JPH0263735A - Preparation of composite panel - Google Patents
Preparation of composite panelInfo
- Publication number
- JPH0263735A JPH0263735A JP63215954A JP21595488A JPH0263735A JP H0263735 A JPH0263735 A JP H0263735A JP 63215954 A JP63215954 A JP 63215954A JP 21595488 A JP21595488 A JP 21595488A JP H0263735 A JPH0263735 A JP H0263735A
- Authority
- JP
- Japan
- Prior art keywords
- sheet
- adhesive layer
- layer
- thermoplastic resin
- density polyethylene
- 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
- 239000002131 composite material Substances 0.000 title claims abstract description 19
- 229910052751 metal Inorganic materials 0.000 claims abstract description 39
- 239000002184 metal Substances 0.000 claims abstract description 39
- 239000012790 adhesive layer Substances 0.000 claims abstract description 36
- 229920005992 thermoplastic resin Polymers 0.000 claims abstract description 19
- 239000010410 layer Substances 0.000 claims abstract description 18
- 229920000098 polyolefin Polymers 0.000 claims abstract description 13
- 229920005989 resin Polymers 0.000 claims abstract description 13
- 239000011347 resin Substances 0.000 claims abstract description 13
- 239000011162 core material Substances 0.000 claims abstract description 12
- 150000001732 carboxylic acid derivatives Chemical class 0.000 claims abstract description 5
- 238000000034 method Methods 0.000 claims description 16
- 238000004519 manufacturing process Methods 0.000 claims description 7
- PCHJSUWPFVWCPO-UHFFFAOYSA-N gold Chemical compound [Au] PCHJSUWPFVWCPO-UHFFFAOYSA-N 0.000 claims 1
- 239000010931 gold Substances 0.000 claims 1
- 229910052737 gold Inorganic materials 0.000 claims 1
- 229910052782 aluminium Inorganic materials 0.000 abstract description 10
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract description 10
- 229920001684 low density polyethylene Polymers 0.000 abstract description 9
- 239000004702 low-density polyethylene Substances 0.000 abstract description 9
- -1 polyethylene Polymers 0.000 abstract description 6
- FPYJFEHAWHCUMM-UHFFFAOYSA-N maleic anhydride Chemical compound O=C1OC(=O)C=C1 FPYJFEHAWHCUMM-UHFFFAOYSA-N 0.000 abstract description 5
- 239000004698 Polyethylene Substances 0.000 abstract description 4
- 238000010438 heat treatment Methods 0.000 abstract description 4
- 229920000573 polyethylene Polymers 0.000 abstract description 4
- 239000000853 adhesive Substances 0.000 description 8
- 230000001070 adhesive effect Effects 0.000 description 8
- 239000000178 monomer Substances 0.000 description 5
- 238000003825 pressing Methods 0.000 description 5
- 238000010030 laminating Methods 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- SOGAXMICEFXMKE-UHFFFAOYSA-N Butylmethacrylate Chemical compound CCCCOC(=O)C(C)=C SOGAXMICEFXMKE-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
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- BAPJBEWLBFYGME-UHFFFAOYSA-N Methyl acrylate Chemical compound COC(=O)C=C BAPJBEWLBFYGME-UHFFFAOYSA-N 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 239000004743 Polypropylene Substances 0.000 description 2
- PPBRXRYQALVLMV-UHFFFAOYSA-N Styrene Chemical compound C=CC1=CC=CC=C1 PPBRXRYQALVLMV-UHFFFAOYSA-N 0.000 description 2
- 238000003475 lamination Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000002156 mixing Methods 0.000 description 2
- 229920001083 polybutene Polymers 0.000 description 2
- 229920001155 polypropylene Polymers 0.000 description 2
- 229920003002 synthetic resin Polymers 0.000 description 2
- 239000000057 synthetic resin 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
- 230000037303 wrinkles Effects 0.000 description 2
- OZMRKDKXIMXNRP-BQYQJAHWSA-N (e)-4-(dibutylamino)-4-oxobut-2-enoic acid Chemical compound CCCCN(CCCC)C(=O)\C=C\C(O)=O OZMRKDKXIMXNRP-BQYQJAHWSA-N 0.000 description 1
- HBQGCOWNLUOCBU-ONEGZZNKSA-N (e)-4-(ethylamino)-4-oxobut-2-enoic acid Chemical compound CCNC(=O)\C=C\C(O)=O HBQGCOWNLUOCBU-ONEGZZNKSA-N 0.000 description 1
- FSQQTNAZHBEJLS-OWOJBTEDSA-N (e)-4-amino-4-oxobut-2-enoic acid Chemical compound NC(=O)\C=C\C(O)=O FSQQTNAZHBEJLS-OWOJBTEDSA-N 0.000 description 1
