayer primer layer, the drawbacks of both can be covered and their characteristics can be utilized.
上記接着性複層プライマー組成物は、鋼材表面に一般に
乾燥膜厚で10〜100μmの範囲で順次塗布され、上
層として貼り付けるプリプレグ被覆層との初期粘着力が
、0.5j9/am以上となるまで、常温で反応硬化さ
せて接着性プライマー層とする。ここで、プライマー層
の硬化状態が上記の条件からはずれる場合、すなわちプ
ライマー層の乾燥・硬化が余り進まない、または進みす
ぎた状態の場合、プリプレグ被覆層との初期密着性が不
足し、貼りつけ作業時のずれ、垂直面でのズリプレグ被
覆層のすり落ちや、曲面でのプリプレグ被覆層の跳ね返
りによる剥れが問題となる。該接着性複層プライマー組
成物は塗布→乾燥→硬化過程で粘着性発揮時間が長く、
常温で反応硬化し、鋼材素地および上層のプリプレグ被
覆層との密着性、防食性に優れるという特徴を有してい
る。The above-mentioned adhesive multilayer primer composition is sequentially applied to the surface of the steel material, generally in a dry film thickness in the range of 10 to 100 μm, and has an initial adhesive strength of 0.5j9/am or more with the prepreg coating layer pasted as an upper layer. to form an adhesive primer layer. Here, if the curing state of the primer layer deviates from the above conditions, that is, if the drying and curing of the primer layer does not proceed much or has proceeded too much, the initial adhesion with the prepreg coating layer will be insufficient, and the adhesion will be difficult. Problems include misalignment during work, slippage of the prepreg coating layer on vertical surfaces, and peeling of the prepreg coating layer due to rebound on curved surfaces. The adhesive multilayer primer composition has a long adhesive time during the application → drying → curing process,
It reacts and hardens at room temperature, and has excellent adhesion to the steel base and the upper prepreg coating layer, as well as excellent corrosion resistance.
また、プライマー層の強度、防食性等の機能をさらに向
上させる必要がある場合には、プライマー組成物にフレ
ーク顔料、防錆顔料などの各種公知のフィラーを分散す
ることによって達成できる。Further, if it is necessary to further improve functions such as strength and corrosion resistance of the primer layer, this can be achieved by dispersing various known fillers such as flake pigments and antirust pigments in the primer composition.
次に、前記した接着性プライマー層に貼り合わされてプ
リプレグ被覆層を形成する重防食用プリプレグ被覆材は
、二次元に広がりを有する繊維加工補強材(以下、「面
状補強材」という)に常温で反応硬化性の液状樹脂組成
物を0.5〜5gの範囲で一定の厚さになるように含浸
させて、永久変形可能な可塑剤が発現する固体状になる
まで硬化させたものである。Next, the heavy-duty anti-corrosion prepreg coating material, which is bonded to the adhesive primer layer described above to form a prepreg coating layer, is applied to a two-dimensionally expanded fiber processed reinforcement material (hereinafter referred to as "planar reinforcement material") at room temperature. It is impregnated with a reaction-curable liquid resin composition to a constant thickness in the range of 0.5 to 5 g, and is cured until it becomes a solid state in which a permanently deformable plasticizer is expressed. .
前記面状補強材は、反応硬化性液状樹脂組成物の均−膜
厚成型性を助け、海洋における漂流物などの衝撃による
塗膜損傷の防止と被覆膜の補強、耐屈曲性を向上させる
役目をはたす。The planar reinforcing material helps form the reaction-curable liquid resin composition into a uniform film thickness, prevents damage to the coating film due to impact from objects floating in the ocean, reinforces the coating film, and improves bending resistance. fulfill one's role.
