WO1999061725A1 - Procede pour reparer et renforcer une structure existante en beton et resine conçue a cet effet - Google Patents
Procede pour reparer et renforcer une structure existante en beton et resine conçue a cet effet Download PDFInfo
- Publication number
- WO1999061725A1 WO1999061725A1 PCT/JP1999/002756 JP9902756W WO9961725A1 WO 1999061725 A1 WO1999061725 A1 WO 1999061725A1 JP 9902756 W JP9902756 W JP 9902756W WO 9961725 A1 WO9961725 A1 WO 9961725A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- resin
- reinforcing
- sheet material
- fiber sheet
- concrete structure
- Prior art date
Links
- 229920005989 resin Polymers 0.000 title claims abstract description 164
- 239000011347 resin Substances 0.000 title claims abstract description 164
- 239000004567 concrete Substances 0.000 title claims abstract description 47
- 238000000034 method Methods 0.000 title claims abstract description 35
- 230000003014 reinforcing effect Effects 0.000 title claims abstract description 27
- 239000012783 reinforcing fiber Substances 0.000 claims abstract description 86
- 239000000463 material Substances 0.000 claims abstract description 84
- 239000000835 fiber Substances 0.000 claims description 34
- 239000000178 monomer Substances 0.000 claims description 23
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 16
- 239000004917 carbon fiber Substances 0.000 claims description 16
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 13
- 230000008439 repair process Effects 0.000 claims description 10
- 230000002787 reinforcement Effects 0.000 claims description 7
- 239000003365 glass fiber Substances 0.000 claims description 6
- 239000012790 adhesive layer Substances 0.000 claims description 5
- 239000002759 woven fabric Substances 0.000 claims description 5
- 125000003647 acryloyl group Chemical group O=C([*])C([H])=C([H])[H] 0.000 claims description 4
- 150000001875 compounds Chemical class 0.000 claims description 4
- 125000005641 methacryl group Chemical group 0.000 claims description 4
- 229920013730 reactive polymer Polymers 0.000 claims description 4
- 239000004744 fabric Substances 0.000 claims description 3
- 125000000524 functional group Chemical group 0.000 claims description 3
- 239000003822 epoxy resin Substances 0.000 description 17
- 239000000203 mixture Substances 0.000 description 17
- 229920000647 polyepoxide Polymers 0.000 description 17
- 239000003795 chemical substances by application Substances 0.000 description 14
- 238000006243 chemical reaction Methods 0.000 description 13
- 229920000642 polymer Polymers 0.000 description 11
- 239000002131 composite material Substances 0.000 description 10
- VVQNEPGJFQJSBK-UHFFFAOYSA-N Methyl methacrylate Chemical compound COC(=O)C(C)=C VVQNEPGJFQJSBK-UHFFFAOYSA-N 0.000 description 8
- 238000011156 evaluation Methods 0.000 description 7
- NIXOWILDQLNWCW-UHFFFAOYSA-N 2-Propenoic acid Natural products OC(=O)C=C NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 6
- 229920000297 Rayon Polymers 0.000 description 6
- PPBRXRYQALVLMV-UHFFFAOYSA-N Styrene Chemical compound C=CC1=CC=CC=C1 PPBRXRYQALVLMV-UHFFFAOYSA-N 0.000 description 6
- -1 acrylate ester Chemical class 0.000 description 6
- 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
- 230000000052 comparative effect Effects 0.000 description 6
- 238000005470 impregnation Methods 0.000 description 6
- 239000004593 Epoxy Substances 0.000 description 5
- 239000012188 paraffin wax Substances 0.000 description 5
- 239000011342 resin composition Substances 0.000 description 5
- RTZKZFJDLAIYFH-UHFFFAOYSA-N Diethyl ether Chemical compound CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 description 4
- CERQOIWHTDAKMF-UHFFFAOYSA-N Methacrylic acid Chemical compound CC(=C)C(O)=O CERQOIWHTDAKMF-UHFFFAOYSA-N 0.000 description 4
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 4
- 239000007822 coupling agent Substances 0.000 description 4
- 239000011159 matrix material Substances 0.000 description 4
- 238000002156 mixing Methods 0.000 description 4
- 229920000193 polymethacrylate Polymers 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- SMZOUWXMTYCWNB-UHFFFAOYSA-N 2-(2-methoxy-5-methylphenyl)ethanamine Chemical compound COC1=CC=C(C)C=C1CCN SMZOUWXMTYCWNB-UHFFFAOYSA-N 0.000 description 3
- NIXOWILDQLNWCW-UHFFFAOYSA-M Acrylate Chemical compound [O-]C(=O)C=C NIXOWILDQLNWCW-UHFFFAOYSA-M 0.000 description 3
- LFQSCWFLJHTTHZ-UHFFFAOYSA-N Ethanol Chemical compound CCO LFQSCWFLJHTTHZ-UHFFFAOYSA-N 0.000 description 3
- 239000002253 acid Substances 0.000 description 3
- 150000001252 acrylic acid derivatives Chemical class 0.000 description 3
- 229920001971 elastomer Polymers 0.000 description 3
- 239000003999 initiator Substances 0.000 description 3
- GEMHFKXPOCTAIP-UHFFFAOYSA-N n,n-dimethyl-n'-phenylcarbamimidoyl chloride Chemical compound CN(C)C(Cl)=NC1=CC=CC=C1 GEMHFKXPOCTAIP-UHFFFAOYSA-N 0.000 description 3
- NWVVVBRKAWDGAB-UHFFFAOYSA-N p-methoxyphenol Chemical compound COC1=CC=C(O)C=C1 NWVVVBRKAWDGAB-UHFFFAOYSA-N 0.000 description 3
- 238000006116 polymerization reaction Methods 0.000 description 3
- 150000007519 polyprotic acids Polymers 0.000 description 3
- 238000002360 preparation method Methods 0.000 description 3