- BSSNZUFKXJJCBG-OWOJBTEDSA-N (e)-but-2-enediamide Chemical compound NC(=O)\C=C\C(N)=O BSSNZUFKXJJCBG-OWOJBTEDSA-N 0.000 description 1
- OZMRKDKXIMXNRP-FPLPWBNLSA-N (z)-4-(dibutylamino)-4-oxobut-2-enoic acid Chemical compound CCCCN(CCCC)C(=O)\C=C/C(O)=O OZMRKDKXIMXNRP-FPLPWBNLSA-N 0.000 description 1
- HBQGCOWNLUOCBU-ARJAWSKDSA-N (z)-4-(ethylamino)-4-oxobut-2-enoic acid Chemical compound CCNC(=O)\C=C/C(O)=O HBQGCOWNLUOCBU-ARJAWSKDSA-N 0.000 description 1
- BSSNZUFKXJJCBG-UPHRSURJSA-N (z)-but-2-enediamide Chemical compound NC(=O)\C=C/C(N)=O BSSNZUFKXJJCBG-UPHRSURJSA-N 0.000 description 1
- PQUXFUBNSYCQAL-UHFFFAOYSA-N 1-(2,3-difluorophenyl)ethanone Chemical compound CC(=O)C1=CC=CC(F)=C1F PQUXFUBNSYCQAL-UHFFFAOYSA-N 0.000 description 1
- JNPCNDJVEUEFBO-UHFFFAOYSA-N 1-butylpyrrole-2,5-dione Chemical compound CCCCN1C(=O)C=CC1=O JNPCNDJVEUEFBO-UHFFFAOYSA-N 0.000 description 1
- HIDBROSJWZYGSZ-UHFFFAOYSA-N 1-phenylpyrrole-2,5-dione Chemical compound O=C1C=CC(=O)N1C1=CC=CC=C1 HIDBROSJWZYGSZ-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
- NIXOWILDQLNWCW-UHFFFAOYSA-N 2-Propenoic acid Natural products OC(=O)C=C NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 1
- VAPQAGMSICPBKJ-UHFFFAOYSA-N 2-nitroacridine Chemical compound C1=CC=CC2=CC3=CC([N+](=O)[O-])=CC=C3N=C21 VAPQAGMSICPBKJ-UHFFFAOYSA-N 0.000 description 1
- VGUWZCUCNQXGBU-UHFFFAOYSA-N 3-[(4-methylpiperazin-1-yl)methyl]-5-nitro-1h-indole Chemical compound C1CN(C)CCN1CC1=CNC2=CC=C([N+]([O-])=O)C=C12 VGUWZCUCNQXGBU-UHFFFAOYSA-N 0.000 description 1
- AYKYXWQEBUNJCN-UHFFFAOYSA-N 3-methylfuran-2,5-dione Chemical compound CC1=CC(=O)OC1=O AYKYXWQEBUNJCN-UHFFFAOYSA-N 0.000 description 1
- OFNISBHGPNMTMS-UHFFFAOYSA-N 3-methylideneoxolane-2,5-dione Chemical compound C=C1CC(=O)OC1=O OFNISBHGPNMTMS-UHFFFAOYSA-N 0.000 description 1
- OIYTYGOUZOARSH-UHFFFAOYSA-N 4-methoxy-2-methylidene-4-oxobutanoic acid Chemical compound COC(=O)CC(=C)C(O)=O OIYTYGOUZOARSH-UHFFFAOYSA-N 0.000 description 1
- HRPVXLWXLXDGHG-UHFFFAOYSA-N Acrylamide Chemical compound NC(=O)C=C HRPVXLWXLXDGHG-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- IEPRKVQEAMIZSS-UHFFFAOYSA-N Di-Et ester-Fumaric acid Natural products CCOC(=O)C=CC(=O)OCC IEPRKVQEAMIZSS-UHFFFAOYSA-N 0.000 description 1
- IEPRKVQEAMIZSS-WAYWQWQTSA-N Diethyl maleate Chemical compound CCOC(=O)\C=C/C(=O)OCC IEPRKVQEAMIZSS-WAYWQWQTSA-N 0.000 description 1
- JIGUQPWFLRLWPJ-UHFFFAOYSA-N Ethyl acrylate Chemical compound CCOC(=O)C=C JIGUQPWFLRLWPJ-UHFFFAOYSA-N 0.000 description 1
- XLYMOEINVGRTEX-ARJAWSKDSA-N Ethyl hydrogen fumarate Chemical compound CCOC(=O)\C=C/C(O)=O XLYMOEINVGRTEX-ARJAWSKDSA-N 0.000 description 1
- PEEHTFAAVSWFBL-UHFFFAOYSA-N Maleimide Chemical compound O=C1NC(=O)C=C1 PEEHTFAAVSWFBL-UHFFFAOYSA-N 0.000 description 1
- CERQOIWHTDAKMF-UHFFFAOYSA-M Methacrylate Chemical compound CC(=C)C([O-])=O CERQOIWHTDAKMF-UHFFFAOYSA-M 0.000 description 1
- CERQOIWHTDAKMF-UHFFFAOYSA-N Methacrylic acid Chemical compound CC(=C)C(O)=O CERQOIWHTDAKMF-UHFFFAOYSA-N 0.000 description 1
- VVQNEPGJFQJSBK-UHFFFAOYSA-N Methyl methacrylate Chemical compound COC(=O)C(C)=C VVQNEPGJFQJSBK-UHFFFAOYSA-N 0.000 description 1
- 239000004952 Polyamide Substances 0.000 description 1
- 239000004793 Polystyrene Substances 0.000 description 1
- OFOBLEOULBTSOW-UHFFFAOYSA-N Propanedioic acid Natural products OC(=O)CC(O)=O OFOBLEOULBTSOW-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- 239000002253 acid Substances 0.000 description 1
- 150000008065 acid anhydrides Chemical class 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 150000001408 amides Chemical class 0.000 description 1
- CQEYYJKEWSMYFG-UHFFFAOYSA-N butyl acrylate Chemical compound CCCCOC(=O)C=C CQEYYJKEWSMYFG-UHFFFAOYSA-N 0.000 description 1
- 150000001735 carboxylic acids Chemical class 0.000 description 1
- HNEGQIOMVPPMNR-IHWYPQMZSA-N citraconic acid Chemical compound OC(=O)C(/C)=C\C(O)=O HNEGQIOMVPPMNR-IHWYPQMZSA-N 0.000 description 1
- 229940018557 citraconic acid Drugs 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 238000005034 decoration Methods 0.000 description 1
