JPH0373578B2 - - Google Patents
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- Publication number
- JPH0373578B2 JPH0373578B2 JP12397583A JP12397583A JPH0373578B2 JP H0373578 B2 JPH0373578 B2 JP H0373578B2 JP 12397583 A JP12397583 A JP 12397583A JP 12397583 A JP12397583 A JP 12397583A JP H0373578 B2 JPH0373578 B2 JP H0373578B2
- Authority
- JP
- Japan
- Prior art keywords
- curing
- molded product
- temperature
- epoxy resin
- molded
- 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.)
- Expired
Links
- 238000001723 curing Methods 0.000 claims description 47
- 239000003822 epoxy resin Substances 0.000 claims description 36
- 229920000647 polyepoxide Polymers 0.000 claims description 36
- 238000000034 method Methods 0.000 claims description 18
- 238000006243 chemical reaction Methods 0.000 claims description 16
- 239000007790 solid phase Substances 0.000 claims description 9
- 239000000463 material Substances 0.000 claims description 7
- 238000010438 heat treatment Methods 0.000 claims description 5
- 238000013007 heat curing Methods 0.000 claims description 4
- 230000009477 glass transition Effects 0.000 claims description 3
- 238000004132 cross linking Methods 0.000 description 9
- 229920005989 resin Polymers 0.000 description 9
- 239000011347 resin Substances 0.000 description 9
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 7
- 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 7
- 239000012744 reinforcing agent Substances 0.000 description 6
- 239000004593 Epoxy Substances 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 4
- 239000003795 chemical substances by application Substances 0.000 description 4
- 238000000465 moulding Methods 0.000 description 4
- 239000000945 filler Substances 0.000 description 3
- 238000002347 injection Methods 0.000 description 3
- 239000007924 injection Substances 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 239000004014 plasticizer Substances 0.000 description 3
- 239000000377 silicon dioxide Substances 0.000 description 3
- 239000007787 solid Substances 0.000 description 3
- 238000001721 transfer moulding Methods 0.000 description 3
- VTYYLEPIZMXCLO-UHFFFAOYSA-L Calcium carbonate Chemical compound [Ca+2].[O-]C([O-])=O VTYYLEPIZMXCLO-UHFFFAOYSA-L 0.000 description 2
- QUSNBJAOOMFDIB-UHFFFAOYSA-N Ethylamine Chemical compound CCN QUSNBJAOOMFDIB-UHFFFAOYSA-N 0.000 description 2
- ADCOVFLJGNWWNZ-UHFFFAOYSA-N antimony trioxide Chemical compound O=[Sb]O[Sb]=O ADCOVFLJGNWWNZ-UHFFFAOYSA-N 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 238000013329 compounding Methods 0.000 description 2
- 239000003085 diluting agent Substances 0.000 description 2
- ZZTCPWRAHWXWCH-UHFFFAOYSA-N diphenylmethanediamine Chemical compound C=1C=CC=CC=1C(N)(N)C1=CC=CC=C1 ZZTCPWRAHWXWCH-UHFFFAOYSA-N 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 239000003063 flame retardant Substances 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- 239000003365 glass fiber Substances 0.000 description 2
- 238000001746 injection moulding Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- -1 phenoxy Modified epoxy resins Chemical class 0.000 description 2
- 239000000049 pigment Substances 0.000 description 2
- 239000000843 powder Substances 0.000 description 2
- 229920001187 thermosetting polymer Polymers 0.000 description 2