面状補強材の材質としては、従来から公知の有機繊維及
び無機繊維が使用される。有機繊維としては、例えば木
綿・麻・羊毛・綱などの天然繊維、アセテート・アクリ
ル・ポリエテル・ポリウレタン・ポリオレフィン・ポリ
アミド・ポリイミドなどの合成繊維を挙げることができ
、また無機繊維としては、例えばガラス・カーボン・ボ
ロン・アルミナ・炭化珪素・窒化珪素・ステンレススチ
ールなどの繊維を挙げることができる。これらは長繊維
または短繊維から加工成型した織布・不織布・ペーパー
・マットなどのメツシュ状成型物や多孔質のフィルム・
シートなどの形状で使用される。Conventionally known organic fibers and inorganic fibers are used as the material for the planar reinforcing material. Examples of organic fibers include natural fibers such as cotton, hemp, wool, and rope; synthetic fibers such as acetate, acrylic, polyether, polyurethane, polyolefin, polyamide, and polyimide; examples of inorganic fibers include glass, Examples include fibers such as carbon, boron, alumina, silicon carbide, silicon nitride, and stainless steel. These are mesh-like molded products such as woven fabrics, non-woven fabrics, paper, and mats made from long or short fibers, porous films, and
Used in the form of sheets, etc.
面状補強材に含浸される反応硬化性液状樹脂組成物は、
常温で反応硬化する2液型エポキシ、ポリウレタン、不
飽和ポリスチル系樹脂などを主成分とするものである。The reaction-curable liquid resin composition impregnated into the planar reinforcing material is
The main ingredients are two-component epoxy, polyurethane, unsaturated polystyl resin, etc., which react and harden at room temperature.
2液型工ポキシ系樹脂組成物としては、ビスフェノール
Aff、ビスフェノールF型、ビスフェノールADを、
フェノール、クレゾール等のノボラック型、アクリレー
ト変性、ウレタン変性、ポリブタジェンゴム変性などの
変性エポキシ樹脂が使用でき、これらは低粘度、素地と
の密着性、防食性、耐衝撃性、可焼性などの性能に優れ
るという特徴を有する。As the two-component poxy resin composition, bisphenol Aff, bisphenol F type, bisphenol AD,
Modified epoxy resins such as novolac type such as phenol and cresol, acrylate modified, urethane modified, and polybutadiene rubber modified can be used, and these have low viscosity, adhesion to the substrate, corrosion resistance, impact resistance, flammability, etc. It is characterized by excellent performance.
これらのエポキシ樹脂は、耐衝撃性、可焼性、耐水性な
どの特徴を有するアミン系硬化剤で反応硬化させるが、
たとえば変性脂肪族アミン、変性芳香族アミン、複素環
状ジアミン、ポリアミン・マンニッヒ誘導体、脂肪族ポ
リアミンマイケル付加物など各種公知のアミン系硬化剤
が使用される。These epoxy resins are cured by reaction with an amine-based curing agent that has characteristics such as impact resistance, sinterability, and water resistance.
For example, various known amine curing agents such as modified aliphatic amines, modified aromatic amines, heterocyclic diamines, polyamine Mannich derivatives, and aliphatic polyamine Michael adducts are used.
ポリウレタン系樹脂組成物は、ポリオール成分として無
溶剤で耐衝撃性、応力緩和性、耐摩耗性、耐候性、耐水
性などに優れるたとえばアルコキシ化ビスフェノールA
ヒマシ油脂肪酸エステル、エポキシ変性ポリオールなど
を用い、これにインシアネート系硬化剤成分として、ト
リレンジインシアネート、ジフェニルメタンジイソシア
ネート、メタキシレンジイソシアネートなどの単量体、
またはビウレット、アロファネート、インシアヌレト、
ウレタンアダクトなどの多量体を配合してなるものであ
る。The polyurethane resin composition is a polyol component that is solvent-free and has excellent impact resistance, stress relaxation properties, abrasion resistance, weather resistance, water resistance, etc., such as alkoxylated bisphenol A.