- LDCRTTXIJACKKU-ONEGZZNKSA-N dimethyl fumarate Chemical compound COC(=O)\C=C\C(=O)OC LDCRTTXIJACKKU-ONEGZZNKSA-N 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 150000002148 esters Chemical class 0.000 description 1
- SUPCQIBBMFXVTL-UHFFFAOYSA-N ethyl 2-methylprop-2-enoate Chemical compound CCOC(=O)C(C)=C SUPCQIBBMFXVTL-UHFFFAOYSA-N 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 239000010408 film Substances 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 239000001530 fumaric acid Substances 0.000 description 1
- XLYMOEINVGRTEX-UHFFFAOYSA-N fumaric acid monoethyl ester Natural products CCOC(=O)C=CC(O)=O XLYMOEINVGRTEX-UHFFFAOYSA-N 0.000 description 1
- NKHAVTQWNUWKEO-UHFFFAOYSA-N fumaric acid monomethyl ester Natural products COC(=O)C=CC(O)=O NKHAVTQWNUWKEO-UHFFFAOYSA-N 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 229920001903 high density polyethylene Polymers 0.000 description 1
- 239000004700 high-density polyethylene Substances 0.000 description 1
- 150000003949 imides Chemical class 0.000 description 1
- 238000009776 industrial production Methods 0.000 description 1
- 239000003999 initiator Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- FSQQTNAZHBEJLS-UPHRSURJSA-N maleamic acid Chemical compound NC(=O)\C=C/C(O)=O FSQQTNAZHBEJLS-UPHRSURJSA-N 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
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- FQPSGWSUVKBHSU-UHFFFAOYSA-N methacrylamide Chemical compound CC(=C)C(N)=O FQPSGWSUVKBHSU-UHFFFAOYSA-N 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
- 239000000203 mixture Substances 0.000 description 1
- NKHAVTQWNUWKEO-NSCUHMNNSA-N monomethyl fumarate Chemical compound COC(=O)\C=C\C(O)=O NKHAVTQWNUWKEO-NSCUHMNNSA-N 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- RPQRDASANLAFCM-UHFFFAOYSA-N oxiran-2-ylmethyl prop-2-enoate Chemical compound C=CC(=O)OCC1CO1 RPQRDASANLAFCM-UHFFFAOYSA-N 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
- 229920002647 polyamide Polymers 0.000 description 1
- 229920000515 polycarbonate Polymers 0.000 description 1
- 239000004417 polycarbonate Substances 0.000 description 1
- 229920002223 polystyrene Polymers 0.000 description 1
- 239000004800 polyvinyl chloride Substances 0.000 description 1
- 229920000915 polyvinyl chloride Polymers 0.000 description 1
- LLLCSBYSPJHDJX-UHFFFAOYSA-M potassium;2-methylprop-2-enoate Chemical compound [K+].CC(=C)C([O-])=O LLLCSBYSPJHDJX-UHFFFAOYSA-M 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 229940047670 sodium acrylate Drugs 0.000 description 1
- SONHXMAHPHADTF-UHFFFAOYSA-M sodium;2-methylprop-2-enoate Chemical compound [Na+].CC(=C)C([O-])=O SONHXMAHPHADTF-UHFFFAOYSA-M 0.000 description 1
- 239000002904 solvent Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 239000010409 thin film Substances 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
- 239000011135 tin Substances 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
Landscapes
- Laminated Bodies (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は熱可塑性樹脂シートと金属シートから成る複合
板の製造方法に関するものであシ、さらに詳しくは熱可
塑性樹脂シートと金属シートとの接着方法の改良に関す
るものである。[Detailed Description of the Invention] [Industrial Application Field] The present invention relates to a method for manufacturing a composite plate consisting of a thermoplastic resin sheet and a metal sheet, and more specifically, to a method for bonding a thermoplastic resin sheet and a metal sheet. It concerns an improvement in the method.
熱可塑性樹脂シートにアルミニウム等の金属箔を積層し
た複合板は建築、家具、装飾用として広く用いられてい
る。そCしてこれらの複合板の樹脂層と金属シートとの
接着性を向上するために、樹脂層に接着成分を混合して
おく方法(特開昭5/−1:、7g9号公報)や、変性
ポリオレフィンを含む接着層を介在させて加圧状態で貼
シ合せる方法(特公昭j; 1f−G(Oe ? /号
公報)等が知られている。Composite boards made by laminating metal foils such as aluminum on thermoplastic resin sheets are widely used for architecture, furniture, and decoration. In order to improve the adhesion between the resin layer and the metal sheet of these composite plates, there is a method of mixing an adhesive component into the resin layer (Japanese Unexamined Patent Publication No. 5/1989, 7g9). , a method of laminating under pressure with an adhesive layer containing a modified polyolefin interposed therebetween (Japanese Patent Publication No. Shoj; 1f-G (Oe?/No. 1), etc. are known.