- IHLWCCXTLOKDTO-UHFFFAOYSA-N 2,6-dioxabicyclo[3.1.0]hexa-1(5),3-diene Chemical compound C1=COC2=C1O2 IHLWCCXTLOKDTO-UHFFFAOYSA-N 0.000 description 1
- YSUQLAYJZDEMOT-UHFFFAOYSA-N 2-(butoxymethyl)oxirane Chemical compound CCCCOCC1CO1 YSUQLAYJZDEMOT-UHFFFAOYSA-N 0.000 description 1
- NACPTFCBIGBTSJ-UHFFFAOYSA-N 2-hydroxy-2-phenyl-1-(2-propan-2-ylphenyl)ethanone Chemical compound CC(C)C1=CC=CC=C1C(=O)C(O)C1=CC=CC=C1 NACPTFCBIGBTSJ-UHFFFAOYSA-N 0.000 description 1
- 229930185605 Bisphenol Natural products 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- BVKZGUZCCUSVTD-UHFFFAOYSA-L Carbonate Chemical compound [O-]C([O-])=O BVKZGUZCCUSVTD-UHFFFAOYSA-L 0.000 description 1
- MQIUGAXCHLFZKX-UHFFFAOYSA-N Di-n-octyl phthalate Natural products CCCCCCCCOC(=O)C1=CC=CC=C1C(=O)OCCCCCCCC MQIUGAXCHLFZKX-UHFFFAOYSA-N 0.000 description 1
- 239000004677 Nylon Substances 0.000 description 1
- CTQNGGLPUBDAKN-UHFFFAOYSA-N O-Xylene Chemical compound CC1=CC=CC=C1C CTQNGGLPUBDAKN-UHFFFAOYSA-N 0.000 description 1
- 229920001665 Poly-4-vinylphenol Polymers 0.000 description 1
- YSMRWXYRXBRSND-UHFFFAOYSA-N TOTP Chemical compound CC1=CC=CC=C1OP(=O)(OC=1C(=CC=CC=1)C)OC1=CC=CC=C1C YSMRWXYRXBRSND-UHFFFAOYSA-N 0.000 description 1
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 1
- 150000008065 acid anhydrides Chemical class 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 150000001298 alcohols Chemical class 0.000 description 1
- 125000002723 alicyclic group Chemical group 0.000 description 1
- WNROFYMDJYEPJX-UHFFFAOYSA-K aluminium hydroxide Chemical compound [OH-].[OH-].[OH-].[Al+3] WNROFYMDJYEPJX-UHFFFAOYSA-K 0.000 description 1
- 150000001412 amines Chemical class 0.000 description 1
- 239000004760 aramid Substances 0.000 description 1
- 229920006231 aramid fiber Polymers 0.000 description 1
- 239000010425 asbestos Substances 0.000 description 1
- BJQHLKABXJIVAM-UHFFFAOYSA-N bis(2-ethylhexyl) phthalate Chemical compound CCCCC(CC)COC(=O)C1=CC=CC=C1C(=O)OCC(CC)CCCC BJQHLKABXJIVAM-UHFFFAOYSA-N 0.000 description 1
- 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 1
- 238000000071 blow moulding Methods 0.000 description 1
- 238000009835 boiling Methods 0.000 description 1
- 229910000019 calcium carbonate Inorganic materials 0.000 description 1
- 239000006229 carbon black Substances 0.000 description 1
- 239000004927 clay Substances 0.000 description 1
- 229910052570 clay Inorganic materials 0.000 description 1
- 230000000052 comparative effect Effects 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 229920001971 elastomer Polymers 0.000 description 1
- 238000010894 electron beam technology Methods 0.000 description 1
- 150000002148 esters Chemical class 0.000 description 1
- RTZKZFJDLAIYFH-UHFFFAOYSA-N ether Substances CCOCC RTZKZFJDLAIYFH-UHFFFAOYSA-N 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 239000007849 furan resin Substances 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- WJRBRSLFGCUECM-UHFFFAOYSA-N hydantoin Chemical compound O=C1CNC(=O)N1 WJRBRSLFGCUECM-UHFFFAOYSA-N 0.000 description 1
- 229940091173 hydantoin Drugs 0.000 description 1
- 150000002460 imidazoles Chemical class 0.000 description 1
- 239000003999 initiator Substances 0.000 description 1
- 239000012784 inorganic fiber Substances 0.000 description 1