Using castor oil fatty acid ester, epoxy-modified polyol, etc., monomers such as tolylene diisocyanate, diphenylmethane diisocyanate, metaxylene diisocyanate, etc. as incyanate curing agent components,
or biuret, allophanate, incyanuret,
It is made by blending a multimer such as urethane adduct.
不飽和ポリエステル系樹脂組成物は、(無水)マレイン
酸、フマル酸、イタコン酸などの不飽和二塩基性酸と、
エチレングリコール、ジエチレングリコール、グリセリ
ン、プロピレングリコールなどの多価アルコールを主体
とし、これに無水フタル酸、イソフタル酸、アジピン酸
などの飽和多塩基酸を一部配合して合成されるポリエス
テル又はアクリル酸、メタクリル酸などの不飽和酸と、
エポキシ樹脂を反応させてなるビニルエステル樹脂を、
スチレン、ビニルトルエン、アクリルエステルなるビニ
ルモノマーに溶解したものである。The unsaturated polyester resin composition contains an unsaturated dibasic acid such as (anhydrous) maleic acid, fumaric acid, and itaconic acid,
Polyester, acrylic acid, and methacrylic acid synthesized by mainly containing polyhydric alcohols such as ethylene glycol, diethylene glycol, glycerin, and propylene glycol, and partially blending saturated polybasic acids such as phthalic anhydride, isophthalic acid, and adipic acid. unsaturated acids such as acids,
Vinyl ester resin made by reacting epoxy resin,
It is dissolved in vinyl monomers such as styrene, vinyltoluene, and acrylic ester.
前記した反応硬化性液状樹脂組成物の耐衝撃性、耐摩耗
性、防食性、応力緩和性などをさらに向上させるために
は、各種公知のフィラーが必要に応じて配合される。In order to further improve the impact resistance, abrasion resistance, corrosion resistance, stress relaxation properties, etc. of the above-mentioned reaction-curable liquid resin composition, various known fillers may be added as necessary.
t;とえば、微粉系フィラーとしては、変性ポリエチレ
ン系微粉、架橋フェノール樹脂系微粉、ポリフェニレン
サルファイド系微粉、フェノキシ樹脂系微粉などが、バ
ルーン系フィラーとしては、ガラスバルーン、シラスバ
ルーン、プラスチックバルーンなどが、フレーク系フィ
ラーとしては、チタンフレーク、アルミフレーク、ステ
ンレスフレーク、クロムフレーク、マイカフレークなど
を挙げることができる。また、体質顔料としては、タル
り、マイカ、タンカル、バリダ、シリカなどを挙げるこ
とができる。For example, fine powder fillers include modified polyethylene fine powder, crosslinked phenol resin fine powder, polyphenylene sulfide fine powder, phenoxy resin fine powder, etc.; balloon fillers include glass balloons, shirasu balloons, plastic balloons, etc. Examples of the flake filler include titanium flakes, aluminum flakes, stainless steel flakes, chrome flakes, and mica flakes. Examples of extender pigments include tartar, mica, tancal, barida, and silica.
前記の反応硬化性液状樹脂組成物は、面状補強材に含浸
されるが、含浸作業性のためには低粘度が望ましく、ま
た膜厚確保、安全衛生面などからは溶剤は少ない方が望
ましい。さらに、低温作業時等に必要に応じて低粘度の
反応性または非反応性希釈剤の使用も可能である。The above reaction-curable liquid resin composition is impregnated into the planar reinforcing material, but a low viscosity is desirable for impregnation workability, and a small amount of solvent is desirable from the viewpoint of ensuring film thickness and safety and hygiene. . Furthermore, it is also possible to use a low-viscosity reactive or non-reactive diluent, if necessary, such as when working at low temperatures.
含浸方法としては、たとえば下記のような方法がある。Examples of impregnation methods include the following methods.
(1)含浸樹脂組成物を一定の厚みに流延し、その上か
ら、面状補強材を沈み込ませる。(1) The impregnated resin composition is cast to a certain thickness, and the planar reinforcing material is sunk thereon.