- 238000010526 radical polymerization reaction Methods 0.000 description 3
- 150000005846 sugar alcohols Polymers 0.000 description 3
- 238000009864 tensile test Methods 0.000 description 3
- JKNCOURZONDCGV-UHFFFAOYSA-N 2-(dimethylamino)ethyl 2-methylprop-2-enoate Chemical compound CN(C)CCOC(=O)C(C)=C JKNCOURZONDCGV-UHFFFAOYSA-N 0.000 description 2
- XDLMVUHYZWKMMD-UHFFFAOYSA-N 3-trimethoxysilylpropyl 2-methylprop-2-enoate Chemical compound CO[Si](OC)(OC)CCCOC(=O)C(C)=C XDLMVUHYZWKMMD-UHFFFAOYSA-N 0.000 description 2
- 239000004925 Acrylic resin Substances 0.000 description 2
- 229920000178 Acrylic resin Polymers 0.000 description 2
- NLHHRLWOUZZQLW-UHFFFAOYSA-N Acrylonitrile Chemical compound C=CC#N NLHHRLWOUZZQLW-UHFFFAOYSA-N 0.000 description 2
- VTYYLEPIZMXCLO-UHFFFAOYSA-L Calcium carbonate Chemical compound [Ca+2].[O-]C([O-])=O VTYYLEPIZMXCLO-UHFFFAOYSA-L 0.000 description 2
- BAPJBEWLBFYGME-UHFFFAOYSA-N Methyl acrylate Chemical compound COC(=O)C=C BAPJBEWLBFYGME-UHFFFAOYSA-N 0.000 description 2
- 239000006087 Silane Coupling Agent Substances 0.000 description 2
- WNLRTRBMVRJNCN-UHFFFAOYSA-N adipic acid Chemical compound OC(=O)CCCCC(O)=O WNLRTRBMVRJNCN-UHFFFAOYSA-N 0.000 description 2
- 125000003118 aryl group Chemical group 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 2
- 229910052791 calcium Inorganic materials 0.000 description 2
- 239000003054 catalyst Substances 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 239000003086 colorant Substances 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- RWGFKTVRMDUZSP-UHFFFAOYSA-N cumene Chemical compound CC(C)C1=CC=CC=C1 RWGFKTVRMDUZSP-UHFFFAOYSA-N 0.000 description 2
- 235000014113 dietary fatty acids Nutrition 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 150000002148 esters Chemical class 0.000 description 2
- 239000000194 fatty acid Substances 0.000 description 2
- 229930195729 fatty acid Natural products 0.000 description 2
- 150000004665 fatty acids Chemical class 0.000 description 2
- 239000003112 inhibitor Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000004745 nonwoven fabric Substances 0.000 description 2
- 230000000704 physical effect Effects 0.000 description 2
- 229920000058 polyacrylate Polymers 0.000 description 2
- 229920000728 polyester Polymers 0.000 description 2
- 239000005060 rubber Substances 0.000 description 2
- 239000000377 silicon dioxide Substances 0.000 description 2
- 238000003786 synthesis reaction Methods 0.000 description 2
- 229920001187 thermosetting polymer Polymers 0.000 description 2
- 229920002818 (Hydroxyethyl)methacrylate Polymers 0.000 description 1
- LYDOQHFHYWDZBS-UHFFFAOYSA-N 1-phenoxyethane-1,2-diol;prop-2-enoic acid Chemical compound OC(=O)C=C.OCC(O)OC1=CC=CC=C1 LYDOQHFHYWDZBS-UHFFFAOYSA-N 0.000 description 1
- GOXQRTZXKQZDDN-UHFFFAOYSA-N 2-Ethylhexyl acrylate Chemical compound CCCCC(CC)COC(=O)C=C GOXQRTZXKQZDDN-UHFFFAOYSA-N 0.000 description 1
- WDQMWEYDKDCEHT-UHFFFAOYSA-N 2-ethylhexyl 2-methylprop-2-enoate Chemical compound CCCCC(CC)COC(=O)C(C)=C WDQMWEYDKDCEHT-UHFFFAOYSA-N 0.000 description 1
- FRIBMENBGGCKPD-UHFFFAOYSA-N 3-(2,3-dimethoxyphenyl)prop-2-enal Chemical compound COC1=CC=CC(C=CC=O)=C1OC FRIBMENBGGCKPD-UHFFFAOYSA-N 0.000 description 1
- VTTSDRCSFUAZOE-UHFFFAOYSA-N 3-ethenylhepta-1,3-diene Chemical compound CCCC=C(C=C)C=C VTTSDRCSFUAZOE-UHFFFAOYSA-N 0.000 description 1
- MECNWXGGNCJFQJ-UHFFFAOYSA-N 3-piperidin-1-ylpropane-1,2-diol Chemical compound OCC(O)CN1CCCCC1 MECNWXGGNCJFQJ-UHFFFAOYSA-N 0.000 description 1
- FYRWKWGEFZTOQI-UHFFFAOYSA-N 3-prop-2-enoxy-2,2-bis(prop-2-enoxymethyl)propan-1-ol Chemical compound C=CCOCC(CO)(COCC=C)COCC=C FYRWKWGEFZTOQI-UHFFFAOYSA-N 0.000 description 1
- 229910002012 Aerosil® Inorganic materials 0.000 description 1
- 101500021165 Aplysia californica Myomodulin-A Proteins 0.000 description 1
- 241000531908 Aramides Species 0.000 description 1
- 239000004342 Benzoyl peroxide Substances 0.000 description 1
- OMPJBNCRMGITSC-UHFFFAOYSA-N Benzoylperoxide Chemical compound C=1C=CC=CC=1C(=O)OOC(=O)C1=CC=CC=C1 OMPJBNCRMGITSC-UHFFFAOYSA-N 0.000 description 1
- 229930185605 Bisphenol Natural products 0.000 description 1
- 239000004386 Erythritol Substances 0.000 description 1
- UNXHWFMMPAWVPI-UHFFFAOYSA-N Erythritol Natural products OCC(O)C(O)CO UNXHWFMMPAWVPI-UHFFFAOYSA-N 0.000 description 1
- VGGSQFUCUMXWEO-UHFFFAOYSA-N Ethene Chemical compound C=C VGGSQFUCUMXWEO-UHFFFAOYSA-N 0.000 description 1
- JIGUQPWFLRLWPJ-UHFFFAOYSA-N Ethyl acrylate Chemical compound CCOC(=O)C=C JIGUQPWFLRLWPJ-UHFFFAOYSA-N 0.000 description 1
- JOYRKODLDBILNP-UHFFFAOYSA-N Ethyl urethane Chemical compound CCOC(N)=O JOYRKODLDBILNP-UHFFFAOYSA-N 0.000 description 1
- 239000005977 Ethylene Substances 0.000 description 1
- KRHYYFGTRYWZRS-UHFFFAOYSA-N Fluorane Chemical compound F KRHYYFGTRYWZRS-UHFFFAOYSA-N 0.000 description 1
- WOBHKFSMXKNTIM-UHFFFAOYSA-N Hydroxyethyl methacrylate Chemical compound CC(=C)C(=O)OCCO WOBHKFSMXKNTIM-UHFFFAOYSA-N 0.000 description 1
- CERQOIWHTDAKMF-UHFFFAOYSA-M Methacrylate Chemical compound CC(=C)C([O-])=O CERQOIWHTDAKMF-UHFFFAOYSA-M 0.000 description 1
- UFWIBTONFRDIAS-UHFFFAOYSA-N Naphthalene Chemical compound C1=CC=CC2=CC=CC=C21 UFWIBTONFRDIAS-UHFFFAOYSA-N 0.000 description 1
- 239000004952 Polyamide Substances 0.000 description 1