- 239000012948 isocyanate Substances 0.000 description 1
- 150000002513 isocyanates Chemical class 0.000 description 1
- 238000004898 kneading Methods 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 239000010445 mica Substances 0.000 description 1
- 229910052618 mica group Inorganic materials 0.000 description 1
- 229920003986 novolac Polymers 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 150000001451 organic peroxides Chemical class 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- 239000012188 paraffin wax Substances 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 150000002989 phenols Chemical class 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 239000004033 plastic Substances 0.000 description 1
- 229920003023 plastic Polymers 0.000 description 1
- 229920000728 polyester Polymers 0.000 description 1
- 229920000642 polymer Polymers 0.000 description 1
- 229920001296 polysiloxane Polymers 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 239000012763 reinforcing filler Substances 0.000 description 1
- 229910052895 riebeckite Inorganic materials 0.000 description 1
- 239000005060 rubber Substances 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 239000004576 sand Substances 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
- 239000000454 talc Substances 0.000 description 1
- 229910052623 talc Inorganic materials 0.000 description 1
- 229920001169 thermoplastic Polymers 0.000 description 1
- 229920002803 thermoplastic polyurethane Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 0.000 description 1
- 235000010215 titanium dioxide Nutrition 0.000 description 1
- 239000008096 xylene Substances 0.000 description 1
Landscapes
- Processes Of Treating Macromolecular Substances (AREA)
Description
本発明はエポキシ系樹脂固化成形物の固相硬化
方法に関する。
従来、エポキシ樹脂の硬化法は、その樹脂の融
点以上の温度で架橋硬化させる方法が一般に採用
されている。即ち、ある型に賦形する為には溶融
状態である必要があり、またできるだけ速く架橋
硬化させる為にも高温即ち溶融状態で硬化させる
のが通例である。また、ある程度架橋反応が進行
し、もはや溶融状態を示さなくなつた場合には、
所謂アフターキユアによつて固相状態で硬化させ
ることも知られている。
しかし、このような硬化方法では(1)融点以上
(液相)で硬化させるので、例えば注形、トラン
スフアー成形、射出成形などの場合には架橋が進
行して固相状態になるまで脱型することができな
い。そして通常この脱型までの時間は10分〜24時
間にも及び多大の時間を要し、型の利用効率が極
めて悪い。(2)この点より急速に高温で硬化させる
方法もあるが、この場合には硬化反応が不均一と
なり、成形物に内部歪を残したり、硬化物が脆く
なつてしまうという欠点がある。
本発明の目的は極めて短時間で脱型することが
可能な工業的に有利なエポキシ系樹脂成形物の硬
化方法を提供することにある。
また本発明の目的は均一な硬化反応により内部
歪を生ずることなく、優れた強度の成形物を製造
することのできるエポキシ系樹脂成形物の硬化方
法を提供することにある。
更に本発明の目的は硬化収縮が非常に小さい成
形物を付与するエポキシ系樹脂成形物の硬化方法
を提供することにある。
本発明はガラス転移温度(Tg)が40〜200℃の
架橋硬化可能なエポキシ系樹脂固化成形物を脱型
後、その成形物のTgより20℃を越えない雰囲気
温度で加熱硬化を行い、硬化の進行と共に上昇す
る該成形物のTgに対応して、該雰囲気温度を該
成形物のTgより20℃を越えない範囲に保持しつ
つ上昇させて硬化反応を完了させることを特徴と
するエポキシ系樹脂固化成形物の固相硬化方法に
係る。
又、本発明は上記雰囲気温度を該成形物のTg
より20℃を越えない範囲に保持しつつ上昇させて
硬化反応を進行させ、上記成形物のTgが、その
硬化の完了により到達し得るTgとその初期のTg
との差の少なくとも60%以上、上昇した後は、雰
囲気温度をTgより20℃を越える範囲にして硬化
させることを特徴とするエポキシ系樹脂固化成形
物の固相硬化方法に係る。
尚、本発明に於けるTgはTMAペネトレーシ
ヨン法で、試料を昇温法により加熱する方法によ
り測定した。
ここで言うエポキシ系樹脂の固化成形物とは、
架橋反応が実質上ほとんど進行しておらず、通常
の成形物の所謂アフターキユア温度(この成形物
が最終的に到達するTg前後の温度が一般に用い
られている)に一気にさらされることによつて、
完全に変形してしまうようなものであり、従来の
アフターキユア前の硬化成形物とは全く異なるも
のである。固化成形物の架橋反応が実質上進行し
ていないことの目安として、常温下で成形物の表
面をアセトンで濡らし、指先で擦つた場合、ベタ
つきが観察される。従来のアフターキユア前の硬
化成形物では架橋反応が大部分進行しており、こ
の程度のアセトンでベタつくようなことは無い。
本発明では固相状態で硬化させるため、型内で
形状を保持しておく必要がなく、型の利用効率が
極めて高く、また特定の雰囲気温度で硬化反応を
均一に行わせることができるため硬化物の物性が
優れ、特に硬化収縮が従来法に比べ非常に小さい
という予期しなかつた効果が得られる。
本発明で用いられるエポキシ系樹脂としては、
例えばビスフエノール型エポキシ樹脂、ノボラツ
ク型エポキシ樹脂、ハロゲン化エポキシ樹脂、水