(2)含浸樹脂組成物で満たされた容器内に面状補強材
を浸漬して、過剰の樹脂組成物をかき取りながらひき上
げる。(2) The planar reinforcing material is immersed in a container filled with the impregnated resin composition, and pulled up while scraping off the excess resin composition.
(3)面状補強材を、二枚の離型紙ではさんで、その間
に含浸樹脂組成物を充填し、一定のクリアランスを有す
る2本ロールをしごきながら通す。(3) The planar reinforcing material is sandwiched between two pieces of release paper, the impregnated resin composition is filled between them, and the material is passed through two rolls having a certain clearance while being squeezed.
前記のようにして、面状補強材に含浸樹脂組成物を含浸
させ、常温で反応硬化させて、これを永久変形可能な可
塑性が発現する固体状となるまで硬化させプリプレグ被
覆材を作成する。このプリプレグ被覆材は、接着性プラ
イマー層に貼り付けられるが、プリプレグ被覆材の硬化
状態は前記した状態にあることが必要である。もしそう
でない場合、例えば硬化が余り進んでいない液状の場合
には貼り付は作業が非常に困難であり、しかも貼り付は
後の溶剤の揮散や樹脂の硬化による歪の発生残存が大き
くなり、被覆系の耐久性が期待できなくなるし、逆に硬
化が進みすぎると、プリプレグの可塑性が失われて、平
面形状以外の鋼構造物への被覆が困難になる。As described above, the planar reinforcing material is impregnated with the impregnated resin composition, and is reacted and cured at room temperature until it becomes a solid state that exhibits plasticity capable of being permanently deformed, thereby producing a prepreg covering material. This prepreg covering material is pasted on the adhesive primer layer, but the cured state of the prepreg covering material needs to be in the above-described state. If this is not the case, for example, if it is a liquid that has not progressed much in curing, it will be very difficult to paste it, and moreover, it will be more likely that distortion will remain due to volatilization of the solvent and hardening of the resin. The durability of the coating system cannot be expected, and conversely, if hardening progresses too much, the prepreg loses its plasticity, making it difficult to coat steel structures other than planar shapes.
[作用及び効果1
本発明において、接着性プライマー層を複層にしたこと
によりプリプレグの貼り付けを余裕をもって行なうこと
ができ、しかも密着性、防食性に優。[Functions and Effects 1] In the present invention, since the adhesive primer layer is made into multiple layers, the prepreg can be attached with ease, and has excellent adhesion and anticorrosion properties.
れたプライマー層となる。その上にプリプレグ被覆材が
貼り合せられ、完全に密着硬化させて得られる完全硬化
膜は、重防食被覆層として用いることができ、その機能
は、
(i)耐衝撃性、強靭性
(ii)鋼材腐食因子(02、H,O,CQなど)の遮
断性
(iii)下層(プライマー)との付着性などに優れ、
下層の防食層(プライマー層)の環境からの保護作用を
するとともに
(iv)上記(i)〜(iii)の長期耐久性にも優れ
るという効果がある。It becomes a primer layer. A prepreg coating material is laminated on top of the prepreg coating material and the completely cured film obtained by completely adhering and curing can be used as a heavy corrosion protection coating layer, and its functions are: (i) Impact resistance and toughness (ii) Excellent barrier properties against steel corrosion factors (02, H, O, CQ, etc.) (iii) and adhesion to the lower layer (primer), etc.
It has the effect of protecting the lower anticorrosion layer (primer layer) from the environment and (iv) having excellent long-term durability as described in (i) to (iii) above.
[実施例コ
以下、本発明を実施例に基づいて具体的に説明する。実
施例中の「部」は「重量部」を意味する。[Example] Hereinafter, the present invention will be specifically explained based on an example. "Parts" in the examples mean "parts by weight."