- 239000004698 Polyethylene Substances 0.000 description 1
- 239000004734 Polyphenylene sulfide Substances 0.000 description 1
- DFPOZTRSOAQFIK-UHFFFAOYSA-N S,S-dimethyl-beta-propiothetin Chemical compound C[S+](C)CCC([O-])=O DFPOZTRSOAQFIK-UHFFFAOYSA-N 0.000 description 1
- 235000021355 Stearic acid Nutrition 0.000 description 1
- LCXXNKZQVOXMEH-UHFFFAOYSA-N Tetrahydrofurfuryl methacrylate Chemical compound CC(=C)C(=O)OCC1CCCO1 LCXXNKZQVOXMEH-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 229920006311 Urethane elastomer Polymers 0.000 description 1
- RMKZLFMHXZAGTM-UHFFFAOYSA-N [dimethoxy(propyl)silyl]oxymethyl prop-2-enoate Chemical compound CCC[Si](OC)(OC)OCOC(=O)C=C RMKZLFMHXZAGTM-UHFFFAOYSA-N 0.000 description 1
- 229920000800 acrylic rubber Polymers 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- 235000011037 adipic acid Nutrition 0.000 description 1
- 239000001361 adipic acid Substances 0.000 description 1
- 238000007605 air drying Methods 0.000 description 1
- 125000001931 aliphatic group Chemical group 0.000 description 1
- 125000000746 allylic group Chemical group 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 150000008064 anhydrides Chemical class 0.000 description 1
- 239000002518 antifoaming agent Substances 0.000 description 1
- 229920003235 aromatic polyamide Polymers 0.000 description 1
- 125000005013 aryl ether group Chemical group 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 235000019400 benzoyl peroxide Nutrition 0.000 description 1
- 230000001680 brushing effect Effects 0.000 description 1
- CDQSJQSWAWPGKG-UHFFFAOYSA-N butane-1,1-diol Chemical compound CCCC(O)O CDQSJQSWAWPGKG-UHFFFAOYSA-N 0.000 description 1
- CQEYYJKEWSMYFG-UHFFFAOYSA-N butyl acrylate Chemical compound CCCCOC(=O)C=C CQEYYJKEWSMYFG-UHFFFAOYSA-N 0.000 description 1
- 229910000019 calcium carbonate Inorganic materials 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 150000001732 carboxylic acid derivatives Chemical class 0.000 description 1
- 229910017052 cobalt Inorganic materials 0.000 description 1
- 239000010941 cobalt Substances 0.000 description 1
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 239000000806 elastomer Substances 0.000 description 1
- 229920006332 epoxy adhesive Polymers 0.000 description 1
- UNXHWFMMPAWVPI-ZXZARUISSA-N erythritol Chemical compound OC[C@H](O)[C@H](O)CO UNXHWFMMPAWVPI-ZXZARUISSA-N 0.000 description 1
- 229940009714 erythritol Drugs 0.000 description 1
- 235000019414 erythritol Nutrition 0.000 description 1
- 125000001033 ether group Chemical group 0.000 description 1
- 238000011049 filling Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- VOZRXNHHFUQHIL-UHFFFAOYSA-N glycidyl methacrylate Chemical compound CC(=C)C(=O)OCC1CO1 VOZRXNHHFUQHIL-UHFFFAOYSA-N 0.000 description 1
- 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 1
- 238000010438 heat treatment Methods 0.000 description 1
- 229960002050 hydrofluoric acid Drugs 0.000 description 1
- 125000002887 hydroxy group Chemical group [H]O* 0.000 description 1
- 230000000977 initiatory effect Effects 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 239000010410 layer Substances 0.000 description 1
- 150000002734 metacrylic acid derivatives Chemical class 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 125000005395 methacrylic acid group Chemical group 0.000 description 1
- 125000002496 methyl group Chemical group [H]C([H])([H])* 0.000 description 1
- DYGOPFFOGFHOIB-UHFFFAOYSA-N methylperoxyethane Chemical compound CCOOC DYGOPFFOGFHOIB-UHFFFAOYSA-N 0.000 description 1
- 239000004570 mortar (masonry) Substances 0.000 description 1
- GYVGXEWAOAAJEU-UHFFFAOYSA-N n,n,4-trimethylaniline Chemical compound CN(C)C1=CC=C(C)C=C1 GYVGXEWAOAAJEU-UHFFFAOYSA-N 0.000 description 1
- QIQXTHQIDYTFRH-UHFFFAOYSA-N octadecanoic acid Chemical compound CCCCCCCCCCCCCCCCCC(O)=O QIQXTHQIDYTFRH-UHFFFAOYSA-N 0.000 description 1
- OQCDKBAXFALNLD-UHFFFAOYSA-N octadecanoic acid Natural products CCCCCCCC(C)CCCCCCCCC(O)=O OQCDKBAXFALNLD-UHFFFAOYSA-N 0.000 description 1
- 150000001451 organic peroxides Chemical class 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- PNJWIWWMYCMZRO-UHFFFAOYSA-N pent‐4‐en‐2‐one Natural products CC(=O)CC=C PNJWIWWMYCMZRO-UHFFFAOYSA-N 0.000 description 1
- 150000002978 peroxides Chemical class 0.000 description 1
- 239000000049 pigment Substances 0.000 description 1
- 229920002647 polyamide Polymers 0.000 description 1
- 229920000768 polyamine Polymers 0.000 description 1
- 229920000573 polyethylene Polymers 0.000 description 1
- 229920001228 polyisocyanate Polymers 0.000 description 1
- 239000005056 polyisocyanate Substances 0.000 description 1
- 239000003505 polymerization initiator Substances 0.000 description 1
- 229920005862 polyol Polymers 0.000 description 1
- 150000003077 polyols Chemical class 0.000 description 1
- 229920000069 polyphenylene sulfide Polymers 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- HJWLCRVIBGQPNF-UHFFFAOYSA-N prop-2-enylbenzene Chemical compound C=CCC1=CC=CC=C1 HJWLCRVIBGQPNF-UHFFFAOYSA-N 0.000 description 1
- 230000009257 reactivity Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000004513 sizing Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 239000008117 stearic acid Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 150000003512 tertiary amines Chemical class 0.000 description 1