添化エポキシ樹脂、脂環族エポキシ樹脂又はヒダ
ントイン系エポキシ樹脂の他に、シリコンエポキ
シ樹脂、エポキシフラン樹脂、エポキシエステル
樹脂、フエノキシ樹脂、エポキシウレタン樹脂或
は液状ゴムの末端基をエポキシ変性したような変
性エポキシ樹脂或いはポリビニルフエノールのよ
うなフエノール類をエポキシ樹脂で硬化させたよ
うな系の樹脂も用いることができる。
これらのエポキシ系樹脂用配合剤として用いら
れるものとしては、公知の補強剤、硬化剤、充填
剤、可塑剤、希釈剤、難燃剤、光重合開始剤、顔
料等が挙げられる。もちろん、上記エポキシ系樹
脂と相溶性のある他の公知の熱可塑性又は熱硬化
性樹脂をブレンドすることもできる。
具体的には、硬化剤としてはアミン類、酸無水
物、イミダゾール類、有機過酸化物等の他、ポリ
マー構造によつてはアルコール類、イソシアネー
ト類等も用いることができる。
補強剤としては、ガラス繊維、炭酸繊維、アス
ベスト等の無機繊維やアラミド繊維、ナイロン、
ポリエステル等の有機繊維のような繊維状補強剤
の他に、酸化アルミ、炭化珪素、グラフアイトの
ようなホイスカーも用いることができる。
その他の配合剤としては、ガラスフレーク、ガ
ラス粉、マイカ、カーボンブラツク、タルク、ク
レー、シリカ、炭酸カルシウム、水酸化アルミニ
ウム、チタン白のような充填剤や顔料、或いはジ
オクチルフタレートやトリクレジルホスフエート
のような可塑剤、ブチルグリシジルエーテル、キ
シレンのような反応性又は非反応性希釈剤、三酸
化アンチモンと塩素化パラフインのような難燃
剤、イソプロピルベンゾインエーテルのような光
重合開始剤等を適宜選択して用いることができ
る。
本発明では上記のようなエポキシ系樹脂配合組
成物を適当な方法で成形して、Tgが40〜200℃の
架橋硬化可能な固化成形物を得る。上記のような
Tgを有する固化成形物を得る具体的な方法とし
ては例えば、
(1) 使用するエポキシ系樹脂自体のTgが約35〜
195℃の範囲のものを選択する。これはエポキ
シ系樹脂に補強剤や充填剤類を混合すると、一
般にTgが上昇する傾向を示すからである。
(2) 使用するエポキシ系樹脂自体のTgが195℃以
上のものを用いる場合には、低いTgを有する
他のエポキシ系樹脂を併用するか、又はTgを
低下させる性質を有する配合剤、例えば熱可塑
性樹脂や可塑剤などを併用することにより200
℃以下に調整しても良い。
(3) Tgが35℃未満のエポキシ系樹脂を使用する
必要がある場合には、Tgの高い他のエポキシ
系樹脂又はその他の熱硬化性樹脂を併用する
か、又はTgを上昇させる補強剤や充填剤、例
えば繊維状補強剤の配合量を増量する等の方法
により、Tgを40〜200℃の範囲に調整しても良
い。
本発明ではTgを上記40〜200℃の範囲にするこ
とにより、硬化時の雰囲気温度を高くして固相で
の硬化時間を短縮することができ、また混練中に
硬化反応が進み過ぎるということを防止すること
ができる。またTgが高すぎることによる硬化温
度の上昇に基因する、エポキシ樹脂の分解が抑制
され、成形温度の許容範囲が広くなる。
本発明では上記Tgを有する固化成形物を脱型
後、その成形物のTgより20℃を越えない雰囲気
温度で加熱硬化を行い、硬化の進行と共に上昇す
る該成形物のTgに対応して、該雰囲気温度を該
成形物のTgより20℃を越えない範囲に保持しつ
つ上昇させて硬化反応を完了させる。雰囲気温度
の上昇方法は、成形物のTgの上昇に追従して連
続的に上昇させても良く、また段階的に上昇させ
ても良い。好ましい雰囲気温度は成形物のTg付
近、もしくはTgより約15℃低い温度範囲であり、
且つその上限はTgより20℃高い温度である。し
かし、常にこの範囲にコントロールすることは一
般に難しく、場合によつては一時的にこの範囲を
逸脱することは差し支えない。架橋反応が実質上
進行していない状態のエポキシ系樹脂の固化成形
物(以下未硬化成形物という)は、その成形物が
もつTg以上の雰囲気温度にさらされると変形す
る。しかし、エポキシ系樹脂は、ふつう分子量に
幅をもつており、ここでいう未硬化成形物のTg
は樹脂全体の平均的なTgを測定していることに
なる。従つて、雰囲気温度がTgより高くなつた
としても、直ちに変形を起こすのではなく、実用
上Tgより20℃を越えない範囲であれば変形しな
い為に、この範囲に限定した。
本発明の好ましい態様として、成形物のTgが、
その硬化の完了により到達し得るTgとその初期
のTgとの差の少なくとも60%以上、上昇した後
は該成形物はもはや溶融したり変形したりする危
険性が無くなるため、その後は雰囲気温度をTg
より20℃を越える範囲とすることができ、これに
より寸法変化等を伴わず固相状態で架橋反応を一
層促進することができる。
本発明においては上記固相硬化方法を効果的に
実施するため、固化成形物の初期のTg上昇速度
が約0.01〜10℃/分の範囲であることが望まし
い。
ここで言う固化成形物の初期のTg上昇速度と
は、実質上熱履歴を受けていない固化成形物の
Tgと同じ雰囲気温度に該固化成形物をさらした
ときに、該固化成形物の時間0におけるTg上昇
速度である。
具体的には固化成形物の初期のTg0を予め測定
し、このTg0と同じ雰囲気温度に固化成形物をさ
らし、Tgの変化を追跡し、Tg上昇曲線の時間0
における傾きから求められる。
前記初期のTg上昇速度の範囲では架橋反応の
進行が速く比較的短時間内で硬化を完了すること
が可能で且つ得られる成形物に内部歪が生じた
り、収縮や反りが発生することがなく好ましい。
一方、雰囲気温度の調整は該固化成形物の初期の
Tg上昇速度の約0.2〜5倍、好ましくは約0.5〜2
倍の範囲の速度で上昇させることにより容易に達
成できる。
本発明において成形方法としては公知の各種の
成形方法を用いることができ、例えば注型方法は
勿論、射出成形法、トランスフアー成形法、押出
成形法、ブロー成形法、常圧注入法等を例示でき
る。また本発明の固相硬化のための熱源として
は、加熱気体(例えば空気)の他に、液体(例え
ば高沸点油のような熱媒)、粉粒体(例えば砂)
などを挙げることができる。また電子線照射やマ
イクロ波照射などを使用することもできる。
以下に実施例を挙げて詳しく説明する。なお単
に部とあるのは重量部を示す。尚、以下Tgは理
学電機(株)製の示差走査熱量計で測定した。
実施例 1
エポキシ樹脂〔予備縮合物、数平均分子量
(Mn)5200、エポキシ当量(EE)1400〕100部、
シリカ(350メツシユ)50部及びBF3モノエチル
アミン錯塩0.7部を混合しペレツト化したものを
金型温度65℃で射出成形し、成形品のTgを測定
したところ71℃であつた。雰囲気温度71℃での初
期のTg上昇速度は0.21℃/分であつた為、この
成形物を65℃から150℃まで0.5℃/分の速度で直
線的に上昇させたところ、変形すること無く硬化
させることができた。硬化後のTgは144℃であつ
た。尚、第1図に雰囲気温度と成形品のTgとの
時間的経過の関係を示す。図により雰囲気温度が
Tg+20℃を越えていないことがわかる。
比較例 1
実施例1で成形した成形品を雰囲気温度を65℃
から150℃まで1.5℃/分の速度で直線的に上昇さ
せたところ、上昇開始後20分間で顕著な変形が見
られ、150℃まで上昇させた後の成形品は原型と
はかなり形の異つたものとなつた。
実施例 2
エポキシ樹脂(予備縮合物、Mn8000、
EE1000)100部、ガラス繊維(チヨツプドストラ
ンドCS−03)30部、ジアミノジフエニルメタン
5.4部を混合し、ペレツト化したものを金型温度