実施例1〜2
表−1に示す被覆プライマー組成物を30OA鋼材表面
にそれぞれ25μITl(乾燥膜厚)になるように塗装
し、種々時間を変えて常温乾燥させ、ついで、その上に
表−1に示す厚さ1.5mmのプリプレグ被覆材を貼り
合せて完全に硬化させた。Examples 1 to 2 The coating primer composition shown in Table 1 was applied to the surface of 30OA steel to a thickness of 25 μITl (dry film thickness), dried at room temperature for various times, and then coated with the coating primer composition shown in Table 1. A prepreg covering material having a thickness of 1.5 mm as shown in Figure 1 was bonded and completely cured.
かくして得られた完全硬化膜の鋼管に対する接着状態お
よび防食性を評価し、表−1に示す結果が得られた。The adhesion state and corrosion resistance of the thus obtained completely cured film to the steel pipe were evaluated, and the results shown in Table 1 were obtained.
比較例1〜3
接着性プライマーとして表−1に示す各プライマー組成
物を単層で用いた。Comparative Examples 1 to 3 Each primer composition shown in Table 1 was used as an adhesive primer in a single layer.
Claims (1)
で反応硬化性のエポキシ樹脂プライマー組成物を塗布し
、ついでポリチオールを硬化剤とする常温で反応硬化性
のエポキシ樹脂プライマー組成物を塗布し、上層となる
下記プリプレグ被覆層との初期粘着力が0.5g/cm
以上になるまで硬化させて接着性複層プライマー層を形
成し、(ii)該接着性複層プライマー層の上に、常温
で反応硬化性の液状樹脂組成物を繊維加工補強材に含浸
させて、永久変形可能な可塑性が発現する固体状になる
まで硬化させたプリプレグ被覆層を貼り合せ、ついで (iii)該接着性複層プライマー層及び該プリプレグ
被覆層の両層を完全に密着硬化させることを特徴とする
プリプレグ被覆方法。[Claims] 1. (i) Apply an epoxy resin primer composition that is reactively curable at room temperature using polyamine as a curing agent to the surface of the steel material, and then apply an epoxy resin primer composition that is reactively curable at room temperature and uses polythiol as a curing agent. Apply the resin primer composition and have an initial adhesive strength of 0.5 g/cm with the upper prepreg coating layer below.
(ii) on the adhesive multilayer primer layer, a liquid resin composition that is reactively curable at room temperature is impregnated into the fiber processing reinforcing material; , bonding a prepreg coating layer that has been cured to a solid state that exhibits permanently deformable plasticity, and then (iii) completely adhering and curing both the adhesive multilayer primer layer and the prepreg coating layer. A prepreg coating method characterized by:
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2133930A JPH0776278B2 (en) | 1990-05-25 | 1990-05-25 | Prepreg coating method using multilayer primer |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2133930A JPH0776278B2 (en) | 1990-05-25 | 1990-05-25 | Prepreg coating method using multilayer primer |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH0428531A true JPH0428531A (en) | 1992-01-31 |
JPH0776278B2 JPH0776278B2 (en) | 1995-08-16 |
Family
ID=15116401
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2133930A Expired - Lifetime JPH0776278B2 (en) | 1990-05-25 | 1990-05-25 | Prepreg coating method using multilayer primer |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0776278B2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103850355A (en) * | 2012-12-04 | 2014-06-11 | 中国科学院大连化学物理研究所 | Structure for thermal protective coating of rocket launching pad and application thereof |
-
1990
- 1990-05-25 JP JP2133930A patent/JPH0776278B2/en not_active Expired - Lifetime
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103850355A (en) * | 2012-12-04 | 2014-06-11 | 中国科学院大连化学物理研究所 | Structure for thermal protective coating of rocket launching pad and application thereof |
CN103850355B (en) * | 2012-12-04 | 2016-08-03 | 中国科学院大连化学物理研究所 | The structure of a kind of rocket launching pad thermal protection coating and application thereof |
Also Published As
Publication number | Publication date |
---|---|
JPH0776278B2 (en) | 1995-08-16 |
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