- 229920005992 thermoplastic resin Polymers 0.000 description 1
- 239000013008 thixotropic agent Substances 0.000 description 1
- 229920001567 vinyl ester resin Polymers 0.000 description 1
- 239000001993 wax Substances 0.000 description 1
- 238000009941 weaving Methods 0.000 description 1
Classifications
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04G—SCAFFOLDING; FORMS; SHUTTERING; BUILDING IMPLEMENTS OR AIDS, OR THEIR USE; HANDLING BUILDING MATERIALS ON THE SITE; REPAIRING, BREAKING-UP OR OTHER WORK ON EXISTING BUILDINGS
- E04G23/00—Working measures on existing buildings
- E04G23/02—Repairing, e.g. filling cracks; Restoring; Altering; Enlarging
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04G—SCAFFOLDING; FORMS; SHUTTERING; BUILDING IMPLEMENTS OR AIDS, OR THEIR USE; HANDLING BUILDING MATERIALS ON THE SITE; REPAIRING, BREAKING-UP OR OTHER WORK ON EXISTING BUILDINGS
- E04G23/00—Working measures on existing buildings
- E04G23/02—Repairing, e.g. filling cracks; Restoring; Altering; Enlarging
- E04G23/0218—Increasing or restoring the load-bearing capacity of building construction elements
-
- E—FIXED CONSTRUCTIONS
- E04—BUILDING
- E04G—SCAFFOLDING; FORMS; SHUTTERING; BUILDING IMPLEMENTS OR AIDS, OR THEIR USE; HANDLING BUILDING MATERIALS ON THE SITE; REPAIRING, BREAKING-UP OR OTHER WORK ON EXISTING BUILDINGS
- E04G23/00—Working measures on existing buildings
- E04G23/02—Repairing, e.g. filling cracks; Restoring; Altering; Enlarging
- E04G23/0218—Increasing or restoring the load-bearing capacity of building construction elements
- E04G2023/0251—Increasing or restoring the load-bearing capacity of building construction elements by using fiber reinforced plastic elements
Definitions
- the present invention relates to a method for repairing and reinforcing an existing concrete structure such as a pier, a bridge, or a pillar of a building, and a resin used for the method.
- the epoxy resin mainly used for impregnating the reinforced fiber sheet material generally requires several days or more even at room temperature to cure and develop sufficient strength, and when the temperature is further lowered to 5 ° C or less. Unless a special heating means is used, there is a problem that the curing hardly progresses and the period of the curing becomes extremely long.
- a method of using a radical polymerizable resin that cures at a low curing temperature of 5 ° C and at a very low temperature of about 10 ° C as an impregnating resin is used.
- a radical polymerizable resin that cures at a low curing temperature of 5 ° C and at a very low temperature of about 10 ° C as an impregnating resin is used.
- Japanese Unexamined Patent Publication (A) Hei 9-184304, Hei 9-184405, Hei 10-775 Japanese Unexamined Patent Publication (A) Hei 9-184304, Hei 9-184405, Hei 10-775.
- the means of using such a radical polymerization type resin as the impregnating resin is to combine with a reinforcing fiber sheet material in a form suitable for a radical polymerization type resin system in the first place.
- the present inventors have conducted intensive studies to solve the above-mentioned problems, and as a result, by using an additional impregnating resin having a specific range of viscosity and curing time, the resin content developed as an impregnating resin with epoxy resin is 1%.
- the present inventors have found that a sufficient reinforcing effect can be exhibited even when a reinforcing fiber sheet material of 5% by weight or less is used, and the present invention has been achieved.
- the present invention relates to a reinforcing fiber sheet material having a resin content of 15% by weight or less, while impregnating a resin having a viscosity of 2.5 to 300 voids and a curing time of 1 to 24 hours with an existing resin.
- the first point is to repair and reinforce existing concrete structures that are attached to the surface of concrete structures and hardened with resin.
- the viscosity is 2.5 to 300 voise and the curing time is 1 to 24.
- the second point is the method of repairing and reinforcing existing concrete structures that impregnate the resin for a certain amount of time and cure the resin.
- the resin to be impregnated later into the reinforced fiber sheet material that is, a resin having a viscosity of 2.5 to 300 voids and a curing time of 1 to 24 hours
- resin a resin having a viscosity of 2.5 to 300 voids and a curing time of 1 to 24 hours
- the additional impregnated resin has a viscosity of 100 to 100 voids and a curing time of 2
- a radically polymerizable resin of up to 12 hours is particularly desirable, and this is the third aspect.
- a reinforcing fiber sheet material composed of reinforcing fibers and a resin having a limit of 15% by weight is preferably used in a repairing and reinforcing method using an epoxy resin as an impregnating resin. Is used.
- the resin (matrix resin) constituting the reinforcing fiber sheet material is impregnated with the reinforcing fiber, or the reinforcing fiber aligned with the bow I or the woven reinforcing fiber is, for example, a release paper or a support. It may be an adhesive layer that adheres to the sheet.