75℃でトランスフアー成形し、成形品のTgを測
定したところ82℃であつた。
この成形品を80℃の雰囲気温度に調整された恒
温器の中に入れ2時間加熱したところ、成形品の
Tgは98℃となつていた。ここで恒温器の温度を
95℃とし、1時間加熱したところ成形品のTgは
110℃となつていた。ここで更に恒温器の温度を
110℃に設定し、0.5時間加熱したところ成形品の
Tgは130℃となつた。
この成形品と同じ配合物の最高到達Tgは154℃
(硬化条件は150℃×3時間、180℃×3時間)で
あり、上記成形品のTgは最高到達Tgの67%に達
していた為、Tgより20℃を越える温度以上に加
熱しても変形しないと判断し、160℃で1時間加
熱した。最終的な成形品のTgは153℃となり、硬
化中に変形することは無かつた。また通常硬化し
たものの収縮率は0.8〜1.0%であつたが、本硬化
法によれば収縮率は0.2%以下であつた。
実施例 3
エポキシ樹脂(予備縮合物、Mn4500、
EE1100)100部、シリカ(350メツシユ)50部、
ジアミノジフエニルメタン4.9部を混合し、ペレ
ツト化したものを金型温度60℃で射出成形し、成
形品のTgを測定したところ68℃であつた。
この成形品を第1表の加熱条件で硬化させた
所、変形することはなく最終のTgである148℃に
到達した。なお最高到達Tgは150℃であつた。
The present invention relates to a solid phase curing method for solidified epoxy resin molded products. Conventionally, as a method of curing epoxy resins, a method of crosslinking and curing at a temperature equal to or higher than the melting point of the resin has generally been adopted. That is, in order to shape it into a certain mold, it needs to be in a molten state, and in order to crosslink and harden it as quickly as possible, it is customary to cure it at a high temperature, that is, in a molten state. In addition, when the crosslinking reaction has progressed to a certain extent and it no longer shows a molten state,
It is also known to cure in a solid state by so-called after-cure. However, in this type of curing method, (1) curing is performed at a temperature above the melting point (liquid phase), so in the case of casting, transfer molding, injection molding, etc., the mold must be removed until crosslinking progresses and the solid state is reached. Can not do it. Usually, it takes a long time to remove the mold, ranging from 10 minutes to 24 hours, and the efficiency of mold utilization is extremely low. (2) From this point of view, there is a method of rapidly curing at a high temperature, but in this case, the curing reaction becomes non-uniform, leaving internal distortion in the molded product, and the cured product becomes brittle. An object of the present invention is to provide an industrially advantageous method for curing epoxy resin molded articles that can be demolded in an extremely short time. Another object of the present invention is to provide a method for curing an epoxy resin molded product that can produce a molded product with excellent strength without causing internal distortion through a uniform curing reaction. A further object of the present invention is to provide a method for curing an epoxy resin molded product which provides a molded product with extremely low curing shrinkage. In the present invention, after demolding a solidified molded product of a cross-linkable epoxy resin with a glass transition temperature (Tg) of 40 to 200°C, heat curing is performed at an ambient temperature not exceeding 20°C above the Tg of the molded product. An epoxy system characterized in that the curing reaction is completed by raising the atmospheric temperature while maintaining the temperature within 20°C above the Tg of the molded material in response to the Tg of the molded material which increases with the progress of curing. This invention relates to a solid phase curing method for resin solidified molded products. Further, the present invention adjusts the above atmospheric temperature to the Tg of the molded product.