樹脂層に接着成分を混合する方法は接着成分が充分に有
効活用されないという問題がある。The method of mixing an adhesive component into the resin layer has a problem in that the adhesive component is not fully utilized effectively.
また接着層を介在させる場合は、連続運転においてあら
かじめ金属シート上に接着層を施しておいてロールに巻
きとった状態で保管すると、接着層の性質ないし保管の
温度によっては金属シート相互間で接着するおそnがあ
る。そこで通常は接着層となる樹脂を予め成形された薄
層フィルムとして別に用意し、金属ソートが芯材となる
樹脂層て貼シ合わされる直前にこの接着層を金属シート
にラミネートするという方法が行なわれている。In addition, if an adhesive layer is used, if the adhesive layer is applied on the metal sheets in advance during continuous operation and stored wound up on a roll, the metal sheets may adhere to each other depending on the properties of the adhesive layer or the storage temperature. There is a chance that I will. Therefore, the usual method is to separately prepare the resin that will serve as the adhesive layer as a pre-formed thin film, and then laminate this adhesive layer to the metal sheet just before the metal sort is laminated with the resin layer that will serve as the core material. It is.
本発明は上述のような繁雑な工程なしに、金属ソートラ
熱可塑性樹脂シートに良好な接着性で貼り合わせる方法
に関するものである。すなわち本発明は熱可塑性樹脂シ
ートの両面に金属ソートを積層した複合板を連続的に製
造する方法において、金属シート表面に接着層として不
飽和カルボン酸またはその誘導体で変性したポリオレフ
ィン層ヲ怖し、その上に芯材となる熱可塑性樹脂シート
と同種の樹脂層を施した二層から成るもの企使用するこ
とを特徴とする複合板の製造方法に存する。The present invention relates to a method of bonding a metal sotra thermoplastic resin sheet with good adhesiveness without the complicated steps described above. That is, the present invention provides a method for continuously manufacturing a composite plate in which metal sorts are laminated on both sides of a thermoplastic resin sheet, in which a polyolefin layer modified with an unsaturated carboxylic acid or a derivative thereof is used as an adhesive layer on the surface of the metal sheet. The present invention relates to a method for manufacturing a composite board, which comprises using a two-layer composite board having a thermoplastic resin sheet serving as a core material and a resin layer of the same type applied thereon.
以下、図面を参照しながら本発明の詳細な説明する。第
1図は本発明に従い複合板を連続的に製造する全体工程
側面図の一例を、第2図は金属ソート断面の拡大図の一
例を示す。Hereinafter, the present invention will be described in detail with reference to the drawings. FIG. 1 shows an example of a side view of the entire process of continuously manufacturing a composite plate according to the present invention, and FIG. 2 shows an example of an enlarged view of a metal sorting cross section.
図中の番号は下記の通りである。The numbers in the figure are as follows.
/ 押出機
2、−′ 加熱圧着ロール
3.3′ アンコイラ−
弘 yl引取ロール
5、S′予熱器
6 熱可塑性樹脂シート
7.7′ 接着層の施された金属シートg 複合板
タ 接着層
70 金属シート
接着層の施された金属シー)7.7’の接着層側を相対
向させ、その間に熱可塑性樹脂ソートが介在するように
加熱圧着ロールコ、2′に供給するに用いられるもので
あれば特に制限はなく、例えばポリエチレン、ポリプロ
ピレン、ポリブテン、ポリ塩化ビニール、ポリスチレン
、ポリアミド、ポリカーボネート等が用いられるが、押
出成形性の点からは、ポリエチレン、ポリプロピレン、
ポリブテン等のポリオレフィン系合成樹脂を使用するの
が好ましい。/ Extruder 2, -' Heat pressure bonding roll 3.3' Uncoiler Hiro yl take-up roll 5, S' preheater 6 Thermoplastic resin sheet 7.7' Metal sheet with adhesive layer g Composite plate adhesive layer 70 A metal sheet (7) with a metal sheet adhesive layer applied thereto, with the adhesive layer sides of 7' facing each other and a thermoplastic resin sorting interposed between them, whichever is used to feed the metal sheet to the heat-pressing roll mill, 2'. There is no particular restriction, and examples of examples of materials that can be used include polyethylene, polypropylene, polybutene, polyvinyl chloride, polystyrene, polyamide, polycarbonate, etc. From the viewpoint of extrusion moldability, polyethylene, polypropylene,
It is preferable to use a polyolefin synthetic resin such as polybutene.
目的とする積層板の厚みによって適宜選ばれる条件とも
密接に関連するが、溶融状態または固体状態のいずれか
で圧着工程に供給される。The material is supplied to the compression process in either a molten state or a solid state, although this is closely related to the conditions that are appropriately selected depending on the desired thickness of the laminate.