- the resin constituting the reinforcing fiber sheet material may be an uncured thermosetting resin or a polymerized thermoplastic resin, and is not particularly limited. Resins are commonly used. Of course, there is no problem even if the reinforcing fiber sheet material is specially manufactured according to the resin to be impregnated later (additional impregnating resin).
- the resin constituting the reinforcing fiber sheet material has a solubility parameter (SP) value of 17 to 2 as described later. It is preferable to use a resin having 8 (MPa) 1/2 .
- the amount of the matrix resin constituting the reinforcing fiber sheet material is 15% by weight or less.
- the amount of the resin exceeds 15% by weight, it is not preferable because curing failure of the additional impregnated resin and deterioration of physical properties of the cured product are caused.
- Reinforced fiber When the amount of the resin constituting the sheet material is 7% by weight or less, when the type of the resin constituting the reinforcing fiber sheet material is different from the type of the resin to be impregnated later, for example, the reinforcing fiber
- the resin constituting the sheet material is an epoxy resin, which is particularly preferable even when the reinforced fiber sheet material is later impregnated with a radical polymerizable resin, since sufficient curability and strength of the cured product can be obtained.
- the amount of resin constituting the reinforced fiber sheet material greatly affects the handleability of the reinforced fiber sheet material
- the amount of the resin is preferably 1% by weight or more.
- the reinforced fiber sheet material has a sufficiently low rigidity so that the resin that composes it can be attached to the existing concrete structure with a curvature, so that the resin constituting the material is uncured or along the attached place with the curvature.
- the resin be cured in a suitable form.
- the pot life (shelf life) at room temperature is long.
- reinforcing fibers constituting the reinforcing fiber sheet material in the present invention fibers usually used as reinforcing fibers such as carbon fiber, aramide fiber and glass fiber are preferably mentioned. Among them, carbon fiber is preferable.
- a high-strength carbon fiber having a tensile strength of 400 OMPa or more is particularly preferable when utilizing the strength, and a high elasticity having an elastic modulus of 250 GPa or more when using the elastic modulus. Carbon fibers are more preferred.
- a compound having a radical polymerizable functional group at at least one end is used as a sizing agent. It is particularly preferable to use the carbon fiber used as the material in view of the strength development of the cured product.
- the reinforcing form in the reinforcing fiber sheet material is not limited at all, and examples include a method in which reinforcing fibers are aligned in one direction or formed into a woven sheet.
- the basis weight of the reinforcing fiber is preferably 150 g Zm 2 or more.
- Examples of the form more preferably used as the reinforcing fiber sheet material used in the present invention include Japanese Patent Application Laid-Open Publications (A) Hei 3-2224901, Hei 3-222 734, Hei 5 As described in No. 3 804, No. 7-364 777, and No. 7-2 287 14, the following forms (1) to (3) are preferable .
- the support sheet a nonwoven fabric of fibers of various polymers such as glass fiber woven fabric, glass scrim cloth, glass fiber paper, glass fiber nonwoven fabric, polyamide, and polyphenylene sulfide is used.
- the adhesive may be any as long as it can at least temporarily adhere the reinforcing fibers to the support, and is preferably a resin having good compatibility with the matrix resin of the reinforcing fiber sheet material.
- the matrix resin is an epoxy resin
- an epoxy adhesive is preferred.
- the reinforcing fiber sheet material used in the present invention is not limited to the above-described reinforcing fiber sheet material.
- the reinforcing fiber sheet is used after reinforcing fibers are aligned in one direction, or after manufacturing.
- a resin in which the resin constituting the material is applied in a linear or dot shape to maintain the form, and a resin in which the above-mentioned support sheet is further bonded thereto can be applied.
- the reinforcing fiber sheet material is impregnated with a curable resin at the same time as or after attaching the reinforcing fiber sheet material to the surface of the existing structure.
- the additional impregnated resin may be a resin having a viscosity of 2.5 to 300 vois and a curing time of 1 to 24 hours, which may be repaired and reinforced using the above-mentioned reinforcing fiber sheet material. It is necessary to enhance the effect.
- the viscosity of the resin to be impregnated here is the viscosity measured at the construction temperature using a B-type viscometer.
- the resin to be impregnated is a radical polymerization type resin
- the viscosity is before addition of an organic peroxide or the like serving as a polymerization initiator.
- the viscosity of this resin exceeds 300 voids, it becomes difficult to impregnate the reinforcing fiber sheet material with the resin.On the contrary, when the viscosity is less than 2.5 voids, the combination with the above-mentioned reinforcing fiber sheet material becomes difficult.
- the reinforcing fibers tend to move, causing a reduction in the reinforcing effect. More preferably, the lower limit of the viscosity is 100 voids and the upper limit is 100 voids.
- the curing time in the present invention is a time from the start of curing of the resin to a time when the tackiness is eliminated by touch with a finger, and when a resin having a curing time of less than 1 hour is used, the development of strength is poor. Conversely, a resin having a curing time exceeding 24 hours is too long for the purpose of the present invention because the curing time is too long.
- the lower limit of the curing time is more preferably 2 hours or more, and the upper limit is more preferably within 12 hours, most preferably within 8 hours.
- a resin that satisfies the requirements of the viscosity and the curing time described above is preferable, and among them, a thermosetting resin is preferable, and a room temperature curable resin is particularly preferable.
- a radical polymerizable resin is particularly preferable, and a radical polymerizable resin composed of a radical polymerizable monomer or oligomer having a methacryl group or an acryloyl group as a terminal reactive group is cured. It is particularly preferable from the viewpoint of the balance between the properties and the properties of the cured product.
- the terminal reactive group may be a composition containing a monomer other than a methyl group or an acryloyl group, for example, styrene.
- Radical polymerizable monomers include acrylates such as methyl acrylate and ethyl acrylate, methyl methacrylate, 2-ethylhexyl methacrylate, hydroxyethyl methacrylate, and tetrahydrofurfuryl methacrylate.
- acrylates and methacrylates are particularly preferred in terms of curability and strength.
- the radical polymerizable monomer in the present invention is preferably a monomer that is compatible with the resin adhering to the reinforcing fiber sheet to some extent, the solubility parameter of the radical polymerizable monomer has an SP value of 17 to 2 Those having a range of 2 (MP a) 2 are particularly preferred.