The temperature is maintained within a range not exceeding 20°C to allow the curing reaction to proceed, and the Tg of the molded product is determined by the Tg that can be reached upon completion of curing and the initial Tg.
This relates to a solid phase curing method for solidified epoxy resin molded products, which is characterized in that after the temperature rises by at least 60% or more of the difference between Incidentally, Tg in the present invention was measured by the TMA penetration method, in which a sample was heated by a temperature raising method. What is the solidified molded product of epoxy resin mentioned here?
By exposing the molded product to the so-called after-cure temperature (the temperature around the Tg that the molded product ultimately reaches is generally used), with virtually no crosslinking reaction taking place,
It is completely deformed, and is completely different from conventional hardened molded products before after-curing. As an indication that the crosslinking reaction of the solidified molded product has not substantially progressed, stickiness is observed when the surface of the molded product is wetted with acetone at room temperature and rubbed with a fingertip. In the conventional cured molded product before after-cure, most of the crosslinking reaction has proceeded, and this level of acetone does not cause it to become sticky. Since the present invention cures in a solid state, there is no need to maintain the shape in the mold, making the mold extremely efficient to use.Also, the curing reaction can be carried out uniformly at a specific ambient temperature, resulting in curing. The unexpected effect of this method is that the physical properties of the product are excellent, and in particular, the curing shrinkage is much smaller than that of conventional methods. The epoxy resin used in the present invention includes:
For example, in addition to bisphenol type epoxy resin, novolak type epoxy resin, halogenated epoxy resin, hydrogenated epoxy resin, alicyclic epoxy resin, or hydantoin type epoxy resin, silicone epoxy resin, epoxy furan resin, epoxy ester resin, phenoxy Modified epoxy resins such as resins, epoxy urethane resins, or liquid rubbers whose end groups are modified with epoxy, and resins such as those obtained by curing phenols such as polyvinylphenol with epoxy resins can also be used. Examples of compounding agents for these epoxy resins include known reinforcing agents, curing agents, fillers, plasticizers, diluents, flame retardants, photopolymerization initiators, pigments, and the like. Of course, other known thermoplastic or thermosetting resins that are compatible with the above epoxy resin can also be blended. Specifically, as the curing agent, in addition to amines, acid anhydrides, imidazoles, organic peroxides, etc., alcohols, isocyanates, etc. can be used depending on the polymer structure. As reinforcing agents, glass fibers, carbonate fibers, inorganic fibers such as asbestos, aramid fibers, nylon,
In addition to fibrous reinforcing agents such as organic fibers such as polyester, whiskers such as aluminum oxide, silicon carbide, and graphite can also be used. Other additives include fillers and pigments such as glass flakes, glass powder, mica, carbon black, talc, clay, silica, calcium carbonate, aluminum hydroxide, titanium white, or dioctyl phthalate and tricresyl phosphate. Plasticizers such as butyl glycidyl ether, reactive or non-reactive diluents such as xylene, flame retardants such as antimony trioxide and chlorinated paraffin, photoinitiators such as isopropyl benzoin ether, etc. are selected accordingly. It can be used as In the present invention, the above-mentioned epoxy resin blended composition is molded by an appropriate method to obtain a crosslinkable and hardenable solidified molded product having a Tg of 40 to 200°C. like above
As a specific method for obtaining a solidified molded product having a Tg, for example: (1) The Tg of the epoxy resin itself used is approximately 35-35.
Choose one in the 195℃ range. This is because when reinforcing agents and fillers are mixed with epoxy resins, Tg generally tends to increase. (2) When using an epoxy resin with a Tg of 195°C or higher, it is necessary to use other epoxy resins with a lower Tg, or to add compounding agents that lower the Tg, such as heat treatment. 200 by using plastic resins, plasticizers, etc.