金属シート/θとしては、アルミニウム、スチール、鉄
、銅、錫又はニッケル或はこれらの合金のシートが用い
られる。金属シート≠の厚みは(7,5an以下であシ
、通常は、o、o5〜0.5団のものが用いられる。As the metal sheet /θ, a sheet of aluminum, steel, iron, copper, tin, nickel, or an alloy thereof is used. The thickness of the metal sheet ≠ should be 7.5 an or less, and usually a metal sheet of o, o5 to 0.5 is used.
接着層は第一図に示されるようにq(a)、9の)の二
層から成る。金属シートIQと接する層?(a)には不
飽和カルボン酸またはその誘導体で変性したポリオレフ
ィンが使用される。具体的には不飽和カルボン酸として
はアクリル酸、メタクリル酸、フマル酸、マレイン酸、
イタコン酸、シトラコン酸等がある。また不飽和カルボ
ン酸の誘導体としては、酸無水物、エステル、アミド、
イミド、金属塩等があり、例えば無水マレイン酸、無水
シトラコン酸、無水イタコン酸、アクリル酸メチル、メ
タクリル酸メチル、アクリル酸エチル、メタクリル酸エ
チル、アクリル酸ブチル、メタクリル酸ブチル、アクリ
ル酸グリシジル、メタクリル酸グリンジル、マレイン酸
モノエチルエステル、マレイン酸ジエチルエステル、フ
マル酸モノメチルエステル、フマル酸ジメチルエステル
、イタコン酸モノメチルエステル、メメコン酸ジエチル
エステル、アクリルアミド、メタクリルアミド、マレイ
ン酸モノアミド、マレイン酸ジアミド、マレイン酸−N
−モノエチルアミド、マレイン酸−NIN−ジエチルア
ミド、マレイン酸−N−モツプチルアミド、マレイン酸
−N、N−ジブチルアミド、フマル酸モノアミド、フマ
ル酸ジアミド、フマル酸−N−モノエチルアミド、フマ
ルe −N、N −ジエチルアミド、フマル酸−N−モ
ツプチルアミド、フマル酸−N、N−ジブチルアミド、
マレイミド、N−ブチルマレイミド、N−フェニルマレ
イミド、アクリル酸ナトリウム、メタクリル酸ナトリウ
ム、アクリル酸カリウム、メタクリル酸カリウム等を挙
げることができる。これらの中では、無水マレイン酸を
使用するのが最も好ましい。The adhesive layer consists of two layers, q(a), 9), as shown in Figure 1. Layer in contact with metal sheet IQ? For (a), a polyolefin modified with an unsaturated carboxylic acid or a derivative thereof is used. Specifically, unsaturated carboxylic acids include acrylic acid, methacrylic acid, fumaric acid, maleic acid,
Itaconic acid, citraconic acid, etc. In addition, unsaturated carboxylic acid derivatives include acid anhydrides, esters, amides,
Imides, metal salts, etc., such as maleic anhydride, citraconic anhydride, itaconic anhydride, methyl acrylate, methyl methacrylate, ethyl acrylate, ethyl methacrylate, butyl acrylate, butyl methacrylate, glycidyl acrylate, and methacrylate. Grindyl acid, maleic acid monoethyl ester, maleic acid diethyl ester, fumaric acid monomethyl ester, fumaric acid dimethyl ester, itaconic acid monomethyl ester, memeconic acid diethyl ester, acrylamide, methacrylamide, maleic acid monoamide, maleic acid diamide, maleic acid N
-Monoethylamide, maleic acid-NIN-diethylamide, maleic acid-N-motuptilamide, maleic acid-N,N-dibutylamide, fumaric acid monoamide, fumaric acid diamide, fumaric acid-N-monoethylamide, fumare-N , N-diethylamide, fumaric acid-N-motuptylamide, fumaric acid-N,N-dibutylamide,
Examples include maleimide, N-butylmaleimide, N-phenylmaleimide, sodium acrylate, sodium methacrylate, potassium acrylate, potassium methacrylate, and the like. Among these, it is most preferred to use maleic anhydride.
上記モノマーをポリオレフィンにグラフトする方法とし
ては、公知の種々の方法を採用することが出来る。例え
ば、ポリオレフィンとグラフトモノマーを溶媒の存在下
または不存在下でラジカル開始剤を添加してまた添加せ
ずに高温で加熱することによって行われる。反応に際し
、スチレンのような他のビニルモノマーを共存させても
よい。ポリオレフィンへのグラフトモノマーのグラフト
される量(以下グラフト率という)は、 10−’な
いし3重量%の範囲にあるよう調製するのが好ましい。Various known methods can be used to graft the monomer onto the polyolefin. For example, it is carried out by heating the polyolefin and the grafting monomer at high temperature in the presence or absence of a solvent with or without the addition of a radical initiator. Other vinyl monomers such as styrene may be present during the reaction. The amount of the graft monomer grafted onto the polyolefin (hereinafter referred to as graft ratio) is preferably adjusted to be in the range of 10-' to 3% by weight.