- polymerizable oligomers include acrylic acid, methacrylic acid, etc. at the ends of oligomers obtained by the reaction of polybasic acids such as fluoric acid and adipic acid with polyhydric alcohols such as ethylene dalicol and butanediol.
- acrylic acid-containing polyester poly (meth) acrylates obtained by reaction with acrylic acid, polybasic acids and polyhydric alcohols
- An aryl group-containing polyester obtained by a reaction with an aryl ether group-containing alcohol, an epoxy poly (meth) acrylate obtained by a reaction of an epoxy resin with (meth) acrylic acid, a polyol and a polyisocyanate, and a hydroxyl group-containing (meth)
- examples thereof include, but are not limited to, urethane poly (meth) acrylate obtained by a reaction with acrylate.
- the molecular weight of the radically polymerizable oligomer used in the present invention is not particularly limited, but it is more preferably 1000 or less in terms of number average molecular weight from the viewpoint of curability at low temperatures.
- an elastomer component having a reactive functional group at the terminal is added to the cured product.
- the mixing ratio of the monomer and the oligomer in the resin for impregnation used in the present invention is not particularly limited as long as the viscosity and curing time of the composition are satisfied.
- initiators for initiating the polymerization of these radically polymerizable monomers and oligomers commonly used curing agent systems, for example, peroxides and metal accelerators and curing accelerators such as tertiary amines are used. Examples thereof include redox catalysts and the like.
- the combination is selected and used such that the curing time is 1 hour or more, 24 hours or less, preferably 12 hours or less.
- the polymer added instead of or in addition to the oligomer of the resin for impregnation is added for the purpose of adjusting the viscosity of the composition and improving the toughness and durability of the cured product.
- Preferred polymers include elastomeric polymers such as acrylic polymers, acrylonitrile rubber rubbers, acrylic rubbers, styrene block polymers, and urethane elastomers. However, it is not limited to this.
- the amount of the polymer to be added is not particularly limited as long as it satisfies the restrictions on the viscosity and curing time of the composition, but is preferably 50% by weight or less in many cases.
- radical polymerizable monomer and the non-reactive polymer be the main components, since the resin viscosity can be appropriately controlled.
- a radical polymerizable monomer and a radical polymerizable oligomer having a number average molecular weight of 1,000 or less and a non-reactive polymer are the main components, the reactivity of the resin and the resin viscosity can be appropriately controlled. preferable.
- the radically polymerizable resin in the present invention includes, in addition to the above-mentioned monomers, oligomers, polymers, and curing agent components, a thixotropic agent, an air-curing agent, a coupling agent, a polymerization inhibitor, and a coloring agent according to the purpose.
- a thixotropy-imparting agent examples include finely divided silica such as "Varodil 200" manufactured by Nippon Aerosil Co., Ltd. and “Nibusir LP” manufactured by Nippon Silica Industry Co., Ltd .; Organic powders such as finely divided calcium carbonate such as "Shirarenka CC" manufactured by Maruo Calcium Co., Ltd.
- the amount used is less than 10% by weight, usually less than 5% by weight.
- the air curing agent include paraffin wax represented by n-paraffin, higher fatty acids such as polyethylene wax and stearic acid, and glycidyl methacrylate, aryl glycidyl ether and the like.
- the addition amount of these air-curing agents is suitably from 0.1 to 10% by weight based on the resin to be impregnated, and if it is less than 0.1% by weight, sufficient air-curing properties cannot be obtained. If the content exceeds 10% by weight, the physical properties of the cured product tend to decrease.
- the range is particularly preferably 0.1 to 5% by weight based on the resin to be impregnated.
- the resin used in the present invention may be, if necessary, a silane coupling agent typified by acryloxypropyltrimethoxysilane, a titanate coupling agent, a zirconate coupling agent, an organic aluminum coupling.
- a power coupling agent such as an agent can be used alone or as a mixture.
- An appropriate amount of addition is 0.5 to 5 parts by weight based on 100 parts by weight of the resin to be impregnated.
- the resin used in the present invention contains an appropriate amount of a polymerization inhibitor in order to secure stability at the distribution stage. Further, a coloring agent, a pigment, an antifoaming agent, and the like can be added as needed.
- the amount of the additional impregnating resin impregnated into the reinforcing fiber sheet material is not particularly limited as long as the reinforcing fiber sheet and the additional impregnating resin become an integrated composite material after impregnation.
- the reinforced fiber sheet material is impregnated with a resin and is attached to the surface of an existing concrete structure to cure the resin, or the reinforced fiber sheet material is coated on the surface of the existing concrete structure. Can be carried out by impregnating with a resin and curing the resin. At this time, before attaching the reinforcing fiber sheet material The resin to be impregnated later may be preliminarily applied to the sticking place.
- the surface of the existing concrete structure to which the reinforcing fiber sheet material is to be attached must be smoothed using a grinder or the like to remove irregularities, steps, defects, cracks, etc. It is preferable to correct by filling in from the viewpoint of improving the bonding strength.
- the primer resin On the surface of the existing concrete structure to which the reinforcing fiber sheet material is to be attached, apply the appropriate amount of primer resin to the surface of the concrete by known means, such as brushing with a roller or spraying, if necessary, after removing the above irregularities. It is preferable to use a resin of the same type as the impregnating resin used later for attaching the reinforcing fiber sheet material. It is preferable that the primer resin has a low viscosity from the viewpoint of adhesiveness to concrete and workability, and the primer resin is a composition that hardens more quickly, for example, a composition that cures in about one hour. Such a primer resin is used by mixing a curing agent and a curing accelerator immediately before use.
- acrylic primer resin examples include, but are not limited to, “Acrycillap DR-80” manufactured by Mitsubishi Rayon Co., Ltd.
- the resin to be impregnated is used by mixing a curing agent and a curing accelerator immediately before use so that a predetermined curing time can be obtained.
- the additional impregnated resin is applied to the surface of an existing concrete structure to which the primer resin has been applied, and the reinforced fiber sheet material is adhered thereon, and then The additional impregnated resin is applied to the reinforcing fiber sheet material while extruding the air contained in the sheet by, for example, applying a defoaming hole to the air through a defoaming port.