It may be adjusted to below ℃. (3) If it is necessary to use an epoxy resin with a Tg of less than 35°C, use other epoxy resins with a higher Tg or other thermosetting resins, or use reinforcing agents that increase the Tg. The Tg may be adjusted within the range of 40 to 200°C by increasing the amount of filler, such as a fibrous reinforcing agent. In the present invention, by setting Tg in the above range of 40 to 200°C, it is possible to increase the atmospheric temperature during curing and shorten the curing time in the solid phase, and also to prevent the curing reaction from proceeding too much during kneading. can be prevented. Furthermore, decomposition of the epoxy resin due to an increase in curing temperature due to too high Tg is suppressed, and the allowable range of molding temperature is widened. In the present invention, after demolding a solidified molded product having the above-mentioned Tg, heat curing is performed at an ambient temperature not exceeding 20°C below the Tg of the molded product, and in response to the Tg of the molded product which increases as the curing progresses, The curing reaction is completed by raising the ambient temperature while maintaining it within a range of 20° C. above the Tg of the molded article. The atmospheric temperature may be raised continuously following the rise in Tg of the molded product, or may be raised stepwise. The preferred ambient temperature is around the Tg of the molded product or about 15°C lower than the Tg,
And its upper limit is 20°C higher than Tg. However, it is generally difficult to control the temperature within this range at all times, and in some cases it is acceptable to temporarily deviate from this range. A solidified molded product of an epoxy resin in a state where the crosslinking reaction has not substantially progressed (hereinafter referred to as an uncured molded product) deforms when exposed to an ambient temperature higher than the Tg of the molded product. However, epoxy resins usually have a wide range of molecular weights, and the Tg of the uncured molded material here is
This means that the average Tg of the entire resin is measured. Therefore, even if the ambient temperature becomes higher than Tg, deformation does not occur immediately, but in practice, deformation does not occur as long as the temperature does not exceed Tg by 20°C, so this range was selected. In a preferred embodiment of the present invention, the Tg of the molded product is
After that temperature is increased by at least 60% of the difference between the initial Tg and the Tg that can be reached upon completion of its curing, the molding is no longer at risk of melting or deforming, and the ambient temperature is then lowered. Tg
The temperature can be set at a temperature exceeding 20° C., thereby further promoting the crosslinking reaction in a solid phase state without causing dimensional changes. In the present invention, in order to effectively carry out the solid phase curing method described above, it is desirable that the initial Tg increase rate of the solidified molded product is in the range of about 0.01 to 10° C./min. The initial Tg increase rate of the solidified molded product referred to here refers to the initial Tg increase rate of the solidified molded product that has not undergone substantial thermal history.
This is the rate of increase in Tg of the solidified molded product at time 0 when the solidified molded product is exposed to the same ambient temperature as Tg. Specifically, the initial Tg 0 of the solidified molded product is measured in advance, the solidified molded product is exposed to the same ambient temperature as this Tg 0 , the change in Tg is tracked, and the time 0 of the Tg increase curve is measured.
It is obtained from the slope at . In the above initial Tg increase rate range, the crosslinking reaction progresses quickly and curing can be completed within a relatively short time, and the resulting molded product does not suffer from internal distortion, shrinkage, or warping. preferable.
On the other hand, the atmospheric temperature is adjusted at the initial stage of the solidified molded product.
Approximately 0.2 to 5 times the Tg increase rate, preferably approximately 0.5 to 2
This can easily be achieved by increasing the speed in the double range. In the present invention, various known molding methods can be used as the molding method, including, of course, the casting method, injection molding method, transfer molding method, extrusion molding method, blow molding method, normal pressure injection method, etc. can. In addition to heating gas (e.g. air), heat sources for solid phase curing of the present invention include liquids (e.g. heat medium such as high-boiling oil), powder (e.g. sand), etc.
etc. can be mentioned. Further, electron beam irradiation, microwave irradiation, etc. can also be used. A detailed explanation will be given below with reference to examples. Note that parts simply indicate parts by weight. Note that Tg below was measured using a differential scanning calorimeter manufactured by Rigaku Denki Co., Ltd. Example 1 100 parts of epoxy resin [precondensate, number average molecular weight (Mn) 5200, epoxy equivalent (EE) 1400],
A pelletized mixture of 50 parts of silica (350 mesh) and 0.7 part of BF 3 monoethylamine complex salt was injection molded at a mold temperature of 65°C, and the Tg of the molded product was measured and found to be 71°C. The initial Tg increase rate at an ambient temperature of 71°C was 0.21°C/min, so when this molded product was raised linearly from 65°C to 150°C at a rate of 0.5°C/min, no deformation occurred. I was able to harden it. The Tg after curing was 144°C. Incidentally, FIG. 1 shows the relationship between the ambient temperature and the Tg of the molded product over time. The diagram shows the atmospheric temperature.
It can be seen that the temperature did not exceed Tg+20℃. Comparative Example 1 The molded product molded in Example 1 was heated to an ambient temperature of 65°C.
When the molded product was raised linearly at a rate of 1.5°C/min from It became a vine. Example 2 Epoxy resin (precondensate, Mn8000,
EE1000) 100 parts, glass fiber (chopped strand CS-03) 30 parts, diaminodiphenylmethane
Mix 5.4 parts and pelletize the mold temperature.
Transfer molding was performed at 75°C, and the Tg of the molded product was measured to be 82°C. When this molded product was placed in a thermostat adjusted to an ambient temperature of 80℃ and heated for 2 hours, the molded product
Tg was 98℃. Here, set the temperature of the thermostat
When heated at 95℃ for 1 hour, the Tg of the molded product was
It was 110 degrees Celsius. Here, further adjust the temperature of the thermostat.
The molded product was heated for 0.5 hours at 110℃.