ポリオレフィンは、一部がグラフトされていても、全体
がグラフトされていてもさしつかえないが、工業的製造
上からは、予めグラフト率10−2ないし6重量%の変
性ポリオレフィンを製造しておき、次に未変性ポリオレ
フィンにこの変性ポリオレフィンを混合することが組成
物中のグラフトモノマーの濃度を適当に調整できるため
、好ましい。The polyolefin may be partially or completely grafted, but from an industrial production point of view, a modified polyolefin with a grafting rate of 10-2 to 6% by weight is produced in advance, and then It is preferable to mix the modified polyolefin with the unmodified polyolefin because the concentration of the graft monomer in the composition can be adjusted appropriately.
接着層の外側となる? (b)としては前記した芯材と
なる熱可塑性樹脂シートbと同種の樹脂を用いることが
できる。Will it be outside the adhesive layer? As (b), the same type of resin as the thermoplastic resin sheet b serving as the core material described above can be used.
なお、芯材となる熱可塑性樹脂シートとしては回収品、
再生品等を全部または部分的に使用することができるが
、上記した外側接着層? (b)としては膜厚制御等が
容易となるように通常バージン品が使用される。また芯
材を高密度ポリエチレンで、外側接着層を低密度ポリエ
チレンで構成するような場合も、本発明の1同種樹脂」
に含まれるものである。In addition, the thermoplastic resin sheet used as the core material is a recycled product,
It is possible to use recycled products in whole or in part, but what about the outer adhesive layer mentioned above? As for (b), a virgin product is usually used so that film thickness can be easily controlled. Also, in cases where the core material is made of high-density polyethylene and the outer adhesive layer is made of low-density polyethylene, the same type of resin according to the present invention may be used.
It is included in
接着層の厚さはq(a)、y(b)あわせて通常5〜1
00μm程度であることが好ましい。The thickness of the adhesive layer is usually 5 to 1 in total for q(a) and y(b).
The thickness is preferably about 00 μm.
薄すぎると金属シートへの均一な塗布施工がむずかしく
、接着強度が低下する原因となる。If it is too thin, it will be difficult to apply it uniformly to the metal sheet, leading to a decrease in adhesive strength.
一方、厚すぎる場合は接着強度の点では特に問題はない
が得られる複合板の表面平滑性が悪くなる。従って接着
強度が充分に保持される限シ接着層はできるだけ薄い方
が有利であるので、好ましくは/ 0−40μmの範囲
から選択される。また二層のうち9G)を薄くする方が
経済的に有利であり ?i好ましくは9(a)が7〜3
08m、9ら)が5−iooμmの範囲から選ばれる。On the other hand, if it is too thick, there will be no particular problem in terms of adhesive strength, but the surface smoothness of the resulting composite plate will deteriorate. Therefore, it is advantageous for the adhesive layer to be as thin as possible in order to maintain sufficient adhesive strength, so it is preferably selected from a range of 0 to 40 μm. Also, is it economically advantageous to make 9G of the two layers thinner? i Preferably 9(a) is 7-3
08m, 9 et al.) are selected from the range of 5-ioom.
金属ソートに二層から構成される接着層を捲すには、常
法て従って別々に、または同時にラミネートする方法が
好適である。In order to apply the two-layer adhesive layer to the metal sort, it is preferable to use the conventional method of laminating them separately or simultaneously.
二層の接着層が施された金属シー)7.7’と熱可塑性
樹脂シート6とを接着するためには、該熱可塑性樹脂シ
ートが固体状で圧着ロールに供給される場合は少なくと
も接着層デの一部、たとえば9卸をその溶融温度以上に
予熱器よ、3′で加分な温度に加熱される。通常は/2
0〜300℃程度である。一方、熱可塑性樹脂シートが
溶融状態で圧着ロールに供給される場合は、金属シート
に捲された接着層は必ずしも溶融している必要はない。In order to bond the thermoplastic resin sheet 6 to the metal sheet (7.7') provided with two adhesive layers, at least an adhesive layer is required when the thermoplastic resin sheet is supplied to the pressure roll in a solid state. A portion of the glass, say 9, is heated to an additional temperature above its melting temperature in the preheater, 3'. Usually /2
The temperature is about 0 to 300°C. On the other hand, when the thermoplastic resin sheet is supplied to the pressure roll in a molten state, the adhesive layer wound around the metal sheet does not necessarily need to be molten.
予熱された接着層?(a)、?(b)が積層された金属
シー)7,7’は熱可塑性樹脂シート6と共に加熱圧着
ローラーλ1,2′間に供給され貼合せが行なわれる。Preheated adhesive layer? (a),? The metal sheets 7, 7' on which (b) is laminated are supplied together with the thermoplastic resin sheet 6 between hot pressure bonding rollers λ1, 2' to perform lamination.
加熱圧着ローラーの温度は芯材となる熱可塑性樹脂の種
類や予熱器5.S′の運転条件によっても左右されるが
、通常は100−2!0°C1好ましくは720〜20
0℃の範囲から選択される。加熱圧着ローラは、駆動ロ
ーラでもよく、駆動力のないフリーローラでもよい。The temperature of the hot pressure roller depends on the type of thermoplastic resin used as the core material and the preheater5. Although it depends on the operating conditions of S', it is usually 100-2!0°C1, preferably 720-20°C.
Selected from the range of 0°C. The heat-pressing roller may be a driven roller or a free roller without driving force.