- the required number of reinforcing fiber sheet materials can be attached while changing the fiber direction, thereby forming a repair reinforcing layer using a reinforcing fiber sheet.
- bisphenol A type epoxy resin ("Epico 1004" manufactured by Yuka Shell Epoxy Co., Ltd.) 1943 parts by weight, 86 parts by weight of methacrylic acid, 40 parts by weight of dimethylaminoethyl methacrylate, 2 parts by weight of hydroquinone monomethyl ether And 1227 parts by weight of methyl methacrylate, and the reaction temperature was raised to 9 O. The reaction was continued until the acid value became 8 (mgKOH / g) or less, to obtain an oligomer 1 containing 50% by weight of methyl methacrylate. Was. The number-average molecular weight of the composition obtained by removing the monomer component of the obtained oligomer 1 was 2,000.
- Epoxy ester (“3002M” manufactured by Kyoei Yushi Kagaku Kogyo Co., Ltd.) whose main component is bisphenol A derivative with methacrylic group at the end 1 wt% the deposited carbon fiber (manufactured by Mitsubishi Rayon Co., Ltd. "TR50") (tensile strength of 490 OMP a) a aligned in one direction so that the weight of the carbon fibers per 1 m 2 is 300 g, the curing agent 15 g per lm 2 of an epoxy resin composition containing no resin ("Base resin for # 350" manufactured by Mitsubishi Rayon Co., Ltd., SP value: 23), and then impregnated with a thickness of 25 ⁇ m as a support. Was bonded to obtain a reinforced fiber sheet material 1.
- the reinforcing fiber sheet material 1 was impregnated with the above impregnated resin so that the amount of resin per lm 2 was approximately 400 g, and was left to cure at 25 ° C. After 2 hours, the resin disappeared from the surface and hardened.
- a sample for a tensile test was prepared from the cured reinforcing fiber sheet material, and the tensile strength in the carbon fiber direction was measured.
- the average tensile strength of this composite was 410 OMPa in terms of 100% of carbon fiber.
- an acrylic primer resin ("Acrylic Wrap DR-80" manufactured by Mitsubishi Rayon Co., Ltd.) was applied to the surface of a concrete sample conforming to JIS (Japanese Industrial Standards) A-1132 at 25 ° C with a brush. after coating at a rate of lm 2 per 200 g, it was adhered reinforcing fiber sheet material 1 in the same manner as described above in concrete surfaces. After curing for one day, a tensile test was performed in accordance with JIS-A-6909. The strength was 2.4 MPa and the failure mode was material failure inside the concrete.
- oligomer 1 The above-mentioned oligomer 1 and an epoxy-based oligomer ("Epoxyester 3000M” manufactured by Kyoeisha Chemical Co., Ltd .; hereinafter, referred to as oligomer 2) were used in combination as the oligomer, and the ratio was changed as shown in Table 1 except that the ratio of each component was changed as shown in Table 1. The procedure was the same as in Example 1. Table 1 shows the evaluation results.
- Example 4 The operation was performed in the same manner as in Example 2 except that the amount of the curing accelerator used was halved. Table 1 shows the evaluation results. (Example 4)
- bisphenol A type epoxy resin (Epicoat 1004" manufactured by Yuka Shell Epoxy Co., Ltd.) 58 3 parts by weight, acrylic acid 43 parts by weight, dimethylaminoethyl methyl
- Add 6.2 parts by weight of acrylate, 0.62 parts by weight of hydroquinone monomethyl ether, and 633 parts by weight of methyl methacrylate raise the reaction temperature to 90 ° C, and reduce the acid value to 5 (mg KOH / g) or less.
- the reaction was continued until the reaction was completed to obtain an oligomer 3 containing 50% by weight of methyl methacrylate.
- the number average molecular weight of the composition obtained by removing the monomer component of the obtained oligomer 3 was 2,300.
- Example 1 The same operation as in Example 1 was carried out except that oligomer 3 was used instead of oligomer 1 as an oligomer component and the ratio of each component was changed as shown in Table 1. Table 1 shows the evaluation results.
- Example 1 was repeated except that an acrylic resin ("Dianal BR-83" manufactured by Mitsubishi Renyon Co., Ltd.) was used instead of Oligomer 1 and the ratio of each component was changed as shown in Table 1. The same operation was performed. Table 1 shows the evaluation results.
- Example 5 The same operation as in Example 5 was carried out except that the amount of the curing accelerator used was halved. Table 1 shows the evaluation results.
- the monomer component and the oligomer component were mixed at the ratios shown in Table 1 to prepare a resin composition having a viscosity of 2 voids at 25 ° C. before mixing the initiator, and the same operation as in Example 1 was performed. It is shown in Table 1.
- the curability of the impregnated resin was extremely good, and the adhesion to the concrete was good, but the tensile strength of the composite was insufficient at 3720 MPa.
- Example 7 Using the same impregnating resin as in Comparative Example 1, the test was performed by changing the sample preparation temperature to 5 ° C. and ⁇ 10 ° C., respectively.
- the amount of the curing accelerator was changed as shown in Table 1 so that the curing time was 5 hours.
- the viscosity of the composition at 5 ° C. was 15 boise, and the viscosity at —10: was 45 boise.
- the curing agent of the resin composition used in Comparative Example 1 was changed so that the curing time was 30 minutes.
- the evaluation results are shown in Table 1, but the tensile strength of the composite was further reduced.
- the monomer component and the polymer component were mixed in the ratio shown in Table 1 to prepare a resin composition having a viscosity of 400 vise at 25 ° C, and the same test was carried out. The subsequent evaluation could not be carried out due to the difficulty of impregnating the resin with the resin.
- Bisphenol ⁇ type epoxy resin (“Epicoat 828” manufactured by Yuka Shell Epoxy Co., Ltd.) 60 parts by weight, trimethylolpropane triglycidyl ether
- the epoxy resin composition was impregnated into the reinforcing fiber sheet used in Example 1 to prepare a composite tensile test piece. When the resin was left for 12 hours, it did not stick, but required 7 days to develop sufficient strength and elasticity. The tensile strength evaluated after 7 days was 420 OMPa.