Tg was 130℃. The highest Tg of the same compound as this molded product is 154℃
(Curing conditions were 150°C x 3 hours, 180°C x 3 hours), and the Tg of the above molded product had reached 67% of the highest achieved Tg, so even if heated to a temperature 20°C higher than Tg. It was determined that there would be no deformation, and it was heated at 160°C for 1 hour. The final molded product had a Tg of 153°C and was not deformed during curing. Further, the shrinkage rate of the cured product was usually 0.8 to 1.0%, but according to this curing method, the shrinkage rate was 0.2% or less. Example 3 Epoxy resin (precondensate, Mn4500,
EE1100) 100 parts, silica (350 mesh) 50 parts,
A mixture of 4.9 parts of diaminodiphenylmethane and pelletized mixture was injection molded at a mold temperature of 60°C, and the Tg of the molded product was measured to be 68°C. When this molded article was cured under the heating conditions shown in Table 1, it did not deform and reached its final Tg of 148°C. The maximum Tg reached was 150°C.
【表】
実施例 4
実施例3と同じ成形物を雰囲気温度70℃から始
めて雰囲気温度を160℃になるまで、0.16℃/分
の速度で直線的に上昇させたところ、変形するこ
と無く硬化させることができた。尚、第2図に雰
囲気温度と成形品のTgとの時間的経過の関係を
示す。図より雰囲気温度がTg+20℃を越えてい
ないことがわかる。[Table] Example 4 The same molded product as in Example 3 was cured without deformation when the ambient temperature was started at 70°C and raised linearly at a rate of 0.16°C/min until it reached 160°C. I was able to do that. Incidentally, Fig. 2 shows the relationship between the ambient temperature and the Tg of the molded product over time. The figure shows that the ambient temperature does not exceed Tg + 20°C.
第1〜2図は実施例1及び実施例4における雰
囲気温度と成形品のTgとの時間的経過の関係を
示すグラフである。
1 and 2 are graphs showing the relationship between the ambient temperature and the Tg of the molded product over time in Examples 1 and 4.
Claims (1)
化可能なエポキシ系樹脂固化成形物を脱型後、加
熱温度として、その上限がその成形物のTgより
20℃を越えない雰囲気温度で加熱硬化を行い、硬
化の進行と共に上昇する該成形物のTgに対応し
て、該雰囲気温度を該成形物のTgより20℃を越
えない範囲に保持しつつ上昇させて硬化反応を完
了させることを特徴とするエポキシ系樹脂固化成
形物の固相硬化方法。 2 ガラス転移温度(Tg)が40〜200℃の架橋硬
化可能なエポキシ系樹脂固化成形物を脱型後、加
熱温度として、その上限がその成形物のTgより
20℃を越えない雰囲気温度で加熱硬化を行い、硬
化の進行と共に上昇する該成形物のTgに対応し
て、該雰囲気温度を該成形物のTgより20℃を越
えない範囲に保持しつつ上昇させて硬化反応を進
行させ、上記成形物のTgが、その硬化の完了に
より到達し得るTgとその初期のTgとの差が少な
くとも60%以上、上昇した後は、雰囲気温度を
Tgより20℃を越える範囲にして硬化させること
を特徴とするエポキシ系樹脂固化成形物の固相硬
化方法。[Claims] 1. After demolding a solidified molded product of a crosslinkable epoxy resin with a glass transition temperature (Tg) of 40 to 200°C, the upper limit of the heating temperature is higher than the Tg of the molded product.
Heat curing is performed at an ambient temperature that does not exceed 20℃, and in response to the Tg of the molded material, which increases as the curing progresses, the ambient temperature is increased while maintaining the Tg of the molded material within a range of no more than 20°C. A method for solid-phase curing of a solidified epoxy resin molded article, characterized in that the curing reaction is completed by curing. 2 After demolding a solidified molded product of a cross-linkable epoxy resin with a glass transition temperature (Tg) of 40 to 200°C, the upper limit of the heating temperature is higher than the Tg of the molded product.
Heat curing is performed at an ambient temperature that does not exceed 20℃, and in response to the Tg of the molded material, which increases as the curing progresses, the ambient temperature is increased while maintaining the Tg of the molded material within a range of no more than 20°C. After the curing reaction has progressed and the difference between the Tg of the molded product and its initial Tg has increased by at least 60%, the ambient temperature should be lowered.
A solid phase curing method for epoxy resin solidified molded products, characterized by curing at a temperature exceeding 20°C above Tg.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12397583A JPS6015431A (en) | 1983-07-06 | 1983-07-06 | Solid-phase curing of solid epoxy resin molding |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP12397583A JPS6015431A (en) | 1983-07-06 | 1983-07-06 | Solid-phase curing of solid epoxy resin molding |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS6015431A JPS6015431A (en) | 1985-01-26 |
| JPH0373578B2 true JPH0373578B2 (en) | 1991-11-22 |
Family
ID=14873937
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP12397583A Granted JPS6015431A (en) | 1983-07-06 | 1983-07-06 | Solid-phase curing of solid epoxy resin molding |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6015431A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3695653B2 (en) | 2002-04-17 | 2005-09-14 | 船井電機株式会社 | Brush motor |
-
1983
- 1983-07-06 JP JP12397583A patent/JPS6015431A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6015431A (en) | 1985-01-26 |
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