一方、該熱可塑性樹脂シートが溶融状態で供給される場
合は、押出機から押出された樹脂の温度と金属シートの
温度の差が大きいと、貼合せ時に金属ソートにシワが発
生しゃすい。とのシワ発生防止を目的として金属シート
の加熱が必要となる。従って加熱圧着ローラーはis。On the other hand, when the thermoplastic resin sheet is supplied in a molten state, if there is a large difference in temperature between the resin extruded from the extruder and the metal sheet, wrinkles are likely to occur in the metal sort during lamination. It is necessary to heat the metal sheet to prevent wrinkles from forming. Therefore, the heated pressure roller is.
〜200℃に加熱され金属シートもigo〜、2.2G
°Cに予熱されることが好ましい。The metal sheet heated to ~200°C is also igo~, 2.2G
Preferably it is preheated to °C.
金属シー) 7.7’はアンコイラ−3,3′から引取
ローラーu、g’によって一定張力の展張状態で弓き出
される。金属シート7.7′にががる張力は引取ロール
<<、tI’の駆動力、加熱圧着ローラコ、−一の駆動
力、アンコイラ−3,3′の制動力等の調節によって任
意に変えることができ、通常は0.2〜10kQ/−の
範囲の一定値に制御される。The metal sheet (7.7') is pulled out from the uncoilers 3, 3' by take-up rollers u, g' under constant tension. The tension at which the metal sheet 7, 7' is bent can be arbitrarily changed by adjusting the driving force of the take-up roll <<, tI', the driving force of the heat-pressing roller -1, the braking force of the uncoilers 3 and 3', etc. is normally controlled to a constant value in the range of 0.2 to 10 kQ/-.
加熱圧着ローラーから送シ出された複合板は必要に応じ
て冷却ロールや千鳥状に配置されたローラーを経て平面
形状が矯正される。The composite plate sent out from the heat-pressing roller is corrected in planar shape by passing through a cooling roll or staggered rollers as necessary.
本発明によると連続的に複合板を製造する工程において
、金属シートと接着層を別々に用意しておくことなく、
接着層付金属シートを一対のアンコイラ−に巻きとって
おき、これを原料として連続的に複合板を製造すること
ができる。According to the present invention, in the process of continuously manufacturing composite plates, there is no need to separately prepare the metal sheet and the adhesive layer.
A metal sheet with an adhesive layer is wound around a pair of uncoilers, and a composite plate can be continuously manufactured using this as a raw material.
しかも金属ソートと合成樹脂シートとの接着性も優れた
ものである。Moreover, the adhesion between the metal sort and the synthetic resin sheet is also excellent.
次に実施例によシ本発明を更に詳細に説明するが、本発
明はその要旨を超えない限シ以下の実施例に限定される
ものではない。Next, the present invention will be explained in more detail with reference to examples, but the present invention is not limited to the following examples as long as the gist thereof is not exceeded.
実施例/
第1図に示される装置において押出機/から樹脂温22
0℃で連続的に押出された低密度ポリエチレンを三本ロ
ール(図示せず)を通して厚さへg閣、幅10100O
のポリエチレンシートを得た。その後自然放冷し固体状
シートとしてから加熱圧着ローラ−,2,,2’へ供給
した。Example/In the apparatus shown in FIG. 1, the resin temperature from the extruder/
Low-density polyethylene continuously extruded at 0°C is passed through three rolls (not shown) to a thickness of 10,100 mm in width.
A polyethylene sheet was obtained. Thereafter, it was allowed to cool naturally to form a solid sheet, which was then supplied to heated pressure rollers 2, 2'.
一方、第2図に示される断面を有する接着層の捲された
アルミニウムシートをアンコイラ−3,3′から供給し
た。アルミニウムシートlθとしては表面平滑処理した
厚さθ、/as、幅1000醪のものを使用した。また
接着層q (a)としては無水マレイン酸をs o o
ppmクラフトして変性した低密度ポリエチレン(厚
さ10μm)、7(b)として芯材のシート6と同種の
低密度ポリエチレン(厚さ10μm)を用いた。この接
着層の施されたアルミニウムシー)7.7’を予熱器S
、5′で加熱し、接着層側を/(10℃の溶融状態に、
金属側を733°Cとして加熱圧着ローラーに供給した
。On the other hand, an aluminum sheet wrapped with an adhesive layer and having a cross section shown in FIG. 2 was fed from uncoilers 3 and 3'. As the aluminum sheet lθ, a surface-smoothed one having a thickness θ, /as and a width of 1000 mm was used. In addition, maleic anhydride is used as the adhesive layer q (a).
Low-density polyethylene (thickness: 10 μm) modified by ppm crafting and low-density polyethylene (thickness: 10 μm) of the same type as the core sheet 6 was used as 7(b). This adhesive layered aluminum sheet) 7.7' is attached to the preheater S.
, 5' to bring the adhesive layer side to a melted state of /(10℃,
The metal side was heated to 733°C and fed to a heated pressure bonding roller.
引取ロールp4’の駆動力とアンコイラ−3,3′の制
動力を制御し、加熱圧着ローラーには駆動力を与えずそ
の間隙を約ハフ鴫に保持した。これによシアルミニウム
シートにa、t2kg/−の張力を付与した。The driving force of the take-up roll p4' and the braking force of the uncoilers 3, 3' were controlled, and no driving force was applied to the hot pressure bonding roller, and the gap therebetween was maintained at about a huff. As a result, a tension of 2 kg/- was applied to the sialuminium sheet.