- vinyl ester resin (“Lipoxy R — 840” manufactured by Showa Polymer Co., Ltd., viscosity at 25 ° C. 25 Boys, SP value: 19) 100 parts by weight, curing catalyst (CH Showa Polymer Co., Ltd.) 1), Naphthene as a curing accelerator
- curing catalyst CH Showa Polymer Co., Ltd.
- Naphthene as a curing accelerator
- Curing time at 25 ° C was 3 hours. Six hours after the resin was impregnated with the reinforcing fiber sheet material, the surface tack had completely disappeared, and the tensile strength of the composite was 402 OMPa.
- Example 9 The same operation as in Example 9 was carried out except that 2 parts by weight of methyl ethyl peroxide as a curing agent and 1 part by weight of cobalt naphthenate as a curing accelerator were used per 100 parts by weight of the resin.
- the curing time at 25 ° C. was 1 hour, and the tensile strength of the obtained composite after 6 hours was 300 OMPa.
- the test was performed in the same manner as in Example 7 except that an n-butyl acrylate oligomer having a methacryl group at one end and a number average molecular weight of 6000 was used instead of phenoxyethylene glycol acrylate. .
- the viscosity of the resin at 5 ° C. was 5 boys.
- the surface of the prepared sample had no tackiness after 6 hours, and the composition had good low-temperature curability.
- the tensile strength of the composite was 4100 MPa, and the failure mode in the adhesion test was material failure of concrete.
- reinforced fiber was used in the same manner as in Example 1 except that "Conwood Net ON 5050" (basis weight Y gZm 2 ) manufactured by Nisseki Palette System Co., Ltd. was used instead of "Scrim Cloth” manufactured by Nitto Boseki Co., Ltd. Sheet 2 was created.
- the same operation as in Example 3 was performed by combining this reinforcing fiber sheet material with the resin used in Example 3.
- the tensile strength of the obtained composite was 4,300 MPa, a value indicating sufficient strength development.
- Example 3 As the carbon fiber, a high elasticity carbon fiber having an elastic modulus of 392 GPa ("HR40" manufactured by Mitsubishi Rayon Co., Ltd., tensile strength 4610MPa) is used. Except for using the resin composition used in Example 3, the same as in Example 1
- the tensile strength of the bird was evaluated.
- the obtained tensile strength was 4.50 MPa, a value indicating sufficient strength development.
- repair and reinforcement of existing concrete structures for example, piers and buildings, etc.
- existing reinforcing fiber sheet materials can be effectively used.
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Abstract
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP99922484A EP1083274A4 (fr) | 1998-05-26 | 1999-05-26 | Procede pour reparer et renforcer une structure existante en beton et resine con ue a cet effet |
CA002333419A CA2333419A1 (fr) | 1998-05-26 | 1999-05-26 | Procede pour reparer et renforcer une structure existante en beton et resine concue a cet effet |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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JP14424998 | 1998-05-26 | ||
JP10/144249 | 1998-05-26 |
Publications (1)
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WO1999061725A1 true WO1999061725A1 (fr) | 1999-12-02 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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PCT/JP1999/002756 WO1999061725A1 (fr) | 1998-05-26 | 1999-05-26 | Procede pour reparer et renforcer une structure existante en beton et resine conçue a cet effet |
Country Status (5)
Country | Link |
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EP (1) | EP1083274A4 (fr) |
KR (1) | KR100429959B1 (fr) |
CA (1) | CA2333419A1 (fr) |
TW (1) | TW508401B (fr) |
WO (1) | WO1999061725A1 (fr) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2002322433A (ja) * | 2001-04-24 | 2002-11-08 | Denki Kagaku Kogyo Kk | 遅硬化型アクリル系接着剤組成物 |
KR20030023901A (ko) * | 2001-09-14 | 2003-03-26 | 주식회사 제트화이버코리아 | 콘크리트 구조물의 보수보강방법 |
JP2004107944A (ja) * | 2002-09-17 | 2004-04-08 | Konishi Co Ltd | 鋼製構造物の補強方法 |
JP2018188557A (ja) * | 2017-05-08 | 2018-11-29 | ショーボンド建設株式会社 | 接着剤注入工法及び接着剤 |
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KR100894677B1 (ko) * | 2007-01-19 | 2009-04-24 | 세종대학교산학협력단 | 교량 보수공법 |
US9321686B2 (en) * | 2013-03-15 | 2016-04-26 | Forta Corporation | Reinforcement fiber coating compositions, methods of making and treating, and uses for improved adhesion to asphalt and portland cement concrete |
KR101426032B1 (ko) | 2013-07-16 | 2014-08-05 | (주)진성테크 | 강화섬유패널 및 이를 이용한 구조물의 보강공법 |
CN108753223A (zh) * | 2018-04-26 | 2018-11-06 | 阜南县慧宏柳木工艺品有限公司 | 一种柳编制品套布的方法 |
KR102046397B1 (ko) * | 2019-04-08 | 2019-11-19 | 김창수 | 토목건축 구조물 보강용 양방향 배열 탄소섬유직물을 이용한 구조물 보강시공방법 |
KR102167528B1 (ko) * | 2020-03-26 | 2020-10-19 | 두정산업 주식회사 | 속경형 콘크리트 균열 보수용 아크릴 올리고머와 단량체 및 착색제를 이용한 균열 씰링제 조성물 및 이를 이용한 균열 보수 시공 방법 |
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- 1999-05-26 EP EP99922484A patent/EP1083274A4/fr not_active Withdrawn
- 1999-05-26 CA CA002333419A patent/CA2333419A1/fr not_active Abandoned
- 1999-05-26 KR KR10-2000-7013275A patent/KR100429959B1/ko not_active Expired - Fee Related
- 1999-05-26 TW TW088108648A patent/TW508401B/zh not_active IP Right Cessation
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Also Published As
Publication number | Publication date |
---|---|
CA2333419A1 (fr) | 1999-12-02 |
KR20010071320A (ko) | 2001-07-28 |
EP1083274A1 (fr) | 2001-03-14 |
KR100429959B1 (ko) | 2004-05-03 |
TW508401B (en) | 2002-11-01 |
EP1083274A4 (fr) | 2005-03-02 |
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