得られた複合板は厚さコ、Owxであシ、表面平滑性良
好でその接着強度はt、rkq/インチであった0
実施例コ
押出機lから連続的に押出された低密度ポリエチレンを
、溶融状態のまま加熱圧着ローラーコ、2′へ供給した
。加熱圧着ローラーの温度はコ10℃とした。The obtained composite plate had a thickness of 0.05 mm, had a good surface smoothness, and had an adhesive strength of t, rkq/inch. , and was supplied in a molten state to a heat-pressing roller roller 2'. The temperature of the hot press roller was set to 10°C.
一方、第2図に示される断面全有する接着層の施された
アルミニウムシートをアンコイラ−3,3′から供給し
た。アルミニウムシートトシテは厚さ0.19m、巾1
000wmのものを使用した。On the other hand, an aluminum sheet coated with an adhesive layer and having the entire cross section shown in FIG. 2 was supplied from uncoilers 3 and 3'. Aluminum sheet toshite is 0.19m thick and 1 wide.
000 wm was used.
また、接1着層?(a)としては無水マレイン酸を約/
000 ppmグラフトして変性した低密度ポリエチ
レン(厚さ5μm)%?(b)として芯材シート6と同
種の低密度ポリエチレン(厚さ758m)を用いた。こ
の接着層の施されたアルミニウムシート7.7′を予熱
器夕、5′でコア0°Cまで加熱し、接着層を溶融状態
とし加熱圧着ローラーコ、2′に供給した。加熱ローラ
ーの間隙を約2.9咽に保持し、溶融樹脂だまり(バン
ク)を形成った。Also, the adhesive layer? As (a), maleic anhydride is about /
000 ppm grafted and modified low density polyethylene (thickness 5 μm)%? As (b), the same type of low-density polyethylene as the core sheet 6 (thickness: 758 m) was used. The aluminum sheets 7 and 7' provided with the adhesive layer were heated to a core temperature of 0° C. in a preheater 5' to melt the adhesive layer and supplied to the hot press roller 2'. The gap between the heating rollers was maintained at approximately 2.9 mm to form a bank of molten resin.
第1図は本発明方法に使用される装置の一例を示す概念
的側面図であシ、第2図は二層の接着層が怖された金属
シート7.’)’の断面図を示す。FIG. 1 is a conceptual side view showing an example of the apparatus used in the method of the present invention, and FIG. 2 shows a metal sheet 7 with two adhesive layers. A cross-sectional view of ')' is shown.
Claims (1)
た複合板を連続的に製造する方法において、金層シート
表面に接着層として不飽和カルボン酸またはその誘導体
で変性したポリオレフィン層を施し、その上に芯材とな
る熱可塑性樹脂シートと同種の樹脂層を施した二層から
成るものを使用することを特徴とする複合板の製造方法
。(1) In a method for continuously manufacturing a composite plate in which metal sheets are laminated on both sides of a thermoplastic resin sheet, a polyolefin layer modified with an unsaturated carboxylic acid or a derivative thereof is applied as an adhesive layer on the surface of the gold layer sheet. A method for manufacturing a composite board characterized by using a two-layer composite board having a thermoplastic resin sheet serving as a core material and a resin layer of the same type applied thereon.
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP21595488A JP2557489B2 (en) | 1988-08-30 | 1988-08-30 | Manufacturing method of composite board |
US07/394,814 US4994130A (en) | 1988-08-30 | 1989-08-17 | Method for producing a composite laminate |
EP89115273A EP0356837B1 (en) | 1988-08-30 | 1989-08-18 | Method for producing a composite laminate |
DE68926006T DE68926006T2 (en) | 1988-08-30 | 1989-08-18 | Method of making a composite panel |
CA000609523A CA1298769C (en) | 1988-08-30 | 1989-08-28 | Method for producing a composite laminate |
KR1019890012424A KR960007006B1 (en) | 1988-08-30 | 1989-08-30 | Method for producing a composite laminate |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP21595488A JP2557489B2 (en) | 1988-08-30 | 1988-08-30 | Manufacturing method of composite board |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH0263735A true JPH0263735A (en) | 1990-03-05 |
JP2557489B2 JP2557489B2 (en) | 1996-11-27 |
Family
ID=16680998
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP21595488A Expired - Lifetime JP2557489B2 (en) | 1988-08-30 | 1988-08-30 | Manufacturing method of composite board |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2557489B2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR100375665B1 (en) * | 2000-12-19 | 2003-03-15 | 삼성종합화학주식회사 | Flame retardent polyolefine resine composition and method for manufacturing aluminum composite panel using thereof |
-
1988
- 1988-08-30 JP JP21595488A patent/JP2557489B2/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR100375665B1 (en) * | 2000-12-19 | 2003-03-15 | 삼성종합화학주식회사 | Flame retardent polyolefine resine composition and method for manufacturing aluminum composite panel using thereof |
Also Published As
Publication number | Publication date |
---|---|
JP2557489B2 (en) | 1996-11-27 |
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